pce-rb0332 - ftav.com€¦ · part no. -n° de piece 9. ... 01 pt6a-34 3020800 various 1 pce-rb0332...

.. ENGINE LOGBOOK PT6A Turboprop

PCE-RB0332

1. Approving national aviation authority Icountry - 2. 3 Form tracking No. - Numero de suiyi du formulaire Autorite de t'aviation du pays d'approbation I pays AUTHORIZED RELEASE CERTIFICATE - BON DE SORTIE AUTORISEE Transport Canada TCCA 24-0078 SEE BLOCK 5

4. Approved organization name and address - Nom et adresse de I'organisme agree Pratt & Whitney Canada Cie .I Pratt & Whitney Canada Corp 5. Work order/contract/invoice -

4045 - 26 AVE. NORTH Bon de travaiUcontrat !facture

0 PraU & Whitney Canada LETHBRIDGE, ALBERTA Une societe de United Technologies/A United Technologies Company T1H 6G2 P.O.# 4000375856

6. Item 7. Description 8. Part No. - N° de piece 9. Elig ibility' - Admjssibiljte~ 10. Qly - alee 11. Serial/balch No.- N° de serie/de lot 12. Status/work - EtaUlravail

Free Turbine Turbo-Prop 01 PT6A-34 3020800 VARIOUS 1 PCE-RB0332 MANUFACTURED

13. Remarks - Remarques

CANADIAN TYPE CERTIFICATE E-6, FAA TYPE CERTIFICATE E4EA

THIS ENGINE CONFORMS TO ITS UNITED STATES TYPE DESIGN (TYPE CERTIFICATE NUMBER E4EA) AND IS IN CONDITION FOR SAFE OPERATION. THIS ENGINE HAS BEEN SUBJECTED BY THE MANUFACTURER TO A FINAL OPERATION CHECK AND IS IN A PROPER STATE OF AIRWORTHINESS.

14. Certifies that the items identified above were manufactured in conformity to: Le present bon certifie que les articles indiques ci-dessus ont ele construits conformement a : 571.10 Maintenance release. - Certification apres maintenance en vertu du RAG 571

[3J Approved design data and are in condition for safe operation.

D des donnees de conceotion aoorouvees et au'ils oeuvenl eIre utilises en louie securite Other requlatio ecified in block 13. - Autre reqlementation precisee a se 13.

D Non Approved design data specified in block 13. - Certifies that, except where otherwise ifled in block 13, the work' Ifled in block12 and described in

des donnees de conception non approuvees indiquees a la case 13. block 13 was performed in accordance with 571. le present bon certifie que, a moins d'indica\ion c ire raissant a la case 13, Ie travail indique a la case 12 et decrit a fa case 13 a et€: effectue confor u RAC 571.

15. Authorized signature Signature aulorisee 16.Certificale I Approval Ref. No. 20 AUlhoc;zed S;9naIUC~ 21. cert;fiC~~

~ J~ N° d'agrementld'aulorisation (f:) r.C.4058

N~ d'agremen ' torisation

"- e NO. OO4

17. Nt e . N°R. J. DAVIES 18. Dale (dd/monlh/yyyy)

2~ 23. Date (dd/mmm/yyyy)

~ 08 DEC 2006 24·0078 (l2JOM'ool) I P&WG 5720 (2005-03) Installer must cross-check eligibility WIth approved data - Le monteur (Iolt contre-verlf ler I admlsslbl1lie avec les donnees approuvees 1. Le present document n'autorise aucunement Ie monlage de la piece. - 1. This document does not constitute authority to install the part. 2. Si Ie monleur 5e base sur la reglementation nation ale d'une au\orile de navigabilite autre que celie indiquee a la case I, if doit s'assurer que i"autorite de navigabHite don! ij reliNe accepte les produits ou les travaux de maintenance de I'aulorite de navigabilite indiquee 11 la case 1. - 2. Where the installer works in accordance with the national regulations of an airworthiness authority other than the authority specified in block 1, the installer must ensure that his/her airworthiness authority accepts products or maintenance from the ailWorthiness authority specified in block 1 . 3. Les enonces des cases 14 et1g ne constituent en aucune falfon une certification du montage. Dans tous les cas, Ie dossier technique de j'aeronef doit renfermer une certification de montage delivree conformement a la reglementalion de l'Etat d'immatriculation, ct ce, avant que tout vol puisse avoir lieu - 3. Statements 14 and 19 do not constitute installation certification. In all cases the aircraf1technical record must contain an installation certification, issued in accordance with Ihe national regulations of the slate 01 registry, before the aircraft may be flown.

