car 66 - licensing of aircraft maintenance engineers

CAR-66

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Issue II, R 2 dated 4th September 2017

CAR – 66 ISSUE II R 2

LICENSING OF AIRCRAFT

MAINTENANCE ENGINEERS

DIRECTORATE GENERAL OF CIVIL AVIATION TECHNICALCENTRE,OPPSAFDURJUNGAIRPORT,NEWDELHI

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SalientFeaturesoftheCAR-66

TheCAR-66

hasbeendraftedin linewiththecurrentRule61and toharmonise the aircraft

maintenancepersonnellicensingsystemwithEASAPart66(General).

details,requirementsforqualifyinganindividualtoobtainanAircraftMaintenance

Engineer’sLicenceandextensionofsuchlicence[CAR-66]

eliminatesthesystemofobtainingAirframe,Engine,Electrical,InstrumentandRa-

dioSystemLicencesseparately[66.A.03]

redefines the syllabus for basic knowledge examination in modular pattern

[66.A.25]

provides for endorsement ofan AME licence aftersuccessful completion of type

trainingandthetypetrainingexamination/typeexaminationwhichshallconsistof

boththeoreticalandpracticalexaminations[66.A.45(c)]

liststhedetailsofpracticaltaskstoqualifyanindividualtoobtainatyperating[Ap-

pendixIItoAMC]

provides for acquiring group type rating of aircraft and certification privileges

[66.A.45(a)]

hasaprovisiontoconverttheexistingAMElicencetoCAR66licence[66.A.70]with

orwithoutlimitation.

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GENERAL

InordertoharmonizeIndianrequirementsfor licensingofaircraftmaintenanceengi-

neerswith internationalrequirements;CAR-66Rev.0dated11thNovember2011,was

introduced.

This CAR is issued on the basis of amended Rule 61(6th amendment) of the AircraftRules,1937asnotifiedvideGSR1001(E)dated22ndDecember2010.ThisCARiseffectivefrom01.01.2012.HowevertheexistingrequirementsofCARSection-2SeriesLwillalsocontinuetillthedatenotifiedbytheDirectorGeneralforfacilitatingsmoothtransitionofaircraftmaintenanceengineerlicensingsystemintoCAR66pattern.TheCAR-66isapplicabletoallpersonnel/Organizationsengagedinmaintenanceand/orcertificationofaircraftregisteredinIndia.TheSectionAofCAR-66establishestherequirementsfortheissueandextensionofan

aircraftmaintenanceengineer’s license,conditionsof itsvalidityanduse. Italsohasa

provisionforconvertingtheaircraftmaintenanceengineer’s(AME)licenseissuedprior

totheCAR-66comingintoforce.TherequirementsarefollowedbyAcceptablemeansof

compliance(AMC)andGuidanceMaterial(GM)

TheAMElicensesinCAR66patternwillbeavailableintwodifferentways:

a)AfterconversionofexistingAMElicenseswithapplicablelimitation.

b)IssueoffreshlicenseafterpassingofapplicablemodulesofBasicKnowledgeExamto

beconductedbyCEO.

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Record of Revisions

Initial Issue (Revision 0) 11th November 2011 ThisCAR66providesrequirementsfortheissueofanaircraftmaintenanceengineer’slicenceandconditionsofitsvalidityanduseforaeroplanesandhelicopters.Revision 1, 23rd April 2015 TheRevision-01toCAR66wasissuedtoreviseconversionof licencesissuedpriortoCAR-66andexaminationcredits.TherevisionalsorevisestheLicenseformat.CAR 66 Issue IITheCAR66IssueIIisbeingissuedtoamendthetraining,examination,knowledgeandexperiencerequirementsfortheissuanceofaircraftmaintenancelicences

SalientfeaturesoftheCAR66IssueIIare:1.Thetraining,examination,knowledgeandexperiencerequirementsfortheissuanceof

aircraftmaintenancelicencesandtoadapttheserequirementstothecomplexityof

thedifferentcategoriesofaircraftamended

2.TheAMCsandGMsrelatedtoapointhavebeenbroughttogetherforeasyreferencepurposes.

3.Provisionforaircraftgroupingadded(66.A.5)4. Requirements for completing all the module for basic knowledge within 10 year

(66.A.25(b))added

5.Headingof(66.A.45)ischangedfromtype/tasktrainingtoEndorsementwithaircraftrating.RelatedAMCandGMamended.

6.Point66.A.50andrelatedAMCaddedtomakeaprovisionforintroducingorremoval

oflimitationfromthelicense7.ExistingAMCsandGMsaresuitableamended.8. Appendix -1- Basic knowledge requirements amended to revise the syllabus for

knowledgeexamination9.Appendix-2-Basicexaminationstandardhavebeenrevised

10. Appendix-3-Type examinationstandardhavebeenamended, minimumstandardanddurationfortypetraining,coursecurriculumhavebeenintroduced,practicalelementsrequirementstobecoveredduringtypetrainingadded,typetrainingexam-inationsandassessmentstandardhavebeenrevised,relevantAMCandGMhavebeenalsoamended/added

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11.Appendix-IIItoAMCofCAR66forcompetencyassessmentofassessorsadded.12.ProceduresforCAR-66(Section–B)isremovedfromthisCARandshallbepartof

AirworthinessProceduresManual(Chapter-17)CAR Issue II Revision 1 TheRevision-01toCAR66IssueIIisproposedtobeissuedtoincorporateamendmentsmadeinRule61oftheAircraftRules,1937publishedvideGSR911(E)dated16-9-2016.SalientrevisionintheCARasfollows:-

1. CAR66.A.3IntheexistingAMElicencecategory,categoryB3isintroducedforcer-

tifyingunpressurisedpistonengineaircraftbelow2000kgsMTOW.

2. ProvisionhasbeenmadeforissueofCategoryAlicencewithouttyperating

3. 66.A.20privilegesofAMElicencehasbeenreplacedwithnewoneinlinewithrule

61.

4. 66.A.30AircraftMaintenanceExperiencerequirementsofissueofCategoryA,B1.2

andB1.4hasbeenrevisedto3years.

5. RelatedparagraphinthisCARrevisedtoincludenewcategoryB3whereeverre-

quired.

6. 66.A.45endorsementonAMElicenceforaircraftratingshasbeenrevisedsuitably

toincludecategoryB3requirement.

7. Appendix–IBasicknowledgerequirementhasbeenrevisedtoincludesyllabusfor

categoryB3.

8. Requirementsforcertifyingstaffengagedincertificationofaircraftcomponentsare

detailedinSubpartC(Component).

9. ApplicationandformatareseparatedfromthemainCARandpublishedintheform

sectiononDGCAwebsite.

CAR Issue II Revision 2

Thesalientfeaturesofthisrevisionareasfollows:

1. 66.A.35amendedtoreplaceskilltestrequirementwithdemonstrationofskill.

2. 66.A.215(b)amendedtoincludeAMECourse.

3. Appendix–II(BasicExaminationStandard)para1.5amendedtomakeprovisionfor

appearinginfailedmodulerelatedtolimitationpapersfrom90daysto30days.

4. GM66.A.35(SkillTestRequirements)–Deleted.

5. Appendix-I(AppendicestoAMCforCAR66)amendedtoaddanoteonTyperating

endorsementcoveringseveralmodels/variant.Group1HelicopterTableamended

inlinewithEASAguidelines.

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CONTENTS

Paragraph Description PageNo

General 3

RecordofRevisions 4

SECTION A TECHNICAL REQUIREMENTS

SUBPART A AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HEL-

COPTERS

66.A.01

66.A.03

66.A.05

Scope

LicenceCategories

AircraftGroups

10

10

10

66.A.10 Application 11

66.A.15 Eligibility 11

66.A.20 Privileges 11

66.A.25 Basicknowledgerequirements 13

66.A.30 BasicExperienceRequirements 13

66.A.35 DemonstrationofSkill 14

66.A.40 Continuedvalidityoftheaircraftmaintenanceengineer’slicence

14

66.A.45

66.A.50

EndorsementwithAircraftratings

Limitations

15

17

66.A.55 Evidenceofqualification 17

66.A.70 Conversionprovisions 17

Subpart-B Aircraft other than Aeroplane and helicopters

66.A.100 General 18

Subpart-C Components

66.A.200 General 19

66.A.205 Requirements 19

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66.A.210 ExtensiontoscopeofAuthorization 20

66.A.215 Privileges 20

66.A.220 ValidityofCertificationAuthorization 21

66.A.225 Suspensions,CancellationandReturnofcertificationAu-thorization

21

Appendices

AppendixIBasicKnowledgeRequirements23

AppendixIIBasicExaminationandStandard80

AppendixIIIAircraftTypetrainingandExaminationStandard84

Onthejobtraining

AppendixIV ExperiencerequirementsforextendingaCAR-66AircraftMaintenanceEngineer’sLicence104

AppendixVApplicationsandFormats(ReferCAR66partII)105

AppendixVI AircraftMaintenanceEngineer’sLicencereferredtoin

Rule61oftheAircraftRules,1937(CAR-66)-CAForm26106

Acceptable Means of Compliance (AMC) and Guidance Material to

SECTION A of CAR 66

GM66.A.03Licencecategories 110

AMC66.A.10Application 110

AMC66.A.15(a)Eligibility110

GM66.A.20(a) Privileges 111

AMC66.A.20(b)2 Privileges 113

GM66.A.20(b)2 Privileges 115

AMC66.A.20(b)3

GM66.A.20(b)4

GM66.A.25(a)

Privileges 115

Privileges117

Basicknowledgerequirements 117

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AMC66.A.30(a) Experiencerequirements117

AMC66.A.30(d) Experiencerequirements118

GM66.A.40 ContinuedvalidityoftheAircraftMaintenanceLicence 118

GM66.A.45(b) Endorsementwithaircraftratings 119

AMC66.A.45(e)

AMC66.A.45(d),

(e)3,(f)1andg)1

GM66.A.45

AMC66.A.50(b)

GM66.A.70

GM66.A.70(c)

Endorsementwithaircraftratings119



Limitations123

ConversionProvisions123

Conversionprovisions 124

GM66.A.70(d)AMCtoSection1ofAppendixIIItoCAR-66AMCtoParagraph3.1(d)ofAppen-dixIIItoCAR-66AMCtoPara-graphs1(b)3.2and4.2ofAppen-dixIIItoCAR-66AMCtoParagraph1(c)ofAppendixIIItoCAR-66AMCtoSection5ofAppendixIIItoCAR-66AMCtoSection6ofAppendixIIItoCAR-66AMCtoAppendixIIItoCAR-66AMC66.A.205(c)

Conversionprovisions 124

AircraftTypeTrainingandExaminationStandard125On-the-JobTraining

“AircraftTypeTrainingandExaminationStandard127On-the-JobTraining“AircraftTypeTrainingandExaminationStandard131On-the-JobTraining“AircraftTypeTrainingandExaminationStandard131On-the-JobTraining“AircraftTypeTrainingandExaminationStandard132On-the-JobTraining“AircraftTypeTrainingandExaminationstandard132On-the-JobTraining

AircraftTypeTrainingandExaminationStandard134On-the-JobTrainingRequirements134

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AMC66.A.205(c)AppendixItoAMCofCAR66AppendixIItoAMCofCAR66

Requirements134Aircrafttyperatings135

AircrafttypepracticalexperienceandOn-the-Job151Traininglistoftask

AppendixIIItoAMCofCAR66

Evaluationofthecompetence:assessmentand158assessors

AppendixIVtoAMCofCAR66

FuelTankSafetytraining162

ApplicationsForm165

HighlightsofCAR66IssueIIR1166

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SECTION A

Technical Requirements

SUBPART A

AIRCRAFT MAINTENANCE ENGINEER’S LICENCE AEROPLANES AND HELICOPTERS

66. A.01 Scope

Thissectiondefinestheaircraftmaintenanceengineer’slicenceandestablishesthere-

quirementsforapplication,issueandconditionsofitsvalidity

66. A.03 Licence categories

(a)Aircraftmaintenancelicencesincludethefollowingcategories:

-CategoryA

-CategoryB1

-CategoryB2

-CategoryB3

-CategoryC

(b) CategoriesAandB1aresubdividedintosubcategoriesrelativetocombinationsof

aeroplanes,helicopters,turbineandpistonengines.Thesubcategoriesare:

-A1andB1.1AeroplanesTurbine

-A2andB1.2AeroplanesPiston

-A3andB1.3HelicoptersTurbine

-A4andB1.4HelicoptersPiston

(c)CategoryB3isapplicabletopiston-enginenon-pressurisedaeroplanesof2000kgMTOMandbelow.

66. A.05 Aircraft groups

Forthepurposeofratingsonaircraftmaintenanceengineerslicences,aircraftshallbe

classifiedinthefollowinggroups:

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1.Group1:complexmotor-poweredaircraftaswellasmultipleenginehelicopters,aer-

oplanes with maximum certified operating altitude exceeding FL290, aircraft

equippedwithfly-by-wiresystemsandotheraircraftrequiringanaircrafttyperating

whendefinedsobytheDGCA

2.Group2:aircraftotherthanthoseinGroup1belongingtothefollowingsubgroups:

—sub-group2a:singleturbo-propellerengineaeroplanes

—sub-group2b:singleturbineenginehelicopters

—sub-group2c:singlepistonenginehelicopters.

3.Group3:pistonengineaeroplanesotherthanthoseinGroup1.

66. A.10. Application

a)Anapplication foran aircraft maintenanceengineer’s licence orchange to such li-

cenceshallbemadeonCAForm19-01/02(ReferAppendix-V)withnecessarydocu-

mentsandfeestoDGCA.

b)Reserved.

c) Inadditiontothedocumentsrequiredinpoints66.A.10(a)asappropriate,theappli-

cantforadditionalcategoriesorsub-categoriestoanaircraftmaintenanceengineer’s

licenceshallsubmithis/hercurrentoriginalaircraftmaintenanceengineer’slicence

totheDGCAtogetherwithCAForm19-02.

d)Reserved

e)Reserved

(f)Eachapplicationshallbesupportedbydocumentationtodemonstratecompliance

withtheapplicabletheoreticalknowledge,practicaltrainingandexperiencerequire-

mentsatthetimeofapplication.

66. A.15.Eligibilitya) The applicant must have passed 10+2 examination in Physics, Chemistry and

Mathematicsfromarecognizedboardoruniversityoritsequivalent

b)Anapplicantforanaircraftmaintenanceengineer’slicenceshallbeatleast18years

ofage.

66. A.20 Privileges

a)Subjecttothecompliancewithparagraph(b),thefollowingprivilegesshallapply:

1. CategoryAlicenceholderto issuecertificates forreleasetoserviceafterminorscheduled line maintenance and simple defect rectification within the limits of

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maintenancetasksspecificallyendorsedontheauthorisationissuedbyamainte-nanceorganisationapprovedunderrule133Bforthebroadcategoryofaircraftendorsedonthelicenceandthecertificationprivilegesshallberestrictedtotheworkcarried outby the licence holderhimself in the maintenanceorganizationthatissuestheauthorisation.

2. CategoryB1licenceholdertoissuecertificatesforreleasetoserviceandactas

supportstafffollowingthemaintenanceperformedonaircraftstructure,power-

plant,mechanicalandelectricalsystems,workonavionicssystemrequiringsim-

pleteststoprovetheirserviceabilityandnotrequiringtroubleshooting,inre-

spectofanaircrafttypeendorsedonthelicence.

NOTE:(a)CategoryB1shallincludetheappropriatesub-categoryofCategoryA;

3CategoryB2licenceholdertoissue―

(a)certificates of release to serviceafter maintenance on avionicandelectrical

systems,avionicsandelectricalsystemwithinengineandmechanicalsystemsre-

quiringonlysimpleteststoprovetheirserviceabilityofaircrafttypeendorsedon

thelicence;

(b)certificatesofreleasetoserviceafterminorscheduledlinemaintenanceand

simpledefectrectificationwithinthelimitsof tasksspecificallyendorsedonthe

certificationauthorisationissuedbyanapprovedmaintenanceorganisationofair-

crafttypeendorsedonthelicenceandthiscertificationprivilegeshallberestricted

toworkthatthelicenceholderhaspersonallyperformedinthemaintenanceor-

ganisationwhichissuedthecertificationauthorisationandlimitedtotheratingal-

readyendorsedonthelicence.

4.CategoryB3licenceholderstoissuecertificatesofreleasetoserviceaftermainte-

nanceonaeroplanestructure,engineandmechanicalandelectricalsystems,work

onavionicsystemsrequiringonlysimpleteststoprovetheirserviceabilityandnot

requiringtroubleshootingof ‘piston-enginenon-pressurisedaeroplanesof2000

kgMaximumTake-offMassandbelow’

5 Category C licence holders to issue certificates of release to service after base

maintenanceinrespectofanaircraftofthetypeendorsedonthelicence.Thepriv-

ilegesapplytotheaircraftinitsentiretyincludingallsystems.

NOTE―Simpletestmeansatestdescribedinapprovedmaintenancedataandsuch

innaturethataircraftsystemserviceability isverifiedthroughaircraftcontrols,

switches,Built-inTestEquipment(BITE),CentralMaintenanceComputer(CMC)

orexternaltestequipmentnotrequiringspecialtraining.”;

b)TheholderofAircraftMaintenanceEngineerlicensemaynotexercisecertification

privilegesunless:

1.in compliance with the applicable requirements of CAR M and/or CAR 145;and

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2.intheprecedingtwoyearperiodhe/shehaseitheracquiredsixmonthsofmainte-

nanceexperienceinaccordancewiththeprivilegesgrantedbytheAircraftMainte-

nanceEngineer’sLicenceormettheprovisionfortheissueofappropriateprivi-

leges;and

3.he/shehastheadequatecompetencetocertifymaintenanceonthecorresponding

aircraft;and

4.he/sheisabletoread,writeandcommunicatetoanunderstandablelevelinthe

language(s) in which the technical documentation and procedures necessary to

supporttheissueofthecertificateofreleasetoservicearewritten.

66. A.25 Basic Knowledge requirements:

a)Anapplicantforanaircraftmaintenanceengineer’slicenceortheadditionofacate-

goryorsubcategorytosuchanaircraftmaintenanceengineer’slicenceshalldemon-

stratebyexamination,alevelofknowledgeintheappropriatesubjectmodulesinac-

cordancewithAppendixItothisCAR.Thebasicknowledgeexaminationshallbecon-

ductedbyCentralExaminationOrganizationofDGCA.

b)Thetrainingcoursesandexaminationsshallbepassedwithin10yearspriortothe

applicationforanaircraftmaintenancelicenceortheadditionofacategoryorsub-

categorytosuchaircraftmaintenancelicence.Shouldthisnotbethecase,examina-

tioncreditsmayhoweverbeobtainedinaccordancewithpoint(c).

(c)TheapplicantmayapplytotheDGCAforfullorpartialexaminationcredittothebasic

knowledgerequirementsfor

1.basicknowledgeexaminationsthatdonotmeettherequirementdescribedinpoint

(b)above;and

2.anyothertechnicalqualificationconsideredbytheDGCAtobeequivalenttothe

knowledgestandardofCAR-66

CreditsshallbegrantedinaccordancewithAPMChapter17.

d)Creditsexpire10yearsaftertheyweregrantedtotheapplicantbytheDGCA.The

applicantmayapplyfornewcreditsafterexpiration.

66. A.30 Basic Experience requirements:

a)Anapplicantforanaircraftmaintenanceengineer’slicenceshallhaveacquired:

1. forcategoryA,subcategoriesB1.2andB1.4andcategoryB3threeyearsofprac-

ticalaircraftmaintenanceexperienceonoperatingaircraft.

2. forcategoryB2andsub-categoriesB1.1andB1.3fiveyearsofpracticalaircraft maintenanceexperienceonoperatingaircraft.

3.forCategoryCwithrespecttolargeaircraft:

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i. threeyearsofexperienceexercisingcategoryB1.1orB1.3orB2privilegeson

largeaircraftorasCAR145B1.1,B1.3orB2supportstaff,or,acombinationof

both;or

ii. fiveyearsofexperienceexercisingcategoryB1.2orB1.4privilegesonlargeair-

craftorasCAR145B1.2orB1.4supportstaff,oracombinationofboth;or

4. forcategoryCwithrespecttononlargeaircraft:

ThreeyearsofexperienceexercisingcategoryB1orB2privilegesonnonlargeair-

craftorasCAR145B1orB2supportstaff,oracombinationofboth.

b)Anapplicantforanextensiontoanaircraftmaintenanceengineer’slicenceshallhave

aminimumcivilaircraftmaintenanceexperiencerequirementappropriatetothead-

ditionalcategoryorsub-categoryoflicenceappliedforasdefinedinAppendixIVto

thisCAR.

c) Theexperienceshallbepracticalandinvolvewitharepresentativecrosssectionof

maintenancetasksonaircraft.

d)Atleastoneyearoftherequiredexperienceshallberecentmaintenanceexperience

onaircraftofthecategory/subcategoryforwhichtheinitialaircraftmaintenanceen-

gineer’slicenceissought.Forsubsequentcategory/subcategoryadditionstoanex-

istingaircraftmaintenanceengineer’slicence,theadditionalrecentmaintenanceex-

periencerequiredmaybelessthanoneyear,butshallbeatleastthreemonths.The

requiredexperienceshallbedependentuponthedifferencebetweenthelicencecat-

egory/subcategoryheldandappliedfor.Suchadditionalexperiencemustbetypical

ofthenewlicencecategory/subcategorysought.

e)Twelveyearsofpracticalaircraftmaintenanceexperience,gainedoutsideacivilair-

craftmaintenanceenvironmentshallbeacceptedasequivalenttotherequirements

laid down in (1) and (2) of Paragraph (a) above, in the relevant category supple-

mentedbyatleastoneyearofrecentexperienceinthecivilaircraftmaintenanceen-

vironment;

(f)Experienceshallhavebeenacquiredwithinthe10yearsprecedingtheapplication

foranaircraftmaintenance licenceortheadditionofacategoryorsubcategoryto

suchalicence.Notwithstandingtothis,theaircraftmaintenanceexperiencegainedin

defenseenvironmentintheprecedingfifteenyearsshallbeacceptable.

66. A. 35 Demonstration of Skill

AnapplicantforgrantorextensionofAircraftMaintenanceEngineer’slicenceshall

demonstratehisaircraftmaintenanceskillinrespectofeachcategoryorsub-category

oflicenseorspecifictypeofaircraftinaccordancewithCAR66.A.45forwhichthe

applicationhasbeenmadetotheDirectorGeneral

66. A.40 Continued validity of the aircraft maintenance engineer’s licence

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(a) Theaircraftmaintenanceengineer’slicencebecomesinvalidafterfiveyearsofits

lastissueorrenewal,unlesstheholdersubmitshis/heraircraftmaintenanceen-

gineer’s licencetotheDGCA,inordertoverifytheinformationcontainedinthe

licenceisthesameasthatcontainedintheDGCArecords,pursuanttopoint66.B.

120.

(b) The holder of an aircraft maintenance engineer’s licence shall complete the CA

Form19-03(ReferAppendix-V)andsubmititwiththe holder’scopyofthelicence

totheDGCA,unlesstheholderworksinamaintenanceorganizationapprovedin

accordancewithCAR145thathasaprocedureinitsexpositionwherebysuchor-

ganisation may submit the necessary documentation on behalf of the aircraft

maintenanceengineer’slicenceholder.

(c) Anycertificationprivilegesbaseduponanaircraftmaintenanceengineer’slicence

becomesinvalidassoonastheaircraftmaintenanceengineer’slicenceisinvalid.

(d) The aircraft maintenance engineer’s licence is only valid when issued and/or

changedbyDGCAandwhentheholderhassignedthedocument.

66. A.45 Endorsement with aircraft ratings

(a)Inordertobeentitledtoexercisecertificationprivilegesonaspecificaircrafttype,theholderofanaircraftmaintenanceengineerlicenceneedtohavehis/herlicenceendorsedwiththerelevantaircraftratings.

—ForcategoryB1,B2orCtherelevantaircraftratingsarethefollowing:

1.Forgroup1aircraft,theappropriateaircrafttyperating.2.Forgroup2aircraft,theappropriateaircrafttyperating,manufacturersub-group

ratingorfullsubgrouprating.3.Forgroup3aircraft,theappropriateaircrafttyperatingorfullgrouprating.

— ForcategoryB3,therelevantratingis‘piston-enginenon-pressurisedaeroplanes

of2000kgMTOMandbelow.

— ForcategoryA,noratingisrequired,subjecttocompliancewiththerequirementsofparagraph145.A.35ofCAR-145.

(b)TheendorsementofaircrafttyperatingsrequiresthesatisfactorycompletionoftherelevantcategoryB1,B2orCaircrafttypetraining.

(c)Inadditiontotherequirementofpoint(b),theendorsementofthefirstaircrafttype

ratingwithinagivencategory/sub-categoryrequiressatisfactorycompletionofthecorrespondingOntheJobTraining,asdescribedinAppendixIIItoCAR-66

(d)Byderogationfrompoints(b)and(c),forgroup2and3aircraft,aircrafttyperat-

ingsmayalsobegrantedafter:

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—satisfactorycompletionoftherelevantcategoryB1andB2orCaircrafttypeex-aminationdescribedinAppendixIIItothisAnnex(CAR-66),and

—inthecaseofB1andB2category,demonstrationofpracticalexperienceonthe

aircrafttype.Inthatcase,thepracticalexperienceshallincludearepresentativecrosssectionofmaintenanceactivitiesrelevanttothelicencecategory.

(e)Forgroup2aircraft:

1.theendorsementofmanufacturersub-groupratingsforcategoryB1andClicenceholdersrequirescomplyingwiththeaircrafttyperatingrequirementsofatleasttwoaircrafttypesfromthesamemanufacturerwhichcombinedarerepresentativeoftheapplicablemanufacturersub-group;

2. theendorsementof fullsub-groupratingsforcategoryB1andC licenceholders

requirescomplyingwiththeaircrafttyperatingrequirementsofatleastthreeair-crafttypesfromdifferentmanufacturerswhichcombinedarerepresentativeoftheapplicablesub-group;

3.theendorsementofmanufacturersub-groupsandfullsub-groupratingsforcate-

goryB2licenceholdersrequiresdemonstrationofpracticalexperiencewhichshallincludearepresentativecrosssectionofmaintenanceactivitiesrelevanttotheli-cencecategoryandtotheapplicableaircraftsub-group.

(f)Forgroup3aircraft:

1.theendorsementofthefullgroup3ratingforcategoryB1,B2andClicenceholdersrequiresdemonstrationofpracticalexperience,whichshallincludearepresenta-tivecrosssectionofmaintenanceactivitiesrelevanttothelicencecategoryandtothegroup3.

2.forcategoryB1,unlesstheapplicantprovidesevidenceofappropriateexperience,

thegroup3ratingshallbesubjecttothefollowinglimitations,whichshallbeen-dorsedonthelicence:

—pressurisedaeroplanes—metalstructureaeroplanes—compositestructureaeroplanes—woodenstructureaeroplanes—aeroplaneswithmetaltubingstructurecoveredwithfabric.

(g)FortheB3licence:1.theendorsementoftherating‘piston-enginenon-pressurisedaeroplanesof2000kgMTOMandbelow’requiresdemonstrationofpracticalexperiencewhichshallincludearepresentativecross-sectionofmaintenanceactivitiesrelevanttothelicencecategory.2.unlesstheapplicantprovidesevidenceofappropriateexperience,theratingre-ferredtoinpoint1shallbesubjecttothefollowinglimitations,whichshallbe

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endorsedonthelicence:—woodenstructureaeroplanes—aeroplaneswithmetaltubingstructurecoveredwithfabric—metalstructureaeroplanes—compositestructureaeroplanes.66. A.50 Limitations (a)Limitationsintroducedonanaircraftmaintenancelicenceareexclusionsfromthe

certificationprivilegesandaffecttheaircraftinitsentirety.(b)Forlimitationsreferredtoinpoint66.A.45,limitationsshallberemovedupon:

1.demonstrationofappropriateexperience;or2.afterasatisfactorypracticalassessmentperformedbytheDGCA.

c)Forlimitationsreferredtoinpoint66.A.70,limitationsshallberemoveduponsatis-factorycompletionofexaminationonthosemodules/subjectsdefinedintheapplica-bleconversionreportreferredtoinAPMChapter17

66. A.55 Evidence of qualification

Personnel exercising certification privileges as well as support staff must produce

theirlicenceasevidenceofqualification,ifrequiredbyanauthorizedpersonofDGCA,

within24hours.

66. A.70 Conversion provisions-

a)TheholderofavalidAircraftMaintenanceEngineer’sLicenceonthedateofcoming

intoforceofthisCARmaycontinuetoexercisetheprivilegesofhislicenceandshall

be issued, with or without limitation andwithout furtherexamination, an Aircraft

MaintenanceEngineer’sLicence in theappropriatecategorysubject tosuchcondi-

tionsspecifiedinAirworthinessProceduresManualChapter17

b)A person undergoing a qualification process, prior to the GSR No. 1001(E) dated

22.12.2010regardingtheRule61oftheAircraftRules,1937shallcontinuetobequal-

ifiedtilldateasspecifiedbytheDirectorGeneral.Theholderofaqualificationgained

followingsuchqualificationprocessmaybeissuedanaircraftmaintenanceengineer’s

licencesubjecttotheconditionsspecifiedinAirworthinessProceduresManualChap-

ter17

c)Wherenecessary,theaircraftmaintenanceengineer’slicenceshallcontainlimitationsinaccordancewithpoint66.A.50toreflectthedifferencesbetween(i)thescopeofthecertifyingstaffqualification(ii)thebasicknowledgerequirementsand thebasicexaminationstandardslaiddowninAppendixIandIItothisCAR66.

d)AircraftMaintenanceEngineer’sLicencesissuedpriortothisCARcomingintoforce

incategory“A”tocoverGliders,Balloonsand incategory“B”, “D”and“X” tocover

Aircraft,Engine,propelleranditemsofequipmenttocarryoutmaintenanceandissue

‘CertificateofReleasetoService’thatcouldnotbetransferredtoCAR-66licence‘Type

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Rating’shallbetransferredtotheCAR-66licencesectionXIV(a)withoutalteringthe

privilegeshithertoexercisedbytheholder.

SUBPART B

AIRCRAFT OTHER THAN AEROPLANES AND HELICOPTERS

66.A.100General

Microlight,lightsportaircraft,glider,balloonoranairshipshallbecertifiedbyanair-craftmaintenanceengineerholdingalicenceinCategoryAorCategoryB1orCategoryB3oranauthorisedpersonsubjecttomeetingtherequirementsasspecifiedintherel-evantCAR.

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SUBPART C

COMPONENTS

66. A. 200 General

Thissubpartlaysdowntheminimumrequirementsinrespectofknowledge,training,experience,examinationandprocedureforissueofauthorisationbyCAR-145/CARMSubpart-Fapprovedorganisationstocertifyingstaffemployedintheirorganisationformaintenance and certification of components /aircraft maintenance as per manufac-turermaintenancedata.66. A.205 Requirements

Candidateforgrantofauthorizationtocarryoutandcertifyoverhaul,majorrepairsof

aircraft,powerplants,componentsandaccessoriesthereof,shallmeetthefollowingre-

quirements:

(a) Heshallnotbelessthan21yearsofage.

(b) Knowledge:-Theapplicantshallhavepassed10+2withPhysics,Chemistryand

Mathematicsorequivalentand

(c) shouldholdCAR66licenceinappropriatecategoryor

i) passed3yearsbasicAMEtrainingcourse/Diploma/DegreeinEngineeringin

theappropriatebranchandmusthavepassedrelevantportionsofmodulesof

CAR66knowledgeexamination approvedbytheDGCAforthepurposeinthe

MOE andexamination conductedby the approvedorganisation in association

withDGCAoreligibleforgrantofsuitablecreditforparticularmodule.

Note 1: Depending on the scope of authorization required, the CAR 145 / CAR M- Sub

Part F approved organization shall documents the module(s) of examination

required to be passed by the applicant in the organisations expositions.

(d) Training:

Theapplicantmusthaveundergoneatrainingprogrammeconductedby:

Manufactureroftheequipment;OR

Anorganizationapprovedtoimpartsuchtraining;OR

Trainedbyapersonhavingspecificapprovalcoveringtheactivityforaperiodof2

years.

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(e) Experience:Applicantsmeetingtheknowledgerequirementsshallhavethefol-

lowingexperience:

i) ForpersonsholdingCAR66AircraftEngineers’License:oneyearexperiencein

overhaul,majorrepairs,modificationsof thesystemcomponentsandaccesso-

ries,includingthreemonthsrecentexperience.

ii) ForpersonsholdingDiploma/DegreeinEngineering:twoyears’experiencein

overhaul,majorrepairs,modificationsof thesystemcomponentsandaccesso-

ries,includingsixmonthsrecentexperience.

iii) Candidateforcertificationofstructuralrepair/modificationshouldhavemini-

mumtwoyearsrelevantfieldexperience,andproduceevidencethathehasper-

formedsimilarstructuralrepairsatleasttwiceunderthesupervisionofanap-

provedpersonintheprecedingsixmonths.

(f) MedicalFitness

Theapplicantshouldhavebeenassessedmedicallyfitbyaregisteredmedical

practitionertoperformthescopeofworkappliedfor.

(g) Competencycheck:-

Beforegrantofauthorizationthecompetencyofthecandidateshallbeassessed

bytheorganization,followingproceduresdocumentedintheorganizationexpo-

sition.

(h) OrganizationsdesirousofusingtheprovisionsofthisCARshalldetailtheirtrain-

ingprogramme,activitiesrequiringcertificationauthorisation,education,expe-

rience,onjobtrainingrequirementsandassessmentprocedureintheirMainte-

nanceOrganizationExposition.

66. A.210 Extension to Scope of Authorization

Candidateseekingextensiontotheirscopeofauthorizationofaparticularstream

(Mechanical orAvionics) , inaddition to meeting the trainingrequirementsof

para66.A.205(c)ofthisCAR,shallhaveadditionalsixmonthsexperienceonthe

typeofcomponentsforwhichcertificationauthorisationisrequired.Whentheau-

thorizationisrequiredtobegrantedforadditionalstream,theapplicantshallhave

24monthsmaintenanceexperienceoutofwhich6monthsmustberecentexperi-

ence.

Beforegrantofextensionofauthorization,thecompetencyofthecandidateshall

beassessedbytheorganization,followingproceduresasmentionedin66.A.205

(g).

66. A.215 Privileges

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Theprivilegesofcomponentcertifyingstaffshallcover ;-

a) Holder of certification authorization on the basis of CAR 66 AME Licence:

Issuance of Certificate of Maintenance (CRS) for shops and systems of air-

craft/engine(whenatshoplevelandnotfittedontheaircraft)

Note: CRS on aircraft and/ or engine shall be done provided the Approval holder

has AME licence in relevant Category.

b) HolderofcertificationauthorizationonthebasisofAMECourse/Diplomain

Engineering/DegreeinEngineering:Certifyworkcarriedoutasendorsedon

thecertificationauthorization

Note 1: Such a certificationauthorizationshall be limited only to shop level

work and shall not include major maintenance of aircraft and/or engine

Note 2: Persons already holding approvals with CRS privileges may continue

to be permitted to issue CRS on being permitted under the CAR 145 / CAR M

Subpart F approval even if they are not meeting the requirement of this CAR.

Such persons may also be considered for grant of additional certification au-

thorizationsubject to meeting the requirements

66. A.220 Validity of Certification Authorization

a) TheCertificationAuthorizationshall bevalidforaperiodofoneyearand

mayberenewedbytheQualityManagersubjecttotheconditionthatthatthe

person

i) Hasexercisedtheprivilegesoftheauthorizationforaminimumperiod of

threemonthsinthepreceding12months;

ii) Hasundergonerefreshercourseinthepreceding24months;

iii) Hasbeenassessedmedicallyfit;and

iv) Continuestoremainintheemploymentoremploymentcontract of the or-

ganization.