Index of Engine Documentation

Engine Number: PCE-RB0332

Document Name

Final Acceptance Test Record Sheet

Engine Serialized

Component Summary

Life Limited Material History Record

Life Limited Blades History Record (when applicable)

Supplementary Information Sheet

(when applicable)

Engine Airworth iness Directive Sheet

Engine Build Record Status

Report (SB)

Eng ine Log Book (Yellow Book)

Final Vibration Survey (when appl icable)

Authorized Released Certificate (Form 24-0078)

Date

Note: This index ref lects the quantity of Shipping Documentation supplied with the engine.

Quantity of Documents

1

(Quantity of set) X (Quantity per set)

1 X 2

6

N/A

N/A


1 X 1 Note: One copy Inserted In section

four of the Yellow Log Book


1 X1 Note: One copy inserted in section

five 01 the Yellow log Book.

1

N/A

1 Note: For release of engine only.

December 8, 2006

Issue Date: October 4'" 2002

PRATT & WHITNEY CANADA CORP . P68 PROGRAM 4.3.44 ================================================================ PT6A-34 S /N :PCE-RB0332 FINAL ACCEPTANCE TEST RECORD

2006 DEC 08 TEST CELL : 3202 BUILD SPEC .: ENGINE TESTED AND ACCEPTED IN ACCORDANCE WITH E&TI

FINAL VANE FLOW AREAS FIRST STAGE SECOND STAGE

1009 245 29501 3S3 29501 4S2

= - - = = = = = = = = = = = = = = = = = = = = = - - =

6.08 15 . 38

= = = PERFORMANCE DATA TAKE-OFF MAX-CRUISE

= = = = = = = = = = = ------------ = = = = = = = = = = = = = = = = = = =

PROP SPEED S.L . S . STD.DAY POWER TRIMMED INTERTURBINE TEMP T5D (DERIVED) GAS GEN . SPEED FUEL FLOW @ 18400 BTU / LB

DEG R DEG R RPM LB/HR

= = = = SPEC = = = 2200.

750 . 1785.

36800 467 .

ACTUAL SPEC - - - -- - - - = = = = =

2200. 2200. 750 . 700 .

1750. 1745 . 1815 .

36450 . 447 . 443.

FUEL TYPE TEST LHV

S . G.

: CPW 204 : 18540.

OIL TYPE OIL CONSUMPTION

T.O. OIL PRESSURE OIL TEMPERATURE

I.T.T. TRIM DELTA T (UNTRIMMED-TRIMMED) I.T.T. TRIM DELTA T (UNTRIMMED-TRIMMED )

I.T.T . TRIM CLASS TRIM RESISTANCE

COLD HARNESS RESISTANCE

: 0.807 @ 61.

PWA 521 0 . 0 94.6 153.5

72 . 0 40.0 40 13.8

0 .6 9

ACTUAL = - - -- - -

2200 . 700.

1710. 1773.

35950. 422.

BTU / LB DEG F

TYPE II LB / HR PSI DEG F

DEG F DEG C

OHMS OHMS

= =

= = = = = = = = = = = = = = = = = = = = = = = = = = = = = = = = - - - -- - - -HANDLING AND CONTROL SETTINGS = = = = = = = = = = = = = = = = = = = = = = = = = = = = = = = = - - - -- - - -

ACCEL .

TRIMMED MAX NG 35535 UNTRIMMED MAX NG 38100 DATA PLATE SPEED 35535

IDLE SPEED 19346 TIME F.I . TO MAX @ T1 2 . 45 SECS SG DOME FINAL SETTING INDEX

ENGINE DRY WEIGHT 334

RPM RPM RPM RPM

@ 53 . 3 CLICK LBS.

DEGF

PRODUCTION SIGNATURE ~~'ED -- -----~~--

-~ <--INSPECTION SIGNATURE ~ IdA(>. •• n Cd)

----------~--GOVERNMENT INSPECTOR

THE UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATELY SETS FORTH THE EVENTS DURING THE TEST MADE ON THE ENGINE THEREIN IDENTIFIED .

DATE 0 8 DEC 2006 FOREMAN, ASSY . &TEST INSP ~ ~ ~"Jg-.~ B.HORVATH

Liste des composants moteur a numeros de serie Engine Serialized Component Summary

P&WC JR3-6830-E (0 5·1998)

Modele PT6A-34 I N° de serie Serial No. PCE-RB0332

Model

N° du materiel DeSi~ation du materiel N° de serie Code de trait.

Material Number aterial Name Serial No. thermique Heat Code

3007338 GEAR-RING,SECOND STAGE REDUCTION PKAAA059482

301 1095 SHAFT-POWER TURBINE RWA55A089 HSCJW

3011713 DISC-COMPRESSOR A0023TXP KAWAD

3012286 COUPLING SHAFT FLEX 2ND STAGE RED'N PKAAA074007

3013111 HUB-COMPRESSOR,REAR RWA56A124 KAWBX

3013132 CARRIER-SECOND STAGE REDUCTION PKAAA042861

3013176 IMPELLER - CENTRIFUGAL TXA1B0683 PZBXM

3013411 DISC-TURBINE A002433T PZBWA

3013712 DISC-COMPRESSOR A0023WOD KAWAD

3018834 COUPLING POWER TURBINE SHAFT PKAAA070664

3019906 FLOW DIVIDER AND DUMP GATE 9959512908

3022339 RING-CONTAINMENT RWA59A011 SGEAJ

3023250 GEAR-SUN,2STG RDCN,46 TEETH PKAAA072832

3023252 ADAPTER-1ST STAGE CARRIER PKAAA073066

3024765 GEAR-SUN,1ST STAGE RDCN,27 TEETH PKAAA066320

3028812 DISC-TURBINE A0023Y59 PZBXX

3027629 BUS BAR-T5 THERMOCOUPLE,ASSY OF HR22934

3028004 BEARING OPTION BB0052562 BB0052579

3028007 BEARING-ROLLER FLANGED BB0052990

3028266 HOUSING ASSY-PROP RED GBOX,FRONT RWA54A990

3032151CL03 VANE RING-TURBINE HLA236C

3032710 HEATER-OIL TO FUEL WA28556

3034794 PUMP-FUEL 002493

3035889 EXCITER-IGNITION NNA06423889

3035926 GOVERNOR-PROPELLER 14934347AE

3037305 GEAR-PLANET,1ST STAGE REDUCTION PKAAA075537 PKAAA075540 PKAAA075560

3043672CL02 VANE RING-POWER TURBINE(MACH) HLAX037

3045839 GEAR-PLANET,SECOND STAGE REDUCTION PKAAA061345 PKAAA061350 PKAAA061357 PKAAA061363 PKAAA061365

3046695-01 SHAFT-PROPELLER EAAAOOOB050 KAWCB

3053085-01 GEAR - RING FIRST STAGE REDUCTION PKAAA069839 3058201-01 GEARS HAFT - DRIVE, ACCESSORY GEARBOX PKAAA065195

3058264-01 COUPLING-COMPRESSOR REAR HUB PKAAA059084

3058641-01 HOUSING-POWER TURBINE STATOR,ASSY OF EDA00504M

3070218-01 GEARSHAFT STARTER GENERATOR DRIVE PKAAA069109

Pratt & Whitney Canada Une s~t4 del United Technologies /A UnilcdTochnologies Compeny