66. A.225 Suspensions, Cancellation and Return of Certification Authorization

(a) ACertificationAuthorizationmaybewithdrawnwhereanenquirycon-

ductedbytheapprovedorganizationorDGCAestablishesthat :-

i) theholderofsuchanauthorizationhasperformedworkorgrantedacer-

tificateinrespectofworkwhichhasnotbeenperformedinacarefuland

competentmanner,or

ii) theholderofsuchanauthorizationhassignedacertificateinrespectof

anymatterwhichheisnotauthorizedtodealwith,or

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iii) itisundesirableforanyotherreasonthattheholderofsuchauthorization

shouldcontinuetoexercisethefunctionsofanapprovalholder.

iv) Authorizationofapersonwithdrawnasaresultofanenquiryshallnotbe

restoredwithoutapprovaloftheDGCA(RegionalAirworthinessOffice).

SuchpersonshallalsonotbegrantedotherAuthorizationwithoutthecon-

currenceoftheDGCA(RegionalAirworthinessOffice).

v) Alldisciplinaryactionstakenagainstapprovedpersonsshallbeimmedi-

ately intimated to the DGCA (Regional Airworthiness Office). Copies of

warnings/memorandaissuedtotheapprovedpersonsshallalsobefor-

wardedtotheDGCA(RegionalAirworthinessOffice).

(BSBHULLAR)

DirectorGeneralofCivilAviation

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AppendixI-BasicKnowledgeRequirements

1. KNOWLEDGE LEVELS - CATEGORY A, B1, B2, B3 AND C AIRCRAFT MAINTENANCE

ENGINEER’s LICENCE

BasicknowledgeforcategoriesA,B1,B2andB3areindicatedbytheknowledgelevels(1,2or3)againsteachapplicablesubject.CategoryCapplicantshallmeeteithercat-egoryB1orB2basicknowledgelevel.Theknowledgelevelindicatorsaredefinedondefinedon3levelsasfollows:

LEVEL 1

Familiarizationwiththeprincipalelementsofthesubject.

Objectives:

(a)Theapplicantshouldbefamiliarwiththebasicelementsofthesubject.

(b)Theapplicantshouldbeabletogiveasimpledescriptionofthewholesubject,

usingcommonwordsandexamples.

(c)Theapplicantshouldbeabletousetypicalterms.

LEVEL 2

Ageneralknowledgeofthetheoreticalandpracticalaspectsofthesubjectand anabilitytoapplythatknowledge. Objectives:

(a) The applicant should be able to understand theoretical fundamentals of thesubject.

(b) The applicant should be able to give a general description of the subject

usingasappropriate,typicalexamples.

(c)Theapplicantshouldbeabletousemathematicalformulaeinconjunction withphysicallawsdescribingthesubject.

(d) Theapplicantshouldbeabletoreadandunderstandsketches,drawingsand

schematicsdescribingthesubject.(e)Theapplicantshouldbeabletoapplyhisknowledgeinapracticalmanner

usingdetailedprocedures.

LEVEL 3

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Adetailedknowledgeofthetheoreticalandpracticalaspectsofthesubjectanda capacity to combine andapply the separate elements of knowledge in a logical and

comprehensivemanner.

Objectives:

(a) The applicant should know the theory of the subject and interrelation shipwithothersubjects.

(b)Theapplicantshouldbeabletogiveadetaileddescriptionofthesubjectusing

theoreticalfundamentalsandspecificexamples.(c) Theapplicantshouldunderstandandbeabletousemathematicalformulae

relatedtothesubject.(d)Theapplicantshouldbeabletoread,understandandpreparesketches,simpledrawingsandschematicsdescribingthesubject.(e) Theapplicantshouldbeabletoapplyhisknowledgeinapracticalmannerus-

ingmanufacturer'sinstructions.(f)Theapplicantshouldbeabletointerpretresultsfromvarioussourcesand

measurementsandapplycorrectiveactionwhereappropriate.

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2. MODULARISATION

QualificationonbasicsubjectsforeachCAR66aircraftmaintenanceengineer’slicence

categoryorsubcategoryshouldbeinaccordancewiththefollowingmatrix.Applicable

subjectsareindicatedbyan‘X’:

SubjectModules

AorB1aeroplanewith AorB1helicopterwith B2

B3

Turbine

engine(s)Piston

engine(s)Turbine

engine(s)Piston

engine(s)Avionics

Piston-engineNon-pressurised

aeroplanes2000kgMTOMandbelow

1 NotApplicable

2 NotApplicable

3 X X X X X X

4 X X X X X X

5 X X X X X X

6 X X X X X X

7A X X X X X

7B X

8 X X X X X X

9A X X X X X

9B X

10 X X X X X X

11A X

11B X

11C X

12 X X

13 X

14 X

15 X X

16 X X X

17A X X

17B X

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MODULES & SYLLABUS LEVEL

A B1 B2 B3

MODULE 1. Reserved - - -

MODULE 2. Reserved - - -

MODULE 3. ELECTRICAL FUNDAMENTALS LEVEL

A B1 B2 B3

3.1 Electron Theory 1 1 1 1

Structure and distribution of electrical charges within: atoms, molecules,ions,compounds;

Molecularstructureofconductors,semiconductorsandinsulators.

3.2 Static Electricity and Conduction 1 2 2 1

Staticelectricityanddistributionofelectrostaticcharges;

Electrostaticlawsofattractionandrepulsion;

Unitsofcharge,Coulomb'sLaw;

Conductionofelectricityinsolids,liquids,gasesandavacuum.

3.3 Electrical Terminology 1 2 2 1

Thefollowingterms,theirunitsandfactorsaffectingthem:potentialdiffer-ence,electromotiveforce,voltage,current,resistance,conductance,charge,conventionalcurrentflow,electronflow.

3.4 Generation of Electricity 1 1 1 1

Productionofelectricitybythefollowingmethods:light,heat,friction,pres-sure,chemicalaction,magnetismandmotion.

3.5 DC Sources of Electricity 1 2 2 2 Constructionandbasicchemicalactionof:primarycells,secondarycells,leadacidcells,nickelcadmiumcells,otheralkalinecells; Cellsconnectedinseriesandparallel;Internalresistanceanditseffectonabattery;

Construction,materialsandoperationofthermocouples;

Operationofphoto-cells.

3.6 DC Circuits - 2 2 1

OhmsLaw,Kirchoff'sVoltageandCurrentLaws;

Calculationsusingtheabovelawstofindresistance,voltageandcurrent;

Significanceoftheinternalresistanceofasupply.

3.7 Resistance/Resistor

(a) - 2 2 1

Resistanceandaffectingfactors;

Specificresistance; Resistorcolour code, values and tolerances, preferred values, wattage rat-ings;

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A B1 B2 B3

Resistorsinseriesandparallel;

Calculationoftotalresistanceusingseries,parallelandseriesparallelcombi-nations;

Operationanduseofpotentiometersandrheostats;

OperationofWheatstoneBridge.

(b) - 1 1 -

Positiveandnegativetemperaturecoefficientconductance;

Fixedresistors,stability,toleranceandlimitations,methodsofconstruction;

Variableresistors,thermistors,voltagedependentresistors;

Constructionofpotentiometersandrheostats;

ConstructionofWheatstoneBridge;

3.8 Power - 2 2 1

Power,workandenergy(kineticandpotential);

Dissipationofpowerbyaresistor;

Powerformula;

Calculationsinvolvingpower,workandenergy.

3.9 Capacitance/Capacitor - 2 2 1

Operationandfunctionofacapacitor;

Factorsaffectingcapacitanceareaofplates,distancebetweenplates,numberofplates,dielectricanddielectricconstant,workingvoltage,voltagerating;

Capacitortypes,constructionandfunction;

Capacitorcolourcoding;

Calculationsofcapacitanceandvoltageinseriesandparallelcircuits;

Exponentialchargeanddischargeofacapacitor,timeconstants;

Testingofcapacitors.

3.10 Magnetism

(a) - 2 2 1

Theoryofmagnetism;

Propertiesofamagnet ActionofamagnetsuspendedintheEarth'smagneticfield;

Magnetisationanddemagnetisation;

Magneticshielding;

Varioustypesofmagneticmaterial;

Electromagnetsconstructionandprinciplesofoperation; Handclasprulestodetermine:magneticfieldaroundcurrentcarryingcon-ductor.

(b) - 2 2 1Magnetomotiveforce,fieldstrength,magneticfluxdensity,permeability,hys-teresisloop,retentivity,coerciveforcereluctance,saturationpoint,eddycur-rents;

Precautionsforcareandstorageofmagnets.

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A B1 B2 B3

3.11 Inductance/Inductor - 2 2 1

Faraday'sLaw;

Actionofinducingavoltageinaconductormovinginamagneticfield;

Inductionprinciples;

Effects of the following on the magnitude of an induced voltage:magneticfieldstrength,rateofchangeofflux,numberofconductorturns;

Mutualinduction;

Theeffecttherateofchangeofprimarycurrentandmutualinductancehasoninducedvoltage;

Factorsaffectingmutualinductance:numberofturnsincoil,physicalsizeofcoil,permeabilityofcoil,positionofcoilswithrespecttoeachother;

Lenz'sLawandpolaritydeterminingrules;

Backemf,selfinduction;

Saturationpoint;

Principleusesofinductors;

3.12 DC Motor/Generator Theory - 2 2 1

Basicmotorandgeneratortheory;

ConstructionandpurposeofcomponentsinDCgenerator;

Operationof,andfactorsaffectingoutputanddirectionofcurrentflowinDCgenerators;

Operationof,andfactorsaffectingoutputpower,torque,speedanddirectionofrotationofDCmotors;

Serieswound,shuntwoundandcompoundmotors;

StarterGeneratorconstruction.

3.13 AC Theory 1 2 2 1

Sinusoidalwaveform:phase,period,frequency,cycle;

Instantaneous,average,rootmeansquare,peak,peaktopeakcurrentvaluesandcalculationsofthesevalues,inrelationtovoltage,currentandpower

Triangular/Squarewaves;

Single/3phaseprinciples.

3.14 Resistive (R), Capacitive (C) and Inductive (L) Circuits - 2 2 1

PhaserelationshipofvoltageandcurrentinL,CandRcircuits,parallel,seriesandseriesparallel;

PowerdissipationinL,CandRcircuits;

Impedance,phaseangle,powerfactorandcurrentcalculations;

Truepower,apparentpowerandreactivepowercalculations.

3.15 Transformers - 2 2 1

Transformerconstructionprinciplesandoperation;

Transformerlossesandmethodsforovercomingthem;

Transformeractionunderloadandno-loadconditions; Powertransfer,efficiency,polaritymarkings;

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A B1 B2 B3

Calculationoflineandphasevoltagesandcurrents;

Calculationofpowerinathreephasesystem;

PrimaryandSecondarycurrent,voltage,turnsratio,power,efficiency;

Autotransformers.

3.16 Filters - 1 1 -

Operation,applicationandusesofthefollowingfilters:lowpass,highpass,bandpass,bandstop.

3.17 AC Generators - 2 2 1

Rotationofloopinamagneticfieldandwaveformproduced;

OperationandconstructionofrevolvingarmatureandrevolvingfieldtypeACgenerators;

Singlephase,twophaseandthreephasealternators;

Threephasestaranddeltaconnectionsadvantagesanduses;

PermanentMagnetGenerators.

3.18 AC Motors - 2 2 1

Construction,principlesofoperationandcharacteristicsof:ACsynchronousandinductionmotorsbothsingleandpolyphase;

Methodsofspeedcontrolanddirectionofrotation; Methods of producing a rotating field: capacitor, inductor, shaded or splitpole.

MODULE 4. ELECTRONIC FUNDAMENTALS LEVEL

A B1 B2 B3

4.1 Semiconductors

4.1.1 Diodes

(a) - 2 2 1

Diodesymbols;

Diodecharacteristicsandproperties;

Diodesinseriesandparallel;

Maincharacteristicsanduseofsiliconcontrolledrectifiers(thyristors),lightemittingdiode,photoconductivediode,varistor,rectifierdiodes;

Functionaltestingofdiodes.

(b) - - 2 -

Materials,electronconfiguration,electricalproperties;

PandNtypematerials:effectsofimpuritiesonconduction,majorityandmi-noritycharacters;

PNjunctioninasemiconductor,developmentofapotentialacrossaPNjunc-tioninunbiased,forwardbiasedandreversebiasedconditions;

Operationandfunctionofdiodesinthefollowingcircuits:clippers,clampers,fullandhalfwaverectifiers,bridgerectifiers,voltagedoublersandtriplers;

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A B1 B2 B3

Detailedoperationandcharacteristicsofthefollowingdevices:siliconcon-trolledrectifier(thyristor), lightemittingdiode,Shottkydiode,photocon-ductivediode,varactordiode,varistor,rectifierdiodes,Zenerdiode.

4.1.2 Transistors

(a) - 1 2 1

Transistorsymbols;

Componentdescriptionandorientation;

Transistorcharacteristicsandproperties.

(b) - - 2 -

ConstructionandoperationofPNPandNPNtransistors;

Base,collectorandemitterconfigurations;

Testingoftransistors.

Basicappreciationofothertransistortypesandtheiruses.

Applicationoftransistors:classesofamplifier(A,B,C);

Simplecircuitsincluding:bias,decoupling,feedbackandstabilisation;

Multistagecircuitprinciples:cascades,push-pull,oscillators,multivibrators,flip-flopcircuits.

4.1.3 Integrated Circuits

(a) - 1 - 1

Description and operation of logic circuits and linear circuits/operationalamplifiers.

(b) - - 2 -

Descriptionandoperationoflogiccircuitsandlinearcircuits;

Introductiontooperationandfunctionofanoperationalamplifierusedas:integrator,differentiator,voltagefollower,comparator;

Operationandamplifierstagesconnectingmethods:resistivecapacitive,in-ductive(transformer),inductiveresistive(IR),direct;

Advantagesanddisadvantagesofpositiveandnegativefeedback.

4.2 Printed Circuit Boards - 1 2 -

Descriptionanduseofprintedcircuitboards.

4.3 Servomechanisms

(a) - 1 - -

Understandingofthefollowingterms:Openandclosedloopsystems,feed-back,followup,analoguetransducers;

Principles of operation and use of the following synchro system compo-nents/features:resolvers,differential,controlandtorque,transformers,in-ductanceandcapacitancetransmitters.

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A B1 B2 B3

(b) - - 2 -

Understandingofthefollowingterms:Openandclosedloop,followup,ser-vomechanism,analogue,transducer,null,damping,feedback,deadband;

Construction operation and use of the following synchro system compo-nents: resolvers,differential, controland torque,E and I transformers, in-ductancetransmitters,capacitancetransmitters,synchronoustransmitters; Servomechanismdefects,reversalofsynchroleads,hunting.

MODULE 5. DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS

LEVEL

A B1.1 B1.3

B1.2 B1.4 B2 B3

5.1 Electronic Instrument Systems 1 2 2 3 1

Typicalsystemsarrangementsandcockpitlayoutofelectronicinstru-mentsystems.

5.2 Numbering Systems - 1 - 2 -

Numberingsystems:binary,octalandhexadecimal;

Demonstrationofconversionsbetweenthedecimalandbinary,octalandhexadecimalsystemsandviceversa.

5.3 Data Conversion - 1 - 2 -

AnalogueData,DigitalData;

Operation and application of analogue to digital, and digital to ana-logueconverters,inputsandoutputs,limitationsofvarioustypes.

5.4 Data Buses - 2 - 2 -

Operation of data buses in aircraft systems, including knowledge ofARINCandotherspecifications.

5.5 Logic Circuits

(a) - 2 - 2 1

Identificationofcommonlogicgatesymbols,tablesandequivalentcir-cuits;

Applicationsusedforaircraftsystems,schematicdiagrams.

(b)Interpretationoflogicdiagrams. - - - 2 -

5.6 Basic Computer Structure

(a) 1 2 - - - Computerterminology(includingbit,byte,software,hardware,CPU,IC,andvariousmemorydevicessuchasRAM,ROM,PROM);

Computertechnology(asappliedinaircraftsystems).

(b) - - - 2 -

Computerrelatedterminology;

Operation, layoutand interfaceof themajorcomponents inamicrocomputerincludingtheirassociatedbussystems; Informationcontainedinsingleandmultiaddressinstructionwords;

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LEVEL

A B1.1 B1.3

B1.2 B1.4 B2 B3

Memoryassociatedterms;

Operationoftypicalmemorydevices;

Operation,advantagesanddisadvantagesofthevariousdatastoragesystems.

5.7 Microprocessors - - - 2 - Functionsperformedandoveralloperationofamicroprocessor;

Basicoperationofeachofthefollowingmicroprocessorelements:controlandprocessingunit,clock,register,arithmeticlogicunit.

5.8 Integrated Circuits - - - 2 -

Operationanduseofencodersanddecoders

Functionofencodertypes Usesofmedium,largeandverylargescaleintegration.

5.9 Multiplexing - - - 2 -

Operation, application and identification in logic diagrams of multi-plexersanddemultiplexers.

5.10 Fibre Optics - 1 1 2 -

Advantagesand disadvantages of fibreoptic data transmission overelectricalwirepropagation;

Fibreopticdatabus;

Fibreopticrelatedterms;

Terminations;

Couplers,controlterminals,remoteterminals;

Applicationoffibreopticsinaircraftsystems.

5.11 Electronic Displays - 2 1 2 1

Principlesofoperationofcommontypesofdisplaysusedinmodernaircraft,including

CathodeRayTubes,LightEmittingDiodesandLiquid

CrystalDisplay.

5.12 Electrostatic Sensitive Devices 1 2 2 2 1 Specialhandlingofcomponentssensitivetoelectrostaticdischarges;

Awarenessof risksand possible damage, component and personnelanti-staticprotectiondevices.

5.13 Software Management Control - 2 1 2 1 Awarenessofrestrictions,airworthinessrequirementsandpossiblecatastrophiceffectsofunapprovedchangestosoftwareprogrammes.

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LEVEL

A B1.1 B1.3

B1.2 B1.4 B2 B3

5.14 Electromagnetic Environment - 2 2 2 1

Influence of the following phenomena on maintenance practices forelectronicsystem:

EMC-ElectromagneticCompatibility

EMI-ElectromagneticInterference

HIRF-HighIntensityRadiatedField

Lightning/lightningprotection

5.15 Typical Electronic/Digital Aircraft Systems - 2 2 2 1 Generalarrangementoftypicalelectronic/digitalaircraftsystemsandassociatedBITE(BuiltInTestEquipment)testingsuchas:

(a) ForB1andB2only:

ACARS-ARINCCommunicationandAddressingandReportingSystem

EICAS-EngineIndicationandCrewAlertingSystem

FBW-FlybyWire

FMS-FlightManagementSystem IRS-Inertialreferencesystem(b) ForB1,B2andB3: ECAM-ElectronicCentralisedAircraftMonitoringEFIS-ElectronicFlightInstrumentSystem GPS-GlobalPositioningSystemTCAS-TrafficCollissionAvoidancesystemIntegratedmodularAvionicaCabinSystemInformationsystem

MODULE 6. MATERIALS AND HARDWARE LEVEL

A B1 B2 B3

6.1 Aircraft Materials — Ferrous

(a) 1 2 1 2

Characteristics, properties and identificationof commonalloy steels used inaircraft;

Heattreatmentandapplicationofalloysteels;

(b) - 1 1 1

Testingofferrousmaterialsforhardness,tensilestrength,fatiguestrengthandimpactresistance.

6.2 Aircraft Materials — Non-Ferrous

(a) 1 2 1 2

Characteristics,propertiesandidentificationofcommonnon-ferrousmaterialsusedinaircraft;

Heattreatmentandapplicationofnon-ferrousmaterials;

(b) - 1 1 1

Testingofnon-ferrousmaterialforhardness,tensilestrength,fatiguestrengthandimpactresistance.

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A B1 B2 B3

6.3 Aircraft Materials - Composite and Non- Metallic

6.3.1 Composite and non-metallic other than wood and fabric

(a)Characteristics,propertiesandidentificationofcommoncompositeandnon-metallicmaterials,otherthanwood,usedinaircraft;

1 2 2 2

Sealantandbondingagents.

(b) 1 2 - 2

Thedetectionofdefects/deteriorationincompositeandnon-metallicmaterial.

Repairofcompositeandnon-metallicmaterial.

6.3.2 Wooden structures 1 2 - 2

Constructionmethodsofwoodenairframestructures;

Characteristics,propertiesandtypesofwoodandglueusedinaeroplanes;

Preservationandmaintenanceofwoodenstructure;

Typesofdefectsinwoodmaterialandwoodenstructures;

Thedetectionofdefectsinwoodenstructure;

Repairofwoodenstructure.

6.3.3 Fabric covering 1 2 - 2

Characteristics,propertiesandtypesoffabricsusedinaeroplanes;

Inspectionsmethodsforfabric;

Typesofdefectsinfabric;

Repairoffabriccovering.

6.4 Corrosion

(a) 1 1 1 1

Chemicalfundamentals; Formationby,galvanicactionprocess,microbiological,stress;

(b) 2 3 2 2

Typesofcorrosionandtheiridentification;

Causesofcorrosion;

Materialtypes,susceptibilitytocorrosion.

6.5 Fasteners

6.5.1 Screw threads 2 2 2 2

Screwnomenclature;

Threadforms,dimensionsandtolerancesforstandardthreadsusedinaircraft;

Measuringscrewthreads;

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A B1 B2 B3

6.5.2 Bolts, studs and screws 2 2 2 2

Bolttypes:specification, identificationandmarkingofaircraftbolts, interna-tionalstandards;

Nuts:selflocking,anchor,standardtypes;

Machinescrews:aircraftspecifications;

Studs:typesanduses,insertionandremoval;

Selftappingscrews,dowels.

6.5.3 Locking devices 2 2 2 2

Tabandspringwashers,lockingplates,splitpins,palnuts,wirelocking,quickreleasefasteners,keys,circlips,cotterpins.

6.5.4 Aircraft rivets 1 2 1 2

Typesofsolidandblindrivets:specificationsandidentification,heattreatment.

6.6 Pipes and Unions

(a) 2 2 2 2

Identificationof,andtypesofrigidandflexiblepipesandtheirconnectorsusedinaircraft;

(b) 2 2 1 2

Standardunionsforaircrafthydraulic,fuel,oil,pneumaticandairsystempipes.

6.7 Springs - 2 1 1

Typesofsprings,materials,characteristicsandapplications.

6.8 Bearings 1 2 2 1

Purposeofbearings,loads,material,construction;

Typesofbearingsandtheirapplication.

6.9 Transmissions 1 2 2 1

Geartypesandtheirapplication;

Gear ratios, reduction and multiplication gear systems, driven and drivinggears,idlergears,meshpatterns;

Beltsandpulleys,chainsandsprockets.

6.10 Control Cables 1 2 1 2

Typesofcables;

Endfittings,turnbucklesandcompensationdevices;

Pulleysandcablesystemcomponents;

Bowdencables;

Aircraftflexiblecontrolsystems.

6.11 Electrical Cables and Connectors 1 2 2 2

Cabletypes,constructionandcharacteristics;

Hightensionandco-axialcables;

Crimping;

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A B1 B2 B3

Connector types, pins, plugs, sockets, insulators, current and voltage rating,coupling,identificationcodes.

MODULE 7A. MAINTENANCE PRACTICES

Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 7B.

LEVEL

A B1 B2

7.1 Safety Precautions-Aircraft and Workshop 3 3 3

Aspectsofsafeworkingpracticesincludingprecautionstotakewhenworkingwithelectricity,gasesespeciallyoxygen,oilsandchemicals.

Also,instructionintheremedialactiontobetakenintheeventofafireoran-otheraccidentwithoneormoreofthesehazardsincludingknowledgeonex-tinguishingagents.

7.2 Workshop Practices 3 3 3

Careoftools,controloftools,useofworkshopmaterials;

Dimensions,allowancesandtolerances,standardsofworkmanship;

Calibrationoftoolsandequipment,calibrationstandards.

7.3 Tools 3 3 3

Commonhandtooltypes;

Commonpowertooltypes;

Operationanduseofprecisionmeasuringtools;

Lubricationequipmentandmethods.

Operation,functionanduseofelectricalgeneraltestequipment;

7.4 Avionic General Test Equipment - 2 3

Operation,functionanduseofavionicgeneraltestequipment.

7.5 Engineering Drawings, Diagrams and Standards 1 2 2

Drawingtypesanddiagrams,theirsymbols,dimensions,tolerancesandpro-jections;

Identifyingtitleblockinformation

Microfilm,microficheandcomputerisedpresentations;

Specification100oftheAirTransportAssociation(ATA)ofAmerica;

Aeronauticalandotherapplicablestandardsincluding

ISO,AN,MS,NASandMIL;

Wiringdiagramsandschematicdiagrams.

7.6 Fits and Clearances 1 2 1

Drillsizesforboltholes,classesoffits;

Commonsystemoffitsandclearances;

Scheduleoffitsandclearancesforaircraftandengines;

Limitsforbow,twistandwear;

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MODULE 7A. MAINTENANCE PRACTICES Note: This module does not apply to category B3. Relevant subject matters for category

B3 are defined in module 7B.

LEVEL

A B1 B2

Standardmethodsforcheckingshafts,bearingsandotherparts.

7.7 Electrical Wiring Interconnection System (EWIS) 1 3 3

Continuity,insulationandbondingtechniquesandtesting;

Useofcrimptools:handandhydraulicoperated;

Testingofcrimpjoints;

Connectorpinremovalandinsertion;

Co-axialcables:testingandinstallationprecautions;

Identificationofwiretypes,theirinspectioncriteriaand

damagetolerance.

Wiringprotectiontechniques:Cableloomingandloom

support,cableclamps,protectivesleevingtechniques

includingheatshrinkwrapping,shielding.

EWISinstallations,inspection,repair,maintenanceand

cleanlinessstandards.

7.8 Riveting 1 2 -

Rivetedjoints,rivetspacingandpitch;

Toolsusedforrivetinganddimpling;

Inspectionofrivetedjoints.

7.9 Pipes and Hoses 1 2 -

Bendingandbelling/flaringaircraftpipes;

Inspectionandtestingofaircraftpipesandhoses;

Installationandclampingofpipes.

7.10 Springs 1 2 -

Inspectionandtestingofsprings.

7.11 Bearings 1 2 -

Testing,cleaningandinspectionofbearings;

Lubricationrequirementsofbearings;

Defectsinbearingsandtheircauses.

7.12 Transmissions 1 2 -

Inspectionofgears,backlash;

Inspectionofbeltsandpulleys,chainsandsprockets;

Inspectionofscrewjacks,leverdevices,push-pullrodsystems.

7.13 Control Cables 1 2 -

Swagingofendfittings;

Inspectionandtestingofcontrolcables;

Bowdencables;aircraftflexiblecontrolsystems.

7.14 Material handling

7.14.1 Sheet Metal - 2 -

Markingoutandcalculationofbendallowance;

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LEVEL

A B1 B2

Sheetmetalworking,includingbendingandforming;

Inspectionofsheetmetalwork.

7.14.2 Composite and non-metallic - 2 -

Bondingpractices;

Environmentalconditions

Inspectionmethods

7.15 Welding, Brazing, Soldering and Bonding

(a) - 2 2

Solderingmethods;inspectionofsolderedjoints.

(b) - 2 -

Weldingandbrazingmethods;

Inspectionofweldedandbrazedjoints;

Bondingmethodsandinspectionofbondedjoints.

7.16 Aircraft Weight and Balance

(a) - 2 2

CentreofGravity/Balancelimitscalculation:useofrelevantdocuments;

(b) - 2 -

Preparationofaircraftforweighing;

Aircraftweighing;

7.17 Aircraft Handling and Storage 2 2 2

Aircrafttaxiing/towingandassociatedsafetyprecautions;

Aircraftjacking,chocking,securingandassociatedsafetyprecautions;

Aircraftstoragemethods;

Refuelling/defuellingprocedures;

De-icing/anti-icingprocedures;

Electrical,hydraulicandpneumaticgroundsupplies.

Effectsofenvironmentalconditionsonaircrafthandlingandoperation.

7.18 Disassembly, Inspection, Repair and Assembly Techniques

(a) 2 3 3

Typesofdefectsandvisualinspectiontechniques.

Corrosionremoval,assessmentandreprotection.

(b) - 2 -

Generalrepairmethods,StructuralRepairManual;

Ageing,fatigueandcorrosioncontrolprogrammes;

(c) - 2 1

Non destructive inspection techniques including, penetrant, radiographic,eddycurrent,ultrasonicandboroscopemethods.

(d)

2

2

2

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LEVEL

A B1 B2

Disassemblyandre-assemblytechniques.

(e) - 2 2

Troubleshootingtechniques

7.19 Abnormal Events

(a) 2 2 2

InspectionsfollowinglightningstrikesandHIRFpenetration.

(b) 2 2 -

Inspectionsfollowingabnormaleventssuchasheavy

landingsandflightthroughturbulence.

7.20 Maintenance Procedures 1 2 2

Maintenanceplanning;

Modificationprocedures;

Storesprocedures;

Certification/releaseprocedures;

Interfacewithaircraftoperation;

MaintenanceInspection/QualityControl/QualityAssurance;

Additionalmaintenanceprocedures.

Controloflifelimitedcomponents

MODULE 7B. MAINTENANCE PRACTICES Note: The scope of this module shall reflect the technology of aeroplanes relevant

to the B3 category.

LEVEL

B3

7.1 Safety Precautions-Aircraft and Workshop 3

Aspectsofsafeworkingpracticesincludingprecautionstotakewhenworkingwithelectricity,gasesespeciallyoxygen,oilsandchemicals.

Also,instructionintheremedialactiontobetakenintheeventofafireoran-otheraccidentwithoneormoreofthesehazardsincludingknowledgeonex-tinguishingagents.

7.2 Workshop Practices 3

Careoftools,controloftools,useofworkshopmaterials;

Dimensions,allowancesandtolerances,standardsofworkmanship;

Calibrationoftoolsandequipment,calibrationstandards.

7.3 Tools 3

Commonhandtooltypes;

Commonpowertooltypes;

Operationanduseofprecisionmeasuringtools;

Lubricationequipmentandmethods.

Operation,functionanduseofelectricalgeneraltestequipment;

7.4 Avionic General Test Equipment -

Operation,functionanduseofavionicgeneraltestequipment.

7.5 Engineering Drawings, Diagrams and Standards 2

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to the B3 category.

LEVEL

B3

Drawingtypesanddiagrams,theirsymbols,dimensions,tolerancesandpro-jections;

Identifyingtitleblockinformation

Microfilm,microficheandcomputerisedpresentations;

Specification100oftheAirTransportAssociation(ATA)ofAmerica;

Aeronauticalandotherapplicablestandardsincluding

ISO,AN,MS,NASandMIL;

Wiringdiagramsandschematicdiagrams.

7.6 Fits and Clearances 2

Drillsizesforboltholes,classesoffits;

Commonsystemoffitsandclearances;

Scheduleoffitsandclearancesforaircraftandengines;

Limitsforbow,twistandwear;

Standardmethodsforcheckingshafts,bearingsandotherparts.

7.7 Electrical Wiring Interconnection System (EWIS) 2

Continuity,insulationandbondingtechniquesandtesting;

Useofcrimptools:handandhydraulicoperated;

Testingofcrimpjoints;

Connectorpinremovalandinsertion;

Co-axialcables:testingandinstallationprecautions;

Identificationofwiretypes,theirinspectioncriteriaand

damagetolerance.

Wiringprotectiontechniques:Cableloomingandloom

support,cableclamps,protectivesleevingtechniques

includingheatshrinkwrapping,shielding.

EWISinstallations,inspection,repair,maintenanceand

cleanlinessstandards.

7.8 Riveting 2

Rivetedjoints,rivetspacingandpitch;

Toolsusedforrivetinganddimpling;

Inspectionofrivetedjoints.

7.9 Pipes and Hoses 2

Bendingandbelling/flaringaircraftpipes;

Inspectionandtestingofaircraftpipesandhoses;

Installationandclampingofpipes.

7.10 Springs 1

Inspectionandtestingofsprings.

7.11 Bearings 2

Testing,cleaningandinspectionofbearings; Lubricationrequirementsofbearings;

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to the B3 category.

LEVEL

B3

Defectsinbearingsandtheircauses.

7.12 Transmissions 2

Inspectionofgears,backlash;

Inspectionofbeltsandpulleys,chainsandsprockets;

Inspectionofscrewjacks,leverdevices,push-pullrodsystems.

7.13 Control Cables 2

Swagingofendfittings;

Inspectionandtestingofcontrolcables;

Bowdencables;aircraftflexiblecontrolsystems.

7.14 Material handling

7.14.1 Sheet Metal 2

Markingoutandcalculationofbendallowance;

Sheetmetalworking,includingbendingandforming;

Inspectionofsheetmetalwork.

7.14.2 Composite and non-metallic 2

Bondingpractices;

Environmentalconditions

Inspectionmethods

7.15 Welding, Brazing, Soldering and Bonding

(a) 2

Solderingmethods;inspectionofsolderedjoints.

(b) 2

Weldingandbrazingmethods;

Inspectionofweldedandbrazedjoints;

Bondingmethodsandinspectionofbondedjoints.

7.16 Aircraft Weight and Balance

(a) 2

CentreofGravity/Balancelimitscalculation:useofrelevantdocuments;

(b) 2

Preparationofaircraftforweighing;

Aircraftweighing;

7.17 Aircraft Handling and Storage 2

Aircrafttaxiing/towingandassociatedsafetyprecautions;

Aircraftjacking,chocking,securingandassociatedsafetyprecautions;

Aircraftstoragemethods;

Refuelling/defuellingprocedures;

De-icing/anti-icingprocedures;

Electrical,hydraulicandpneumaticgroundsupplies.

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to the B3 category.

LEVEL

B3

Effectsofenvironmentalconditionsonaircrafthandlingandoperation.

7.18 Disassembly, Inspection, Repair and Assembly Techniques

(a) 3

Typesofdefectsandvisualinspectiontechniques.

Corrosionremoval,assessmentandreprotection.

(b) 2

Generalrepairmethods,StructuralRepairManual;

Ageing,fatigueandcorrosioncontrolprogrammes;

(c) 2

Non destructive inspection techniques including, penetrant, radiographic,eddycurrent,ultrasonicandboroscopemethods.

(d)

2

Disassemblyandre-assemblytechniques.

(e) 2

Troubleshootingtechniques

7.19 Abnormal Events

(a) 2

InspectionsfollowinglightningstrikesandHIRFpenetration.

(b) 2

Inspectionsfollowingabnormaleventssuchasheavy

landingsandflightthroughturbulence.

7.20 Maintenance Procedures 2

Maintenanceplanning;

Modificationprocedures;

Storesprocedures;

Certification/releaseprocedures;

Interfacewithaircraftoperation;

MaintenanceInspection/QualityControl/QualityAssurance;

Additionalmaintenanceprocedures.

Controloflifelimitedcomponents

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MODULE 8. BASIC AERODYNAMICS LEVEL

A B1 B2 B3

8.1 Physics of the Atmosphere 1 2 2 1

InternationalStandardAtmosphere(ISA),applicationtoaerodynamics.

8.2 Aerodynamics 1 2 2 1

Airflowaroundabody;

Boundarylayer,laminarandturbulentflow,freestreamflow,relativeairflow,upwashanddownwash,vortices,stagnation;

The terms:camber,chord,meanaerodynamicchord,profile(parasite)drag,induceddrag,centreofpressure,angleofattack,washinandwashout,fine-nessratio,wingshapeandaspectratio;

Thrust,Weight,AerodynamicResultant;

GenerationofLiftandDrag:AngleofAttack,Liftcoefficient,

Dragcoefficient,polarcurve,stall;

Aerofoilcontaminationincludingice,snow,frost.