Pratt & \-, Canada Cie. / Pratt & Wi lltney Canada Corp. 1000, Marie-VlCtorin Longueuil, Quebec, Canada J4G 1A1 450-677-9411

Page

I Caract. de montage Build Spec NO. BS1009

N° de serle du N° de lot pour trait. N° de materiel du fournisseur materiel forge thermique Vendor Material No. Forging Senal No. Heat Treat Batch No.

44138

44069

004 169

44138

012

con"

Liste des composants moteur a numeros de serie Engine Serialized Component Summary

P&WC JR3-6830-E (05-1998)

Modele PT6A-34 I N° de serie PCE-RB0332 Model Serial No.

N° du materiel DeSiSJ.1ation du materiel N° de serie Code de trait.

Material Number aterial Name Serial No. thermique Heat Code

3100829-03 VALVE ASSY-COMPRESSOR BLEED AHXOO7201

310141 9-01 CARRIER-FIRST STAGE REDUCTION PKAAA046527

3101635-01 BEARING-BALL FLANGED FAA0626562

3101864-01 BEARING-BALL FAA0626531 3102227-01 BEARING-BALL FLANGED BB0053106 3102336-01 SHAFT-STUB,COMPRESSOR,FRONT RWA54A626 EPEIB 3110863-07 CASE ASSY-GAS GENERATOR RWA63A426 3111780-01 DUCT-TURBINE EXHAUST, ASYO RWA62A214 3112368-01 BEARING-ROLLER FLANGED,.94X1 .65X.47 FAA0635427

FAA0635428 FAA0635437 FAA0635438 FAA0635440 FAA0635450 FAA0635451 FAA0635452 FAA0635453 FAA0635464 FAA0635468 FAA0635469

3117924-01 WIRING HARN-T5,THERMOCOUPLE NRA23820

3122633-01 LINER-COMBUSTION CHAMBER,ASSY OF RWA62A331 3122696-03 FUEL CONTI)PL-TURBOPROP C25822

Approve Jar Approve By II /L .. ~ B. HORVA11t

'0-~, T,c,,·,.

I. lit NO. 022

Pratt & Whitney Canada Una societe de United Technologies /A United Technologies Company

Pratt & VI .2 Canada Cia. I Pratt & Whitney Canada Corp. 1000, Marie-Victorin Longueuil. Quebec. Canada J4G lAl 450-677-94 11

Page 2

I Caract. de montage Build Spec NO. B51009

N° de serie du N° de lot pour trait. N° de materiel du fournisseur materiel forge thermique Vendor Material No. Forging Senal No. Heat Treat Batch No.

Date 2006.12.08

Historique du materiel a duree de vie limitee Life Limited Material History Record

Numero du dessin ST3582-01 - Drawing Number ST3582-01

P&WC JR3-6834·E (6834) (2004-02)

Designation du materiel Material Name

DISC-COMPRESSOR

N° du materiel N° de serie du materiel Material No. Material Serial No.

3011713 A0023TXP

Donnees sur Ie moteur ! module - Engine I Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de sene du depuis !'installation du moteur / module Modele I'enlevement

materiel du materiel Er!ine/ModUIe En~e I Module Model En~ 1 Module

SNWhen erial No. T N When Material Material Installed Removed

0 PCE-RB0332 PT6A-34 0

Pratt & Whitney Canada Une soci4t ' de United Technol t>gies/A United Technolooies Company

Pratt & Whitney Canaoa Cie. I Pratt & Whitney Canada Corp_ 1000, Marie·Victorin LongueUil

J Quebec

Canada 4G 1A 1

Nota: Pour connaitre les durees de vie Code de traitement thermique !'.mis Ie (A-M-J ~ accumulee et residuelle du materiel, Heat Code Issue Date (Y- -D) consulter Ie Manuel d'entretien du

KAWAD 2006. 12.08 mateur ou Ie Bulletin de service approprie, selon Ie cas.

N° de sene du mat'1. forge Temps depuis Cycles depuis Forging Mat'I Senal No neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material , refer

0 0 to the e"aine aintenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel - Material Data

Cumul. de ceUe installation Cumul. jus~u'a present Observations

(Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

!¢-M-J\ -M-D Remarks

(Maintenance/Overhaul, Facility, Sales Temps- Time Cycles Temps - Time Cycles Order & inspection stamp)

Inserer Ie present historique dans Ie livre du mateur ou du module au la piece est Installee. - This record must be kept with the engine/module logbook where this part IS Installed.



P&WC JR3-6834-E 16834\ (2004.()2)


HUB-COMPRESSOR,REAR


3013111 RWA56A124

Donnees sur Ie moteur I module - Engine I Module Data

Temps de Temps de fonclionnement fonctionnement

depuis N° de serie du depuis I'installation du moteur I module Mo(U~le J'enlewement

materiel du materiel E~lne/Module En~ne , Module Model En~ I Module


0 PCE-RB0332 PT6A-34 0

Pratt & Whitney Canada o Una societe de United Technologies /A UnllodTechnologl88 Company

Pratt & Whitney Cana". 2e. I Pratt & Whitney Canada Corp. 1000, Marie·Victorin LongueUiJI Quebec Canada 4G 1A1

Nota : Pour connaitre les dun~es de vie Code de traitement thermique Emis Ie (A-M-J~ accumulee et residuelle du materiel, Heat Code Issue Date (Y - -0) consulter Ie Manuel d'entretien du

KAWBX 2006.12.08 moteur au Ie Bulletin de service approprie, selon Ie cas.

N° de serie du mafl. forge Temps depuis Cycfes depuis Forging Mat'l. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and rernainin~ives on this material, refer

0 0 to the en~ine ainlenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel - Material Data

Cumul. de cette installation Cumul. jus~u'a present Observations (Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

!¢-M-J\ -M-O Remarks (Maintenance/Overhaul, Facility Sales

Temps- Time Cycles Temps- Time Cycles Order & inspection stamp')

Inserer Ie present historique dans Ie livre du moteur au du module oD la piece est Installee. - ThiS record must be kept With the engine/module logbook where this part is installed.



P&WC JR3·6834-E {6834] (2004.{l2)


IMPELLER - CENTRIFUGAL


3013176 TXA1B0683

Donnees sur Ie moteur I module - Engine / Module Data

Temps de Temps de fonctionnemenl fonctionnement

depuis N° de serie du depuis I'installation du moteur / module Modele I'enlevement

materiel du materiel E~ine/Module Enre J Module Model Eng ' Module


0 PCE-RB0332 PT6A-34 0

) Pratt & Whitney Canada Une societe de Unlled Technologies /A UnitodTechnologies Company

Pratt & Whitney Canaoa Cie.1 Pratt & Whitney Canada Corp. 1000, Marie-Victorin LongueUiJI Quebec Canada 4G 1A1

Nota: Pour connaitre les dun~es de vie Code de traitement thermique ~mis Ie (A-M-J~ accumulee et residuelle du materiel . Heat Code Issue Date (Y- -D) consulter Ie Manuel d'entretien du

PZBXM 2006.12.08 moteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de serie du matl forge Temps depuis Cycles depuis Forging Mat'!. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material, refer 004 0 0 to the enaine aintenance Manual Of

Service ulletin, as applicable. Donnees sur Ie materiel - Material Data

CumuL de cette installation Cumul. jus~u'a present Observations

(Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur) !¢-M-J)

-M-D) Remarks (Maintenance/Overhaul, Facility, Sales

Temps- Time Cycles Temps - Time Cycles Order & inspection stamp)

lnserer Ie present historique dans Ie livre du mateur au du module au la piece est Installee. - ThiS record must be kept With the engine/module logbook where thiS part IS Installed.