8.3 Theory of Flight 1 2 2 1

Relationshipbetweenlift,weight,thrustanddrag;

Glideratio;

Steadystateflights,performance;

Theoryoftheturn;

Influenceofloadfactor:stall,flightenvelopeandstructurallimitations;

Liftaugmentation.

8.4 Flight Stability and Dynamics 1 2 2 1

Longitudinal,lateralanddirectionalstability(activeandpassive).

MODULE 9A. HUMAN FACTORS Note: This module does not apply to category B3. Relevant subject matters for category


LEVEL

A B1 B2

9.1 General 1 2 2

Theneedtotakehumanfactorsintoaccount;

Incidentsattributabletohumanfactors/humanerror;

‘Murphy's’law.

9.2 Human Performance and Limitations 1 2 2

Vision;

Hearing;

Informationprocessing;

Attentionandperception;

Memory;

Claustrophobiaandphysicalaccess.

9.3 Social Psychology 1 1 1

Responsibility:individualandgroup;

Motivationandde-motivation;

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MODULE 9A. HUMAN FACTORS Note: This module does not apply to category B3. Relevant subject matters for category


LEVEL

A B1 B2

Peerpressure;

‘Culture’issues;

Teamworking;

Management,supervisionandleadership

9.4 Factors Affecting Performance 2 2 2

Fitness/health;

Stress:domesticandworkrelated;

Timepressureanddeadlines;

Workload:overloadandunderload;

Sleepandfatigue,shiftwork;

Alcohol,medication,drugabuse.

9.5 Physical Environment 1 1 1

Noiseandfumes;

Illumination;

Climateandtemperature;

Motionandvibration;

Workingenvironment.

9.6 Tasks 1 1 1

Physicalwork;

Repetitivetasks;

Visualinspection;

Complexsystems.

9.7 Communication 2 2 2

Withinandbetweenteams;

Workloggingandrecording;

Keepinguptodate,currency;

Disseminationofinformation.

9.8 Human Error 1 2 2

Errormodelsandtheories;

Typesoferrorinmaintenancetasks;

Implicationsoferrors(i.eaccidents)

Avoidingandmanagingerrors.

9.9 Hazards in the Workplace 1 2 2

Recognisingandavoidinghazards;

Dealingwithemergencies.

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MODULE 9B. HUMAN FACTORS Note: The scope of this module shall reflect the less demanding environment of mainte-

nance for B3 licence holders.

LEVEL

B3

9.1 General 2

Theneedtotakehumanfactorsintoaccount;

Incidentsattributabletohumanfactors/humanerror;

‘Murphy's’law.

9.2 Human Performance and Limitations 2

Vision;

Hearing;

Informationprocessing;

Attentionandperception;

Memory;

Claustrophobiaandphysicalaccess.

9.3 Social Psychology 1

Responsibility:individualandgroup;

Motivationandde-motivation;

Peerpressure;

‘Culture’issues;

Teamworking;

Management,supervisionandleadership

9.4 Factors Affecting Performance 2

Fitness/health;

Stress:domesticandworkrelated;

Timepressureanddeadlines;

Workload:overloadandunderload;

Sleepandfatigue,shiftwork;

Alcohol,medication,drugabuse.

9.5 Physical Environment 1

Noiseandfumes;

Illumination;

Climateandtemperature;

Motionandvibration;

Workingenvironment.

9.6 Tasks 1

Physicalwork;

Repetitivetasks;

Visualinspection;

Complexsystems.

9.7 Communication 2

Withinandbetweenteams; Workloggingandrecording;

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MODULE 9B. HUMAN FACTORS Note: The scope of this module shall reflect the less demanding environment of mainte-

nance for B3 licence holders.

LEVEL

B3

Keepinguptodate,currency;

Disseminationofinformation.

9.8 Human Error 2

Errormodelsandtheories;

Typesoferrorinmaintenancetasks;

Implicationsoferrors(i.eaccidents)

Avoidingandmanagingerrors.

9.9 Hazards in the Workplace 2

Recognisingandavoidinghazards;

Dealingwithemergencies.

MODULE 10. AVIATION LEGISLATION LEVEL

A B1 B2 B3

10.1 Regulatory Framework 1 1 1 1

RoleofInternationalCivilAviationOrganisation;

TheAircraftActandRulesmadethereunder

RoleoftheDGCA;

RelationshipbetweenCAR-21,CAR-M,CAR-145,CAR-66,CAR147

TheAircraftRules(ApplicabletoAircraftMaintenanceandRelease)

Aeronautical InformationCirculars(ApplicabletoAircraftMaintenanceandRelease)

CARSections1and2

10.2 CAR-66 Certifying Staff - Maintenance 2 2 2 2

DetailedunderstandingofCAR-66.

10.3 CAR-145 — Approved Maintenance Organisations 2 2 2 2

DetailedunderstandingofCAR-145andCARMSubpartF

10.4 Aircraft Operations 1 1 1 1

CommercialAirTransport/CommercialOperations

AirOperatorsCertificates;

OperatorsResponsibilities, in particular regarding continuing airworthinessandmaintenance;

Documentstobecarriedonboard;

AircraftPlacarding(Markings);

10.5 Aircraft Certification

(a)General - 1 1 1

Certificationrules:suchasFAA&EACS23/25/27/29; TypeCertification;

SupplementalTypeCertification;

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MODULE 10. AVIATION LEGISLATION LEVEL

A B1 B2 B3

CAR-21Design/ProductionOrganisationApprovals.

AircraftModificationsandrepairsapprovalandcertification

Permittoflyrequirements

(b)Documents - 2 2 2

CertificateofAirworthiness;

CertificateofRegistration;

NoiseCertificate;

WeightSchedule;

RadioStationLicenceandApproval.

10.6 CAR-M DetailunderstandingofCARMprovisionsrelatedtoContinuingAirworthiness

2 2 2 2

DetailedunderstandingofCAR-M.

10.7 Applicable National and International Requirements

(a) 1 2 2 2

MaintenanceProgramme,Maintenancechecksandinspections;

MasterMinimumEquipmentLists,MinimumEquipment

List,DispatchDeviationLists;

AirworthinessDirectives;

ServiceBulletins,manufacturersserviceinformation;

Modificationsandrepairs;

Maintenancedocumentation:maintenancemanuals,structuralrepairmanual,illustratedpartscatalogue,etc.;

(b) - 1 1 1

Continuingairworthiness;

Testflights;

ETOPS/EDTO,maintenanceanddispatchrequirements;

RVSM,maintenanceanddispatchrequirements

RNP,MNPSOperations

AllWeatherOperations,

Category2/3operationsandminimumequipmentrequirements.

10.8 Safety Management System 2 2 2

StateSafetyProgramme

BasicSafetyConcepts

Hazards&SafetyRisks

SMSOperation

SMSSafetyperformance

SafetyAssurance

10.9 Fuel Tank Safety 2 2 2

SpecialFederalAviationRegulations(SFARs)from14CFRSFAR88oftheFAAandofJAATGL47

ConceptofCDCCL,

AirworthinessLimitationsItems(ALI)

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MODULE 11A. TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYS-TEMS

LEVEL

A1 B1.1

11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2

Operationandeffectof: —rollcontrol:aileronsandspoilers; —pitchcontrol:elevators,stabilators,variableincidencestabilisersandcanards; —yawcontrol,rudderlimiters; Controlusingelevons,ruddervators; Highliftdevices,slots,slats,flaps,flaperons; Draginducingdevices,spoilers,liftdumpers,speedbrakes; Effectsofwingfences,sawtoothleadingedges; Boundary layercontrolusing, vortexgenerators, stall wedgesor leadingedgede-vices; Operationandeffectoftrimtabs,balanceandantibalance(leading)tabs,servotabs,springtabs,massbalance,controlsurfacebias,aerodynamicbalancepanels;

11.1.2 High Speed Flight 1 2

Speedofsound,subsonicflight,transonicflight,supersonicflight,

Mach number, critical Mach number, compressibility buffet, shock wave, aerody-namicheating,arearule; Factorsaffectingairflowinengineintakesofhighspeedaircraft; EffectsofsweepbackoncriticalMachnumber. 11.2 Airframe Structures — General Concepts (a) 2 2

Airworthinessrequirementsforstructuralstrength; Structuralclassification,primary,secondaryandtertiary; Failsafe,safelife,damagetoleranceconcepts; Zonalandstationidentificationsystems; Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue;

Drainsandventilationprovisions; Systeminstallationprovisions; Lightningstrikeprotectionprovision. Aircraftbonding

(b) 1 2

Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,methodsofskinning,anti-corrosiveprotection,wing,empennageandengineattachments; Structureassemblytechniques:riveting,bolting,bonding

Methodsofsurfaceprotection,suchaschromating,anodising,painting; Surfacecleaning. Airframesymmetry:methodsofalignmentandsymmetrychecks.

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LEVEL

A1 B1.1

11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 1 2

Constructionandpressurisationsealing; Wing,stabiliser,pylonandundercarriageattachments; Seatinstallationandcargoloadingsystem;

Doorsandemergencyexits:construction,mechanisms,operationandsafetydevices; Windowsandwindscreenconstructionandmechanisms.

11.3.2 Wings (ATA 57) 1 2

Construction; Fuelstorage;

Landinggear,pylon,controlsurfaceandhighlift/dragattachments.

11.3.3 Stabilisers (ATA 55) 1 2

Construction; Controlsurfaceattachment. 11.3.4 Flight Control Surfaces (ATA 55/57) 1 2

Constructionandattachment; Balancing—massandaerodynamic. 11.3.5 Nacelles/Pylons (ATA 54) 1 2

Construction; Firewalls; Enginemounts. 11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 11.4.1 Air supply 1 2

Sourcesofairsupplyincludingenginebleed,APUandgroundcart; 11.4.2 Air Conditioning 1 3 Airconditioningsystems; Aircycleandvapourcyclemachines Distributionsystems; Flow,temperatureandhumiditycontrolsystem. 11.4.3 Pressurisation 1 3

Pressurisationsystems; Controlandindicationincludingcontrolandsafetyvalves; Cabinpressurecontrollers. 11.4.4 Safety and warning devices 1 3

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LEVEL

A1 B1.1

Protectionandwarningdevices. 11.5 Instruments/Avionic Systems 11.5.1 Instrument Systems (ATA 31) 1 2

Pitotstatic:altimeter,airspeedindicator,verticalspeedindicator; Gyroscopic:artificialhorizon,attitudedirector,directionindicator,horizontalsitua-tionindicator,turnandslipindicator,turncoordinator; Compasses:directreading,remotereading; Angleofattackindication,stallwarningsystems;GlassCockpit Otheraircraftsystemindication. 11.5.2 Avionic Systems 1 1

Fundamentalsofsystemlay-outsandoperationof; AutoFlight(ATA22); Communications(ATA23); NavigationSystems(ATA34). 11.6 Electrical Power (ATA 24) 1 3

BatteriesInstallationandOperation; DCpowergeneration; ACpowergeneration; Emergencypowergeneration; Voltageregulation; Powerdistribution; Inverters,transformers,rectifiers; Circuitprotection. External/Groundpower; 11.7 Equipment and Furnishings (ATA 25) (a) 2 2

Emergencyequipmentrequirements; Seats,harnessesandbelts. (b)

1

1

Cabinlay-out; Equipmentlay-out; CabinFurnishingInstallation; Cabinentertainmentequipment; Galleyinstallation; Cargohandlingandretentionequipment; Airstairs.

11.8 Fire Protection (ATA 26)

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LEVEL

A1 B1.1

(a) 1 3

Fireandsmokedetectionandwarningsystems; Fireextinguishingsystems;

Systemtests. (b) 1 1 Portablefireextinguisher 11.9 Flight Controls (ATA 27) 1 3

Primarycontrols:aileron,elevator,rudder,spoiler; Trimcontrol; Activeloadcontrol; Highliftdevices; Liftdump,speedbrakes; Systemoperation:manual,hydraulic,pneumatic,electrical,fly-by-wire; Artificialfeel,Yawdamper,Machtrim,rudderlimiter,gustlockssystems; Balancingandrigging; Stallprotection/warningsystem. 11.10 Fuel Systems (ATA 28) 1 3

Systemlay-out; Fueltanks; Supplysystems; Dumping,ventinganddraining; Cross-feedandtransfer; Indicationsandwarnings; Refuellinganddefuelling; Longitudinalbalancefuelsystems.

11.11 Hydraulic Power (ATA 29) 1 3

Systemlay-out; Hydraulicfluids; Hydraulicreservoirsandaccumulators; Pressuregeneration:electric,mechanical,pneumatic; Emergencypressuregeneration;Filters PressureControl; Powerdistribution; Indicationandwarningsystems; Interfacewithothersystems.

11.12 Ice and Rain Protection (ATA 30) 1 3

Iceformation,classificationanddetection; Anti-icingsystems:electrical,hotairandchemical; De-icingsystems:electrical,hotair,pneumaticandchemical; Rainrepellant;

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LEVEL

A1 B1.1

Probeanddrainheating. Wipersystems 11.13 Landing Gear (ATA 32) 2 3

Construction,shockabsorbing; Extensionandretractionsystems:normalandemergency; Indicationsandwarning; Wheels,brakes,antiskidandautobraking; Tyres; Steering.Air-groundsensing 11.14 Lights (ATA 33) 2 3

External:navigation,anti-collision,landing,taxiing,ice; Internal:cabin,cockpit,cargo; Emergency. 11.15 Oxygen (ATA 35) 1 3

Systemlay-out:cockpit,cabin; Sources,storage,charginganddistribution; Supplyregulation; Indicationsandwarnings; 11.16 Pneumatic/Vacuum (ATA 36) 1 3

Systemlay-out; Sources:engine/APU,compressors,reservoirs,groundsupply; Pressurecontrol; Distribution; Indicationsandwarnings; Interfaceswithothersystems. 11.17 Water/Waste (ATA 38) 2 3

Watersystemlay-out,supply,distribution,servicinganddraining; Toiletsystemlay-out,flushingandservicing; Corrosionaspects.

11.18 On Board Maintenance Systems (ATA 45) 1 2

Centralmaintenancecomputers; Dataloadingsystem; Electroniclibrarysystem; Printing; Structuremonitoring(damagetolerancemonitoring).

11.19 Integrated Modular Avionics (ATA42 )

1

2

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LEVEL

A1 B1.1 FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTraf-fic Communication, Avionics Communication Router, Electrical LoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingCon-trol,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndica-tion,OleoPressureIndication,BrakeTemperatureMonitoring,etc.

11.20 Cabin Systems (ATA44) Theunitsandcomponentswhichfurnishameansofentertainingthepassengersandprovidingcommunicationwithintheaircraft(CabinIntercommunicationDataSys-tem)andbetweentheaircraftcabinandgroundstations(CabinNetworkService).Includesvoice,data,musicandvideotransmissions.The Cabin Intercommunication Data System provides an interface between cock-pit/cabincrewandcabinsystems.Thesesystemssupportdataexchangeofthedif-ferentrelatedLRU'sandtheyaretypicallyoperatedviaFlightAttendantPanels.TheCabinNetworkServicetypicallyconsistsonaserver,typicallyinterfacingwith,amongothers,thefollowingsystems:—Data/RadioCommunication,In-FlightEntertainmentSystem.TheCabinNetworkServicemayhostfunctionssuchas:—Accesstopre-departure/departurereports,—E-mail/intranet/Internetaccess,—Passengerdatabase;CabinCoreSystem;In-flightEntertainmentSystem;ExternalCommunicationSystem;CabinMassMemorySystem;CabinMonitoringSystem;MiscellaneousCabinSystem.11.21 Information Systems (ATA46)

Theunitsandcomponentswhichfurnishameansofstoring,updatingandretrievingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.Includesunitsthatarededicatedtotheinformationstorageandretrievalfunctionsuchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponents installedforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNet-workServerSystemsAircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;

1

1

2

2

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LEVEL

A1 B1.1 MiscellaneousInformationSystem.

MODULE 11B. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS-TEMS

LEVEL

A2 B1.2

Note 1: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 11C. Note: The scope of this Module should reflect the technology of aeroplanes pertinent to the A2 and B1.2 subcategory.

11.1 Theory of Flight

11.1.1 Aeroplane Aerodynamics and Flight Controls 1 2

Operationandeffectof: —rollcontrol:aileronsandspoilers;

—pitchcontrol:elevators,stabilators,variableincidencestabilisersandcanards; —yawcontrol,rudderlimiters; Controlusingelevons,ruddervators; Highliftdevices,slots,slats,flaps,flaperons; Draginducingdevices,spoilers,liftdumpers,speedbrakes; Effectsofwingfences,sawtoothleadingedges; Boundary layercontrolusing,vortexgenerators, stallwedgesor leadingedgede-vices;

Operationandeffectoftrimtabs,balanceandantibalance(leading)tabs,servotabs,springtabs,massbalance,controlsurfacebias,aerodynamicbalancepanels; 11.1.2 High Speed Flight — N/A — - -

11.2 Airframe Structures — General Concepts (a) 2 2

Airworthinessrequirementsforstructuralstrength; Structuralclassification,primary,secondaryandtertiary; Failsafe,safelife,damagetoleranceconcepts; Zonalandstationidentificationsystems;

Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue; Drainsandventilationprovisions; Systeminstallationprovisions; Lightningstrikeprotectionprovision. Aircraftbonding (b) 1 2

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A2 B1.2

Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,methodsofskinning,anti-corrosiveprotection,wing,empennageandengineattachments; Structureassemblytechniques:riveting,bolting,bonding; Methodsofsurfaceprotection,suchaschromating, anodising,painting; Surfacecleaning; Airframesymmetry:methodsofalignmentandsymmetrychecks. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 1 2

Constructionandpressurisationsealing; Wing,tail-planepylonandundercarriageattachments; Seatinstallation; Doorsandemergencyexits:constructionandoperation; Windowandwindscreenattachment. 11.3.2 Wings (ATA 57) 1 2

Construction; Fuelstorage; Landinggear,pylon,controlsurfaceandhighlift/dragattachments. 11.3.3 Stabilisers (ATA 55) 1 2

Construction; Controlsurfaceattachment. 11.3.4 Flight Control Surfaces (ATA 55/57) 1 2

Constructionandattachment; Balancing—massandaerodynamic. 11.3.5 Nacelles/Pylons (ATA 54)

1 2

Nacelles/Pylons: —Construction; —Firewalls; —Enginemounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 1 3

Pressurisationandairconditioningsystems; Cabinpressurecontrollers,protectionandwarningdevices HeatingSystems

11.5 Instruments/Avionic Systems

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11.5.1 Instrument Systems (ATA 31) 1 2

Pitotstatic:altimeter,airspeedindicator,verticalspeedindicator; Gyroscopic:artificialhorizon,attitudedirector,directionindicator,horizontalsitua-tionindicator,turnandslipindicator,turncoordinator;

Compasses:directreading,remotereading; Angleofattackindication,stallwarningsystems.Glasscockpit; Otheraircraftsystemindication.

11.5.2 Avionic Systems 1 1

Fundamentalsofsystemlay-outsandoperationof: —AutoFlight(ATA22); —Communications(ATA23); —NavigationSystems(ATA34). 11.6 Electrical Power (ATA 24) 1 3

BatteriesInstallationandOperation; DCpowergeneration; Voltageregulation; Powerdistribution; Circuitprotection; Inverters,transformers. 11.7 Equipment and Furnishings (ATA 25) (a) 2 2

Emergencyequipmentrequirements; Seats,harnessesandbelts. (b) 1 1

Cabinlay-out; Equipmentlay-out; CabinFurnishingInstallation(level2); Cabinentertainmentequipment; Galleyinstallation; Cargohandlingandretentionequipment; Airstairs. 11.8 Fire Protection (ATA 26) (a) 1 3

Fireextinguishingsystems; Fireandsmokedetectionandwarningsystems; Systemtests. (b) 1 3 Portablefireextinguisher. 11.9 Flight Controls (ATA 27) 1 3

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Primarycontrols:aileron,elevator,rudder; Trimtabs; Highliftdevices; Systemoperation:manual; Gustlocks; Balancingandrigging; Stallwarningsystem. 11.10 Fuel Systems (ATA 28) 1 3

Systemlay-out; Fueltanks; Supplysystems; Cross-feedandtransfer; Indicationsandwarnings; Refuellinganddefuelling. 11.11 Hydraulic Power (ATA 29) 1 3

Systemlay-out; Hydraulicfluids; Hydraulicreservoirsandaccumulators; Pressuregeneration:electric,mechanical;Filters PressureControl; Powerdistribution; Indicationandwarningsystems. 11.12 Ice and Rain Protection (ATA 30) 1 3

Iceformation,classificationanddetection; De-icingsystems:electrical,hotair,pneumaticandchemical; Probeanddrainheating; Wipersystems. 11.13 Landing Gear (ATA 32) 2 3

Construction,shockabsorbing; Extensionandretractionsystems:normalandemergency; Indicationsandwarning; Wheels,brakes,antiskidandautobraking; Tyres; Steering.Air-groundsensing 11.14 Lights (ATA 33) 2 3

External:navigation,anticollision,landing,taxiing,ice; Internal:cabin,cockpit,cargo; Emergency.

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11.15 Oxygen (ATA 35) 1 3

Systemlay-out:cockpit,cabin; Sources,storage,charginganddistribution; Supplyregulation; Indicationsandwarnings; 11.16 Pneumatic/Vacuum (ATA 36) 1 3

Systemlay-out; Sources:engine/APU,compressors,reservoirs,groundsupply; Pressurecontrol; Distribution; Indicationsandwarnings; Interfaceswithothersystems. 11.17 Water/Waste (ATA 38) 2 3

Watersystemlay-out,supply,distribution,servicinganddraining; Toiletsystemlay-out,flushingandservicing; Corrosionaspects.

MODULE 11C. PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYS-TEMS

LEVEL

B3

Note: The scope of this module shall reflect the technology of aeroplanes pertinent to the B3 category.

11.1 Theory of Flight

11.1.1 Aeroplane Aerodynamics and Flight Controls 1

Operationandeffectof: —rollcontrol:aileronsandspoilers;

—pitchcontrol:elevators,stabilators,variableincidencestabilisersandcanards; —yawcontrol,rudderlimiters; Controlusingelevons,ruddervators; Highliftdevices,slots,slats,flaps,flaperons; Draginducingdevices,spoilers,liftdumpers,speedbrakes; Effectsofwingfences,sawtoothleadingedges;

Boundary layercontrolusing,vortexgenerators, stallwedgesor leadingedgede-vices;

Operationandeffectoftrimtabs,balanceandantibalance(leading)tabs,servotabs,springtabs,massbalance,controlsurfacebias,aerodynamicbalancepanels;

11.2 Airframe Structures — General Concepts

(a)

2

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Airworthinessrequirementsforstructuralstrength;

Structuralclassification,primary,secondaryandtertiary; Failsafe,safelife,damagetoleranceconcepts; Zonalandstationidentificationsystems;

Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue; Drainsandventilationprovisions; Systeminstallationprovisions; Lightningstrikeprotectionprovision. Aircraftbonding (b) 2

Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,methodsofskinning,anti-corrosiveprotection,wing,empennageandengineattachments; Structureassemblytechniques:riveting,bolting,bonding; Methodsofsurfaceprotection,suchaschromating, anodising,painting; Surfacecleaning; Airframesymmetry:methodsofalignmentandsymmetrychecks. 11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 1 Constructionandpressurisationsealing; Wing,tail-planepylonandundercarriageattachments; Seatinstallation; Doorsandemergencyexits:constructionandoperation; Windowandwindscreenattachment. 11.3.2 Wings (ATA 57) 1 Construction; Fuelstorage; Landinggear,pylon,controlsurfaceandhighlift/dragattachments. 11.3.3 Stabilisers (ATA 55) 1 Construction; Controlsurfaceattachment. 11.3.4 Flight Control Surfaces (ATA 55/57) 1 Constructionandattachment; Balancing—massandaerodynamic. 11.3.5 Nacelles/Pylons (ATA 54)

1 Nacelles/Pylons:

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—Construction; —Firewalls; —Enginemounts.

11.4 Air Conditioning (ATA 21) 1 HeatingandventilationSystems

11.5 Instruments/Avionic Systems

11.5.1 Instrument Systems (ATA 31) 1 Pitotstatic:altimeter,airspeedindicator,verticalspeedindicator; Gyroscopic:artificialhorizon,attitudedirector,directionindicator,horizontalsitua-tionindicator,turnandslipindicator,turncoordinator;

Compasses:directreading,remotereading; Angleofattackindication,stallwarningsystems.Glasscockpit; Otheraircraftsystemindication.

11.5.2 Avionic Systems 1 Fundamentalsofsystemlay-outsandoperationof: —AutoFlight(ATA22); —Communications(ATA23); —NavigationSystems(ATA34). 11.6 Electrical Power (ATA 24) 2 BatteriesInstallationandOperation; DCpowergeneration; Voltageregulation; Powerdistribution; Circuitprotection; Inverters,transformers. 11.7 Equipment and Furnishings (ATA 25) 2 Emergencyequipmentrequirements; Seats,harnessesandbelts. 11.8 Fire Protection (ATA 26) 2 Portablefireextinguisher. 11.9 Flight Controls (ATA 27) 3 Primarycontrols:aileron,elevator,rudder; Trimtabs; Highliftdevices; Systemoperation:manual; Gustlocks; Balancingandrigging;

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Stallwarningsystem. 11.10 Fuel Systems (ATA 28) 2 Systemlay-out; Fueltanks; Supplysystems; Cross-feedandtransfer; Indicationsandwarnings; Refuellinganddefuelling. 11.11 Hydraulic Power (ATA 29) 2 Systemlay-out; Hydraulicfluids; Hydraulicreservoirsandaccumulators; Pressuregeneration:electric,mechanical;Filters PressureControl; Powerdistribution; Indicationandwarningsystems. 11.12 Ice and Rain Protection (ATA 30) 1 Iceformation,classificationanddetection; De-icingsystems:electrical,hotair,pneumaticandchemical; Probeanddrainheating; Wipersystems. 11.13 Landing Gear (ATA 32) 2 Construction,shockabsorbing; Extensionandretractionsystems:normalandemergency; Indicationsandwarning; Wheels,brakes,antiskidandautobraking; Tyres; Steering. 11.14 Lights (ATA 33) 2 External:navigation,anticollision,landing,taxiing,ice; Internal:cabin,cockpit,cargo; Emergency. 11.15 Oxygen (ATA 35) 2 Systemlay-out:cockpit,cabin; Sources,storage,charginganddistribution; Supplyregulation; Indicationsandwarnings;

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11.16 Pneumatic/Vacuum (ATA 36) 2 Systemlay-out; Sources:engine/APU,compressors,reservoirs,groundsupply; PressureandvaccumpumpsPressurecontrol; Distribution; Indicationsandwarnings; Interfaceswithothersystems.

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS LEVEL

A3 A4

B1.3 B1.4

12.1 Theory of Flight — Rotary Wing Aerodynamics 1 2

Terminology; Effectsofgyroscopicprecession; Torquereactionanddirectionalcontrol; Dissymmetryoflift,Bladetipstall; Translatingtendencyanditscorrection; Corioliseffectandcompensation; Vortexringstate,powersettling,overpitching; Auto-rotation; Groundeffect. 12.2 Flight Control Systems 2 3

Cycliccontrol; Collectivecontrol; Swashplate; Yawcontrol:Anti-TorqueControl,Tailrotor,bleedair; MainRotorHead:DesignandOperationfeatures; BladeDampers:Functionandconstruction; RotorBlades:Mainandtailrotorbladeconstructionandattachment;

Trimcontrol,fixedandadjustablestabilisers; Systemoperation:manual,hydraulic,electricalandflyby-wire; Artificialfeel; BalancingandRigging. 12.3 Blade Tracking and Vibration Analysis 1 3

Rotoralignment; Mainandtailrotortracking; Staticanddynamicbalancing; Vibrationtypes,vibrationreductionmethods; Groundresonance. 12.4 Transmissions 1 3

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A3 A4

B1.3 B1.4

Gearboxes,mainandtailrotors; Clutches,freewheelunitsandrotorbrake. Tailrotordriveshafts,flexiblecouplings,bearings, vibrationdampersandbearinghangers 12.5 Airframe Structures (a) 2 2

Airworthinessrequirementsforstructuralstrength; Structuralclassification,primary,secondaryandtertiary; Failsafe,safelife,damagetoleranceconcepts; Zonalandstationidentificationsystems; Stress,strain,bending,compression,shear,torsion,tension,hoopstress,fatigue; Drainsandventilationprovisions; Systeminstallationprovisions; Lightningstrikeprotectionprovision. (b) 1 2 Constructionmethodsof:stressedskinfuselage,formers,stringers,longerons,bulk-heads,frames,doublers,struts,ties,beams,floorstructures,reinforcement,meth-odsofskinningandanti-corrosiveprotection.

Pylon,stabiliserandundercarriageattachments; Seatinstallation; Doors:construction,mechanisms,operationandsafetydevices; Windowsandwindscreenconstruction; Fuelstorage; Firewalls; Enginemounts; Structureassemblytechniques:riveting,bolting,bonding; Methodsofsurfaceprotection,suchaschromating,anodising,painting; Surfacecleaning. Airframesymmetry:methodsofalignmentandsymmetrychecks. 12.6 Air Conditioning (ATA 21) 12.6.1 Air supply 1 2

Sourcesofairsupplyincludingenginebleedandgroundcart; 12.6.2 Air Conditioning 1 3

Airconditioningsystems; Distributionsystems; Flowandtemperaturecontrolsystems; Protectionandwarningdevices. 12.7 Instruments/Avionic Systems 12.7.1 Instrument Systems (ATA 31) 1 2

Pitotstatic:altimeter,airspeedindicator,verticalspeedindicator;

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A3 A4

B1.3 B1.4

Gyroscopic:artificialhorizon,attitudedirector,directionindicator,horizontalsitua-tionindicator,turnandslipindicator,turncoordinator; Compasses:directreading,remotereading; Vibrationindicatingsystems—HUMS;GlassCockpit Otheraircraftsystemindication. 12.7.2 Avionic Systems 1 1

Fundamentalsofsystemlayoutsandoperationof: AutoFlight(ATA22); Communications(ATA23); NavigationSystems(ATA34). 12.8 Electrical Power (ATA 24) 1 3

BatteriesInstallationandOperation; DCpowergeneration,ACpowergeneration; Emergencypowergeneration; Voltageregulation,Circuitprotection. Powerdistribution; Inverters,transformers,rectifiers; External/Groundpower. 12.9 Equipment and Furnishings (ATA 25) (a) 2 2

Emergencyequipmentrequirements; Seats,harnessesandbelts; Liftingsystems. (b) 1 1

Emergencyflotationsystems; Cabinlay-out,cargoretention; Equipmentlay-out; CabinFurnishingInstallation. 12.10 Fire Protection (ATA 26) 1 3

Fireandsmokedetectionandwarningsystems; Fireextinguishingsystems; Systemtests.

12.11 Fuel Systems (ATA 28) 1 3

Systemlay-out; Fueltanks; Supplysystems; Dumping,ventinganddraining; Cross-feedandtransfer; Indicationsandwarnings;

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A3 A4

B1.3 B1.4

Refuellinganddefuelling. 12.12 Hydraulic Power (ATA 29) 1 3

Systemlay-out; Hydraulicfluids; Hydraulicreservoirsandaccumulators; Pressuregeneration:electric,mechanical,pneumatic; Emergencypressuregeneration;Filters PressureControl; Powerdistribution; Indicationandwarningsystems; Interfacewithothersystems. 12.13 Ice and Rain Protection (ATA 30) 1 3

Iceformation,classificationanddetection; Anti-icingandde-icingsystems:electrical,hotairandchemical;

Rainrepellantandremoval;

Probeanddrainheating. Wipersystem 12.14 Landing Gear (ATA 32) 2 3

Construction,shockabsorbing; Extensionandretractionsystems:normalandemergency; Indicationsandwarning; Wheels,tyres,brakes; Steering;Air-groundsensing Skids,floats.

12.15 Lights (ATA 33) 2 3

External:navigation,landing,taxiing,ice; Internal:cabin,cockpit,cargo; Emergency.

12.16 Pneumatic/Vacuum (ATA 36) 1 3

Systemlay-out; Sources:engine,compressors,reservoirs,groundsupply.; Pressurecontrol; Distribution; Indicationsandwarnings; Interfaceswithothersystems.12.17 Integrated Modular Avionics (ATA42)

1

2

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A3 A4

B1.3 B1.4

FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTrafficCommunication,Avion-icsCommunicationRouter,ElectricalLoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingControl,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndication,OleoPressureIndication,BrakeTemperatureMonitoring,etc.CoreSystem;NetworkComponents.12.18 On Board Maintenance Systems (ATA45) Centralmaintenancecomputers;Dataloadingsystem;Electroniclibrarysystem;Printing;Structuremonitoring(damagetolerancemonitoring).12.19 Information Systems (ATA46) Theunitsandcomponentswhichfurnishameansofstoring,updatingandretrievingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.Includesunitsthatarededicatedtotheinformationstorageandretrievalfunctionsuchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponentsinstalledforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNet-workServerSystems.AircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;MiscellaneousInformationSystem.

1

1

2

2

MODULE 13. AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

LEVEL

B2

13.1 Theory of Flight 1

(a)AeroplaneAerodynamicsandFlightControls

Operationandeffectof:

—rollcontrol:aileronsandspoilers,

—pitchcontrol:elevators,stabilators,variableincidencestabilisersandcanards,

—yawcontrol,rudderlimiters;

Controlusingelevons,ruddervators;

Highliftdevices:slots,slats,flaps;

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B2

Draginducingdevices:spoilers,liftdumpers,speedbrakes;

Operationandeffectoftrimtabs,servotabs,controlsurfacebias;

(b)HighSpeedFlightSpeedofsound,subsonicflight,transonicflight,supersonicflight;Machnumber,criticalMachnumber;(c)RotaryWingAerodynamicsTerminology;Operationandeffectofcyclic,collectiveandanti-torquecontrols.

1

1

13.2 Structures — General Concepts

(a)Fundamentalsofstructuralsystems;

1

(b)Zonalandstationidentificationsystems;Electricalbonding;Lightningstrikeprotectionprovision.

2

13.3 Autoflight (ATA 22) 3

Fundamentalsofautomaticflightcontrolincludingworkingprinciplesandcurrent

terminology;

Commandsignalprocessing;

Modesofoperation:roll,pitchandyawchannels;

Yawdampers;

StabilityAugmentationSysteminhelicopters;

Automatictrimcontrol;

Autopilotnavigationaidsinterface;

Autothrottlesystems;

AutomaticLandingSystems:principlesandcategories,modesofoperation,ap-

proach,glideslope,land,

go-around,systemmonitorsandfailureconditions.

13.4 Communication/Navigation (ATA 23/34)

Fundamentalsofradiowavepropagation,antennas,transmissionlines,communi-

cation,receiverand

transmitter;

Workingprinciplesoffollowingsystems:

—VeryHighFrequency(VHF)communication,

—HighFrequency(HF)communication,

—Audio,

—EmergencyLocatorTransmitters,

—CockpitVoiceRecorder,

—VeryHighFrequencyomnidirectionalrange(VOR),

—AutomaticDirectionFinding(ADF),

—InstrumentLandingSystem(ILS),

—MicrowaveLandingSystem(MLS),

3

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B2

—FlightDirectorsystems,DistanceMeasuringEquipment(DME),

—VeryLowFrequencyandhyperbolicnavigation(VLF/Omega),

—Dopplernavigation,

—Areanavigation,RNAVsystems,

—FlightManagementSystems,

—GlobalPositioningSystem(GPS),GlobalNavigationSatelliteSystems(GNSS),

—InertialNavigationSystem,

—AirTrafficControltransponder,secondarysurveillanceradar,

—TrafficAlertandCollisionAvoidanceSystem(TCAS),

—Weatheravoidanceradar,

—Radioaltimeter,

—ARINCcommunicationandreporting.