P&WC JR3-6834·E [6634[ (2004.()2)


DISC-TURBINE


3013411 A002433T

Donnees sur Ie moteur / module - Engine I Module Data

Temps de Temps de ronclionnement fonctionnernenl

depuis N° de serie du depuis !'installation du moteur / module Modele I'enlevement

materiel du materiel E~ine/Module En~ne / Module Model En~/ Module

SN When erial No. T N When Material Malerial Installed Removed

0 PCE-RB0332 PT6A-34 0

) Pratt & Whitney Canada Une societe de United Technolotj8s /A United Technologies Company

Pratt & Whitney Canada Cie. J Pratt & Whitney Canada Corp. 1000, Marie-Victorin LongueUi

J' Quebec

Canada 4G 1 A 1

Nota: Pour connaitre les durees de vie Code de traitement thermique ~mis Ie (A-M-J~ accumulee et residuelle du materiel, Heat Gcx:le Issue Date (Y- -D) consulter Ie Manuel d'entretien du

PZBWA 2006.12.08 moteur ou Ie Bulletin de service approprie, selon Ie cas.

N° de serie du mat'!. forge Temps depuis Cycles deputs Forging Mat'1. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material , refer 169 0 0 to the en~ine aintenance Manual or

Service ulletin, as applicable. Donnees sur Ie materiel - Material Data

Cumul. de cette installation Cumul. jus~u'a present Observations

(Installation d'entretien, de revision, Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

!¢-M-J\ -M-D Remarks

(Maintenance/Overhaul , Facility , Sales Temps- Time Cydes Temps - Time Cycles Order & inspection stamp)

Inserer Ie present hlstorique dans Ie livre du moteur ou du module au la PIece est installee. - ThiS record must be kepi with the engine/module logbook where this part is installed.



P&WC JR3-6834-E (68341 (2004-02)


DISC-COMPRESSOR

N° du materiel N° de serle du materiel Material No. Material Serial No.

3013712 A0023WOD

Donnees sur Ie meteur I module· Engine I Module Data

Temps de Temps de fonctionnement fonctionnement

depuis N° de sene du depuis !'installation du moteur I module Mad~le I'enlevement

materiel du materiel E~ine/ModUle En~ne ! Module Madel En~! Module


0 PCE-RB0332 PT6A-34 0

Pratt & Whitney Canada o Une social' de United TechnologiesJA Unltod Technologies Company

Pratt & Whitney Cana"d 2 e. I Pratt & Whitney Canada Corp. 1000, Marie-Victorin LongUeUijl Quebec Canada 4G 1A1

Nota: Pour connaitre les dun~es de vie Code de traitement thermique Emis Ie (A-M-J~ accumuh~e et residuelle du materiel . HeatCade Issue Date (Y- ·0) consulter Ie Manuel d'entretien du

KAWAD 2006.12.08 moteur ou Ie Bulletin de service approprie, selon Ie cas .

N° de serie du mat'!. forge Temps depuis Cycles depuis Forging Mat'l. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~jVeS on this material. refer

0 0 to the enaine aintenance Manual or Service ulletin, as applicable.

Donnees sur Ie materiel· Material Data

Cumul. de cette installation Cumu!. jUS~U'~ present Observations (Installation d'entretien, de revision , Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur)

!¢-M-J\ -M-O Remarks

(Maintenance/Overhaul, Facility ~ Sales Temps· Time Cycles Temps· Time Cycles Order & inspection stamp

Inserer Ie present historiQue dans Ie livre du moteur ou du module ou la piece est installee .• This record must be kept with the engine/module logbook where this part is installed.



P&WC JR3-6834·E [6834] (2004-02)


DISC-TURBINE

N° du materiel N° de sene du materiel Material No. Material Serial No.

3026812 A0023Y59

Donnees sur Ie moteur I module · Engine I Module Data

Temps de Temps de fonctionnemenl fonctionnement

depuis Ntl de sMe du depuis I'installation du moleur I module Modele I'enlevement

matenel du materiel E~ine/ModUle En~e / Module Model En~ 1 Module

SN VVhen erial No. T N When Material Material Installed Removed

0 PCE-RB0332 PT6A-34 0

Pratt & Whitney Canada Una !oclett. de United Technolog!es/A United Technologies Company

Pratt & Whitney canaa,,~e. I Pratt & Whitney Canada Corp. 1000, Marie·Victorin LongueUiJI Quebec Canada 4G 1A1

Nota : Pour connaitre les durees de vie Code de traitement thermique Emis Ie (A-M-J~ accumulee et residueUe du materiel, Heat Code Issue Date (Y- -D) consulter Ie Manuel d'entretien du

PZBXX 2006.12.08 moteur au Ie Bulletin de service approprie, selon Ie cas.

N° de sene du mat'1. forge Temps depuis Cycles depuis Forging Marl. Serial No. neuf neuf Note: For determination of accumulated

Time Since New Cycles Since New and remainin~ives on this material, refer 012 0 0 to the enaine aintenance Manual or

Service ulletin, as applicable. Donnees sur Ie materiel· Material Data

Cumul. de cette installation Cumul. jus~u'a present Observations

(Installation d'entretien, de revision , Bulletin Accumulated This Installation Total Accumu ated To Date Date de vente et timbre du verificateur) /¢-M-J\ -M-D Remarks

(Maintenance/Overhaul , Facility) Sales Temps· Time Cycles Temps· Time Cycles Order & inspection stamp

Inserer Ie present historique dans Ie livre du moteur ou du module ou la piece est installee . . This record must be kept with the engine/module logbook where this parI is installed.

1+1 Transport Canada

Transports Canada

Engine Logbook

TP 14182E

1111 111 11 11 11111111111 11111111111111111 11111111 111

(Revised OS/2005)

Canada

Volume #: _--=",-1 __ _ Opened on: 1 3 DEC 2006

ENGINE DETAILS

1 M f t Pratt & Whitney Canada Corp. . anu ac urer __

I 2. Type/Model/Series PT6A-~3---..L.-4-L-____ B/S:_---L/---..::{)::.....:{)=------t.J _

3. Serial Number pcE-_--+-K-\--'---"B:.......::([)=::...-' -=:::3'-"-3"'-4--'--____ _

(il

Section 1: Record of engine maintenance and elementary work

Date --/--/--

1 3 DEC 2005

Time since new

D·D

Time since overhaul

c). 0

Total cycles

o

Details of task

New engine final acceptance test and inhibiting run completed satisfactorH and is in coridition for safe operation

Date: 04119112 Engine SIN: PCE-RB0334 I Time since new: 0.0 I TSMOH: NIA I Total Engine Cycles: 0.0 MAINTINEANCE PERFORMED:

Removed all propeller reversing system parts listed in Table 1 of PWC IPC Chapter 76-10-00, FIG 1 and PWC maintenance manual chapter 76-10-00. Installed 2 new MS9320-12 washers on on prop reduction gearbox cover studs after removal of reverseing lever guide pin assy.

T~rqued all faste~!ff/~W PW~e7f1ce manual PIN 3011244 Chapter 76-10-00. Signature: ~~Aff O~ William Ostrander Cert. No: 3278840

0 - 1 NLA 0 <3

TTSN 0.0

Serial #: PCE-RB0334

Model #: PT6A-34

N382SB

I certify that this engine has been inspected in

accordance with the Pratt and Whitney maintenance

manual Part # 3021242 and was deemed safe for flight.

~~-=s, Charles M. Armstrong Jr.