13.5 Electrical Power (ATA 24)

BatteriesInstallationandOperation;

DCpowergeneration;

ACpowergeneration;

Emergencypowergeneration;

Voltageregulation;

Powerdistribution;

Inverters,transformers,rectifiers;

Circuitprotection;

External/Groundpower.

3

13.6 Equipment and Furnishings (ATA 25)

Electronicemergencyequipmentrequirements;

Cabinentertainmentequipment.

3

13.7 Flight Controls (ATA 27)(a)Primarycontrols:aileron,elevator,rudder,spoiler;Trimcontrol;Activeloadcontrol;Highliftdevices;Liftdump,speedbrakes;Systemoperation:manual,hydraulic,pneumatic;Artificialfeel,Yawdamper,Machtrim,rudderlimiter,gustlocks.Stallprotectionsystems;(b)Systemoperation:electrical,fly-by-wire.

2

3

13.8 Instruments (ATA 31) Classification;Atmosphere;Terminology;Pressuremeasuringdevicesandsystems;Pitotstaticsystems;

3

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Altimeters;Verticalspeedindicators;Airspeedindicators;Machmeters;Altitudereporting/alertingsystems;Airdatacomputers;Instrumentpneumaticsystems;Directreadingpressureandtemperaturegauges;Temperatureindicatingsystems;Fuelquantityindicatingsystems;Gyroscopicprinciples;Artificialhorizons;Slipindicators;Directionalgyros;GroundProximityWarningSystems;Compasssystems;FlightDataRecordingsystems;ElectronicFlightInstrumentSystems;Instrumentwarningsystemsincludingmasterwarningsystemsandcentralisedwarningpanels;Stallwarningsystemsandangleofattackindicatingsystems;Vibrationmeasurementandindication;Glasscockpit

13.9 Lights (ATA 33) 3

External:navigation,landing,taxiing,ice;

Internal:cabin,cockpit,cargo;

Emergency.

13.10 On Board Maintenance Systems (ATA 45)

Centralmaintenancecomputers;

Dataloadingsystem;

Electroniclibrarysystem;

Printing;

Structuremonitoring(damagetolerancemonitoring).

3

13.11 Air Conditioning and Cabin Pressurisation (ATA21) 1)Airsupply Sourcesofairsupplyincludingenginebleed,APUandgroundcart; 2)AirConditioningAirconditioningsystems;Aircycleandvapourcyclemachines;Distributionsystems;Flow,temperatureandhumiditycontrolsystem.

2

2313

3)Pressurisation

Pressurisationsystems;

Controlandindicationincludingcontrolandsafetyvalves;

Cabinpressurecontrollers.

3

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B2

4)Safetyandwarningdevices

Protectionandwarningdevices. 3

13.12 Fire Protection (ATA 26) 3

(a)Fireandsmokedetectionandwarningsystems;Fireextinguishingsystems;Systemtests;

(b)Portablefireextinguisher

1

13.13 Fuel Systems (ATA 28)Systemlay-out;Fueltanks;Supplysystems;Dumping,ventinganddraining;Cross-feedandtransfer;Indicationsandwarnings;Refuellinganddefuelling;Longitudinalbalancefuelsystems.

11112323

13.14 Hydraulic Power (ATA 29)Systemlay-out;Hydraulicfluids;Hydraulicreservoirsandaccumulators;Pressuregeneration:electrical,mechanical,pneumatic;Emergencypressuregeneration;Filters;Pressurecontrol;Powerdistribution;Indicationandwarningsystems;Interfacewithothersystems.

1113313133

13.15 Ice and Rain Protection (ATA 30) Iceformation,classificationanddetection;Anti-icingsystems:electrical,hotairandchemical;De-icingsystems:electrical,hotair,pneumatic,chemical;Rainrepellent;Probeanddrainheating;WiperSystems.

223131

13.16 Landing Gear (ATA 32)

Construction,shockabsorbing; 1

Extensionandretractionsystems:normalandemergency; 3

Indicationsandwarnings; 3

Wheels,brakes,antiskidandautobraking; 3

Tyres; 1

Steering; 3

Air-groundsensing. 3

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13.17 Oxygen (ATA 35)

Systemlay-out:cockpit,cabin; 33Sources,storage,charginganddistribution;

Supplyregulation; 3

Indicationsandwarnings. 3

13.18 Pneumatic/Vacuum (ATA 36)

Systemlay-out; 2

Sources:engine/APU,compressors,reservoirs,groundsupply; 2

Pressurecontrol; 3

Distribution; 1

Indicationsandwarnings; 3

Interfaceswithothersystems. 3

13.19 Water/Waste (ATA 38) 2

Watersystemlay-out,supply,distribution,servicinganddraining;

Toiletsystemlay-out,flushingandservicing.

13.20 Integrated Modular Avionics (ATA42) 3

FunctionsthatmaybetypicallyintegratedintheIntegratedModularAvionic(IMA)modulesare,amongothers:

BleedManagement,AirPressureControl,AirVentilationandControl,AvionicsandCockpitVentilationControl,TemperatureControl,AirTrafficCommunication,Avion-icsCommunicationRouter,ElectricalLoadManagement,CircuitBreakerMonitoring,ElectricalSystemBITE,FuelManagement,BrakingControl,SteeringControl,LandingGearExtensionandRetraction,TyrePressureIndication,OleoPressureIndication,BrakeTemperatureMonitoring,etc.;

CoreSystem;

NetworkComponents.

13.21 Cabin Systems (ATA44) 3

Theunitsandcomponentswhichfurnishameansofentertainingthepassengersandprovidingcommunicationwithintheaircraft(CabinIntercommunicationDataSys-tem)andbetweentheaircraftcabinandgroundstations(CabinNetworkService).Includesvoice,data,musicandvideotransmissions.

The Cabin Intercommunication Data System provides an interface between cock-pit/cabincrewandcabinsystems.Thesesystemssupportdataexchangeofthedif-ferentrelatedLRU'sandtheyaretypicallyoperatedviaFlightAttendantPanels.

TheCabinNetworkServicetypicallyconsistsonaserver,typicallyinterfacingwith,amongothers,thefollowingsystems:

—Data/RadioCommunication,In-FlightEntertainmentSystem

TheCabinNetworkServicemayhostfunctionssuchas:

—Accesstopre-departure/departurereports,—E-mail/intranet/Internetaccess,—Passengerdatabase;

CabinCoreSystem;

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In-flightEntertainmentSystem;

ExternalCommunicationSystem;CabinMassMemorySystem;CabinMonitoringSystem;MiscellaneousCabinSystem.

13.22 Information Systems (ATA46) 3

Theunitsandcomponentswhichfurnishameansofstoring,updatingandretriev-ingdigitalinformationtraditionallyprovidedonpaper,microfilmormicrofiche.In-cludesunitsthatarededicatedtotheinformationstorageandretrievalfunctionsuchastheelectroniclibrarymassstorageandcontroller.Doesnotincludeunitsorcomponentsinstalledforotherusesandsharedwithothersystems,suchasflightdeckprinterorgeneralusedisplay.TypicalexamplesincludeAirTrafficandInformationManagementSystemsandNetworkServerSystems.AircraftGeneralInformationSystem;FlightDeckInformationSystem;MaintenanceInformationSystem;PassengerCabinInformationSystem;MiscellaneousInformationSystem.

MODULE 14. PROPULSION

LEVEL

B2

14.1 Turbine Engines (a) 1

Constructionalarrangementandoperationofturbojet,turbofan,turboshaftandturbopropellerengines; (b) 2 ElectronicEnginecontrolandfuelmeteringsystems(FADEC). 14.2 Engine Indicating Systems 2

Exhaustgastemperature/Interstageturbinetemperaturesystems; Enginespeed;

EngineThrustIndication:EnginePressureRatio,engineturbinedischargepressureorjetpipepressuresystems; Oilpressureandtemperature; Fuelpressure,temperatureandflow;

Manifoldpressure; Enginetorque; Propellerspeed.14.3 Starting and Ignition Systems Operationofenginestartsystemsandcomponents;Ignitionsystemsandcomponents;Maintenancesafetyrequirements

2

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MODULE 15. GAS TURBINE ENGINE

LEVEL

A

B1

15.1 Fundamentals 1 2 Potentialenergy,kineticenergy,Newton'slawsofmotion,Braytoncycle;

Therelationshipbetweenforce,work,power,energy,velocity,acceleration;

Constructionalarrangementandoperationofturbojet,turbofan,turboshaft,turboprop.

15.2 Engine Performance - 2 Gross thrust, net thrust, choked nozzle thrust, thrust distribution, resultant thrust,thrusthorsepower,equivalentshafthorsepower,specificfuelconsumption; Engineefficiencies; By-passratioandenginepressureratio;

Pressure,temperatureandvelocityofthegasflow;

Engineratings,staticthrust,influenceofspeed,altitudeandhotclimate,flatrating,limitations.

15.3 Inlet 2 2

Compressorinletducts Effectsofvariousinletconfigurations; Iceprotection. 15.4 Compressors 1 2

Axialandcentrifugaltypes; Constructionalfeaturesandoperatingprinciplesandapplications; Fanbalancing; Operation: Causesandeffectsofcompressorstallandsurge; Methods of air flow control: bleed valves, variable inlet guide vanes, variable statorvanes,rotatingstatorblades; Compressorratio.

15.5 Combustion Section 1 2

Constructionalfeaturesandprinciplesofoperation. 15.6 Turbine Section 2 2

Operationandcharacteristicsofdifferentturbinebladetypes; Bladetodiskattachment; Nozzleguidevanes; Causesandeffectsofturbinebladestressandcreep. 15.7 Exhaust 1 2

Constructionalfeaturesandprinciplesofoperation; Convergent,divergentandvariableareanozzles; Enginenoisereduction;

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LEVEL

A

B1

Thrustreversers. 15.8 Bearings and Seals - 2 Constructionalfeaturesandprinciplesofoperation. 15.9 Lubricants and Fuels 1 2

Propertiesandspecifications; Fueladditives; Safetyprecautions. 15.10 Lubrication Systems 1 2

Systemoperation/lay-outandcomponents. 15.11 Fuel Systems 1 2

Operationofenginecontrolandfuelmeteringsystems includingelectronicenginecontrol(FADEC); Systemslay-outandcomponents. 15.12 Air Systems 1 2 Operation of engine air distribution and anti-ice control systems, including internalcooling,sealingandexternalairservices. 15.13 Starting and Ignition Systems 1 2

Operationofenginestartsystemsandcomponents; Ignitionsystemsandcomponents; Maintenancesafetyrequirements. 15.14 Engine Indication Systems 1 2

ExhaustGasTemperature/InterstageTurbine Temperature; EngineThrustIndication:EnginePressureRatio,engineturbinedischargepressureorjetpipepressuresystems; Oilpressureandtemperature; Fuelpressureandflow; Enginespeed; Vibrationmeasurementandindication; Torque; Power. 15.15 Power Augmentation Systems - 1

Operationandapplications; Waterinjection,watermethanol; Afterburnersystems. 15.16 Turbo-prop Engines 1 2

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LEVEL

A

B1

Gascoupled/freeturbineandgearcoupledturbines; Reductiongears; Integratedengineandpropellercontrols; Overspeedsafetydevices. 15.17 Turbo-shaft engines 1 2

Arrangements,drivesystems,reductiongearing, couplings,controlsystems. 15.18 Auxiliary Power Units (APUs) 1 2

Purpose,operation,protectivesystems. 15.19 Power plant Installation 1 2

Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibrationmounts,hoses,pipes,feeders,connectors,wiringlooms,controlcablesandrods,liftingpointsanddrains. 15.20 Fire Protection Systems 1 2

Operationofdetectionandextinguishingsystems. 15.21 Engine Monitoring and Ground Operation 1 3

Proceduresforstartingandgroundrun-up; Interpretationofenginepoweroutputandparameters;

Trend(includingoilanalysis,vibrationandboroscope)monitoring; Inspectionofengineandcomponentstocriteria,tolerancesanddataspecifiedbyenginemanufacturer; Compressorwashing/cleaning; ForeignObjectDamage. 15.22 Engine Storage and Preservation - 2

Preservationanddepreservationfortheengineandaccessories/systems.

MODULE 16. PISTON ENGINE LEVEL

A B1 B3

16.1 Fundamentals 1 2 2

Mechanical,thermalandvolumetricefficiencies;

Operatingprinciples—2stroke,4stroke,OttoandDiesel;

Pistondisplacementandcompressionratio;

Engineconfigurationandfiringorder.

16.2 Engine Performance 1 2 2

Powercalculationandmeasurement;

Factorsaffectingenginepower;

Mixtures/leaning,pre-ignition.

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A B1 B3

16.3 Engine Construction 1 2 2

Crankcase,crankshaft,camshafts,sumps;

Accessorygearbox;

Cylinderandpistonassemblies;

Connectingrods,inletandexhaustmanifolds;

Valvemechanisms;

Propellerreductiongearboxes.

16.4 Engine Fuel Systems

16.4.1 Carburetors 1 2 2

Types,constructionandprinciplesofoperation;

Icingandheating.

16.4.2 Fuel injection systems 1 2 2

Types,constructionandprinciplesofoperation.

16.4.3 Electronic engine control 1 2 2

Operationofenginecontrolandfuelmeteringsystems

includingelectronicenginecontrol(FADEC);

Systemslay-outandcomponents.

16.5 Starting and Ignition Systems 1 2 2

Startingsystems,pre-heatsystems;

Magnetotypes,constructionandprinciplesofoperation;

Ignitionharnesses,sparkplugs;

Lowandhightensionsystems.

16.6 Induction, Exhaust and Cooling Systems 1 2 2

Constructionandoperationof:inductionsystems

includingalternateairsystems;

Exhaustsystems,enginecoolingsystems—airandliquid.

16.7 Supercharging/Turbocharging 1 2 2

Principlesandpurposeofsupercharginganditseffectsonengineparameters;

Constructionandoperationofsupercharging/turbochargingsystems;

Systemterminology;

Controlsystems;

Systemprotection.

16.8 Lubricants and Fuels 1 2 2

Propertiesandspecifications;

Fueladditives;

Safetyprecautions.

16.9 Lubrication Systems 1 2 2

Systemoperation/lay-outandcomponents.

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A B1 B3

16.10 Engine Indication Systems 1 2 2

Enginespeed;

Cylinderheadtemperature;

Coolanttemperature;

Oilpressureandtemperature;

ExhaustGasTemperature;

Fuelpressureandflow;

Manifoldpressure.

16.11 Powerplant Installation 1 2 2 Configuration of firewalls, cowlings, acoustic panels, engine mounts, anti-vibrationmounts,hoses,pipes,feeders,connectors,wiringlooms,controlcablesandrods,lift-ingpointsanddrains.

16.12 Engine Monitoring and Ground Operation 1 3 2 Proceduresforstartingandgroundrun-up;

Interpretationofenginepoweroutputandparameters;

Inspectionofengineandcomponents:criteria,tolerances,anddataspecifiedbyenginemanufacturer.

16.13 Engine Storage and Preservation - 2 1

Preservationanddepreservationfortheengineandaccessories/systems

MODULE 17A. PROPELLER Note: ThismoduledoesnotapplytocategoryB3.Relevantsubjectmattersforcategory

B3aredefinedinmodule17B.

LEVEL

A B1

17.1 Fundamentals 1 2

Bladeelementtheory; High/lowbladeangle,reverseangle,angleofattack,rotationalspeed; Propellerslip; Aerodynamic,centrifugal,andthrustforces; Torque; Relativeairflowonbladeangleofattack; Vibrationandresonance.

17.2 Propeller Construction 1 2 Constructionmethodsandmaterialsusedinwooden,compositeandmetalpropellers;

Bladestation,bladeface,bladeshank,bladebackandhubassembly; Fixedpitch,controllablepitch,constantspeedingpropeller; Propeller/spinnerinstallation.

17.3 Propeller Pitch Control 1 2

Speedcontrolandpitchchangemethods,mechanicalandelectrical/electronic; Featheringandreversepitch;

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Overspeedprotection.

17.4 Propeller Synchronising - 2 Synchronisingandsynchrophasingequipment.

17.5 Propeller Ice Protection 1 2 Fluidandelectricalde-icingequipment. 17.6 Propeller Maintenance 1 3

Staticanddynamicbalancing; Bladetracking; Assessmentofbladedamage,erosion,corrosion,impactdamage,delamination; Propellertreatment/repairschemes; Propellerenginerunning.

17.7 Propeller Storage and Preservation 1 2

Propellerpreservationanddepreservation

MODULE 17B. PROPELLER Note: ThescopeofthisModuleshallreflectthepropellertechnologyofaeroplanesper-

tinenttotheB3category.

LEVEL

B3

17.1 Fundamentals 2

2

2

2

2

Bladeelementtheory;

High/lowbladeangle,reverseangle,angleofattack,rotationalspeed;

Propellerslip;

Aerodynamic,centrifugal,andthrustforces;

Torque;

Relativeairflowonbladeangleofattack;

Vibrationandresonance.

17.2 Propeller Construction Constructionmethodsandmaterialsusedinwooden,compositeandmetalpropellers;

Bladestation,bladeface,bladeshank,bladebackandhubassembly;

Fixedpitch,controllablepitch,constantspeedingpropeller;

Propeller/spinnerinstallation.

17.3 Propeller Pitch Control

Speedcontrolandpitchchangemethods,mechanicalandelectrical/electronic;

Featheringandreversepitch;

Overspeedprotection.

17.4 Propeller Synchronising Synchronisingandsynchrophasingequipment.

17.5 Propeller Ice Protection Fluidandelectricalde-icingequipment.

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17.6 Propeller Maintenance

2

2

Staticanddynamicbalancing;

Bladetracking;

Assessmentofbladedamage,erosion,corrosion,impactdamage,delamination;

Propellertreatment/repairschemes;

Propellerenginerunning.

17.7 Propeller Storage and Preservation

Propellerpreservationanddepreservation

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Appendix II –Basic Examination Standard

1. General

1.1 Allbasicexaminationsmustbecarriedoutusingthemultiplechoicequestion.

1.2 Eachmultiplechoicequestionsmusthavemorethantwoalternativeanswers

ofwhichonlyonemustbethecorrectanswerandthecandidateshallbeallowed

atimepermodulewhichisbaseduponanominalaverageof75secondsper

question.

1.3 ThepassmarkforCAR-66moduleandsub-modulemultiplechoicepartofthe

examinationis75%.

1.4 Penalty marking systems is not used to determine whether a candidate has

passed.

1.5 Afailedmodulemaynotberetakenforatleast90daysfollowingthedateofthefailedmoduleexaminationexceptinthecaseofanapprovedmaintenancetrain-ingorganisationwhichconductsacourseofretrainingtailoredtothefailedsub-jectsintheparticularmodule.Insuchcase,thefailedmodulemayberetakenafter30days.Further,incaseoffailedmodulerelatedtolimitationpapers,suchmodulesmayberetakenafter30days.

1.6 Thetimeperiodsrequiredbypoint66.A.25applytoeachindividualmoduleex-

amination,withtheexceptionofthosemoduleexaminationswhichwerepassed

aspartofanothercategorylicence,wherethelicencehasalreadybeenissued

1.7 Themaximumnumberofconsecutiveattemptsforeachmoduleisthree.Fur-

thersetsofthreeattemptsareallowedwitha1yearwaitingperiodbetween

sets.

1.8 TheapplicantshallconfirminwritingtotheDGCAforanexamination,thenum-

beranddatesofattemptsduringthelastyearwheretheseattemptstookplace.

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2. Question Numbers and Examination Duration for the CAR-66 Appendix I

Modules

ModuleCategory

MultiplechoiceQues-

tions

Timeallowed(Minutes)No. Subject

1 Mathematics AllCategories NotApplicable

2 Physics AllCategories NotApplicable

3 ElectricalFundamentals

A 20 25

B1 52 65

B2 52 65

B3 24 30

4 ElectronicFundamentals

A NotApplicable

B1 20 25

B2 40 50

B3 8 10

5DigitalTechniques/ElectronicInstrumentSystems

A 16 20

B1.1,B1.3 40 50

B1.2,B1.4 20 25

B2 72 90

B3 16 20

6 MaterialsandHardware

A 52 65

B1 72 90

B2 60 75

B3 60 75

7A MaintenancePractices

A 72 90

B1 80 100

B2 60 75

7B MaintenancePractices B3 60 75

8 BasicAerodynamics

A 20 25

B1 20 25

B2 20 25

B3 20 25

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ModuleCategory

MultiplechoiceQues-

tions


9A Humanfactors

A 20 25

B1 20 25

B2 20 25

9B Humanfactors B3 16 20

10 AviationLegislation

A 32 40

B1 40 50

B2 40 50

B3 32 40

11ATurbineAeroplaneAerody-namics,StructuresandSys-tems

A 108 135

B1 140 175

B2 0 0

11BPistonAeroplaneAerodynam-ics,StructuresandSystems

A 72 90

B1 100 125

B2 0 0

11CPistonAeroplaneAerodynam-ics,StructuresandSystems

B3 60 75

12HelicopterAerodynamics,StructuresandSystems

A 100 125

B1 128 160

B2 0 0

13

AircraftAerodynamics,Struc-turesandSystems

A 0 0

B1 0 0

B2 180 225

14 Propulsion

A 0 0

B1 0 0

B2 24 30

15 GasTurbineEngine

A 60 75

B1 92 115

B2 00

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ModuleCategory

MultiplechoiceQues-

tions


16

PistonEngine

A 52 65

B1 72 90

B2 0 0

B3 68 85

17A Propeller

A 20 25

B1 32 40

B2 0 0

17B Propeller B3 28 35

3. ISSUANCE OF CERTIFICATE Applicantswhohavepassedallbasicknowledgeexaminationmodulesinrespectofa

particularcategory/sub-categoryofAMElicencemayapplytoCEO,DGCAonFormCA

19-11fortheissuanceofBasicKnowledgeExaminationCertificate.

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Appendix III -Type training and Examination Standard

On the job training

1. General

Aircrafttypetrainingshallconsistoftheoreticaltrainingandexamination,and,except

forthecategoryCratings,practicaltrainingandassessment.

(a)Theoreticaltrainingandexaminationshallcomplywiththefollowingrequirements:

(i) Shall be conducted by a maintenance training organisation appropriately ap-

provedinaccordancewithCAR-147or,whenconductedbyotherorganisations,as

directlyapprovedbytheDGCA.

(ii)Shallcomply,exceptaspermittedbythedifferencestrainingdescribedinpoint

(c),with:

- therelevantelementsdefinedinthemandatorypartoftheoperationalsuita-

bilitydataestablishedinaccordancewithCAR66orthestandarddescribed

inpoint3.1ofthisAppendix,and

- thetypetrainingexaminationstandarddescribedinpoint4.1ofthisAppendix.

(iii)Reserved

(iv)Shallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplica

tionforatyperatingendorsement.

(b)Practicaltrainingandassessmentshallcomplywiththefollowingrequirements:

(i) Shall be conducted by a maintenance training organisation appropriately ap-

provedinaccordancewithCAR-147or,whenconductedbyotherorganisations,

asdirectlyapprovedbytheDGCA.

(ii)Shallcomply,exceptaspermittedbythedifferencestrainingdescribedinpoint

(c),with:

- therelevantelementsdefinedinthemandatorypartoftheoperationalsuita-

bilitydataestablishedor,thestandarddescribedinpoint3.2ofthisAppendix,

and

- thetypetrainingassessmentstandarddescribedinpoint4.2ofthisAppendix.

(iii)Shallincludearepresentativecrosssectionofmaintenanceactivitiesrelevantto

theaircrafttype.

(iv) Shall include demonstrations using equipment, components, simulators, other

trainingdevicesoraircraft.

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(v)Shallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplica-

tionforatyperatingendorsement.

(c)Differencestraining

(i)Differencestrainingisthetrainingrequiredinordertocoverthedifferencesbe-

tweentwodifferentaircrafttyperatingsofthesamemanufacturerasdetermined

bytheDGCA.

(ii)Differencestraininghastobedefinedonacase-to-casebasistakingintoaccount

therequirements containedinthisAppendixIIIinrespectofboththeoreticaland

practicalelementsoftyperatingtraining

(iii)Atyperatingshallonlybeendorsedonalicenceafterdifferencestrainingwhen

theapplicantalsocomplieswithoneofthefollowingconditions:

—havingalreadyendorsedonthelicencetheaircrafttyperatingfromwhichthe

differencesarebeingidentified,or

—havingcompletedthetypetrainingrequirementsfortheaircraftfromwhich

thedifferencesarebeingidentified.

2. Aircraft Type training levels

The three levels listed below define the objectives, the depth of training and level of

knowledgethattrainingisintendedtoachieve.

Level 1

Abriefoverviewoftheairframe,systemsandpowerplantsasoutlinedintheSystems

DescriptionSectionoftheAircraftMaintenanceManual/InstructionsforContinuedAir-

worthiness.

Course objectives:Uponcompletionofthecourse,thestudentwillbeableto:

a) provideasimpledescriptionofthewholesubject,usingcommonwordsandex-

amples, using typical terms and identify safety precautions related to the air-

frame,itssystemsandpowerplant;

b) identifyaircraftmanuals,maintenancepractices important to the airframe, its

systemsandpowerplant;

c) definethegenerallayoutoftheaircraft'smajorsystems;

d) definethegenerallayoutandcharacteristicsofthepowerplant;

e) identifyspecialtoolingandtestequipmentusedwiththeaircraft

Level 2

Basicsystemoverviewofcontrols,indicators,principalcomponentsincludingtheir

locationandpurpose,servicingandminortroubleshooting. Generalknowledgeof the

theoretical andpracticalaspectsofthesubject

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Course objectives:InadditiontotheinformationcontainedintheLevel1,training,at

thecompletionofthisLevel2,trainingthestudentwillbeableto:

(a)understandthetheoreticalfundamentals;applyknowledgeinapracticalmannerus-

ingdetailedprocedures;

(b)recallthesafetyprecautionstobeobservedwhenworkingonorneartheaircraft,

powerplantandsystems;

(c) describe systems andaircraft handling particularly access, power availability and

sources;

(d)identifythelocationsoftheprincipalcomponents;

(e)explainthenormalfunctioningofeachmajorsystem,includingterminologyandno-

menclature;

(f)performtheproceduresforservicingassociatedwiththeaircraftforthefollowing

systems:Fuel,PowerPlants,Hydraulics,LandingGear,Water/Waste,andOxygen;

(g)demonstrateproficiencyinuseofcrewreportsandon-boardreportingsystems(mi-

nortroubleshooting)anddetermineaircraftairworthinesspertheMEL/CDL;

(h)demonstratetheuse,interpretationandapplicationofappropriatedocumentation

includinginstructionsforcontinuedairworthiness,maintenancemanual,illustrated

partscatalogue,etc.

Level 3

Detailed description,operation,component location,removal/installationandbiteand

troubleshootingprocedurestomaintenancemanuallevel.

Course objectives:InadditiontotheinformationcontainedinLevel1andLevel2train-

ing,atthecompletionofLevelIII,thestudentwillbeableto:

(a) demonstrateatheoreticalknowledgeofaircraftsystemsandstructuresandinterre-lationshipswithothersystems,provideadetaileddescriptionofthesubjectusingthe-oretical fundamentals and specific examples and to interpret results from varioussourcesandmeasurementsandapplycorrectiveactionwhereappropriate;

(b) Performsystem,powerplant,componentandfunctionalchecksasspecifiedinthe

maintenancemanual.

(c) demonstrate the use, interpret and apply appropriate documentation includingstructuralrepairmanual,troubleshootingmanual,etc.;

(d) Correlateinformationforthepurposeofmakingdecisionsinrespectoffaultdiag-nosisandrectificationtomaintenancemanuallevel.

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(e) Describeproceduresforreplacementofcomponentsuniquetoaircrafttype

3. Aircraft Type training standard Althoughaircrafttypetrainingincludesboththeoreticalandpracticalelements,courses

canbeapprovedforthetheoreticalelement,thepracticalelementorforacombinationof

both.

3.1 Theoretical element

(a) Objective

Oncompletionofatheoreticaltrainingcoursethestudentshallbeabletodemonstrate,to

thelevelsidentifiedintheAppendixIIIsyllabus,thedetailedtheoreticalknowledgeofthe

aircraft's applicable systems, structure, operations, maintenance, repair, and trouble-

shootingaccordingtoapprovedmaintenancedata.Thestudentshallbeabletodemon-

stratetheuseofmanualsandapprovedprocedures,includingtheknowledgeofrelevant

inspectionsandlimitations.

(b) Level of training:

Traininglevelsarethoselevelsdefinedinpoint2above.Afterthefirsttypecoursefor

categoryCcertifyingstaffallsubsequentcoursesneedonlybetolevel1.Duringalevel3

theoreticaltraining,level1and2trainingmaterialmaybeusedtoteachthefullscopeof

thechapterifrequired.However,duringthetrainingthemajorityofthecoursematerial

andtrainingtimeshallbeatthehigherlevel

(c) Duration:

Thetheoreticaltrainingminimumtuitionhoursarecontainedinthefollowingtable:

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Category Hours

Aeroplanes with a maximum take-off mass above 30 000 kg:

B1.1 150

B1.2 120

B2 100

C 30Aeroplanes with a maximum take-off mass equal or less than 30 000 kg and above 5 700

kg:

B1.1 120

B1.2 100

B2 100

C 25Aeroplanes with a maximum take-off mass of 5 700 kg and below(

B1.1 80

B1.2 60

B2 60

C 15Helicopters(2)

B1.3 120

B1.4 100

B2 100

C 25

(1)Fornon-pressurisedpistonengineaeroplanesbelow2000kgMTOMthemin-

imumdurationcanbereducedby50%.

(2)Forhelicoptersingroup2(asdefinedinpoint66.A.42)theminimumduration

canbereducedby30%.

Forthepurposeofthetableabove,atuitionhourmeans60minutesofteachingandex-

cludeanybreaks,examination,revision,preparationandaircraftvisit.Thesehoursapply

onlytotheoreticalcoursesforcompleteaircraft/enginecombinationsaccordingtothe

typeratingasdefinedbytheDGCA.

(d) Justification of course duration:

Trainingcoursescarriedoutinamaintenancetrainingorganisationapprovedinaccord-

ancewithCAR-147andcoursesdirectlyapprovedbytheDGCAshalljustifytheirhourdu-

rationandthecoverageofthefullsyllabusbyatrainingneedsanalysisbasedon:

—thedesignoftheaircrafttype,itsmaintenanceneedsandthetypesofoperation,

—detailedanalysisofapplicablechapters

—seecontentstableinpoint3.1(e)below,

— detailed competency analysis showing that the objectives as stated in point 3.1(a)

abovearefullymet.

Wherethetrainingneedsanalysisshowsthatmorehoursareneeded,courselengthsshall

belongerthantheminimumspecifiedinthetable.

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Similarly,tuitionhoursofdifferencescoursesorothertrainingcoursecombinations(such

ascombinedB1/B2courses),andincasesoftheoreticaltypetrainingcoursesbelowthe

figuresgiveninpoint3.1(c)above,theseshallbejustifiedtotheDGCAbythetraining

needsanalysisasdescribedabove.

Inaddition,thecoursemustdescribeandjustifythefollowing:

—Theminimumattendancerequiredtothetrainee,inordertomeettheobjectivesofthe

course.

—Themaximumnumberofhoursoftrainingperday,takingintoaccountpedagogical

andhumanfactorsprinciples.

Iftheminimumattendancerequiredisnotmet,thecertificateofrecognitionshallnotbe

issued.Additionaltrainingmaybeprovidedbythetrainingorganisationinordertomeet

theminimumattendancetime.

(e) Content:

Asaminimum,theelementsintheSyllabusbelowthatarespecifictotheaircrafttypeshall

becovered.Additionalelementsintroducedduetotypevariations,technologicalchanges,

etc.shallalsobeincluded.Thetrainingsyllabusshallbefocusedonmechanicalandelec-

tricalaspectsforB1personnel,andelectricalandavionicaspectsforB2.

Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics

B1 C B1 C B1 C B1 C B2

Introduction module:

05 Time limits/maintenance checks

1 1 1 1 1 1 1 1 1

06 Dimensions/Areas (MTOM, etc.)

1 1 1 1 1 1 1 1 1

07 Lifting and Shoring 1 1 1 1 1 1 1 1 1

08 Levelling and weighing 1 1 1 1 1 1 1 1 1

09 Towing and taxiing 1 1 1 1 1 1 1 1 1

10 Parking/mooring, Storing and Return to Service

1 1 1 1 1 1 1 1 1

11 Placards and Markings 1 1 1 1 1 1 1 1 1

12 Servicing 1 1 1 1 1 1 1 1 1

20 Standard practices — only type particular

1 1 1 1 1 1 1 1 1

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Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


Helicopters

18. Vibration and Noise Anal-ysis( Blade tracking )

– -- – – 3 1 3 1 –

60 Standard Practices Rotor - - - - 3 1 3 1 -

62 Rotors – – – – 3 1 3 1 1

62A Rotors — Monitoring and indicating

_ _ _ _ 3 1 3 1 3

63 Rotor Drives -- -- -- -- 3 1 3 1 1

63A Rotor Drives — Monitor-ing and indicating

-- -- -- -- 3 1 3 1 3

64 Tail Rotor – – – – 3 1 3 1 1

64A Tail rotor — Monitoring and indicating

-- -- -- -- 3 1 3 1 3

65 Tail Rotor Drive -- – – – 3 1 3 1 1

65A Tail Rotor Drive — Mon-

itoring and indicating -- -- -- -- 3 1 3 1 3

66 Folding Blades/Pylon – – – – 3 1 3 1 –

67 Rotors Flight Control -- -- -- -- 3 1 3 1 --

53 Airframe Structure (Heli-

copter) -- -- -- -- 3 1 3 1 --

25 Emergency Flotation

Equipment -- -- -- -- 3 1 3 1 1

Airframe Structure

51 Standard practices and

structures (damage classifica-

tion, assessment and repair)

3 1 3 1 – – – – 1

53 Fuselage 3 1 3 1 – – – – 1

54 Nacelles/Pylons 3 1 3 1 – – – – 1

55 Stabilizers 3 1 3 1 – – – – 1

56 Windows 3 1 3 1 – – – – 1

57 Wings 3 1 3 1 – – – – 1

27A Flight Control Surfaces ( All )

3 1 3 1 – – – – 1

52 Doors 3 1 3 1 – – – – 1

Zonal & Station Identification Systems

1 1 1 1 1 1 1 1 1

Airframe Systems

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Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


21 Air Conditioning 3 1 3 1 3 1 3 1 3

21A Air Supply 3 1 3 1 1 3 3 1 2

21B Pressurization 3 1 3 1 3 1 3 1 3

21C Safety & Warning Devices 3 1 3 1 3 1 3 1 3

22 Autoflights 2 1 2 1 2 1 2 1 3

23 Communication 2 1 2 1 2 1 2 1 3

24 Electrical Power 3 1 3 1 3 1 3 1 3

25 Equipment & Furnishings 3 1 3 1 3 1 3 1 1

25A Electronic Emergency Equip. & Cabin Entertainment Equipment

1 1 1 1 1 1 1 1 3

26 Fire Protection 3 1 3 1 3 1 3 1 3

27 Flight Controls 3 1 3 1 3 1 3 1 2

27A Sys. Operation: Electri-cal/Fly-by-Wire

3 1 – – – – – – 3

28 Fuel Systems 3 1 3 1 3 1 3 1 2

28A Fuel Systems — Monitor-ing and indication

3 1 3 1 3 1 3 1 3

29 Hydraulic Power 3 1 3 1 3 1 3 1 2

29A Hydraulic Power — Mon-itoring and indicating

3 1 3 1 3 1 3 1 3

30 Ice & Rain Protection 3 1 3 1 3 1 3 1 3

31 Indicating/Recording Sys-tems

3 1 3 1 3 1 3 1 3

31A Instrument Systems 3 1 3 1 3 1 3 1 3

32 Landing Gear 3 1 3 1 3 1 3 1 2

32A Landing Gear — Monitor-ing and indicating

3 1 3 1 3 1 3 1 3

33 Lights 3 1 3 1 3 1 3 1 3

34 Navigation 2 1 2 1 2 1 2 1 3

35 Oxygen 3 1 3 1 – – – – 2

36 Pneumatic 3 1 3 1 3 1 3 1 2

36A Pneumatic — Monitoring and indicating

3 1 3 1 3 1 3 1 3

37 Vacuum 3 1 3 1 3 1 3 1 2

38 Water/Waste 3 1 3 1 -- -- -- -- 2

41 Water Ballast 3 1 3 1 -- -- -- -- 1

42 Integrated modular avion-ics

2 1 2 1 2 1 2 1 3

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Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


44 Cabin Systems 2 1 2 1 2 1 2 1 3

45 On-board Maintenance Systems

3 1 3 1 3 1 – – 3

46 Information Systems 2 1 2 1 2 1 2 1 3

50 Cargo and Accessory Com-partments

3 1 3 1 3 1 3 1 1

Turbine Engines:

70 Standard Practices — En-gines,

3 1 – – 3 1 – – 1

70A constructional arrange-ment and operation (Installa-tion Inlet, Compressors, Com-bustion Section, Turbine Sec-tion, Bearings and Seals, Lu-brication Systems).

3 1 -- -- 3 1 -- -- 1

70B Engine Performance 3 1 – – 3 1 – – 1

71 Powerplant 3 1 – – 3 1 – – 1

72 Engine Turbine/Turbo Prop/Ducted Fan/Unducted fan

3 1 -- -- 3 1 -- -- 1

73 Engine Fuel and Control 3 1 – – 3 1 – – 1

75 Air 3 1 – – 3 1 – – 1

76 Engine controls 3 1 – – 3 1 – – 1

78 Exhaust 3 1 – – 3 1 – – 1

79 Oil 3 1 – – 3 1 – – 1

80 Starting 3 1 – – 3 1 – – 1

82 water injection 3 1 – – 3 1 – – 1

83 Accessory Gear Boxes 3 1 – – 3 1 – – 1

84 Propulsion Augmentation 3 1 – – 3 1 – – 1

73A FADEC 2 1 – – 2 1 – – 3

74 Ignition 3 1 – – 3 1 – – 3

77 Engine Indicating Systems 3 1 – – 3 1 – – 3

49 Auxiliary Power Units (APUs)

3 1 – – -- -- – – 2

Piston Engines:

70 Standard Practices — En-gines

-- -- 3 1 – – 3 1 1

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Level Chapters

Aeroplanes Turbine

Aeroplane Piston

Helicopter turbine

Helicopter Piston

Avi-on-ics


70A Constructional arrangement and operation (Installation, Car-burettors, Fuel injection sys-tems, Induction, Exhaust and Cooling Systems, Supercharging/ Turbocharging, Lubrication Sys-tems).

– – 3 1 -- -- 3 1 1

70B Engine Performance _ _ 3 1 -- -- 3 1 1

71 Powerplant – – 3 1 – – 3 1 1

73 Engine Fuel and Control – – 3 1 – – 3 1 1

76 Engine Control – – 3 1 – – 3 1 1

79 Oil – – 3 1 – – 3 1 1

80 Starting – – 3 1 – – 3 1 1

81 Turbine -- -- 3 1 -- -- 3 1 1

82 Water Injections – – 3 1 – – 3 1 1

83 Accessory Gear Boxes – – 3 1 – – 3 1 1

84 Propulsion Augmentation – – 3 1 – – 3 1 1

73A FADEC – – 3 1 – – 3 1 3

74 Ignition – – 3 1 – – 3 1 3

77 Engine Indication Systems – – 3 1 – – 3 1 3

Propellers:

60A Standard Practices — Pro-peller

3 1 3 1 – – – – 1

61 Propellers/Propulsion 3 1 3 1 – – – – 1

61A Propeller Construction 3 1 3 1 -- -- -- -- 1

61B Propeller Pitch Control 3 1 3 1 – – – – –

61C Propeller Synchronizing 3 1 3 1 – – – – 1

61D Propeller Electronic con-trol

2 1 2 1 – – – – 3

61E Propeller Ice Protection 3 1 3 1 – – – – –

61F Propeller Maintenance 3 1 3 1 – – – – 1

(f)MultimediaBasedTraining(MBT)methodsmaybeusedtosatisfythetheoreticaltrain-

ingelementeitherintheclassroomorinavirtualcontrolledenvironmentsubjecttothe

acceptanceoftheDGCAapprovingthetrainingcourse.

3. 2Practical element

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a) Objective:

Theobjectiveofpracticaltrainingistogaintherequiredcompetenceinperformingsafe

maintenance, inspections and routine work according to the maintenance manual and

otherrelevantinstructionsandtasksasappropriateforthetypeofaircraft,forexample

troubleshooting,repairs,adjustments,replacements,riggingandfunctionalchecks.Itin-

cludestheawarenessoftheuseofalltechnicalliteratureanddocumentationfortheair-

craft,theuseofspecialist/specialtoolingandtestequipmentforperformingremovaland

replacementofcomponentsandmodulesuniquetotype,includinganyon-wingmainte-

nanceactivity.

b) Content:

Atleast50%ofthecrosseditemsinthetablebelow,whicharerelevanttotheparticular

aircrafttype,shallbecompletedaspartofthepracticaltraining.

Taskscrossedrepresentsubjectsthatareimportantforpracticaltrainingpurposestoen-

surethattheoperation,function,installationandsafetysignificanceofkeymaintenance

tasksisadequatelyaddressed;particularlywherethesecannotbefullyexplainedbythe-

oreticaltrainingalone.Althoughthelistdetailstheminimumpracticaltrainingsubjects,

otheritemsmaybeaddedwhereapplicabletotheparticularaircrafttype.

Taskstobecompletedshallberepresentativeoftheaircraftandsystemsbothincomplex-

ityandinthetechnicalinputrequiredtocompletethattask.Whilerelativelysimpletasks

maybeincluded,othermorecomplextasksshallalsobeincorporatedandundertakenas

appropriatetotheaircrafttype.

Glossaryoftable:LOC:Location;FOT:Functional/OperationTest;SGH:ServiceandGround;Handling;R/I:Removal/Installation;MEL:MinimumEquipmentList;TS:TroubleShooting

Chapters B1/B2 B1 B2

LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

Introduction module:

05 Time limits/maintenance checks X/X -- -- -- -- -- -- -- -- -- -

06 Dimensions/Areas (MTOM, etc.) X/X -- -- -- -- -- -- -- -- -- -

07 Lifting and Shoring X/X -- -- -- -- -- -- -- -- -- -

08 Levelling and weighing X/X -- X -- -- -- -- X -- -- -

09 Towing and Taxing X/X -- X -- -- -- -- X -- -- -

10 Parking/Mooring storing and return to service

X/X -- X -- -- -- -- X -- -- -

11 Playcard and marking X/X -- -- -- -- -- -- -- -- -- -

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LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

12 Servicing X/X -- X -- -- -- -- X -- -- -

20 Standard practices –only type partic-ular

X/X -- X -- -- -- -- X -- -- -

Helicopters:

18 Vibration and Noise Analysis (Blade tracking)

X/-- -- -- -- -- X -- -- -- -- -

60 Standard Practices Rotor — only type specific

X/X -- X -- -- -- -- X -- -- -

62 Rotors X/-- -- X X -- X -- -- -- -- -

62A Rotors — Monitoring and indicating X/X X X X X X -- -- X -- x

63 Rotor Drives X/-- X -- -- -- X -- -- -- -- -

63A Rotor Drives — Monitoring and indi-cating

X/X X -- X X X -- -- X -- X

64 Tail Rotor X/-- -- X -- -- X -- -- -- -- -

64A Tail rotor -Monitoring and indicating X/X X -- X X X -- -- X -- X

65 Tail Rotor Drive X/-- X -- -- -- X -- -- -- -- -

65A Tail Rotor Drive — Monitoring and indicating

X/X X -- X X X -- -- X -- X

66 Folding Blades/Pylon X/-- X X -- -- X -- -- -- -- -

67 Rotors Flight Control X/-- X X -- X X -- -- -- -- -

53 Airframe Structure (Helicopter) Note: covered under Airframe structures

25 Emergency Flotation Equipment X/X X X X X X X X -- -- -

Airframe structures:

51 Standard Practices and Structures (damage classification, assessment and repair

53 Fuselage X/-- -- -- -- -- X -- -- -- -- -

54 Nacelles/Pylons X/-- -- -- -- -- -- -- -- -- -- -

55 Stabilisers X/-- -- -- -- -- -- -- -- -- -- -

56 Windows X/-- -- -- -- -- X -- -- -- -- -

57 Wings X/-- -- -- -- -- -- -- -- -- -- -

27A Flight Control Surfaces X/-- -- -- -- -- X -- -- -- -- -

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LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

52 Doors X/X X X -- -- -- -- X -- -- -

Airframe systems:

21 Air Conditioning X/X X X -- X X X X -- X X

21A Air Supply X/X X -- -- -- -- X -- -- -- -

21B Pressurisation X/X X -- -- X X X -- -- X X

21C Safety and warning Devices X/X -- X -- -- -- -- X -- -- -

22 Autoflight X/X -- -- -- X -- X X X X X

23 Communications X/X -- X -- X -- X X X X X

24 Electrical Power X/X X X X X X X X X X X

25 Equipment and Furnishings X/X X X X -- -- X X X -- -

25A Electronic Equipment including emergency equipment

X/X X X X -- -- X X X -- -

26 Fire Protection X/X X X X X X X X X X X

27 Flight Controls X/X X X X X X X -- -- -- -

27A Sys. Operation: Electrical/Fly-by- Wire

X/X X X X X -- X -- X -- X

28 Fuel Systems X/X X X X X X X X -- X -

28A Fuel Systems — Monitoring and in-dicating

X/X X -- -- -- -- X -- X -- X

29 Hydraulic Power X/X X X X X X X X -- X -

29A Hydraulic Power — Monitoring and indicating

X/X X -- X X X X -- X X X

30 Ice and Rain Protection X/X X X -- X X X X -- X X

31 Indicating/Recording Systems X X/X X X X X X X X X X X

31A Instrument Systems X/X X X X X X X X X X X

32 Landing Gear X/X X X X X X X X X X -

32A Landing Gear — Monitoring and in-dicating

X/X X -- X X X X -- X X X

33 Lights X/X X X -- X -- X X X X -

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LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

34 Navigation X/X -- X -- X -- X X X X X

35 Oxygen X/-- X X X -- -- X X -- -- -

36 Pneumatic X/-- X -- X X X X -- X X X

36A Pneumatic — Monitoring and indi-cating

X/X X X X X X X X X X X

37 Vacuum X/-- X -- X X X -- -- -- -- -

38 Water/Waste X/-- X X -- -- -- X X -- -- -

41 Water Ballast X/-- -- -- -- -- -- -- -- -- -- -

42 Integrated modular avionics X/X -- -- -- -- -- X X X X X

44 Cabin Systems X/X -- -- -- -- -- X X X X X

45 On-Board Maintenance System (or covered in 31)

X/X X X X X X X X X X X

46 Information Systems X/X -- -- -- -- -- X -- X X X

50 Cargo and Accessory Compartments X/X -- X -- -- -- -- -- -- -- -

Turbine/Piston Engine Module:

70 Standard Practices — Engines — only type particular

--- -- X -- -- -- -- X -- -- -

70A Constructional arrangement and op-eration (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X -- -- -- -- -- -- -- -- - -

Turbine engines:

70B Engine Performance -- -- -- -- -- X -- -- -- -- -

71 Power Plant X/-- X X -- -- -- -- X -- -- -

72 Engine Turbine/Turbo Prop/Ducted Fan/ Unducted fan

X/-- -- -- -- -- -- -- -- -- -- -

73 Engine Fuel and Control X/X X -- -- -- -- -- -- -- -- -

73A FADEC Systems X/X X -- X X X X -- X X X

74 Ignition X/X X -- -- -- -- X -- -- -- -

75 Air X/-- -- -- X -- X -- -- -- -- -

76 Engine Controls X/-- X -- -- -- X -- -- -- -- -

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LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

77 Engine Indicating X/X X -- -- X X X -- -- X X

78 Exhaust X/-- X -- -- X -- -- -- -- -- -

79 Oil X/-- -- X X -- -- -- -- -- -- -

80 Starting X/-- X -- -- X X -- -- -- -- -

82 Water Injection X/-- X -- -- -- -- -- -- -- -- -

83 Accessory Gearboxes X/-- -- X -- -- -- -- -- -- -- -

84 Propulsion Augmentation X/-- X -- -- -- -- -- -- -- -- -

Auxiliary Power Units (APUs):

49 Auxiliary Power Units (APUs) X/-- X X -- -- X -- -- -- -- -

Piston Engines:

70 Standard Practices — Engines — only type particular

-- -- X -- -- -- -- X -- -- -

70A Constructional arrangement and op-eration (Installation Inlet, Compressors, Combustion Section, Turbine Section, Bearings and Seals, Lubrication Systems)

X/X -- -- -- -- -- -- -- -- - -

70B Engine Performance -- -- -- -- -- X -- -- -- -- -

71 Power Plant X/-- X X -- -- -- -- X -- -- -

73 Engine Fuel and Control X/X X -- -- -- -- -- -- -- -- -

73A FADEC Systems X/X X -- X X X X X X X X

74 Ignition X/X X -- -- -- -- X -- -- -- -

76 Engine Controls X/-- X -- -- -- X -- -- -- -- -

77 Engine Indicating X/X X -- -- X X X -- -- X X

78 Exhaust X/-- X -- -- X X -- -- -- -- -

79 Oil X/-- -- X X -- -- -- -- -- -- -

80 Starting X/-- X -- -- X X -- -- -- -- -

81 Turbines X/-- X X X -- X -- -- -- -- -

82 Water Injection X/-- X -- -- -- -- -- -- -- -- -

83 Accessory Gearboxes X/-- -- X X -- -- -- -- -- -- -

84 Propulsion Augmentation X/-- X -- -- -- -- -- -- -- -- -

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LOC FOT SGH

R/I MEL TS FOT SGH

R/I ME

L TS

Propellers:

60A Standard Practices — Propeller -- -- -- X -- -- -- -- -- -- -

61 Propellers/Propulsion X/X X X -- X X -- -- -- -- -

61A Propeller Construction X/-- -- X -- -- -- -- -- -- -- -

61B Propeller Pitch Control X/-- X -- X X X -- -- -- -- -

61C Propeller Synchronising X/-- X -- -- -- X -- -- -- X -

61D Propeller Electronic control X/X X X X X X X X X X X

61E Propeller Ice Protection X/-- X -- X X X -- -- -- -- -

61F Propeller Maintenance X/X X X X X X X X X X X

4. Type training examination and assessment standard

4.1.Theoreticalelementexaminationstandard

Afterthetheoreticalportionoftheaircrafttypetraininghasbeencompleted,awritten

examinationshallbeperformed,whichshallcomplywiththefollowing:

(a)Formatoftheexaminationisofthemulti-choicetype.Eachmulti-choicequestionshall

have3alternativeanswersofwhichonlyoneshallbethecorrectanswer.Thetotal

timeisbasedonthetotalnumberofquestionsandthetimeforansweringisbased

uponanominalaverageof90secondsperquestion.

(b)Theincorrectalternativesshallseemequallyplausibletoanyoneignorantofthesub-

ject.Allthealternativesshallbeclearlyrelatedtothequestionandofsimilarvocabu-

lary,grammaticalconstructionandlength.

(c)Innumericalquestions,theincorrectanswersshallcorrespondtoproceduralerrors

suchastheuseofincorrectsense(+versus-)orincorrectmeasurementunits.They

shallnotbemererandomnumbers.

(d)Thelevelofexaminationforeachchapter(1)shallbetheonedefinedinpoint2‘Air-

crafttypetraininglevels’.However,theuseofalimitednumberofquestionsatalower

levelisacceptable.

(e)Theexaminationshallbeoftheclosedbooktype.Noreferencematerialispermitted.

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AnexceptionwillbemadeforthecaseofexaminingaB1orB2candidate'sabilityto

interprettechnicaldocuments.

(f) Thenumberofquestionsshallbeatleast1questionperhourofinstruction.Thenum-

berofquestionsforeachchapterandlevelshallbeproportionateto:

—theeffectivetraininghoursspentteachingatthatchapterandlevel,

—thelearningobjectivesasgivenbythetrainingneedsanalysis.

DGCAwillassessthenumberandthelevelofthequestionswhenapprovingthecourse.

(g)Theminimumexaminationpassmarkis75%.Whenthetypetrainingexaminationis

splitinseveralexaminations,eachexaminationshallbepassedwithatleasta75%

mark.Inordertobepossibletoachieveexactlya75%passmark,thenumberofques-

tionsintheexaminationshallbeamultipleof4.

(h)Penaltymarking(negativepointsforfailedquestions)isnottobeused.

(i)Endofmodulephaseexaminationscannotbeusedaspartofthefinalexamination

unlesstheycontainthecorrectnumberandlevelofquestionsrequired.

4.2.Practicalelementassessmentstandard.

Afterthepracticalelementoftheaircrafttypetraininghasbeencompleted,anassess-

mentmustbeperformed,whichmustcomplywiththefollowing:

(a)Theassessmentshallbeperformedbydesignatedassessorsappropriatelyqualified.

(b)Theassessmentshallevaluatetheknowledgeandskillsofthetrainee.

5. Type examination standard

Typeexaminationshallbeconductedbytrainingorganisationsappropriatelyapproved

underCAR-147orbytheDGCA

Theexaminationshallbeoral,writtenandorpracticalassessmentbased,oracombina-

tionthereofanditshallcomplywiththefollowingrequirements:

(a)Oralexaminationquestionsshallbeopen.

(b)Writtenexaminationquestionsshallbeessaytypeormulti-choicequestions.

(c)Practicalassessmentshalldetermineaperson'scompetencetoperformatask.

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(d)Examinationsshall be on a sample of chapters (1) drawn from point 3 type train-

ing/examinationsyllabus,attheindicatedlevel.

(e)Theincorrectalternativesshallseemequallyplausibletoanyoneignorantofthesub-

ject.Allofthealternativesshallbeclearlyrelatedtothequestionandofsimilarvocab-

ulary,grammaticalconstructionandlength.

(f)Innumericalquestions,theincorrectanswersshallcorrespondtoproceduralerrors

suchascorrectionsappliedinthewrongsenseorincorrectunitconversions:theyshall

notbemererandomnumbers.

(g)Theexaminationshallensurethatthefollowingobjectivesaremet:

1.Properlydiscusswithconfidencetheaircraftanditssystems.

2.Ensuresafeperformanceofmaintenance,inspectionsandroutineworkaccording

tothemaintenancemanualandotherrelevantinstructionsandtasksasappropriate

forthetypeofaircraft,forexampletroubleshooting,repairs,adjustments,replace-

ments,riggingandfunctionalcheckssuchasenginerun,etc.,ifrequired.

3.Correctlyusealltechnicalliteratureanddocumentationfortheaircraft.

4.Correctlyusespecialist/specialtoolingandtestequipment,performremovalandre-

placement of components and modules unique to type, including any on-wing

maintenanceactivity

(h)Thefollowingconditionsapplytotheexamination:

1. Themaximumnumberofconsecutiveattemptsisthree.Furthersetsofthreeattempts

areallowedwitha1yearwaitingperiodbetweensets.Awaitingperiodof30daysis

requiredafterthefirstfailedattemptwithinoneset,andawaitingperiodof60daysis

requiredafterthesecondfailedattempt.

TheapplicantshallconfirminwritingtotheDGCAthenumberanddatesofattempts

duringthelastyear..DGCAisresponsibleforcheckingthenumberofattemptswithin

theapplicabletimeframes.

2.Thetypeexaminationshallbepassedandtherequiredpracticalexperienceshallbe

completedwithinthe3yearsprecedingtheapplicationfortheratingendorsementon

theaircraftmaintenancelicence.

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3.Typeexaminationshallbeperformedwithatleastoneexaminerpresent.Theexam-

iner(s)shallnothavebeeninvolvedintheapplicant'straining.

(i)Awrittenandsignedreportshallbemadebytheexaminer(s)toexplainwhythecan-

didatehaspassedorfailed.

6. On the Job Training

OntheJobTraining(OJT)shallbeapprovedbytheDGCA.

Itshallbeconductedatandunderthecontrolofamaintenanceorganisationappropri-

atelyapprovedforthemaintenanceoftheparticularaircrafttypeandshallbeassessedby

designatedassessorsappropriatelyqualified.

Itshallhavebeenstartedandcompletedwithinthe3yearsprecedingtheapplicationfor

atyperatingendorsement.

(a) Objective:

TheobjectiveofOJTistogaintherequiredcompetenceandexperienceinperformingsafe

maintenance.

Content:

OJTshallcoveracrosssectionoftasksacceptabletotheDGCA.TheOJTtaskstobecom-

pletedshallberepresentativeoftheaircraftandsystemsbothincomplexityandinthe

technicalinputrequiredtocompletethattask.Whilerelativelysimpletasksmaybein-

cluded,othermorecomplexmaintenancetasksshallalsobeincorporatedandundertaken

asappropriatetotheaircrafttype.

Eachtaskshallbesignedoffbythestudentandcountersignedbyadesignatedsupervisor.

Thetaskslistedshallrefertoanactualjobcard/worksheet,etc.

ThefinalassessmentofthecompletedOJTismandatoryandshallbeperformedbyades-

ignatedassessorappropriatelyqualified.

ThefollowingdatashallbeaddressedontheOJTworksheets/logbook:

1.NameofTrainee;

2.DateofBirth;

3.ApprovedMaintenanceOrganisation;

4.Location;

5.Nameofsupervisor(s)andassessor,(includinglicencenumberifapplicable);

6.Dateoftaskcompletion;

7.Descriptionoftaskandjobcard/workorder/techlog,etc.;

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8.Aircrafttypeandaircraftregistration;

9.Aircraftratingappliedfor.

InordertofacilitatetheverificationbytheDGCA,demonstrationoftheOJTshallconsist

of i)detailedworksheets/logbookand(ii)acompliancereportdemonstratinghowthe

OJTmeetstherequirementofthisPart.

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Appendix IV - Experience requirements for extending a CAR-

66 Aircraft Maintenance Engineer’s Licence

Thetablebelowshowstheexperiencerequirementsforaddinganewcategoryorsub-

categorytoanexistingCAR-66licence.

Theexperiencemustbepracticalmaintenanceexperienceonanoperatingaircraftinthe

subcategoryrelevanttotheapplication.

Theexperienceistobesignedbythepostholderonlyandthisprocedureistobere-

flectedinMOE

Theexperiencerequirementwillbereducedby50%iftheapplicanthascompletedan

approvedCAR-147courserelevanttothesubcategory

To: A1 A2 A3 A4 B1.1 B1.2 B1.3 B1.4 B2 B3

From - - - - - - - - -

A1 X 6months 6months 2years 6months 2years 1year 2years 6months

A2 6months X 6months 6months 2years 6months 2years 1year 2years 6months

A3 6months 6months X 6months 2years 1year 2years6

months2years 1year

A4 6months 6months 6months X 2years 1years 2years6

months2years 1year

B1.1 NONE 6months 6months 6months

X6months

6months

6months

1year 6months

B1.2 6months NONE 6months 6months 2years

X2years

6months

2years NONE

B1.3 6months 6months NONE 6months6

months6months

X

6months

1year 6months

B1.4 6months 6months 6months NONE 2years 6months 2years X 2years 6months

B2 6months 6months 6months 6months 1year 1year 1year 1year X 1year

B3 6months NONE 6months 6months 2years 6months 2years 1year 2years --

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Appendix V- Applications and Formats

Application forms

(published in DGCA Website dgca.nic.in )

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AppendixVI-AircraftMaintenanceEngineer’sLicencereferredtoinRule61oftheAircraftRules,1937-CAForm26

CA26

GOVERNMENTOFINDIA

DIRECTORATEGENERALOFCIVILAVIATION

CAR-66

AIRCRAFTMAINTENANCEENGINEER’sLICENCE

I INDIA IX. CONDITIONS

II. Aircraft Maintenance Engineer’s Licence a. Certified that holder is authorized to exercise the privi-

legesofthelicenceasgiveninRule61oftheAircraftRules,

1937.

b.EndorsementofaircrafttypesatsectionXII(b)titledAIR-

CRAFTTYPERATINGmeanstheholderisqualifiedtoissue

acertificateofreleasetoserviceforsuchaircraftfromthe

dateofendorsementwithavalidauthorizationissuedby

approvedmaintenanceorganization.

c.Holderofthislicenceshallnotexercisetheprivilegesof

thelicenceandrelatedratingsatanytimewhenhe/sheis

awareofanydecreaseinmedicalfitnesswhichmightren-

derhim/herunable tosafelyandproperlyexercise these

privileges.

d.Thislicenceisnotvalidunlessitbearsthesignatureoftheholder.

e.ThislicenceremainscurrentuntiltheexpirydatespecifiedatsectionXIVwhilstincompliancewiththeAircraftRule61andCAR66unlesspreviouslysuspendedorrevoked.

f. This licence when endorsed with an aircraft type ratingmeetstheintentofICAOAnnex1.

g. Entry, endorsement or alteration in the licence shall bemadebypersonauthorizedforthispurposebytheDirectorGeneral.

III. Licencenumber

STAMPSIZE

PHOTOIV.

Nameofholder

infull

IVa Dateofbirth

V. Addressof

holder

VI. Nationality

VII. SignatureofHolder

VIII.

IssuedinaccordancewiththeprovisionsoftheAircraftAct

1934,andAircraftRules1937.

X SignatureofIssu-

ingAuthority

………………………………………………..……

(fortheDirectorGeneralofCivilAviation)

DaDateofIssue:

XI. StampoftheIs-

suingAuthority

1 III. LIC No. 2

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XII (a). LICENCE (SUB) CATEGORIES XII (b). AIRCARFT TYPE RATING

CATEGORIES A B1 B2 B3 C DATE AIRCRAFTTYPEORGROUPCATE-

GORYSTAMP&DATE

AEROPLANESTUR-

BINE

n/

a

n/

a

n/

a

AEROPLANESPISTON n/

a

n/

a

n/

a

HELICOPTERSTUR-

BINE

n/

a

n/

a

n/

a

HELICOPTERSPISTON n/

a

n/

a

n/

a

AVIONICSn/

a

n/

a

n/

a

n/

a

AIRCRAFTn/

a

n/

a

n/

a

n/

a

PISTON-ENGINENON-

PRESSURISEDAERO-

PLANESOF2000KG

MTOMANDBELOW

n/

a

n/

a

n/

a

n/

a

III. LIC No. 3 III. LIC No. 4

XIII. LIMITATIONS XIV. LICENCE VALIDITY

AIRCRAFT

TYPEOR

GROUP

CATEGORY

LIMITA-

TION

CODE

SIGNATUREWITH

DATE(REMOVALOF

LIMITATION)

DATEOFEXPIRYSIGNATUREWITH

DATESEAL

III. LIC No. 5 III. LIC No 6

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XIV a). LICENCE ENDORSEMENTS INHERITED FROM THE AME

LICENCE HELD PRIOR TO CAR-66 LICENCE XIV (b). REMARKS

RATING CATEGORYSIGNATUREWITH

DATE

III. LIC No. 7 III. LIC No. 8

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1. Theaircraftmaintenanceengineer’slicenceonceissuedisrequiredtobekeptbytheperson

towhomitappliesingoodconditionandwhoshallremainaccountableforensuringthatno

unauthorizedentriesaremade.

2. Failuretocomplywithparagraph1mayinvalidatethedocumentandcouldleadtotheholdernotbeingpermittedtoholdanyCAR-145certificationauthorization.

3. Failuretocomplywithparagraph1mayalsoresultinprosecutionunderrelevantIndianPe-

nalCode.

4. Eachpageissuedshallbeinthisformatandcontainthespecifiedinformationforthatpage.

5. Iftherearenolimitationsapplicable,theLIMITATIONSpagewillbeissuedstating‘Nolimi-

tations’.

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Acceptable Means of Compliance (AMC) / Guidance Material

(GM) to SECTION A of CAR-66

ThischaptercontainsAcceptableMeans ofCompliance(AMC)andGuidanceMaterial(GM)toCAR-66SectionA–TechnicalRequirements.AcceptableMeansofCompliance(AMC)illustrateameans,orseveralalternativemeans,butnotnecessarilytheonlypos-siblemeansbywhicharequirementcanbemet.

SECTION A

TECHNICAL REQUIREMENTS

GM 66.A.03 Licence categories

Individualaircraftmaintenancelicenceholdersneednotberestrictedtoasinglecate-gory.Providedthateachqualificationrequirementissatisfied,anycombinationofcate-goriesmaybegranted.

AMC 66.A.10 Application

1.Maintenanceexperienceshouldbewritteninamannerthatthereaderhasareason-

able understanding of where, when and what maintenance constitutes the experi-

ence.Ataskbytaskaccountisnotnecessarybutatthesametimeablankstatement

“Xyear’smaintenanceexperiencecompleted”isnotacceptable.Alogbookofmainte-

nanceexperience isdesirableandbekept. It is acceptable tocrossrefer in theCA

Form19-01tootherdocumentscontaininginformationonmaintenance.

2. Applicants claimingthe maximumreduction in 66.A.30(a) total experience based

uponhavingsuccessfullycompletedapprovedbasictrainingshouldincludethecer-

tificateofapprovalwithitsvalidityscheduleofthetrainingestablishment.

3.Applicantsclaimingreductionin66.A.30(a)totalexperiencebaseduponhavingsuc-

cessfullycompletedtechnicaltraininginanorganizationorinstituterecognizedby

DGCAasacompetentorganizationorinstituteshouldincludetherelevantcertificate

ofsuccessfulcompletionoftraining.

AMC 66.A.15 (a) Eligibility

DiplomainAeronautical,Mechanical,ElectricalandElectronicsengineeringrecognized

bystatetechnicaleducationboardshallbeconsideredasequivalentqualification.

Toprovetheequivalenceto10+2,theapplicantisrequiredtosubmitacertificatefrom

acompetentauthoritysuchasAssociationofIndianUniversities(AIU).

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GM 66.A.20 (a) Privileges

1. Thefollowingdefinitionsapply:

Electrical systemmeanstheaircraftelectricalpowersupplysource,plusthedistri-butionsystemtothedifferentcomponentscontainedintheaircraftandrelevantcon-nectors.Lightingsystemsarealsoincludedinthisdefinition.Whenworkingoncablesandconnectorswhicharepartoftheseelectricalsystems,thefollowingtypicalprac-ticesareincludedintheprivileges:

Continuity,insulationandbondingtechniquesandtesting; Crimpingandtestingofcrimpedjoints; Connectorpinremovalandinsertion; Wiringprotectiontechniques.

Avionics system means an aircraft system that transfers, processes, displays orstoresanalogueordigitaldatausingdatalines,databuses,coaxialcables,wirelessorotherdatatransmissionmedium,andincludesthesystem’scomponentsandconnect-ors.Examplesofavionicssystemsincludethefollowing:

Autoflight; Communication,RadarandNavigation; Instruments(seeNOTEbelow); In-FlightEntertainmentSystems; IntegratedModularAvionics(IMA); On-BoardMaintenanceSystems; InformationSystems; Fly-by-WireSystems(relatedtoATA27“FlightControls”); FibreOpticControlSystems.

NOTE: Instruments are formally included in the privileges of the B2 licence holders. How-ever, maintenance on electromechanical and pitot-static components may also be re-leased by a B1 license holder.

Simple testmeansatestdescribedinapprovedmaintenancedataandmeetingallthefollowingcriteria:

Theserviceabilityofthesystemcanbeverifiedusingaircraftcontrols,switches,Built-inTestEquipment(BITE),CentralMaintenanceComputer(CMC)orexternal

testequipmentnotinvolvingspecialtraining. Theoutcomeofthetestisauniquego–nogoindicationorparameter,whichcan

beasinglevalueoravaluewithinanintervaltolerance.Nointerpretationofthetestresultorinterdependenceofdifferentvaluesisallowed.

The test does not involve more than 10 actions as described in the approved

maintenancedata(notincludingthoserequiredtoconfiguretheaircraftpriortothetest,i.e.jacking,flapsdown,etc.,ortoreturntheaircrafttoitsinitialconfigu-ration).Pushingacontrol,switchorbutton,andreadingthecorrespondingout-comemaybeconsideredasasinglestepevenifthemaintenancedatashowsthemseparated.

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Troubleshootingmeanstheproceduresandactionsnecessaryusingapprovedmainte-nancedata,inordertoidentifytherootcauseofadefectormalfunction.ItmayincludetheuseofBITEorexternaltestequipment.

Line maintenance meansanymaintenancethatiscarriedoutbeforeflighttoensurethattheaircraftisfitfortheintendedflight.Itmayinclude:

troubleshooting;

defectrectification;

componentreplacementwiththeuseofexternaltestequipment,ifrequired.Com-ponentreplacementmayincludecomponentssuchasenginesandpropellers;

scheduledmaintenanceand/orchecksincludingvisualinspectionsthatwilldetectobviousunsatisfactoryconditions/discrepanciesbutdonotrequireextensivein-depthinspection.Itmayalsoincludeinternalstructure,systemsandpowerplantitemswhicharevisiblethroughquickopeningaccesspanels/doors;

minorrepairsandmodificationswhichdonotrequireextensivedisassemblyand

canbeaccomplishedbysimplemeans; fortemporaryoroccasionalcases(AirworthinessDirectives,hereinafterAD;ser-

vicebulletins,hereinafterSB)thequalitymanagermayacceptbasemaintenancetasks to be performedby a line maintenanceorganisation providedall require-mentsarefulfilled.TheDGCAwillprescribetheconditionsunderwhichthesetasksmaybeperformed.

Base MaintenancemeansanytaskfallingoutsidethecriteriaaregivenaboveforLineMaintenance.

NOTE:

Aircraftmaintainedinaccordancewith“progressive”typeprogrammesneedtobeindi-viduallyassessedinrelationtothisparagraph.Inprinciple,thedecisiontoallowsome“progressive”checkstobecarriedout isdeterminedbytheassessmentthatall taskswithintheparticularcheckcanbecarriedoutsafelyto therequiredstandardsat thedesignatedlinemaintenancestation.2.ThecategoryB3licencedoesnotincludeanyAsubcategory.Nevertheless,thisdoes

notpreventtheB3licenceholderfromreleasingmaintenancetaskstypicaloftheA1.2subcategoryforpiston-enginenon-pressurizedaeroplanesof2000kgMTOMandbe-low,withinthelimitationscontainedintheB3licence.

3.ThecategoryClicencepermitscertificationofscheduledbasemaintenancebytheis-

sueofasinglecertificateofreleasetoserviceforthecompleteaircraftafterthecom-pletionofallsuchmaintenance.ThebasisforthiscertificationisthatthemaintenancehasbeencarriedoutbycompetentmechanicsandcategoryB1,B2andB3supportstaff,asappropriate,havesignedforthemaintenancetasksundertheirrespectivespecialization.TheprincipalfunctionofthecategoryCcertifyingstaffistoensurethatallrequiredmaintenancehasbeencalledupandsignedoffbythecategoryB1,B2and

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B3supportstaff,asappropriate,beforeissueofthecertificateofreleasetoservice.OnlycategoryCpersonnelwhoalsoholdcategoryB1,B2orB3qualificationsmayperformbothrolesinbasemaintenance.