IA415981577

-r

I

Vi AME

,CD Signature ACA/AMO SCA/AMO

-'1 ad . I . )ril\ I

TRIMSPEEDNg ]5517 ,% NgMAX: 14.cr G.tJ'~MANN .on , . /

-@ /Ii W///l1YVJ/ 1/ G<f;l~. T.C. 4·58 -~ NO . 049

/ -f

--------,' .~

-------~ ~

~ /

b I I

- ) ;.'>1

I

I

I

I

I .,Q 1lfIO~ .

i\~ ------

,

Page 1

-Sect ion 1: Record of engine maintenance and elementary work

Date -- /-- / --

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Time since new

Time since overhaul

Total cycles

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Details of task

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Engine Airworthiness Directives pwc 2371(2000-01)

Reference AD.'s

To ensure the early detection of reduction gearbox FAA A.D . deterioration and for improved blade containment. 75-06-01 S.B. 1138, 1216& 1220 or their later revision or

superseding S.B. incorporated at manufacture.

Sign

~4dtfA/ ----G. tU!RMANN

For engine incorporating an unmodified power 1t.~ / FAA A.D . turbine shaft housing assembly part number / / %1Af/ 75-11-04 3010548. Not applicable due to part number. Modification incorporated at manufacture. G.HERMANN

Engine incorporates the inproved power turbine ~4z}t~~/ CF-78-03 containment modification. S.B. 1217 & 1220 or their later revision or superseding S.B. incorporated at

G.HIERMANN manufacture.

CF-96-24 To preclude malfunction of the compressor bleed of vriir#!1/ ,/ FAA A.D . valve. S.B 1538 or its later revision or superseding _ 97-04-12 S.B .. incorporated at manufacture. G. iiERMANN

Pratt & Whitney Canada Corp_ 1000, Marie-Victorin Longueuil, Quebec Canada J4G 1 A 1

IEnginel ?/N PCE-RB0334

Lic. # Date

or Stamp

(!:) T.C. 4-58 "..t. 0NO . 04g 1 3 DEC 2DD5

(!) T.C. 4-58 1 3 DEC 2006 "- /. NO .049 o -

~ T.C.4·58 1 3 DEC 2006 "-/. NO . 049· <'l -

(!:) T.C. 4-58 .... NO. 049 o - 1 3 DEC 2006

l Page no 1

PRATT & WHITNEY CANADA

ENGINE BUILD RECORD STATUS

THE FOLLOWING SERVICE BULLETINS ARE BASIC TO

ENGINE SERIAL NO. PCE-RB0334

ENGINE MODEL PT6A-34

BUILD SPEC 1009

SERVICE BULLETINS

1103 1129 1148 1165 1167 1168 1169 1170 1173 1176 1178 1179 1183 1185 1190 1191 1192 1194 1200 1201 1202 1203 1207 1211 1212 1215 1216 1217 1219 1220 1223 1224 1225 1226 1227 .1228 1229 1231 1232 1236 1242 1247 1248 1249 1251 1254 1255 1259 1261 1263 1270 1275 1276 1277 1280 1281 1288 1293 1300 1310 1316 1318 1320 1321 1322 1326 1327 1331 1332 1334 1336 1338 1339 1352 1354 1357 1358 1361 1367 1370 1372 1374 1379 1381 1388 1389 1390 1391 1393 1394 1395 1397 1404 1409 1410 1416 1418 1427 1428 1430 1434 1439 1441 1446 1457 1459 1470 1473

( 1474 1490* 1493* 1498 1500 1503 1508 1513 1518 1519 1520 1524 1527 1528 1534 1537 1540 1544 1545 1553 1554 1556 1560 1562 1564 1567 1570 1572 1591 1598 1613 1614 1621 1627 1630 1637 1638 1647 1650 1651 1652 1654 1655

* DENOTES PARTIAL INCORPORATION OF SERVICE BULLETIN SB# PARTS INTRODUCED AT ENGINE BUILD. 1490 3039939 3116033-01 1493 3117225-01 3117228-01 3117230-02 3117233-01

APPROVED BY DATE 2006.12.13