AMC 66.A.20 (b) (2) Privileges

The6monthsmaintenanceexperiencein2yearsshouldbeunderstoodasconsistingof

twoelements,durationandnatureoftheexperience.Theminimumtomeettherequire-

mentsfortheseelementsmayvarydependingonthesizeandcomplexityoftheaircraft

andtypeofoperationandmaintenance.

1.Duration:

Withinanapprovedmaintenanceorganization:

6monthscontinuousemploymentwithinthesameorganisation;or

6monthssplitupintodifferentblocks,employedwithinthesameorindifferent

organisations.

The6monthsperiodcanbereplacedby100daysofmaintenanceexperienceinac-

cordancewiththeprivileges,whetherthesehavebeenperformedwithinanapproved

organisationorasindependentcertifyingstaffaccordingtoM.A.801(b)2orasacom-

binationthereof.

WhenlicenceholdermaintainsandreleasesaircraftinaccordancewithM.A.801(b)

2,incertaincircumstancesthisnumberofdaysmayevenbereducedby50%when

agreedinadvancebytheDGCA.Thesecircumstancesconsiderthecaseswherethe

holderof a CAR-66 licencehappens to be theownerofan aircraft and carriesout

maintenanceonhisownaircraft,orwherealicenceholdermaintainsanaircraftop-

eratedfor lowutilization, thatdoesnotallowthelicenceholdertoaccumulatethe

requiredexperience.Thisreductionshouldnotbecombinedwiththe20%reduction

permittedwhencarryingouttechnicalsupport,ormaintenanceplanning,continuing

airworthinessmanagementorengineeringactivities.Toavoidatoolongperiodwith-

outexperience,theworkingdaysshouldbespreadovertheintended6monthspe-

riod.

2.Natureoftheexperience:

Dependingonthecategoryoftheaircraftmaintenanceengineer’slicence,thefollowing

activitiesareconsideredrelevantformaintenanceexperience:

-Servicing;

-Inspection;

-Operationalandfunctionaltesting;

-Trouble-shooting;

-Repairing;

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-Modifying;

-Changingcomponent;

-Supervisingtheseactivities;

-Releasingaircrafttoservice.

ForcategoryAlicenceholder,theexperienceshouldincludeexercisingtheprivileges,

bymeansofperformingtasksrelatedtotheauthorizationonatleastoneaircrafttype

foreachlicencesubcategory.ThismeanstasksasmentionedinAMC145.A.30(g),in-

cludingservicing,componentchangesandsimpledefectrectifications.

ForcategoryB1,B2andB3,foreveryaircrafttyperatingincludedintheauthorization

theexperienceshouldbeonthatparticularaircraftoronasimilaraircraftwithinthe

samelicence(sub)category.Twoaircraftcanbeconsideredassimilarwhentheyhave

similar technology, construction and comparable systems, which means equally

equippedwiththefollowing(asapplicabletothelicencecategory):

(a) Propulsionsystems(pistonorturboproporturbofanorturboshaftorjet-engine

orpushpropellers);and

(b) Flightcontrolsystems(onlymechanicalcontrolsorhydro-mechanicallypowered

controlsorelectro-mechanicallypoweredcontrols);and

(c) Avionicsystems(analogsystemsordigitalsystems);and

(d) Structure(manufacturedofmetalorcompositeorwood).

Forlicensesendorsedwith(sub)groupratings: InthecaseofB1licenceendorsedwith(sub)groupratings(eithermanufacturer

subgrouporfull(sub)group)asdefinedin66.A.45theholdermayshowexperi-

enceonatleastoneaircrafttypeper(sub)groupandperaircraftstructure(metal,

composite,wood).

InthecaseofaB2licenceendorsedwith(sub)groupratings(eithermanufacturer

grouporfull(sub)group)asdefinedin66.A.45theholdermayshowexperience

onatleastoneaircrafttypeper(sub)group.

InthecaseofaB3licenceendorsedwiththerating‘piston-enginenon-pressurized

aeroplanesof2000kgMTOMandbelow’asdefinedin66.A.45,theholdershould

showexperienceonatleastoneaircrafttypeperaircraftstructure(metal,compo-

site,wooden).

ForcategoryC,theexperienceshouldcoveratleastoneoftheaircrafttypesendorsed

onthelicence.

Foracombinationofcategories,theexperienceshouldincludesomeactivitiesofthena-

tureshowninparagraph2ineachcategory.

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Amaximumof20%oftheexperiencedurationrequiredmaybereplacedbythefollow-

ingrelevantactivitiesonanaircrafttypeofsimilartechnology,constructionandwith

comparablesystems:

Aircraftmaintenancerelatedtrainingasaninstructor/assessororasastudent;

Maintenancetechnicalsupport/engineering;

Maintenancemanagement/planning.

Theexperienceshouldbedocumentedinanindividuallogbookorinanyotherrecord-

ingsystem(whichmaybeanautomatedone)containingthefollowingdata:

(a) Dateandtime;

(b) Aircrafttype;

(c) Aircraftidentificationi.e.registration;

(d) ATAchapter;

(e) Operation performed i.e. 100FH check, MLG wheel change, engine oil check and

complement, SB embodiment, trouble shooting, structural repair, STC embodi-

ment…;

(f) Typeofmaintenancei.e.base,line;

(g) Typeofactivityi.e.perform,supervise,release;

(h) CategoryusedA,B1,B2,B3orC.

(i) Durationindaysorpartial-days.

GM 66.A.20 (b) 2 Privileges

Thesentence“mettheprovisionfortheissueoftheappropriateprivileges”includedin

66.A.20(b)2meansthatduringtheprevious2yearsthepersonhasmetalltherequire-

mentsfortheendorsementofthecorrespondingaircraftrating(forexample,inthecase

ofaircraft inGroup1,theoreticalpluspracticalelementplus, ifapplicable,on-the-job

training).Thissupersedestheneedfor6monthsofexperienceforthefirst2years.How-

ever,therequirementof6monthsofexperienceinthepreceding2yearswillneedtobe

metafterthesecondyear.

AMC 66.A.20 (b) 3 Privileges

Thewording“hastheadequatecompetencetocertifymaintenanceonthecorrespond-

ing aircraft” means that the licence holder and, if applicable, the organisation where

he/sheiscontracted/employed,shouldensurethathe/shehasacquiredtheappropriate

knowledge,skills,attitudeandexperiencetoreleasetheaircraftbeingmaintained.This

isessentialbecausesomesystemsandtechnologypresentintheparticularaircraftbeing

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maintained may not have been covered by the training/examination/experience re-

quiredtoobtainthelicenceandratings.

Thisistypicallythecase,amongothers,inthefollowingsituations:

TyperatingswhichhavebeenendorsedonalicenceinaccordancewithAppendix

ItoAMCtoCAR-66“ListofTypeRatings”afterattendingtypetraining/on-the-job

trainingwhichdidnotcoverallthemodels/variantsincludedinsuchrating.For

example, a licence endorsed with the rating Airbus A318/A319/A320/A321

(CFM56)afterattendingtypetraining/on-the-jobtrainingcoveringonlytheAir-

bus320(CFM56).

TyperatingswhichhavebeenendorsedonalicenceinaccordancewithAppendix

ItoAMCtoCAR-66“ListofTypeRatings”afteranewvarianthasbeenaddedto

therating inAppendixI,withoutperformingdifferencetraining.Forexample,a

licenceendorsedwiththeratingBoeing737-600/700/800/900forapersonwho

alreadyhadtheratingBoeing737-600/700/800,withoutperforminganydiffer-

encetrainingforthe737-900.

Work being carried out on a model/variant for which the technical design and

maintenancetechniqueshavesignificantlyevolvedfromtheoriginalmodelused

inthetypetraining/on-the-jobtraining.

Specific technologyandoptions selected byeachcustomerwhichmay not have

beencoveredbythetypetraining/on-the-jobtraining. ChangesinthebasicknowledgerequirementsofAppendixItoCAR-66notrequir-

ingreexaminationofexistinglicenceholders(grandfatheredprivileges).

Theendorsementofgroup/subgroupratingsbasedonexperienceonarepresenta-

tivenumberoftasks/aircraftorbasedontypetraining/examinationonarepre-

sentativenumberofaircraft.

Personsmeetingtherequirementsof6monthsofexperienceevery2yearsonly

oncertainsimilaraircrafttypesasallowedbyAMC66.A.20(b)2.

PersonsholdingaCAR-66licencewithlimitations,obtainedthroughconversionof

pre-existingqualifications(66.A.70),wheresuchlimitationsaregoingtobelifted

afterperformingthe corresponding basic knowledgeexaminations. In this case,

thetyperatingsendorsedinthelicencemayhavebeenobtainedwithoutcovering

alltheaircraftsystems(becauseofthepreviouslimitations)andtherewillbeneed

toassessand,ifapplicable,totrainthispersononthemissingsystems.

AdditionalinformationisprovidedinAMC145.A.35(a).

GM 66. A. 20 (b) 4 Privileges

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1.HoldersofaCAR-66aircraftmaintenancelicencemaynotexercisecertificationpriv-ilegesunlesstheyhaveageneralknowledgeofthelanguageusedwithinthemainte-nanceenvironmentincludingknowledgeofcommonaeronauticaltermsinthelan-guage.Thelevelofknowledgeshouldbesuchthatthelicenceholderisableto:

read and understand the instructions and technical manuals in use within the

organisation; makewrittentechnicalentriesandanymaintenancedocumentationentries,which

canbeunderstoodbythosewithwhomtheyarenormallyrequiredtocommuni-cate;

readandunderstandthemaintenanceorganisationprocedures; communicateatsuchalevelastopreventanymisunderstandingwhenexercising

certificationprivileges.

2. Inallcases,thelevelofunderstandingshouldbecompatiblewiththelevelofcertifi-cationprivilegesexercised.

GM 66.A.25 (a) Basic knowledge requirements

Thelevelsofknowledgeforeachlicence(sub)categoryaredirectlyrelatedtothecom-

plexityof thecertificationsrelatedto thecorrespondinglicence(sub)category,which

meansthatcategoryAshoulddemonstratealimitedbutadequatelevelofknowledge,

whereascategoryB1,B2andB3shoulddemonstrateacompletelevelofknowledgein

theappropriatesubjectmodule.

AMC 66.A.30 (a) Experience requirements

1. Providedthattheexperiencerequirementspecifiedat66.A.30.a.(1)and(2)shallbereducedbyoneyearincaseofanapplicantwhohassatisfactorilycompletedtrain-inginanytrainingorganizationapprovedunderrule133BorwhohasacquiredaDegreeinanalliedfieldofEngineeringfromarecognizedUniversity;

2. While an applicant to a CAR-66 Category C licence may be qualified by having 3

years’experienceascategoryB1orB2certifyingstaffonlyinlinemaintenance,itis

however rrecommended that anyapplicant fora categoryCholding a B1orB2

licencedemonstrateatleast12monthsexperienceasaB1orB2basemaintenance

supportstaff.

3.Askilledworkerisapersonwhohassuccessfullycompletedatrainingacceptableto

theDGCAandinvolvingthemanufacture,repair,overhaulorinspectionofmechan-

ical,electricalorelectronicequipment.Thetrainingwouldincludetheuseoftools

andmeasuringdevices.

4.Maintenanceexperienceonoperatingaircraft:

-Meanstheexperienceofbeinginvolvedinmaintenancetasksonaircraftwhicharebeingoperatedbyairlines,airtaxiorganisations,owners,etc.;

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-Shouldcoverawiderangeoftasksinlength,complexityandvariety;-Aimsatgainingsufficientexperienceintherealenvironmentofmaintenanceas

opposedtoonlythetrainingschoolenvironment;-Maybegainedwithindifferenttypesofmaintenanceorganisations(CAR-145,

M.A.SubpartFetc.)orunderthesupervisionofindependentcertifyingstaff;-MaybecombinedwithCAR-147approvedtrainingsothatperiodsoftrainingcan

beintermixedwithperiodsofexperience,similartoanapprenticeship

AMC 66.A.30 (d) Experience requirements

Tobeconsideredasrecentexperience;atleast50%oftherequired12monthexperienceshouldbegainedwithinthe12monthperiodpriortothedateofapplicationfortheCAR-66 aircraft maintenance license. The remainder of the experience should have beengainedwithinthe7 yearperiodpriortoapplication. Itmustbenotedthattherestofthebasicexperiencerequiredby66.A.30mustbeobtainedwithinthe10yearspriortotheapplicationasrequiredby66.A.30(f).

AMC 66.A.30 (e) Experience requirements 1. For category A the additional experience of civil aircraft maintenance should be a

minimumof6months.ForcategoryB1,B2orB3,theadditionalexperienceofcivil

aircraftmaintenanceshouldbeaminimumof12months.

2. Aircraftmaintenanceexperiencegainedoutsideacivilaircraftmaintenanceenviron-

ment can include aircraft maintenance experience gained in armed forces, coast

guards,policeetc.orinaircraftmanufacturing.

GM 66.A.40 Continued validity of the aircraft maintenance licence

ValidityoftheCAR-66aircraftmaintenancelicenceisnotaffectedbyrecencyofmainte-nanceexperiencewhereasthevalidityofthe66.A.20privilegesisaffectedbymainte-nanceexperienceasspecifiedin66.A.20(a).

GM 66.A.45 (b) Endorsement with aircraft ratings

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Anaircrafttyperatingincludesalltheaircraftmodels/variantslistedincolumn2ofAp-pendixItoAMCtoCAR-66.

When a person already holds a type rating on the licence and such type rating isamendedintheAppendixItoAMCtoCAR-66inordertoincludeadditionalmodels/var-iants,thereisnoneedforadditionaltypetrainingforthepurposeofamendingthetyperatinginthelicence.Theratingshouldbeamendedtoincludethenewvariants,uponrequestbytheapplicant,withoutadditionalrequirements.However,itistheresponsi-bilityofthelicenceholderand,ifapplicable,themaintenanceorganisationwherehe/sheisemployedtocomplywith66.A.20(b)3,145.A.35(a)andM.A.607(a),asapplicable,be-forehe/sheexercisescertificationprivileges.

Similarly, type training courses covering certain, but not all the models/variants in-cludedinatyperating,arevalidforthepurposeofendorsingthefulltyperating

AMC 66.A.45 (e) Endorsement with aircraft ratings

1. ForthegrantingofmanufacturersubgroupratingsforGroup2aircraft,forB1andC

licenceholders,thesentence“atleasttwoaircrafttypesfromthesamemanufacturer

whichcombinedarerepresentativeoftheapplicablemanufacturersubgroup”means

thattheselectedaircrafttypesshouldcoverallthetechnologiesrelevanttotheman-

ufacturersubgroupinthefollowingareas:

-Flightcontrolsystems(mechanicalcontrols/hydromechanicallypoweredcon-

trols/electromechanicallypoweredcontrols);and-Avionicsystems(analoguesystems/digitalsystems);and-Structure(manufacturedofmetal/composite/wood).

Incaseswherethereareverydifferentaircrafttypeswithinthesamemanufacturer

subgroup,itmaybenecessarytocovermorethantwoaircrafttypestoensureade-

quaterepresentation.

Forthispurposeitmaybepossibletouseaircrafttypesfromthesamemanufacturer

classifiedinGroup1aslongastheselectedaircraftbelongtothesamelicencesub

categoryforwhichtheratingwillbeendorsed.

2. Forthegrantingof fullsubgroupratings forGroup2aircraft, forB1 andC licence

holders, the sentence “at least three aircraft types from different manufacturers

whichcombinedarerepresentativeoftheapplicablesubgroup”meansthatthese-

lectedaircrafttypesshouldcoverallthetechnologiesrelevanttothemanufacturer

subgroupinthefollowingareas:

- Flight control systems (mechanical controls/hydro mechanically powered con-

trols/electromechanicallypoweredcontrols);and-Avionicsystems(analoguesystems/digitalsystems);and

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-Structure(manufacturedofmetal/composite/wood).

Incaseswherethereareverydifferentaircrafttypeswithinthesamesubgroup,itmaybenecessarytocovermorethanthreeaircrafttypestoensureadequaterepresentation.ForthispurposeitmaybepossibletouseaircrafttypesfromdifferentmanufacturersclassifiedinGroup1aslongastheselectedaircraftbelongtothesamelicencesubcate-goryforwhichtheratingwillbeendorsed.3. Formanufacturersubgroupratings, the term“manufacturer”meanstheTCholder

definedinthecertificationdatasheet,whichisreflectedinthelistoftyperatingsin

AppendixItoAMCtoCAR-66.

InthecaseofanaircraftratingwherethetyperatingreferstoaTCholdermadeofaCombinationoftwomanufacturerswhichproduceasimilaraircraft(i.e.AGUSTA/BEL-LELICOPTERTEXTRONoranycaseofaircraftsimilarlybuiltbyanothermanufacturer),thiscombinationshouldbeconsideredasonemanufacturer.Asaconsequence: Whenalicenceholdergetsamanufacturertypeoramanufacturersubgrouprating

madeofacombinationofmanufacturers,itcoversthecombinationofsuchmanu-facturers.

Whenalicenceholderwhointendstoendorseafullsubgroupratingselectsthree

aircraftfromdifferentmanufacturers,thismeansfromdifferentcombinationsofmanufacturersasapplicable.

AMC 66.A.45 (d), (e) 3, (f) 1 and (g) 1 Endorsement with aircraft ratings

1 The“practicalexperience”shouldcoverarepresentativecrosssectionincludingat

least50%oftaskscontainedinAppendixIItoAMCrelevanttothelicencecategory

andtotheapplicableaircrafttyperatingsoraircraft(sub)groupratingsbeingen-

dorsed.ThisexperienceshouldcovertasksfromeachparagraphoftheAppendixII

list.OthertasksthanthoseintheAppendixIImaybeconsideredasareplacement

when they are relevant. In the case of (sub)group ratings, this experience may be

shownbycoveringoneorseveralaircrafttypesoftheapplicable(sub)groupandmay

includeexperienceonaircraftclassifiedingroup1,2and/or3aslongastheexperi-

enceisrelevant.Thepracticalexperienceshouldbeobtainedunderthesupervision

ofauthorisedcertifyingstaff.

2 InthecaseofendorsementofindividualtyperatingsforGroup2andGroup3aircraft,

forthesecondaircrafttypeofeachmanufacturer(sub)groupthepracticalexperience

shouldbereducedto30%ofthetaskscontainedinAppendixIItoAMCrelevantto

thelicencecategoryandtotheapplicableaircrafttype.Forsubsequentaircrafttypes

ofeachmanufacturer(sub)groupthisshouldbereducedto20%.

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3.Practicalexperienceshouldbedemonstratedbythesubmissionofrecordsoralog-

bookshowingtheAppendixIItasksperformedbytheapplicant.Typicaldatatobe

recordedaresimilartothosedescribedinAMC66.A.20(b)2.

GM 66.A.45 Endorsement with aircraft ratings

Thefollowingtableshowsasummaryoftheaircraftratingrequirementscontainedin

66.A.45,66.A.50andAppendixIIItoCAR-66.

Thetablecontainsthefollowing: Thedifferentaircraftgroups;

Foreachlicence(sub)category,whichratingsarepossible(atthechoiceoftheappli-

cant)

oIndividualtyperatings;

oFulland/orManufacturer(sub)groupratings;

Foreachratingoption,whicharethequalificationoptions;

FortheB1.2licence(Group3aircraft)andfortheB3licence(piston-enginenon-pres-

surizedaeroplanesof2000kgMTOMandbelow)whicharethepossiblelimitations

tobeincludedinthelicenceifnotsufficientexperiencecanbedemonstratedinthose

areas.

Note:OJTmeans“On-the-JobTraining”(AppendixIIItoCAR-66,Section6)andisonly

requiredforthefirstaircraftratinginthelicence(sub)category.

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Aircraft rating requirements

Aircraft Groups B1/B3 Licence B2 licence C licence

Group 1

Complex motor powered

aircraft.

Multiple engine helicopters.

Aeroplanes certified above

FL290.

Aircraft equipped with

fly-by-wire.

Other aircraft when defined

DGCA

(For B1) Individual TYPE RATING Type training: - Theory + examination - Practical + assessment PLUS OJT (for first aircraft in licence subcat-egory

Individual TYPE RATING Type training: - Theory + examina-tion - Practical + assess-ment PLUS OJT (for first aircraft in licence category

Individual TYPE RATING Type training:

- Theory + examination

Group 2: Subgroups: 2a: single turboprop aeroplanes (*) 2b: single turbine engine helicopters (*) 2c: single piston-engine helicopters (*) (*) Except those classified in Group 1.

(For B1.1, B1.3, B1.4) Individual TYPE RATING (type training + OJT) or (type examination + practical experi-ence) Full SUBGROUP RATING (type training + OJT) or (type exami-nation + practical experience) on at least 3 aircraft representative of that subgroup Manufacturer SUBGROUP RATING (type training + OJT) or (type examination + practical experi-ence) on at least 2 aircraft representative of that manufacturer subgroup

Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full SUBGROUP RATING based on demonstra-tion of practical experi-ence Manufacturer SUBGROUP RATING based on demonstra-tion of practical experi-ence

Individual TYPE RATING type training or type examination Full SUBGROUP RATING type training or type examination on at least 3 aircraft representa-tive of that subgroup Manufacturer SUBGROUP RATING type training or type examination on at least 2 aircraft representa-tive of that manufac-turer subgroup

Group 3 Piston-engine aeroplanes (except those classified in

Group 1.

(For B1.2) Individual TYPE RATING (type training + OJT) or (type examination + practical experi-ence) Full GROUP 3 RATING based on demonstration of practical experience Limitations:

Pressurised aeroplanes

Metal aeroplanes

Composite aeroplanes

Wooden aeroplanes

Metal tubing & fabric aeroplanes

Individual TYPE RATING (type training + OJT) or (type examination + practical experience) Full GROUP 3 RAT-ING based on demonstra-tion of practical experi-ence

Individual TYPE RATING type training or type examination Full GROUP 3 RAT-ING based on demonstra-tion of practical experi-ence

Piston-engine nonpressur-ized aeroplanes of 2 000 kg MTOM and below

(For B3) FULL RATING "Piston-engine non-pressurized aeroplanes of 2 000 kg MTOM and below" based on demonstration of practical experience Limitations: Metal aeroplanes Composite aeroplanes Wooden aeroplanes Metal tubing & fabric aeroplanes

Not applicable

Not applicable

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AMC 66.A.50 (b) Limitations

1.Theappropriateexperiencerequiredtoremovethelimitationsreferredtoin66.A.45

(f)and(g)shouldconsistoftheperformanceofavarietyoftasksappropriatetothe

limitationsunderthesupervisionofauthorisedcertifyingstaff.Thisshouldinclude

thetasksrequiredbya scheduledannual inspection.Alternatively, thisexperience

mayalsobegained,ifagreedbytheDGCA,bytheoreticalandpracticaltrainingpro-

videdbythemanufacturer,aslongasanassessmentisfurthercarriedoutandrec-

ordedbythismanufacturer.

2.Itmaybeacceptabletohavethisexperienceonjustoneaircrafttype,providedthat

thistypeisrepresentativeofthe(sub)groupinrelationtothelimitationbeingre-

moved.

3.Theapplicationforthelimitationremovalshouldbesupportedbyarecordofexperi-

encesignedbytheauthorisedcertifyingstafforbyanassessmentsignedbytheman-

ufactureraftercompletionoftheapplicabletheoreticalandpracticaltraining.

GM 66.A.70 Conversion provisions

1. Asdescribedinpoint66.A.70,theconversionprovisionsapplytotheholderofaAME

LicencepriortothedateofentryintoforceofCAR-66..

2. Theconversionappliesto“certifyingstaffqualifications”suchas,forexample:

HoldingaAMElicence(orcompletedtheprocesstoobtainsuchalicence;)

Thisdoesnotmeanthatinordertobeentitledtoaconversionprocess,theapplicanthas

tobeexercisingcertificationprivileges.Apersonmayholda“certifyingstaffqualifica-

tion”whilenothavingcertificationprivileges(orwhileexercisingverylimitedcertifica-

tionprivilegesbelowhis/herqualification)fordifferentreasonssuchas, forexample,

thefollowing:

Thepersonisworkingas“supportstaff”inthebasemaintenanceenvironment;

Thepersonhasbeenauthorisedonlyforaverylimitedrangeoftasks(lowerthan

whathe/shewouldbeentitledifhis/herqualificationisconsidered)sincetheper-

sonisworkinginalinestationwherethescopeoftasksisverylimited;

Thepersonholdsalicencewithawiderscopethanthescopeoftheorganisation

wherehe/sheisemployed;

Thepersonisworkingoutsidetheaviationindustryoristemporarilyonleavedue

todifferentreasons(medical,personal,etc.).

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Thesepersonsareentitledtohavetheconversionperformedinaccordancewiththefull

scopeoftheirqualificationandthefullprivilegesthattheywouldbeentitledtoholdon

thebasisofsuchqualification.

3. Asdescribedinpoint66.A.70,certifyingstaffqualificationseligibleforconversionare

thosevalid“priortothedateofentryintoforceofCAR-66.

4.Althoughonlythosecertifyingstaffqualificationsgainedasindicatedaboveareeligi-

bleforconversion,thisdoesnotmeanthattheapplicationforconversionhastobe

submittedpriortothosedates.Theapplicantisentitledtohavetheconversionper-

formedirrespectiveofwhenhe/sheappliesforconversion.

5.Acertifyingstaffqualificationcanbesubjecttomorethanoneconversionprocessand

canalsobeconvertedtomorethanonelicence(withanyapplicablelimitations).This

couldbethecase,forexample,forapersonwhoalreadyhadthecertifyingstaffqual-

ificationconvertedtoaB1.2licencewithlimitationslinkedtosomemissingelements

oftheCAR-66AppendixIandIIstandard(following66.A.70(c)).Thispersonwould

beentitledtoapplyandhavehis/hercertifyingstaffqualificationconvertedtoaB1.2

oraB3licenceonthebasisof66.A.70(d),whichwouldmeanthatthereisnoneedto

comparewiththeCAR-66AppendixIandIIstandard,introducingonlythoselimita-

tionsrequiredtomaintaintheexistingprivileges.

GM 66.A.70(c) Conversion provisions

Forexample,alimitationcouldbewhereapersonholdsapre-existingcertifyingstaff

qualificationwhichcovered,tothestandardofCAR-66AppendixIandII,allthemod-

ules/subjectscorrespondingtotheB1licenceexceptforelectricalpowersystems.This

personwouldreceiveaCAR-66aircraftmaintenancelicenceintheB1categorywitha

limitation(exclusion)onelectricalpowersystems.

Forremovaloflimitations,referto66.A.50(c).

GM 66.A.70 (d) Conversion provisions

Inthecaseofaircraftnotinvolvedincommercialairtransportotherthanlargeaircraft,

an example of limitations could be where a person holds a pre CAR-66 qualification

whichcoveredprivilegestoreleaseworkperformedonaircraftstructures,powerplant,

mechanicalandelectricalsystemsbutexcludedprivilegesonaircraftequippedwithtur-

bineengine,aircraftabove2000kgMTOM,pressurisedaircraftandaircraftequipped

withretractablelandinggear.ThispersonwouldreceiveaCAR-66aircraftmaintenance

licenceintheB1.2orB3(sub)categorywiththefollowinglimitations(exclusions):

Aircraftinvolvedincommercialairtransport(thislimitationalwaysexists);

Aircraftabove2000kgMTOM;

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Pressurizedaircraft;

Aircraftequippedwithretractablelandinggear.

Anotherexampleoflimitationscouldbewhereapilot-ownerholdsapreCAR-66quali-

fication which covered privileges to release work performed on aircraft structures,

powerplant,mechanicalandelectricalsystemsbutlimitedtohis/herownaircraftand

toaparticularaircrafttype(forexample,aCessna172).Thispilot-ownerwouldreceive

aCAR-66aircraftmaintenancelicenceintheB1.2orB3(sub)categorywiththefollow-

inglimitations(exclusions):

Aircraftinvolvedincommercialairtransport(thislimitationalwaysexists);

AircraftotherthanaCessna172;

Aircraftnotownedbythelicenceholder.

Theessentialaspectisthatthelimitationsareestablishedinordertomaintainthepriv-

ilegesofthepreCAR-66qualification,withoutcomparingthepreviousqualificationwith

thestandardofCAR-66AppendixIandII.

Forremovaloflimitations,referto66.A.50(c).

AMC to Section 1 of Appendix III to CAR-66 “Aircraft Type Training and Examina-

tion Standard. On-the-Job Training”

Aircrafttypetraining1.Aircrafttypetrainingmaybesubdividedinairframeand/orpowerplantand/or

avionics/electricalsystemstypetrainingcourses

i. Airframetypetrainingcoursemeansatypetrainingcourseincludingallrele-

vant aircraft structure and electrical and mechanical systems excluding the

powerplant.

ii. Powerplanttypetrainingcoursemeansatypetrainingcourseonthebareen-

gine,includingthebuild-uptoaquickenginechangeunit.

iii. Theinterfaceoftheengine/airframesystemsshouldbeaddressedbyeitherair-

frameorpowerplanttypetrainingcourse.Insomecases,suchasforgeneral

aviation,itmaybemoreappropriatetocovertheinterfaceduringtheairframe

courseduetothelargevarietyofaircraftthatcanhavethesameenginetype

installed.

iv. Avionics/electricalsystemstypetrainingcoursemeanstypetrainingonavion-

ics andelectrical systemscoveredbybut not necessarily limited toATA(Air

TransportAssociation)Chapters22,23,24,25,27,31,33,34,42,44,45,46,73

and77orequivalent.

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2.Practicaltrainingmaybeperformedeitherfollowingorintegratedwiththetheoreti-

calelements.However,itshouldnotbeperformedbeforetheoreticaltraining.

3.Thecontentofthetheoreticalandpracticaltrainingshould:

i. addressthedifferentpartsoftheaircraftwhicharerepresentativeofthestruc-

ture,thesystems/componentsinstalledandthecabin;and

ii. includetrainingontheuseoftechnicalmanuals,maintenanceproceduresand

theinterfacewiththeoperationoftheaircraft.

iii. Therefore,itshouldbebasedonthefollowingelements:

a. Typedesignincludingrelevanttypedesignvariants,newtechnologyandtech-

niques;

b. Feedbackfromin-servicedifficulties,occurrencereporting,etc.;

c. Significantapplicableairworthinessdirectivesandservicebulletins;

d. Knownhumanfactorissuesassociatedwiththeparticularaircrafttype;

e. Useofcommonandspecificdocumentation,(whenapplicable,suchasMMEL,

AMM,MPD, TSM, SRM, WD, AFM, tool handbook), philosophy of the trouble-

shooting,etc.;

f. Knowledgeofthemaintenanceon-boardreportingsystemsandETOPSmainte-

nanceconditions,whenapplicable;

g. Useofspecial toolingandtestequipment andspecificmaintenancepractices

includingcriticalsafetyitemsandsafetyprecautions;

h. Significant and critical tasks/aspects from the MMEL, CDL, Fuel Tank Safety

(FTS),airworthinesslimitationitems(ALI)includingCriticalDesignConfigura-

tionControlLimitations(CDCCL),CMRandallICAdocumentationsuchasMRB,

MPD,SRM,AMM,etc.,whenapplicable.

i. Maintenanceactionsandprocedurestobefollowedasaconsequenceofspecific

certificationrequirements,suchas,butnotlimitedto,RVSM(ReducedVertical

SeparationMinimum)andNVIS(NightVisionImagingSystems);

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j. Knowledgeofrelevantinspectionsandlimitationsasapplicabletotheeffectsof

environmentalfactorsoroperationalproceduressuchascoldandhotclimates,

wind,moisture,sand,de-icing/anti-icing,etc.

Thetypetrainingdoesnotnecessarilyneedtoincludeallpossiblecustomeroptions,correspondingtothetyperatingdescribedintheAppendixItoAMCtoCAR-66.4.LimitedavionicsystemtrainingshouldbeincludedinthecategoryB1typetraining

astheB1privilegesincludeworkonavionicssystemsrequiringsimpleteststoprove

theirserviceability.

5.ElectricalsystemsshouldbeincludedinbothcategoriesofB1andB2typetraining.

6.Thetheoreticalandpracticaltrainingshouldbecomplementaryandmaybe:

i. Integratedorsplit;

ii. Supportedbytheuseoftrainingaids,suchas,trainers,virtualaircraft,aircraft

components, synthetic training devices (STD), computer-based training de-

vices(CBT),etc.

AMC to Paragraph 3.1(d) of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training” Training Needs Analysis for the theoretical element of the aircraft type training 1.Theminimumdurationforthetheoreticalelementofthetyperatingtrainingcourse,

asdescribedinAppendixIIItoCAR-66,hasbeendeterminedbasedon:

i. genericcategoriesofaircraftandminimumstandardequipmentfit;ii. theestimatedaveragedurationofstandardcoursesimparted.

2.ThepurposeoftheTrainingNeedsAnalysis(TNA)istoadaptandjustifytheduration

ofthecourseforaspecificaircrafttype.ThismeansthattheTNAisthemaindriverfordeterminingthedurationofthecourse,regardlessofwhetheritisaboveorbelowtheminimumdurationdescribedinAppendixIIItoCAR-66.

Intheparticularcaseoftypetrainingcoursesapprovedonthebasisoftherequire-mentsvalidbeforethisCARisapplicableandhavingadurationforthetheoreticalelementequaltoorabovetheminimumdurationcontainedinparagraph3.1(c)ofAppendixIIItoCAR-66,itisacceptablethattheTNAonlycoversthedifferencesin-troducedbythisCARinparagraph3.1(e)“Content”andthecriteriaintroducedinpar-agraph3.1(d)“Justificationofcourseduration”relatedtotheminimumattendanceandthemaximumnumberoftraininghoursperday.ThisTNAmayresultinachangeinthedurationofthetheoreticalelement.

3.ThecontentandthedurationderivingfromtheTNAmaybesupportedbyananalysis

fromtheTypeCertificateholder.

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4.Inordertoapproveareductionofsuchminimumduration,theevaluationdonebythe DGCAshouldbe performedon a case-by-case basis appropriate to theaircrafttype.Forexample,whileitwouldbeexceptionalforatheoreticalcourseforalargetransportcategoryaircraftsuchasanA330orB757tobebelowtheminimumdura-tionshown,itwouldnotnecessarilybeexceptionalinthecaseofaGeneralAviation(GA)businessaircraftsuchasaLearjet45orsimilar.Typically,theTNAforaGAair-craftcoursewoulddemonstratethatacourseofashorterdurationsatisfiesthere-quirements.

5.WhendevelopingtheTNA,thefollowingshouldbeconsidered:

a)TheTNAshouldincludeananalysisidentifyingalltheareasandelementswherethere

isaneed fortrainingaswellas theassociatedlearningobjectives,consideringthedesignphilosophyoftheaircrafttype,theoperationalenvironment,thetypeofoper-ationsandtheoperationalexperience.Thisanalysisshouldbewritteninamannerwhichprovidesareasonableunderstandingofwhichareasandelementsconstitutethecoursetomeetthelearningobjectives.

b)Asaminimum,theTrainingNeedAnalysis(TNA)shouldtakeintoaccountallthe applicableelementscontainedinparagraph3.1ofCAR-66AppendixIIIandassociatedAMCs.c)TheTNAshouldsetupthecoursecontentconsideringtheAppendixIIIobjectivesfor

eachleveloftrainingandtheprescribedtopicsinthetheoreticalelementtablecon-tainedinparagraph3.1ofCAR-66AppendixIII.

d)ForeachChapterdescribedinthetheoreticalelementtablecontainedinparagraph

3.1ofCAR-66AppendixIII,thecorrespondingtrainingtimeshouldberecordede)Typicaldocumentstobeusedtoidentifytheareasandelementswherethereisaneed

fortrainingtypicallyinclude,amongothers,theAircraftMaintenanceManual,MRBreport,CMRs,airworthinesslimitations,TroubleshootingManual,StructuralRepairManual,IllustratedPartsCatalogue,AirworthinessDirectivesandServiceBulletins.

f)Duringtheanalysisofthesedocuments:

i) Considerationshouldbegiventothefollowingtypicalactivities:

1. Activation/reactivation;2. Removal/installation;3. Testing;4. Servicing;5. Inspection,checkandrepairs;6. Troubleshooting/diagnosis.

ii) Forthepurposeofidentifyingthespecificelementsconstitutingthetraining

course,itisacceptabletouseafilteringmethodbasedoncriteriasuchas:

1. Frequencyofthetask;2. Humanfactorissuesassociatedtothetask;3. Difficultyofthetask;

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4. Criticalityandsafetyimpactofthetask;5. In-serviceexperience;6. Novelorunusualdesignfeatures(notcoveredbyCAR-66AppendixI);7. Similaritieswithotheraircrafttypes;8. Specialtestsandtools/equipment.

iii) Itisacceptabletofollowanapproachbasedon:

1. Tasksorgroupsoftasks;or2. Systemsorsubsystemsorcomponents.

g)TheTNAshould:

i. Identifythelearningobjectivesforeachtask,groupoftasks,system,subsystemorcomponent;

ii. Associatetheidentifiedtaskstobetrainedtotheregulatoryrequirements(ta-

bleinparagraph3.1ofAppendixIIItoCAR-66);

iii. Organisethetrainingintomodulesinalogicalsequence(adequatecombinationofchaptersasdefinedinAppendixIIIofCAR-66);

iv. Determinethesequenceoflearning(withinalessonandforthewholesylla-

bus);

v. IdentifythescopeofinformationandlevelofdetailwithregardtotheminimumstandardtowhichthetopicsoftheTNAshouldbetaughtaccordingtotheset-upobjectives.

vi. Addressthefollowing:

1. Descriptionofeachsystem/componentincludingthestructure(where

applicable);2. System/componentoperationtakingintoaccount:

a. Complexityofthesystem(e.g.theneedoffurtherbreakdownintosubsystems,etc.);

b.Designspecificswhichmayrequiremoredetailedpresentationormaycontributetomaintenanceerrors;c.Normalandemergencyfunctioning;d.Troubleshooting;e.Interpretationofindicatorsandmalfunctions.

f.Useofmaintenancepublications;

g.Identificationofspecialtoolsandequipmentrequiredforservicingand

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maintainingtheaircraft;h.MaintenancePractices;

i.Routineinspections,functionaloroperationaltests,rigging/adjustment,etc.vii. Describethefollowing:

1. Theinstructionalmethodsandequipment,teachingmethodsandblendingof

theteachingmethodstoensuretheeffectivenessofthetraining;2. Themaintenancetrainingdocumentation/materialtobedeliveredtothestu-

dent;Facilitateddiscussions,questioningsession,additionalpractice-orientedtraining,etc.;

3. Thehomework,ifdeveloped;4. Thetrainingprovider’sresourcesavailabletothelearner.

h)Itisacceptabletodifferentiatebetweenissueswhichhavetobeledbyaninstructor

andissueswhichmaybedeliveredthroughinteractivesimulationtrainingdevicesand/orcoveredbyweb-basedelements.Overalltimeofthecoursewillbeallocatedaccordingly.

i)Themaximumnumberoftraininghoursperdayforthetheoreticalelementoftype

trainingshouldnotbemorethan6hours.Atraininghourmeans60minutesoftuitionexcludinganybreaks,examination,revision,preparationandaircraftvisit.Inexcep-tionalcases, theDGCAmayallowdeviation fromthisstandardwhen it isproperlyjustifiedthattheproposednumberofhoursfollowspedagogicalandhumanfactorsprinciples.Theseprinciplesareespeciallyimportantinthosecaseswhere:

i. Theoreticalandpracticaltrainingareperformedatthesametime;

ii. Training and normal maintenance duty/apprenticeship are performed at thesametime.

j)Theminimumparticipationtimeforthetraineetomeettheobjectivesofthecourse

shouldnotbelessthan90%ofthetuitionhoursofthetheoreticaltrainingcourse.Additionaltrainingmaybeprovidedbythetrainingorganisationinordertomeettheminimumparticipationtime.Iftheminimumparticipationdefinedforthecourseisnotmet,acertificateofrecognitionshouldnotbeissued.

k)TheTNAisalivingprocessandshouldbereviewed/updatedbasedonoperationfeedback,maintenanceoccurrences,AirworthinessDirectives,majorservicebulle-

tinsimpactingmaintenanceactivitiesorrequiringnewcompetenciesformechanics,alertservicebulletins,feedbackfromtraineesorcustomersatisfaction,evolutionofthe maintenance documentation such as MRBs, MPDs, MMs, etc. The frequency atwhichtheTNAshouldbereviewed/updatedislefttothediscretionoftheorganisa-tionconductingthecourse.

NOTE: The examination is not part of the TNA. However, it should be prepared in accord-

ance with the learning objectives described in the TNA. AMC to Paragraphs 1(b), 3.2 and 4.2 of Appendix III to CAR-66 “Aircraft Type Training and Examination Standard. On-the-Job Training”

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Practical element of the aircraft type training 1.Thepracticaltrainingmayincludeinstructioninaclassroomorinsimulatorsbutpart

ofthepracticaltrainingshouldbeconductedinarealmaintenanceormanufacturerenvironment.

2.Thetasksshouldbeselectedbecauseoftheirfrequency,complexity,variety,safety,criticality,novelty,etc.Theselectedtasksshouldcoverallthechaptersdescribedin

thetablecontainedinparagraph3.2ofAppendixIIItoCAR-66.3.Thedurationofthepracticaltrainingshouldensurethatthecontentoftrainingre-

quiredbyparagraph3.2ofAppendix III to CAR-66 is completed.Nevertheless, foraeroplaneswithaMTOMequalorabove30000kg,thedurationforthepracticalele-ment of a type rating training course should not be less than two weeks, unless ashorterdurationmeetingtheobjectivesofthetrainingandtakingintoaccountpeda-gogicalaspects(maximumdurationperday)isjustifiedtotheDGCA.

4.Theorganisationprovidingthepracticalelementofthetypetrainingshouldprovide

traineeswithascheduleorplan indicating thelistof taskstobeperformedunderinstructionorsupervision.Arecordofthetaskscompletedshouldbeenteredintoalogbookwhichshouldbedesignedsuchthateachtaskorgroupoftasksmaybecoun-tersignedbythedesignatedassessor.Thelogbookformatanditsuseshouldbeclearlydefined.

5.Inparagraph4.2ofAppendixIIItoCAR-66,theterm“designatedassessorsappropri-

atelyqualified”meansthattheassessorsshoulddemonstratetrainingandexperienceontheassessmentprocessbeingundertakenandbeauthorisedtodosobytheorgan-isation.

FurtherguidanceabouttheassessmentandthedesignatedassessorsisprovidedinAppendixIIItoAMCtoCAR-66.6.Thepracticalelement(forpowerplantandavionicsystems)oftheTypeRatingTrain-

ingmaybesubcontractedbytheapprovedCAR-147organisationunderitsqualitysystemaccordingtotheprovisionsof147.A.145(d)3andthecorrespondingGuid-anceMaterial.

AMC to Paragraph 1(c) of Appendix III to CAR-66 “Aircraft Type Training and Ex-amination Standard. On-the-Job Training” Differences training Approveddifferencetrainingisnotrequiredfordifferentvariantswithinthesameair-crafttyperating(asspecifiedinAppendixItoAMCtoCAR-66)forthepurposeoftyperatingendorsementontheaircraftmaintenancelicence.However,thisdoesnotnecessarilymeanthatnotrainingisrequiredbeforeacertifyingstaffauthorizationcanbeissuedbythemaintenanceorganisation(refertoAMC66.A.20(b)3).

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AMC to Section 5 of Appendix III to CAR-66 “Aircraft Type Training and Examina-tion Standard. On-the-Job Training” Type Examination Standard This Section 5 “Type Examination Standard” does not apply to the examination per-formedaspartoftypetraining.ThisSectiononlyappliestothosecaseswheretypeex-aminationisperformedasasubstitutefortypetraining.AMC to Section 6 of Appendix III to CAR-66 “Aircraft Type Training and Examina-tion Standard. On-the-Job Training” On-the-Job Training (OJT) 1.“Amaintenanceorganisationappropriatelyapprovedforthemaintenanceofthepar-

ticularaircrafttype”meansaCAR-145orM.A.SubpartFapprovedmaintenanceor-ganisationholdinganAratingforsuchaircraft.

2.TheOJTshouldincludeone-to-onesupervisionandshouldinvolveactualworktaskperformanceonaircraft/components,coveringlineand/orbasemaintenancetasks.3.TheuseofsimulatorsforOJTshouldnotbeallowed.4.TheOJTshouldcoveratleast50%ofthetaskscontainedinAppendixIItoAMCto

CAR-66.SometasksshouldbeselectedfromeachparagraphoftheAppendixIIlist.Tasksshouldbeselectedamongthoseapplicabletothetypeofaircraftandlicence(sub)categoryappliedfor.OthertasksthanthoseintheAppendixIImaybeconsid-eredasareplacementwhentheyarerelevant.Typically,inadditiontothevarietyandthecomplexity,theOJTtasksshouldbeselectedbecauseoftheirfrequency,safety,novelty,etc.

5.Upto50%oftherequiredOJTmaybeundertakenbeforetheaircrafttheoreticaltype

trainingstarts.6.Theorganisationprovidingtheon-the-jobtrainingshouldprovidetraineesaschedule

orplanindicatingthelistoftaskstobeperformedundersupervision.Arecordofthetaskscompletedshouldbeenteredintoalogbookwhichshouldbedesignedsuchthateachtaskorgroupof tasks iscountersignedbythecorrespondingsupervisor.Thelogbookformatanditsuseshouldbeclearlydefined.

7.Regardingtheday-to-daysupervisionoftheOJTprogrammeintheapprovedmainte-

nanceorganisationandtheroleofthesupervisor(s),thefollowingshouldbeconsid-ered:

i. It issufficient that the completionof individual OJTtasks isconfirmedbythe

directsupervisor(s),withoutbeingnecessarythedirectevaluationoftheasses-sor.

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ii. Duringtheday-to-dayOJTperformance,thesupervisionaimsatoverseeingthecompleteprocess,includingtaskcompletion,useofmanualsandprocedures,ob-servanceofsafetymeasures,warningsandrecommendationsandadequatebe-haviorinthemaintenanceenvironment.

iii. Thesupervisor(s)shouldpersonallyobservetheworkbeingperformedtoen-

surethesafecompletenessandshouldbereadilyavailable forconsultation, ifneededduringtheOJTperformance.

iv. The supervisor(s) should countersign the tasks and release the maintenance

tasksasthetraineeisstillnotqualifiedtodoso.

v. Thesupervisor(s)shouldtherefore:

a) havecertifyingstafforsupportstaffprivilegesrelevanttotheOJTtasks;b) becompetentfortheselectedtasks;c) besafety-orientated;d) becapabletocoach(settingobjectives,givingtraining,performingsupervi-

sion,evaluating,handlingtrainee’sreactionsandculturalissues,managingobjectivelyandpositivelydebriefingsessions,determiningtheneedforex-tratrainingorreorientatethetraining,reporting,etc.);

e) bedesignatedbytheapprovedmaintenanceorganisationtocarryoutthe

supervision.

8.Regardingtheassessor,thefollowingshouldbeconsidered:

a) Thefunctionoftheassessor,asdescribedinSection6ofAppendixIIItoCAR-66,istoconductthefinalassessmentofthecompletedOJT.ThisassessmentshouldincludeconfirmationofthecompletionoftherequireddiversityandquantityofOJTandshouldbebasedonthesupervisor(s)reportsandfeedback.

b) InSection6ofAppendixIIItoCAR-66,theterm“designatedassessorappropri-atelyqualified”meansthattheassessorshoulddemonstratetrainingandexpe-rienceontheassessmentprocessbeingundertakenandshouldbeauthorisedtodosobytheorganisation.

FurtherguidanceabouttheassessmentandthedesignatedassessorsisprovidedinAp-pendixIIItoAMCtoCAR-66.9 The procedures for OJT should be included into the Exposition Manual of the ap

provedmaintenanceorganisation(Chapter3.15,asindicatedinAMC145.A.70(a)).TheseproceduresintheExpositionManualareapprovedbytheDGCA,andproviding

trainingisnotoneoftheprivilegesofamaintenanceorganisation,theycanonlybeusedwhenthelicencingauthorityistheDGCA.Inothercases,itisuptothelicencingauthoritytodecidewhetheritacceptssuchproceduresforthepurposeofapprovingtheOJT(refertoAMC66.B.115).

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AMC to Appendix III to CAR-66 “Aircraft Type Training and Examination Stand-ard. On-the-Job Training” Aircraft type training and On-the-Job Training

Thetheoreticalandpracticaltrainingproviders,aswellastheOJTprovider,maycontracttheservicesofalanguagetranslatorinthecasewheretrainingisimpartedtostudentsnotconversantinthelanguageofthetrainingmaterial.Nevertheless,itremainsessen-tialthatthestudentsunderstandalltherelevantmaintenancedocumentation.Duringthe performance of examinations and assessments, the assistance of the translatorshouldbelimitedtothetranslationofthequestions,butshouldnotprovideclarifica-tionsorhelpinrelationtothosequestions.

SUBPART C AMC 66.A.205 (c) Requirements

MusthavepassedrelevantmodulesofCAR66approvedbytheDGCAmeansmodulesappropriatefortheknowledgerequiredforthemaintenanceofclassofcomponentsforwhichcertificationauthorizationisrequired.

AMC 66.A.205 (g) Requirements.

Forthegrantofcertificationauthorizationthecompetencyofthecandidateshallbeassessed by the organization, followingprocedures documented in the organizationexposition.GuidelinesforcompetencycheckisdetailedinAMCandGMofCAR145-30(e).

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APPENDICES to AMC for CAR-66

Appendix I

AIRCRAFT TYPE RATINGS

FOR CAR-66 AIRCRAFT MAINTENANCE ENGINEER’S LICENCE

The following aircraft type ratings should be used to ensure a common standard

throughoutIndia.

Theinclusionofanaircrafttypeinthelicencedoesnotindicatethattheaircrafttypehas

beengrantedatypecertificateundertheAircraftRuleNo.49AandCAR-21,thislistis

onlyintendedforthemaintenancepurposes.

Inordertokeepthislistcurrentandtyperatingsconsistent,suchinformationshouldbe

firstpassedontotheDGCAdaw@dgca.nic.inbyaffectedpersonnelororganizationsto

issueatyperatingthatisnotincludedinthislist.

Notes:

Whenamodificationisintroducedtoanaircrafttyperatingortoanenginedesignation

intheratingwhichaffectlicencesalreadyissued,theratingsontheAMElicencesmay

bemodifiedatthenextrenewalorwhenthelicenceisreceivedforendorsement/re-

issued,unlessthereisanurgentreasontomodifythelicence.

NotesonaircraftmodifiedbySupplementalTypeCertificateSTC: WhenanaircrafthasbeenmodifiedbyanSTCforinstallationofanotherengine,

theCAR-66typeratingofthisaircraftmaychangei.e. fromGroup2toGroup1.

Thisisnotreflectedinthisdocument.Incasetheapplicanttoalicencefacessuch

acase,theholderofAMELicensemayinformtheDGCAandanewtyperatingwill

bedefinedbytheDGCA

Notes on Type Rating endorsement covering several models/variant:

Theendorsementofatyperating(TR)ontheAircraftMaintenanceEngineer’s(AME)

licensecoveringseveralmodels/variants,doesnotautomaticallyimplythattheAMEli-

cenceholderhasacquiredtheappropriateknowledgeoneachmodel/variant.TheTR

coursereceivedortheexperiencetheAMElicenceholderhasgained,mayhavebeen

limitedtooneorseveralmodel(s)/variant(s)butnottoallmodels/variants.Todemon-

strate adequate competence on the relevant model(s)/variant(s), the AMEL holder

and/orthemaintenanceorganisationwheretheAMElicenceholderiscontracted/em-

ployed,areresponsibletoverifywhetherthemodel/varianthasbeenadequatelycov-

eredbytheTRcourseorgainedexperience.

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Inthefollowingtables:

Thecolumn‘TCHolder’includestheTCholderasdefinedintheTypeCertificateDataSheetsTCDS(EASA,FAAorother)ortheSpecificAirworthinessSpecifications(SAS).

InGroup3,athirdcolumnhasbeenaddedwhichiscalled ‘Typeofstructure’and

whichintendstoassisttheDGCAinidentifyingtheexperiencerequiredforthistype

withaviewonremovingexistinglimitationsonthelicence.

Woodenstructurecoveredwithfabricisconsideredtofallunderwoodenstructure.

For Aeroplanes with a combination of structures; e.g. metal tubing fuselage and

woodenwings,bothexperience‘metaltubecoveredwithfabric’and‘woodenstruc-

ture’arerequired.

InGroup3,afourthcolumnhasbeenaddedwhichiscalled‘MTOM’andwhichintends

to assist in identifying the aeroplanes types where the Maximum Take-Off Mass

(MTOM)is:

—above2TandissubjecttoaB1.2licence,or

—2TandbelowandissubjecttoaB1.2orB3licence.

Column1includestheTCholderasdefinedintheTCDS(EASA,FAAorother).

Foraeroplanesofgroup1and2andhelicopters,theColumn2includestheaircraftmod-

elsasdefinedintherelevantTCDS(EASA,FAAorother).

Thefollowingcolumnincludesthe“commercialdesignation”whenavailable.

Column3includestherelevantindividualtyperating.Onlythedesignationsofratings

incolumn3shouldbeusedforendorsingindividualtyperatingsonCAR-66licences.

Note:aircraftSTCdataarenotincludedinthistable.

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Group -1 Aeroplanes

Group -1 Aeroplanes

1. TC holder 2 Aeroplanes Model Commercial Desig-nation

3 Type Rating Endorsement

Airbus

A310-304

AirbusA310(GECF6)

A310-324 AirbusA310(PW4000)

A318-110series

Airbus A318/A319/A320/A321(CFM56)

A319-110series

A320-111

A320-210series

A321-110series

A321-210series

A319-130series

Airbus A319/A320/A321 (IAEV2500)

A320-230series

A321-130series

A321-230series

A319-170 A319NEO Airbus A319/A320/A321 (IAEPW1100G)

A320-270 A320NEO

A321-270 A321NEO

A319-150 A319NEO Airbus A319/A320/A321 (CFMLEAP-1A)

A320-250 A320NEO

A321-250 A321NEO

A330-200series

AirbusA330(GECF6)

A330-300series

A330-220series

AirbusA330(PW4000)

A330-320series

A330-240Series AirbusA330(RRRB211Trent700)A330-340Series

A340-210 AirbusA340(CFM56)A340-310

AIRCRAFT IN-DUSTRIES

L410ML-410UVP-E9

Turbolet

LetL-410(WalterM601)

ATR42-200

ATR 42-200/300 series (PWCPW120)

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Group -1 Aeroplanes



ATR-GIE Avionsde Transport Ré-gionals

ATR42-320

ATR72-212 ATR72-200series(PWCPW120)

ATR42-50042-50042-600 ATR42-400/500/72-212A(PWC

PW120)ATR72-212A

72-500,72-600

BAESYSTEMS

BAeATP ATP(PWCPW120)

AVRO146-RJ70 BAe146/AVRO146-RJ(HoneywellALF500Series)

HS.748Series1

HS748(RRDDart)

HS.748Series2

HS748Series2A

HS748Series2B

Boeing

B737-200

Boeing737-200(PWJT8D)

B737-400, B737-300/500

Boeing737-300/400/500(CFM56)

B737-700

Boeing737-700/800/900(CFM56)

B737-800

B737-900

B737-900ER

B747-400

Boeing747-400(PW4000)B747-400F/SF(BCF)

B747-400 Boeing747-400(GECF6)B747-400F/SF(BCF)

B757-200

Boeing757-200/300(PW2000)B757-200PF

B757-300

B757-200

Boeing757-200(RRRB211)

B777-200

Boeing777-200/300(GE90)

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Group -1 Aeroplanes



B777-200LR

B777-300ER

B777-200

Boeing777-200/300(PW4000)

B777-300

B787-8 DreamlinerBoeing 787-8 (GE GEnx)

B787-8 DreamlinerBoeing 787-8 (RR RB 211 Trent 1000)

BOMBARDIER

BD-100-1A10 Challenger300Bombardier BD-100-1A10 (Honey-wellAS907)

BD-700-1A10GlobalExpressGlobal6000

BombardierBD-700Series(RRDBR710)BD-700-1A11

Global5000Global5000GVFD

CL-600-2B16 (CL 604Variant)

Challenger-604(MSN<5701)

BombardierCL-600-2B16(variantCL604)(GECF34}

CL-600-2B16 (CL 604Variant)

Challenger-605(MSN>5701)

CL-600-2B19 Regional Jet Series100/200

BombardierCL-600-2B19(GECF34)

CRJ200BombardierCRJ200(GECF34)

CL-600-2C10Regional Jet Series700/701/702 Bombardier CL-600-2C10/-2D15/-

2D24/-2E25(GECF34)

CL-600-2D15Regional Jet Series705

DHC-8-401DHC-8-402

DHC-8 Series 400 Bombardier DHC-8-400 (PWC PW150)

CESSNA AIR-CRAFTCompany

525Citation Jet CJ1

Cessna 525/525A (Williams FJ 44)

525A

Citation Jet CJ2

525B CitationJetCJ3 CessnaC(WilliamsFJ44)

525C CitationJetCJ4 CessnaC(WilliamsFJ44)

550 CitationBravo

Cessna550/560(PWCPW530/535)560 CitationEncore

560 CitationEncore+

550 CitationII Cessna550/560(PWCJT15D)

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Group -1 Aeroplanes



S550 CitationS/II

560 CitationV

560 CitationUltra

560XL CitationExcel

Cessna560XL/XLS(PWCPW545)

560XLS CitationXLS

650 CitationIII–VIIV

Cessna650(HoneywellTFE731)

650 CitationVII

Cessna

680SovereignSovereign+

Cessna680(PWCPW306)

750 CitationX Cessna750(RRCorpAE3007C)

DassaultAviation

Falcon900EX Falcon900EX(HoneywellTFE731)

Falcon900EX F900EXEASy

Falcon 900EX EASy (HoneywellTFE731)

Falcon900EX F900DX

Falcon900EX F900LX

Falcon2000 Falcon2000(CFE738)

Falcon2000EX Falcon2000EX(PWCPW308)

Falcon2000EX F2000EXEASy

Falcon2000EXEASy(PWCPW308)

Falcon2000EX F2000DX

Falcon2000EX F2000LX

Falcon7X

Falcon7X(PWCPW307A)

RUAG AerospaceGmbH (DORN-IER)

228-200series Dornier228(HoneywellTPE331)

EMBRAER

EMB-500 Phenon-100 EmbraerEMB-500(PWCPW617)

EMB-135BJEMB145

Legacy600Legacy650

Embraer EMB-135/145 (RR CorpAE3007A)

ERJ170-100LRERJ170-200LR

ERJ-170ERJ-175

EmbraerERJ-170Series(GECF34)

ERJ190-100/200ERJ-190ERJ-195

EmbraerERJ-190Series(GECF34)

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Group -1 Aeroplanes



FOKKER SER-VICES

F27Mark100 Friendship

FokkerF27/FairchildF-27/FH-227(RRDDart)





GULFSTREAM

AEROSPACELP

(GALP)c/oIsrael

Aircraft

Industries

Gulfstream200/Galaxy Galaxy200Gulfstream (IAI) 200/Galaxy (PWCPW306)

GulfstreamG150

GulfstreamG150

Gulfstream(IAI)G150(HoneywellTFE731

GIVGIV/SP

GulfstreamGIV/GIV/SP

GulfstreamGIVSeries(RRDTay)

GV-SP(G500)GV-SP(G550)

GulfstreamG500GulfstreamG550

GulfstreamGVSPSeries(RRD–BR710)

G100GulfstreamG100 GulfstreamG100(HoneywellTFE

731)

HAWKERBEECHCRAFTCorporation

HS.125series700 "HawkerSiddeley"BAe 125 Series 700 (HoneywellTFE731)

Hawker750 Hawker750

BAe 125 Series750/800XP/850XP/900XP (Honey-wellTFE731)

Hawker800XP Hawker800XP



300 SuperKingAir

Beech300Series(PWCPT6)

300LW SuperKingAir

B300 SuperKingAir350

B300C SuperKingAir350C

400 BeechjetBeech 400 / Mitsubishi MU-300(PWCJT15)

400ABeechjet (Hawker400XP)

1900 Airliner Beech1900(PWCPT6)

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Group -1 Aeroplanes



1900C Airliner

1900D Airliner

4000 Hawker4000 Hawker4000(PWCPW308)

LearJet

Learjet45 LJ45Learjet Model 45 (HoneywellTFE731)

Learjet40 LJ45

Learjet60 LJ60

LJ60XR

Learjet60(PWCPW305)

BEECHCRAFTCorporationBEECHCRAFT

Corporation

65-90

KingAir

Beech90Series(PWCPT6)

C90

C90A

C90GT

C90GTi

B200/B200C

Beech200Series(PWCPT6)B200CT

B200GT

B200T

390 Premier1,1A Beech390(WilliamsFJ44)

99/99A/100 KingAir Beech99/100Series(PWCPT6)

PIAGGIOAeroIn-dustries

P180 Avanti PiaggioP180Avanti/AvantiII(PWCPT6)

P180 AvantiII

PILATUS AIR-CRAFT

PC-12 PilatusPC-12(PWCPT6)

ASIAviation

F406 Caravan2 Reims-CessnaF406(PWCPT6)

VIKING AIR(Bombardier)(DeHavilland)

DHC-6-1 TwinOtter

DeHavillandDHC-6(PWCPT6)

DHC-6-100/110

DHC-6-200/210

DHC-6-300/310/320

DHC-6-400

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Group 1 Helicopter

1 TC Holder 2 Aeroplanes Model Commercial Designation

3 Type rating endorsement

AGUSTAWestland A109E

Agusta A109 Series (PWCPW206/207)

A109S

AW109SP

AW/109N

A109

Agusta A109 Series (RR Corp250)

A109A

109C

AW139 AgustaAW139(PWCPT6)

BELL HELICOPTER TEX-TRON

212

Bell212/AgustaAB212(PWCPT6)

412 Bell412/AgustaAB412(PWCPT6)

412EP

412CF

BELL HELICOPTER CAN-ADA

427 Bell427(PWCPW207D)

222 Bell222(HoneywellLTS101)

222B

222U

230 230 Execu-tive

Bell230(RRCorp250)

230Utility

230EMS

429 Bell429(PWCPW207D)

430 Bell430(RRCorp250)

AIRBUSHELICOPTERS

AS355E Eurocopter AS 355 (RR Corp250)AS355F

AS355F1

AS355F2

AS355N EurocopterAS355(TurbomecaArrius1)

AS355NP

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Group 1 Helicopter

1 TC Holder 2 Aeroplanes Model Commercial Designation


AIRBUSHELICOPTERS

SA365N Dauphin Eurocopter SA 365 N (Tur-bomecaArriel1)

SA365N1 Dauphin Eurocopter SA 365 N1, AS 365N2(TurbomecaArriel1)

AS365N2

AS365N3 Dauphin Eurocopter AS 365 N3 (Tur-bomecaArriel2C)

EC155B EurocopterEC155(TurbomecaArriel2)

EC155B1

EUROCOPTERDeutschlandGMBH

EC135P1Series EurocopterEC135(PWC206)

EC135P2Series

EC135P3Series

EC135T1

EurocopterEC135(TurbomecaArrius2B)

EC135T2

EC135T3

MBB-BK117C2 EC145 Eurocopter MBB-BK 117 C2(TurbomecaArriel1)

MBB-BK117D2 EC145T2 Eurocopter MBB-BK 117 D2(TurbomecaArriel2)

HINDUSTAN AERO-NAUTICSLtd.

DHRUV DHRUV (Turbomeca TM 333-2B2)

MDHELICOPTERS,INC. MD900 MD Helicopters MD900 (PWCPW206/207)

MOSCOWHELICOPTERSPLANT

MI172

M1 172 - Klimo TV/TB-3-117VM/BM

SIKORSKYAIRCRAFT

S-76C S-76C+ Sikorsky S-76C(Turbomeca Ar-riel2)S-76C S-76C++

S-76C

Sikorsky S-76C(Turbomeca Ar-riel1)

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SUBGROUP 2a: SINGLE TURBO-PROPELLER ENGINE AEROPLANES (Other than those in Group 1)

TC holder Type rating endorsement

CESSNAAIRCRAFTCompany Cessna208Series(PWCPT6)

PILATUSAIRCRAFT

PilatusPC-6Series(PWCPT6)

PilatusPC-6Series(TurbomecaAstazou)

PilatusPC-6Series(HoneywellTPE331)

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SUBGROUP 2b: SINGLE TURBINE ENGINE HELICOPTERS (Other than those in Group 1)

1 TC Holder 2 Helicopter Model Commercial Designation


AGUSTA A119AW119MKII

Koala Agusta A119/Agusta AW119MKII(PWCPT6)

BELLHELICOPTERCANADA 407 Bell407(RRCorp250)

AGUSTA

AB206A

AgustaAB206/Bell206(RRCorp250)

AB206B

BELL HELICOPTER TEX-TRONCANADALIMITED

206seriesfromAtoL

THE ENSTROM HELICOP-TERCORPORATION

480 Enstrom480(RRCorp250)

480B

AIRBUS HELICOP-TERS

AS350 Ecureuil EurocopterAS350(TurbomecaArriel1)

AS350B1

AS350B2

AS350BA

AS350BB

AS350B3 EurocopterAS350(TurbomecaArriel2)

AS350D Eurocopter AS 350 (HoneywellLTS101)

EC120B Colibri EurocopterEC120(TurbomecaArrius2F)

EC130B4EC130T2

EurocopterEC130(TurbomecaArriel2)

SA315B Lama Eurocopter SA 315B (Tur-bomecaArtouste)

SA316BAlouetteIII

EurocopterSA316B(Tur-bomecaArtouste)

MDHELICOPTERSINC.(MDHI)

500N

MDHelicopters500NN/

AMD500N(RRCorp250)

MD600N

ROBINSONHELICOPTER R66 RobinsonR66(RRCorps250)

SCHEIZERAIRCRAFTCORP 269D Scgeizer269D(RRCorp250)

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SUBGROUP 2C: SINGLE PISTON ENGINE HELICOPTERS (Other than those in Group 1)

1 TC Holder 2 Helicopter Model Commercial Designation


THE ENSTROM HELICOP-TERCORPORATION

F-28series

EnstromF-28(Lycoming)

SEI(BREDA-NARDI) NH300C Model300C Schweizer / Breda Nardi(Hughes)269/300(Lycoming)

SCHWEIZERAIRCRAFTCORPORATION

269A

269B

269C

ROBINSONHELICOPTERCOMPANY

R22R44

RobinsonR22/R44Series(Ly-coming)

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GROUP – 3 PISTON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of struc-ture

Maximum Take off Mass

2 T and Be-low

Above 2 T

AEROSTARAIRCRAFTCorporation

PiperPA-60/61Series(Ly-coming)

Metal X

AmericanChampion Champion8Series(Ly-coming)

Wood+Metaltubingfabrics

X

CESSNA AIRCRAFT Com-pany/REIMSAVIATION

Cessna310/320Series(Conti-nental)

Metal X

Cessna336(Continental) Metal X

Cessna421(Continental) Composite X

CessnaT303(Continental) Metal X

Beech55Series(Continental) Metal X

Beech58Series(Continental) Metal X

Beech58P(Continental) Metal+Pres-surised

X

Beech65-80Series(Ly-coming)

Metal X

Beech76(Lycoming) Metal X

Beech95Series(Lycoming) Metal X

PiperAircraft

PiperPA-30Series(Ly-coming)

Composite

X


Composite

X

PiperPA-31P(Lycoming) Metal+Pres-surised

X


Metal X

PiperPA-34Series(Continen-tal)

Metal X

VULCANAIR VulcanairP.68Series(Ly-coming)

Metal X

CessnaAircraftCompany

Cessna/Reims-Cessna150/F150Series(Continen-tal)

Metal X

Cessna/Reims-Cessna152/F152Series(Lycoming)

Metal X


Metal X


Metal X

Cessna172Series(Thielert) Metal X

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GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of struc-ture


2 T and Be-low

Above 2 T

Cessna175Series(Conti-nental)

Metal X

Cessna177Series(Ly-coming)

Metal X


Metal X


Metal X


Metal X

Cessna/Reims-Cessna182/F182Series(SMA)

Metal X


Metal X


Metal X

Cessna206Series(Ly-coming)

Metal X

HAWKERBEECHCRAFTCorporation

Beech35Series(Continen-tal)

Metal X

Beech36Series(Continen-tal)

Metal X

LAVIAArgentinaS.A(La-viasa)


Metal X

PILATUSAIRCRAFT PilatusPC-6Series(Ly-coming)

Metal X

PIPERAIRCRAFT PiperPA-23Aztec(Ly-coming)

Metal X


Metal X


Metal X

PiperPA-28Series(Conti-nental)

Metal X

PiperPA-28Series(Thielert) Metal X


Metal X


Metal X

PiperPA-36Series(Conti-nental)

Metal X

SKYInt AviatHuskyA(Lycoming) Metal

X

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GROUP – 3 PITON ENGINE AEROPLANE ( Other than in Group – 1 )

TC holder Type rating endorsement Type of structure


2 T and Be-low

Above 2 T

DIAMONDAIRCRAFTIndus-tries

DiamondDA42Series(Thielert) Composite

X

DiamondDA42Series(AustroEn-gine)

Composite

X

CIRRUSDesignCorporation CirrusSR20(Continental) Composite

X

Cirrus SR22 Series (Continen-tal)

DIAMOND AIRCRAFT In-dustries

DiamondDA40(Lycoming) Composite

X

DiamondDA40D(Thielert) Composite

X

Diamond DA40 (Austro En-gine)

Composite

X

NATIONAL AEROSPACELABORATORIES

Hansa3(Rotax) Composite

X

ZlinAircraft(MoravanAvi-ation

ZlinZ-242L(Lycoming) Metal x

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AppendixIItoAMCtoCAR-66

Aircraft type practical experience and On-the-Job Training

list of tasks

I Time limits/Maintenance checks (

ATA 05 ) a. 100hourcheck(generalaviation

aircraft). b. BorCCheck(transport

categoryaircraft) c. Assistcarryingoutascheduled

maintenancechecki.a.w.AMMd. Reviewaircraftmaintenancelog

forcorrectcompletione. Reviewrecordsforcompliancewith

airworthinessdirectives. f. Reviewrecordsforcompliancewith

componentlifelimits.g. ProcedureforInspectionfollowing

heavylanding.h. ProcedureforInspectionfollowing

lightningstrike.II Dimensions/Areas(ATA 06)

a. Locatecomponent(s)bystationnumber.

b. Performsymmetrycheck.

III Lifting and Shoring(ATA 07) Assistin:

a. Jackaircraftnoseortailwheel.b. Jackcompleteaircraft.c. Slingortrestlemajorcomponent.

IV Leveling /Weighing(ATA 08) a. Levelaircraft.b. Weighaircraft.c. Prepareweightandbalanceamend-

ment.d. Checkaircraftagainstequipment

list.V Towing and Taxiing( ATA 09 )

a. Prepareforaircrafttowingb. Towaircraftc. Bepartofaircrafttowingteam.

VI Parking and mooring(ATA 10) a. Tiedownaircraft.b. Park,secureandcoveraircraft.c. Positionaircraftindock. d. Securerotorblades.

VII Placards and Marking ( ATA11) a. Checkaircraftforcorrectplacards.b. Checkaircraftforcorrectmarkings.

VII Servicing ( ATA 12 ) a. Refuelaircraft.b. Defuelaircraftc. Carryouttanktotankfueltransferd. Check/adjusttirepressures.e. Check/replenishoillevel.f. Check/replenishhydraulicfluid

level.g. Check/replenishaccumulatorpres-

sure.h. Chargepneumaticsystem.i. Greaseaircraft.j. Connectgroundpower.k. Servicetoilet/watersysteml. Performpre-flight/dailycheck

IX Vibration and Noise Analysis ( ATA 18 )

a. Analyzehelicoptervibrationprob-lem.

b. Analyzenoisespectrum. c. Analyseenginevibration.

X Air Conditioning ( ATA 21 )

a. Replacecombustionheater. b. Replaceflowcontrolvalve.c. Replaceoutflowvalve.d. Replacesafetyvalve.e. Replacevapourcycleunit.f. Replaceaircycleunit.g. Replacecabinblower.h. Replaceheatexchanger.i. Replacepressurizationcontroller.j. Cleanoutflowvalves.k. Deactivate/reactivatecargoisola-

tionvalve.l. Deactivate/reactivateavionicsventi-

lationcomponentsm. Checkoperationofair

conditioning/heatingsystemn. Checkoperationofpressurization

systemo. Troubleshootfaultysystem

XI Auto flight ( ATA 22)

a. Installservos.b. Rigbridlecablesc. Replacecontroller.d. Replaceamplifier.

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e. Replacementoftheautoflightsys-temLRUsincaseoffly-by-wireair-craft

f. Checkoperationofauto-pilot.g. Checkoperationofauto-throttle/

autothrust.h. Checkoperationofyawdamper.i. Checkandadjustservoclutch.j. Performautopilotgainadjustments.k. Performmachtrimfunctionalcheck.l. Troubleshootfaultysystem.m. Checkautolandsystemn. Checkflightmanagementsystemso. Checkstabilityaugmentationsystem

XII Communications ( ATA 23 ) a. ReplaceVHFcomunit.b. ReplaceHFcomunit.c. Replaceexistingantenna.d. Replacestaticdischargewicks.e. Checkoperationofradios.f. PerformantennaVSWRcheck.g. PerformSelcaloperationalcheck.h. Performoperationalcheckofpas-

sengeraddresssystem.i. Functionallycheckaudiointegrating

system.j. Repairco-axialcable.k. Troubleshootfaultysystem

XIII Electrical Power ( ATA 24 )

a. Chargelead/acidbattery.b. ChargeNi-Cdbattery.c. Checkbatterycapacity.

d. Deep-cycleNi-Cdbattery.e. ReplaceIntegrateddrive/genera-

tor/alternator.f. Replaceswitches.

g. Replacecircuitbreakers.h. Adjustvoltageregulator.i. Amendelectricalloadanalysisre-

port.j. Repair/replaceelectricalfeederca-

ble.k. PerformfunctionalcheckofIDG/

Generator/Alternatorl. Performfunctionalcheckofvoltage

regulator.m. Performfunctionalcheckofemer-

gencygenerationsystem.n. Troubleshootfaultysystem

XIV Equipment/Furnishings (ATA 25 )

a. Replacecarpetsb. Replacecrewseats.c. Replacepassengerseats.

d. Checkinertiareels.e. Checkseats/beltsforsecurity.f. Checkemergencyequipment.g. CheckELTforcompliancewithregu-

lations.h. Repairtoiletwastecontainer.i. Repairupholstery.j. Changecabinconfiguration.

k. Replaceescapeslides/ropes

l. Replacecargoloadingsystemactua-tor.

m. Testcargoloadingsystem.XV Fire protection ( ATA 26)

a. Checkfirebottlecontents.

b. Check/testoperationoffire/smokedetectionandwarningsys-tem.

c. Checkcabinfireextinguishercon-tents.

d. Checklavatorysmokedetectorsys-tem.

e. Checkcargopanelsealing.f. Installnewfirebottle.g. Replacefirebottlesquib.h. Troubleshootfaultysystem.i. Inspectenginefirewiredetection

systems.XVI Flight Controls ( ATA 27 )

a. Inspectprimaryflightcontrolsandrelatedcomponentsi.a.w.AMM.

b. Extending/retractingflaps&slats.c. Replacehorizontalstabilizer.d. Replacespoiler/liftdamper.e. Replaceelevator.f. Deactivation/reactivationofaileron

servocontrol.g. Replaceaileron.h. Replacerudder.i. Replacetrimtabs.j. Installcontrolcableandfittings.k. Replaceslats.l. Replaceflaps.m. Replacepoweredflyingcontrolunit.n. Replaceflapactuatoro. Adjusttrimtab.p. Adjustcontrolcabletension.q. Checkcontrolrangeanddirectionof

movement.r. Checkforcorrectassemblyandlock-

ing.s. Troubleshootfaultysystem.t. Functionaltestofprimaryflightcon-

trols.u. Functionaltestofflapsystem.

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v. Operationaltestofthesidestickas-sembly.

w. OperationaltestoftheTHS.

x. THSsystemwearcheck.

XVII Fuel ( ATA 28 )

a. Waterdrainsystem(operation).

b. Replaceboosterpump.

c. Replacefuelselector.

d. Replacefueltankcells.

e. Replace/testfuelcontrolvalves.

f. Replacemagneticfuellevelindica-tors.

g. Replacewaterdrainvalve.h. Checkfilters.i. Flowchecksystem.

j. Checkcalibrationoffuelquantitygauges.

k. Checkoperationfeed/selectorsl. Checkoperationoffueldump/jetti-

sonsystem.m. Fueltransferbetweentanks.n. Pressuredefuel.Pressurerefuel

(manualcontrol).o. Troubleshootfaultysystem.

XVIII Hydraulics ( ATA 29 ) a. Replaceenginedrivenpump.b. Check/replacecasedrainfilter.c. Replacehydraulicmotorpump/gen-

erator.d. Replacestandbypump.e. Replaceaccumulator.f. Checkoperationofshutoffvalve.g. Checkfilters/Clogindicators.h. Checkindicatingsystems.i. Performfunctionalchecks.j. Pressurisation/depressurisationof

thehydraulicsystem.k. PowerTransferUnit(PTU)opera-

tionl. ReplacementofPTU.m. Troubleshootfaultysystem.

XIX Ice and rain protection ( ATA 30 ) a. Replacepump.b. Replacetimer.c. Inspectrepairpropellerdeiceboot.d. Testpropellerde-icingsystem.e. Inspect/testwingleadingedgede-

icerboot.f. Replaceanti-ice/deicevalve.g. Installwipermotor.h. Checkoperationofsystems.

i. Operationaltestofthepitot-probeiceprotection.

j. OperationaltestoftheTATicepro-tection.

k. Operationaltestofthewingicepro-tectionsystem.

l. Assistancetotheoperationaltestoftheengineair-intakeiceprotection(withenginesoperating)

m. Troubleshootfaultysystem.

XX Indicating/recording systems (ATA 31 )

a. Replaceflightdatarecorder.b. Replacecockpitvoicerecorder.c. Replaceclock.d. Replacemastercautionunit.e. ReplaceFDR.f. PerformFDRdataretrieval.g. Troubleshootfaultysystem.h. ImplementESDSprocedures

i. InspectforHIRFrequirementsj. Start/stopEISprocedure.k. BitetestoftheCFDIU.l. Groundscanningofthecentral

warningsystem.XXI Landing Gear ( ATA 32 )

a. Buildupwheel.b. Replacemainwheel.c. Replacenosewheel.d. Replacesteeringactuator.e. Replacetrucktiltactuator.

f. Replacegearretractionactuator.g. Replaceuplock/downlockassembly.h. Replaceshimmydamper.i. Rignosewheelsteering.j. Replaceshockstrutseals.k. Servicingofshockstrut.l. Replacebrakeunit.m. Replacebrakecontrolvalve.n. Bleedbrakes.o. Replacebrakefan.p. Testanti-skidunit.q. Testgearretraction.r. Changebungees.s. Adjustmicroswitches/sensors.t. Chargestrutswithoilandair.u. Troubleshootfaultysystem.v. Testauto-brakesystem.w. Replacerotorcraftskids.x. Replacerotorcraftskidshoes.

y. Packandcheckfloats.z. Flotationequipment.aa. Check/testemergencyblowdown

(emergencylandinggearextension).

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bb. Operationaltestofthelandinggeardoors.

XXII Lights ( ATA 33 )

a. Repair/replacerotatingbeacon.b. Repair/replacelandinglights.c. Repair/replacenavigationlights.d. Repair/replaceinteriorlights.e. Replaceiceinspectionlights.

f. Repair/replacelogolights.g. Repair/replaceemergencylighting

system.h. Performemergencylightingsystem

checks.i. Troubleshootfaultysystem

XXIII Navigation ( ATA 34 )

a. Calibratemagneticdirectionindica-tor.

b. Replaceairspeedindicator.c. Replacealtimeter.d. Replaceairdatacomputer.e. ReplaceVORunit.f. ReplaceADI.g. ReplaceHSI.h. Checkpitotstaticsystemforleaks.i. Checkoperationofdirectionalgyro.j. Functionalcheckweatherradar.k. FunctionalcheckDoppler.

l. FunctionalcheckTCAS.m. FunctionalcheckDME.n. FunctionalcheckATCTransponder.o. Functionalcheckflightdirectorsys-

tem.p. Functionalcheckinertialnavsys-

tem.q. Completequadrantalerrorcorrec-

tionofADFsystem.r. Updateflightmanagementsystem

database.s. Checkcalibrationofpitotstaticin-

struments.

t. Checkcalibrationofpressurealti-tudereportingsystem.

u. Troubleshootfaultysystem.v. Checkmarkersystems.w. Compassreplacementdirect/indi-

rect.x. CheckSatcom.y. CheckGPS.z. TestAVM.

XXIV Oxygen ( ATA 35 )

a. Inspectonboardoxygenequipment.b. Purgeandrechargeoxygensystem.c. Replaceregulator.

d. Replaceoxygengenerator.e. Testcrewoxygensystem.f. Performautooxygensystemdeploy-

mentcheck.

g. Troubleshootfaultysystem.

XXV Pneumatic systems ( ATA 36 )

a. Replacefilter.

b. Replaceairshutoffvalve.

c. Replacepressureregulatingvalve.

d. Replacecompressor.

e. Rechargedessicators.

f. Adjustregulator.

g. Checkforleaks.

h. Troubleshootfaultysystem.XXVI Vacuum systems ( ATA 37 )

a. Inspectthevacuumsystemi.a.w.AMM.

b. Replacevacuumpump.

c. Check/replacefilters.

d. Adjustregulator.e. Troubleshootfaultysystem.

XXVII Water/Waste ( ATA 38 )

a. Replacewaterpump.

b. Replacetap.

c. Replacetoiletpump.

d. Performwaterheaterfunctionalcheck.

e. Troubleshootfaultysystem.

f. Inspectwastebinflapclosure.

XXVIII Central Maintenance System ( ATA45 )

a. RetrievedatafromCMU.

b. ReplaceCMU.

c. PerformBitecheck.

d. Troubleshootfaultysystem.

XXIX Airborne Auxiliary power (ATA 49)

a. Removal/InstallationofAPU.

b. Removal/installationoftheinletguide-vaneactuator.

c. OperationaltestoftheAPUemergencyshut-downtest.

d. OperationaltestofAPU.

XXX Structures ( ATA 51 )

a. Assessmentofdamage.

b. Sheetmetalrepair.

c. Fibreglassrepair.

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d. Woodenrepair.

XXXI Fabric repair ( ATA 51 )

a. Recoverfabriccontrolsurface.

b. Treatcorrosion.

c. Applyprotectivetreatment.

XXXI Doors (ATA 52 )

a. Inspectpassengerdoori.a.w.AMM.b. Rig/adjustlockingmechanism.c. Adjustairstairsystem.d. Checkoperationofemergencyexits.e. Testdoorwarningsystem.f. Troubleshootfaultysystem.g. Removeandinstallpassengerdoor

i.a.w.AMM.h. Removeandinstallemergencyexit

i.a.w.AMM.i. Inspectcargodoori.a.w.AMM.

XXXII Windows ( ATA 56 )

a. Replacewindshield.b. Replacedirectvisionwindow.c. Replacecabinwindowd. Repairtransparency.

XXXIII Wings (ATA 57 )

e. Skinrepair.f. Recoverfabricwing.g. Replacetip.h. Replacerib.i. Replaceintegralfueltankpanel.j. Checkincidence/rig.

XXXIV Propeller (ATA 61 )

a. Assemblepropaftertransportation.b. Replacepropeller.c. Replacegovernor.d. Adjustgovernor.e. Performstaticfunctionalchecks.f. Checkoperationduringgroundrun.g. Checktrack.h. Checksettingofmicroswitches.i. Dressoutbladedamage.j. Dynamicallybalanceprop.k. Troubleshootfaultysystem.

XXXV Main Rotors ( ATA 62 )

a. Replaceblades.b. Replacedamperassembly.c. Checktrack.d. Checkstaticbalance.e. Checkdynamicbalance.f. Troubleshoot.

XXXVI Rotor Drive (ATA 63 )

a. Replacemast.

b. Replacedrivecoupling.

c. Replaceclutch/freewheelunit

d. Replacedrivebelt.

e. Installmaingearbox.

f. Overhaulmaingearbox.

g. Checkgearboxchipdetectors.

XXXVII Tail Rotors (ATA 64 )

a. Installrotorassembly.

b. Replaceblades.

c. Troubleshoot.

XXXVIII Tail Rotor Drive ( ATA 65 )

a. Replacebevelgearbox.b. Replaceuniversaljoints.c. Overhaulbevelgearbox.d. Installdriveassembly.e. Checkchipdetectors.f. Check/installbearingsandhangers.g. Check/service/assembleflexible

couplings.h. Checkalignmentofdriveshafts.i. Installandrigdriveshafts.

XXXIX Rotorcraft flight controls (ATA 67 )

a. Installswashplate.b. Installmixingbox.c. Adjustpitchlinks.d. Rigcollectivesystem.e. Rigcyclicsystem.f. Riganti-torquesystem.g. Checkcontrolsforassemblyand

locking.h. Checkcontrolsforoperationand

sense.i. Troubleshootfaultysystem.

XL Power Plant ( ATA 71 ) a. BuildupECU.b. Replaceengine.c. Repaircoolingbaffles.d. Repaircowling.e. Adjustcowlflaps.f. Repairfaultywiring.g. Troubleshoot.h. Assistindrymotoringcheck.i. Assistinwetmotoringcheck.j. Assistinenginestart(manual

mode).XLI Piston Engines(ATA 72 )

a. Remove/installreductiongear.b. Checkcrankshaftrun-out.c. Checktappetclearance.

d. Checkcompression.

e. Extractbrokenstud.

CAR-66

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f. Installhelicoil.

g. Performgroundrun.

h. Establish/checkreferenceRPM.

i. Troubleshoot.

XLII Turbine Engines ( ATA 72 )

a. Replacemodule.b. Replacefanblade.

c. Hotsectioninspection/borescopecheck.

d. Carryoutengine/compressorwash.

e. Carryoutenginedrycycle.

f. Enginegroundrun.

g. Establishreferencepower.

h. Trendmonitoring/gaspathanalysis.

i. Troubleshoot.

XLIII Fuel and control, piston ( ATA 73 )

a. Replaceenginedrivenpump.

b. AdjustAMC.

c. AdjustABC.

d. Installcarburetor/injector.

e. Adjustcarburetor/injector.

f. Cleaninjectornozzles.

g. Replaceprimerline.

h. Checkcarburetorfloatsetting.

XLIV Fuel and control, turbine (ATA 73)

a. ReplaceFCU.

b. Replaceengineelectroniccontrolunit(FADEC).

c. Replacefuelmeteringunit(FADEC).

d. Replaceenginedrivenpump.

e. Clean/testfuelnozzles.

f. Clean/replacefilters.

g. AdjustFCU.

h. Troubleshootfaultysystem.

i. FunctionaltestofFADEC.

XLV Ignition systems, piston (ATA 74)

a. Changemagneto.

b. Changeignitionvibrator.

c. Changeplugs.

d. Testplugs.

e. CheckH.T.leads.

f. Installnewleads.

g. Checktiming.

h. Checksystembonding.

i. Troubleshootfaultysystem.

XLVI Ignition systems, turbine (ATA 74)

a. Performfunctionaltestoftheigni-tionsystem.

b. Checkglowplugs/ignitors.

c. CheckH.T.leads.

d. Checkignitionunit.

e. Replaceignitionunit.

f. Troubleshootfaultysystem.

XLVII Engine Controls( ATA 76 )

a. Rigthrustlever.

b. RigRPMcontrol.

c. RigmixtureHPcocklever.

d. Rigpowerlever.

e. Checkcontrolsync(multi-eng).

f. Checkcontrolsforcorrectassemblyandlocking.

g. Checkcontrolsforrangeanddirec-tionofmovement.

h. Adjustpedestalmicro-switches.


XLVIII Engine Indicating ( ATA 77 )

a. Replaceengineinstruments(s).

b. Replaceoiltemperaturebulb.

c. Replacethermocouples.

d. Checkcalibration.


XLIX Exhaust, piston ( ATA 78 )

a. Replaceexhaustgasket.

b. Inspectweldedrepair.

c. Pressurecheckcabinheatermuff.

d. Troubleshootfaultysystem.

L Exhaust, turbine ( ATA 78 )

a. Changejetpipe.

b. Changeshroudassembly.

c. Installtrimmers.

d. Inspect/replacethrustreverser.

e. Replacethrustreversercomponent.

f. Deactivate/reactivatethrustre-verser.

g. Operationaltestofthethrustre-versersystem.

LI Oil ( ATA 79 )

a. Changeoil.

b. Checkfilter(s).

c. Adjustpressurereliefvalve.

d. Replaceoiltank.

e. Replaceoilpump.

f. Replaceoilcooler.

CAR-66

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g. Replacefirewallshutoffvalve.

h. Performoildilution.


LII

Starting ( ATA 80 )

a. Replacestarter.

b. Replacestartrelay.

c. Replacestartcontrolvalve.

d. Checkcrankingspeed.


LIII Turbines, piston engines ( 70 )

a. ReplacePRT.

b. Replaceturbo-blower.

c. Replaceheatshields.

d. Replacewastegate.

e. Adjustdensitycontroller.

LIV Engine water injection ( ATA 82 )

a. Replacewater/methanolpump.

b. Flowcheckwater/methanolsystem.

c. Adjustwater/methanolcontrolunit.

d. Checkfluidforquality.

e. Troubleshootfaultysystem

LV Accessory gear boxes ( ATA 83)

a. Replacegearbox.

b. Replacedriveshaft.

c. CheckChipdetector

CAR 66

159 Issue II R 2 4th September 2017

APPENDIX III to AMC of CAR-66

Evaluation of the competence: assessment and assessors

ThisAppendixappliestothecompetenceassessmentperformedbythedesignatedas-sessors(andtheirqualifications).

1) What does “competence” mean and areas of focus for assessment

Theassessmentshouldaimatmeasuringthecompetencebyevaluatingthreemajorfac-torsassociatedtothelearningobjectives: Knowledge; Skills; Attitude.

Generally,knowledgeisevaluatedbyexamination.Thepurposeofthisdocumentisnotto describe the examination process: this material mainly addresses the evaluation of“skills” and “attitude” after training containing practical elements. Nevertheless, thetraineeneedstodemonstratesufficientknowledgetoperformtherequiredtasks.“Attitude”isindivisiblefromthe“skill”asthisgreatlycontributestothesafeperfor-manceofthetasks.Theevaluationofthecompetenceshouldbebasedonthelearningobjectivesofthetraining,inparticular: the(observable)desiredperformance.Thiscoverswhatthetraineeisexpectedtobe

abletodoandhowthetraineeisexpectedtobehaveattheendofthetraining; the(measurable)performancestandardthatmustbeattainedtoconfirmthe

trainee’slevelofcompetenceintheformoftolerances,constraints,limits,perfor-manceratesorqualitativestatements;and

theconditionsunderwhichthetraineewilldemonstratecompetence.Conditions

consistofthetrainingmethods,theenvironmental,situationalandregulatoryfac-tors.

Theassessmentshouldfocusonthecompetenciesrelevanttotheaircrafttypeanditsmaintenanceincluding,butnotlimitedto: Environmentalawareness(actsafely,applysafetyprecautionsandpreventdanger-

oussituations);

Systemsintegration(demonstrateunderstandingofaircraftsystemsinteraction,identify,describe,explain,plan,execute);

CAR 66


Knowledgeandunderstandingofareasrequiringspecialemphasisornovelty(areaspeculiartotheaircrafttype,domainsnotcoveredbyCAR66AppendixI,practicaltrainingelementsthatcannotbeimpartedthroughsimulationdevices,etc.);

Usingreportsandindications(theabilitytoreadandinterpret); Aircraftdocumentationfindingandhandling(identifytheappropriateaircraft documentation,navigate,executeandobeytheprescribedmaintenanceprocedures); Performmaintenanceactions(demonstratesafehandlingofaircraft,engines, componentsandtools); Aircraftfinal/close-upandreport(applycloseup,initiateappropriateactions/fol-

low-up/recordsoftesting,establishandsignmaintenancereords/logbooks).2) How to assess

Asfarasfeasible,theobjectivesoftheassessmentshouldbeassociatedwiththelearningobjectivesandthepassinglevel;itmeansthatobservablecriteriashouldbesettomeas-uretheperformanceandshouldremainasobjectiveaspossible.The general characteristics of effective assessment are: objective, flexible, acceptable,comprehensive, constructive, organized and thoughtful. At the conclusion, the traineeshould have no doubt about what he/she did well, what he/she did poorly and howhe/shecanimprove.Thefollowingisanon-exhaustivelistofquestionsthatmaybeposedtoassisttheas-sessment:

Whatarethesuccessfactorsforthejob? Whataretypicalcharacteristicsofacorrectbehaviorforthetask? Whatcriteriashouldbeobserved? Whatlevelofexpertiseisexpected? Isthereanystandardavailable? Whatisthepassmark?Forexample:

o“Go-nogo”situation;oHowtoallocatepoints?Minimumamounttosucceed;o“Mustknoworexecute”versus“Goodtoknoworexecute”versus“Don’texpectthecandidatetobeanexpert”.

Minimumormaximumtimetoachieve?Usetimeeffectivelyandefficiently. Whatifthetraineefails?Howmanytimesisthetraineeallowedtofail? Whenandhowshouldthetraineebepreparedfortheassessment? Whatproportionofjudgmentbytheinstructoroutofcollaborationwiththetrainee

isneededduringtheevaluationstage?

Theassessmentmaybe: diagnostic(priortoacourse),formative(reorientatethecourseonareaswherethere

isaneedtoreinforce)orsummative(partialorfinalevaluation);

CAR 66


performedtask-by-task,asagroupoftasksorasafinalassessment.Onemethodmightbeaninitialassessmenttobeperformedbythetraineehimself/her-self,thendiscussingareaswheretheperceptionsofthetrainee’sperformancebytheas-sessorsdifferinorderto: developtheself-assessmenthabits; maketheassessmentmoreacceptableandunderstandabletobothparties.A “box-ticking” exercise would be pointless. Experience has shown that assessmentsheetshave largelyevolvedover time intoassessmentofgroupsof “skills”because inpracticesuchthingseventuallydetractedfromthetrainingandassessmentthatitwasintendedtoserve:evaluateatapointoftime,encourageandorientatethetrainingneeds,improvesafetyandultimatelyqualifypeoplefortheirduties.Inaddition,manyotheraspectsshouldbeappropriatelyconsideredduringtheassess-mentprocesssuchasstressandenvironmentalconditions,difficultyofthetest,historyofevaluation(suchastangibleprogressesorsuddenandunexpectedpoorperformancemadebythetrainee),amountoftimenecessarytobuildcompetence,etc. Allthesereasonsplacemoreemphasisontheassessorandhighlightthefunctionoftheorganisation’sapproval. 3) Who should assess Inordertoqualify,theassessorshould: Beproficientandhavesufficientexperienceorknowledgein: o humanperformanceandsafetyculture;otheaircrafttype(necessarytohavethecertifyingstaffprivilegesincaseofCRSissuances);otraining/coaching/testingskills;oinstructionaltoolstouse;

Understandtheobjectiveandthecontentofthepracticalelementsofthetraining

thatisbeingassessed;

Haveinterpersonalskillstomanagetheassessmentprocess(professionalism,sincer-ityobjectivityandneutrality,analysisskills,senseofjudgment,flexibility,capabilityofevaluatingthesupervisor’sorinstructor’sreports,handlingoftrainee’sreactionstofailingassessmentwiththeculturalenvironment,beingconstructive,etc.);

Beultimatelydesignatedbytheorganisationtocarryouttheassessment.Therolesmaybecombinedfor: theassessorandtheinstructorforthepracticalelementsoftheTypeRatingTrain-

ing;or

CAR 66


theassessorandthesupervisorfortheOn-the-JobTrainingProvidedthattheobjectivesassociatedwitheachroleareclearlyunderstoodandthatthecompetenceandqualificationcriteriaaccordingtothecompany’sproceduresaremetforbothfunctions.Wheneverpossible(dependingonthesizeoftheorganisation),itisrecommendedtosplittheroles(twodifferentpersons)inordertoavoidanycon-flictsofinterests.Whenthefunctionsarenotcombined,theroleofeachfunctionshouldbeclearlyunder-stood

CAR 66


Appendix IV to AMC of CAR- 66. A. 45(d)

Fuel Tank Safety training

ThisappendixincludesgeneralinstructionsforprovidingtrainingonFuelTankSafety

issues.

1. LeveloftrainingrequiredbythisAnnexisonlylevel2.

Level2Detailedtraining

Objectives:Theattendantshould,afterthecompletionofthetraining:

1. knowthe historyand the theoreticalandpractical elementsof the subject,havean

overviewofSpecialFederalAviationRegulations(SFARs)from14CFRSFAR88ofthe

FAAandofJAATGL47,beabletogiveadetaileddescriptionoftheconceptofCDCCL,

AirworthinessLimitationsItems(ALI)andusingtheoreticalfundamentalsandspecific

examples,

2. havethecapacitytocombineandapplytheseparateelementsofknowledgeinalogical

andcomprehensivemanner.

3. havedetailedinformationonhowtheaboveitemsaffecttheaircraftinthescopeofthe

activityoftheorganisationorinthefleet.

4. understandandcarryoutactivitieswiththeuseofmanufacturerandregulatoryau-

thoritydataprovidinginstructionsondesignandmaintenance,suchasServiceBulle-

tins,AirworthinessDirectives,AircraftMaintenanceManual,ComponentMaintenance

Manualetc.

5. useeasilythemanufacturer’sdocumentationfromvarioussourcesandapplycorrec-

tiveactionwhereappropriate.

6. identifythecomponentsorpartsortheaircraftsubjecttoFTSfromthemanufacturer’s

documentation,plantheactionorapplyaServiceBulletinandanAirworthinessDi-

rective.

Continuingtraining

The interval betweencontinuing trainingshallbe establishedbytheorganisation em-

ployingsuchpersonnel,butshouldnotexceedtwoyears.Thecontinuingtrainingshall

includeknowledgeonevolutionofmaterial,tools,documentationandmanufacturer’sor

DGCAdirectives.

2. ThepersonneldirectlyinvolvedinFuelTankSafety(FTS)systemsshallbequalifiedaccordingtothefollowingtable:

CAR 66


Organisation Personnel Level of

knowledge

Continuing

training

CAR-66licenceholdersina

continuing airworthiness

managementorganisation

Theairworthinessre-

viewstaffasrequired

byM.A.707.

2 Yes

CAR-66 licence holders in

aircraft and component

maintenanceorganisations

Maintenance organi-

sation support and

certifyingstaff

2 Yes

3. Generalrequirements

Thetrainingforthepersonneldesignatedintableabovehastobecarriedoutbeforeany

airworthinessreviewcertificateisissuedoranymaintenancetaskiscertifiedonanair-

craftoracomponent.

Thetrainingshouldbemadeinappropriatefacilitiescontainingexamplesofcomponents,

systems and parts affected by FTS issues and having access to aircraft or component

wheretypicalexamplesofFTSissuescanbeshown.Theuseofpictures,filmsandpracti-

calexamplesofthemaintenanceonfueltanksystemisrecommended.Thetrainingshall

includea representativenumberofrepair and inspections as requiredby the mainte-

nanceprogrammeshowingthenecessityofusingthemanufacturer’sdata.

4. Characteristicsofthetraining

Thefollowingcharacteristicsshallbetakenintoconsiderationwhenthelevel2training

programmearebeingestablished:

(a) understandingofthebackgroundandconceptsoffueltanksafetyasdevelopeddur-

ingthelast10years,and

(b) howinmaintenanceorganisationsmechanicscanrecognize,interpretandhandlethe

improvements that have been made or are being made during fuel tank system

maintenance,

(c) awarenessofanyhazardsworkingontheFuelSystem,andespeciallywithaFlam-

mabilityReductionSystemusingnitrogen.

a),b)andc)shouldbeintroducedinthetrainingprogrammeaddressingthefollowing

issues:

i) Thetheoreticalbackgroundbehindthefueltanksafety:theexplosionsofmixtures

offuelandair,thebehaviorofthosemixturesinanaviationenvironment,theeffects

oftemperatureandpressure,energyneededforignitionetc,the‘firetriangle’,-Ex-

plain2conceptstopreventexplosions:(1)ignitionsourcepreventionand(2)flam-

mabilityreduction,

ii) Themajoraccidentsandaccidentinvestigationsandtheirconclusions,

CAR 66


iii) SFARsfrom14CFRSFAR88oftheFAAandJAAInternalPolicyINTPOL25/12:

reasonofthesedocuments,andwhatwastheultimategoal,marginsoffuelsystem

safetyimprovements(from10-6to10-9,infactimprovementbyafactor100-1000,

to identifyunsafe conditions and to correct them, to systematically improvefuel

tankmaintenance),

iv) Explaintheconceptsthatarebeingused:theresultsofSFAR88oftheFAAandJAA

INT/POL25/12:modifications,airworthinesslimitationsandCDCCL,

v) Whererelevantinformationcanbefoundbythemechanicsandhowtouseandin-

terpretthisinformation(maintenancemanuals,componentmaintenancemanuals)

vi) FuelTankSafetyandMaintenance:fueltankentryandexitprocedures,cleanwork-

ingenvironment,whatismeantbyconfigurationcontrol,wireseparation,bonding

ofcomponentsetc,

vii) Flammabilityreductionsystems:reasonfortheirpresence,theireffects,thehaz-

ards of an FRS using nitrogen for maintenance, safety precautions in mainte-

nance/workingwithanFRS,

viii) Recordingmaintenanceactions,recordingmeasuresandresultsofinspections.

CAR 66


DGCA application forms for licenses and examinations

Form No Description

CA Form 19-01ApplicationForInitialIssueOfCAR-66AircraftMaintenanceEngineer’s

Licence

CA Form 19-02 ApplicationforextensionofCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-03 ApplicationforrenewalofCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-04 Applicationforconversion/removaloflimitationsofCAR-66aircraft

maintenanceengineer’slicence

CA Form 19-05 ApplicationforissueofduplicateCAR-66aircraftmaintenanceengineer’sli-

cence

CA Form 19-06 Medicalcertificate

CA Form 19-07 ApplicationforallotmentofcomputernumberforappearinginAMEli-

cenceexaminations

CA Form 19-08A Applicationforappearinginwrittenpaper(s)ofCAR66basicknowledge

examination

CA Form 19-08B Application for appearing in CAR 66 type examination

CA Form 19-09 ApplicationforappearinginskilltestofCAR-66AMElicence

CA Form 19-10 Formatofaircraftmaintenanceengineerworkrecord/logbook

CA Form 19-11 Applicationforissueofbasicknowledgeexaminationcertificate

CAR 66


Highlights of the CAR 66 Issue II R1

Sl.

No.

CAR66Issue02R1Reference Description

1. 66.A.03LicenceCategories IntheexistingAMElicencecategory,categoryB3isintroducedfor

certifying unpressurised piston engine aircraft below 2000kgs

MTOW

2. 66.A.20Privileges

66.A.20 privileges of AME licence has been replaced with

newoneinlinewithrule61

3. 66.A.30Experiencerequire-

ments

66.A.30AircraftMaintenanceExperiencerequirementsofis-

sueofCategoryA,B1.2andB1.4hasbeenrevisedto3years

from4years.

4. 66.A.45 Endorsement with air-

craftratings

66.A.45(a)(3)endorsementonAMElicenceforaircraftrat-

ings has been revised suitably to include category B3 re-

quirement.

Provision has been made for issue of Category- A licence

withouttyperating.

5. Sub-partB

66.A.100General

Provision for the certification of Microlight, light sport aircraft,

glider,balloonoranairshipsubjecttomeetingtherequirements

asspecifiedintherelevantCAR

6. Sub-partC66.A.200–225General

Requirementsforcertifyingstaffforcertificationofaircraftcom-

ponentsintroduced.

7. GM66.A.20(a)Privileges

DefinitionofTroubleshootinghasbeenamended.

InBasemaintenanceanewparahasbeenaddedtoincludecate-

goryB3.

8. GM 66.A.25(a) Basic knowledge

requirements

ThisparahasbeenamendedtoincludecategoryB3.

9. AMC 66.A.30 (e) Experience re-

quirements


10. GM 66.A.45 Endorsement with

aircraftratings.


11. GM66.A.70Conversionprovi-sions

GM66.A.70hasbeenamendedtoincludecategoryB3.

12. GM66.A.70(d)Conversionprovi-

sions


13. AMC66.A.205(c)Requirements NewAMChasbeenaddedtoexplain“relevantmodulesofCAR66

approvedbytheDGCA”.

14. AMC66.A.205(g)Requirements NewAMChasbeenaddedtoexplainrequirementforthegrantof

certificationauthorization.

15. AppendixI–

BasicKnowledgeRequirements

Appendix–IBasicknowledgerequirementhasbeenrevised

toincludesyllabusforcategoryB3.

CAR 66


Newknowledgelevelhasbeenaddedinmodules3,4,5,6,8,10and

16forB3category.

NewModules7B,9B,11Cand17Bhasbeenaddedtomeetcate-

goryB3knowledgerequirements.

16. AppendixII–

BasicExaminationStandard

QuestionnumberandExaminationdurationhasbeenamendedto

includeB3category.

17. AppendixIV–

Experiencerequirementsforex-

tendingaCAR-66Aircraft

MaintenanceEngineer’sLicence

Experiencerequirements for adding a new category or subcate-

gorytoanexistingCAR-66licencehasbeenamendedtoinclude

CategoryB3

18. AppendixV-

Applicationandforms

AppendixV-Applicationandformatareseparatedfromthe

mainCARandpublishedintheformsectiononDGCAweb-

site.

19. AppendixVI–

AircraftMaintenanceEngineer’s

LicencereferredtoinRule61of

theAircraftRules,1937-CA

Form26

InLicencebook“XII(a).LICENCE(SUB)CATEGORIES”columnhas

beenamendedtoincludeCategoryB3

20. AppendixItoAMCofCAR66Air-

craftTyperatings

List of Aircraft updated to include new aircraft inducted in thecountry.

Highlights of the CAR 66 Issue II R2

Sl.

No.

CAR66Issue02R1Reference Description

1. 66.A.35 Amendedtoreplaceskilltestrequirementwithdemonstra-

tionofskill.

2. 66.A.215(b) AmendedtoincludeAMECourse.

3. Appendix–II(BasicExamina-

tionStandard)para1.5

Amendedtomakeprovisionforappearinginfailedmodule

relatedtolimitationpapersfrom90daysto30days.

4. GM 66.A.35 (Skill Test Re-

quirements)

Deleted.

5. Appendix-I (Appendices to

AMCforCAR66)

AmendedtoaddanoteonTyperatingendorsementcovering

severalmodels/variant.Group1HelicopterTableamended

inlinewithEASAguidelines.

*********