i not measurement sensitive eeel -...

I NOT MEASUREMENTSENSITIVE I

EEEl MIL-sTD-1808 (USAF)NOTICE 128 March 1992

MILITARY STANDARDSYSTEM/SUBSYSTEM/SUBJECT NUMBER (S/S/SN)

NUMBERING SYSTEM

TO ALL HOLDERS OF MIL-STD-1808 (USAF)

1. THE FOLLOWING PAGES OF MIL-STD-1808 (USAF) HAVE BEEN REVISED ANDSUPERSEDE THE PAGES LISTED:

SUPERSEDED PAGE DATENEW PAGE DATE

iiiiv

v/vi9

1011121314212231323738656683848586

141142143144145146147148

~1

28 March 199228 March 199228 March 1992

10 October 199028 March 199228 March 1992

10 October 199028 March 1992

10 October 199010 October 199028 March 199210 October 199028 March 199210 October 199028 March 199228 March 199228 March 199228 March 1992

10 October 199010 October 199028 March 199228 March 199228 March 199228 March 199228 March 199228 March 199228 March 199228 March 199228 March 1992

Page number change

iiiiv

v/vi9

1011121314212231323738656683848586

141142143144145146147148

10 October 199010 October 199010 October 1990

REPRINTED WITHOUT CHANGE10 October 199010 October 1990

REPRINTED WITHOUT CHANGE10 October 1990

REPRINTED WITHOUT CHANGEREPRINTED WITHOUT CHANGE

10 October 1990REPRINTED WITHOUT CHANGE

10 October 1990REPRINTED WITHOUT CHANGE

10 October 199010 October 199010 October 199010 October 1990

REPRINTED WITHOUT CHANGEREPRINTED WITHOUT CHANGE

10 October 199010 October 199010 October 199010 October 1990 ~/10 October 1990 &/10 October 1990 l_/10 October 1990 &/10 October 1990 IJ10 October 1990

only. Information has not changed.

NO DELIVERAB LE DATA REQUIRED BY THIS DOCUMENT AREA TMss

DIs~IBuTIOM sTA_~ A. Approved f..wbli.release;distrib.cionisunlimited.

1

Downloaded from http://www.everyspec.com

MIL-STD-1808 (uSAF)NOTICE 1

2. RETAIN THIS NOTICE AND INSERT BEFORE TABLE OF CONTENTS.

3. Holders of MIL-STD-1808 (USAF) will verify that page changes andadditions indicated above have been entered. This notice page will beretained as a check sheet. This issuance, together with appendedpages, is a separate publication. Each notice is to be retained bystocking points until the military standard is completely revised orcancelled.

Custodian: Preparing Activity:Air Force - 16 Air Force - 16

Reviewing Activities: (Project TMSS-F598)Air Force - 10, 11, 13, 14, 15, ‘

19, 85, 91, 99

2


MIL-STD-1808 (USAF)

CONTENTS

PARAGRAPH

1. SCOPE . . . . . . . . . . . . . . . . . . .1.1 Scope . . . . . . . . . . . . . . . . . .1.2 Acquisition applicability . . . . . . . .

2. REFERENCE DOCUMENTS .2.1 Government documents2.2 Order of precedence

3. DEFINITIONS . . . . .3.1 Definitions . . . .

4. GENERAL REQUIREMENTS .

. . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .4.1 System/Subsystem/Subject Number (S/S/SN)

numbering system . . . . . . . . . . . .

5. DETAILED REQUIREMENTS . . . . . . . . . . .5.1 UseofS/S/SN . . . . . . . . . . . . . .5.2 Definition of aircraft groups, systems and

subsystems. . . . . . . . . . . . . . .5.3 System number index . . . . . . . . . . .

System

0001 THRU 04050607

08091011121314151617

AIRCRAFT GENERAL . . . . . . . . . . .RESERVED. . . . . . . . . . . . . . .TIME LIMITS/MAINTENANCE CHECKS . . . .DIMENSIONS AND AREAS . . . . . . . . .LIFTING, SHORING, RECOVERING ANE

TRANSPORTING . . . .LEVELING AWE WEIGHINGTOWING AND TAXIING . .PARKING AND MOORING .PLACARDS AND MARKINGSSERVICING . . . . . .EOUIPMENT STORAGE . .

. . . . . . . .

. . . . . . . .

. . . . . . . .

. . . . . . . .

. . . . . . . .

. . . . . . . .

. . . . . . . .A;RCRAFT LOADING AND OFF-LOADING . . .SUPPORT EQUIPMENTSITING INSTALLATION” : : : : : : : : :PREPARATION FOR USE AND SHIPMENT . . .WEAPONS INSTRUMENTATION . . . . . . .TRAINING EQUIPMENT . ! . . . . . . . .STANDARD PRACTICES - AIRFRAME SYSTEMSAIR CONDITIONING . . . . . . . . . . .AUTO FLIGHT . . . . . . . . . . . . .

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~

11

1

223

44

5

5

77

99

14161719

20222526282931323435363738394043

Supersedes page iii ofMIL-STD-1808 (USAF) iii


MIL-sTD-1808 (USAF)

CONTENTS

PARAGRAPH

2324252627282930313233343536373839

404142434445

50515253545556

COMMUNICATIONS . . . .ELECTRICAL POWER . . .EQUIPMENT/FURNISHINGSFIRE PROTECTION . . .FLIGHT CONTROLS . . .FUEL. . . . . . . . .HYDRAULIC POWER . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .

. . . . . . . . . . .ICE AND RAIN PROTECTIONINDICATING/RECORDING SYST&& : : : : : : : :LANDING’GEAR. . . . . . . . . . . . . . . .LIGHTS .’.. . . . . . . . . . . . . . . . .NAVIGATION. . . . . . . . . . . . . . . . .OXYGEN. . . . . . . . . . . . . . . . . . .PNEUMATIC . . . . . . . . . . . . . . . . .VACU~’. . . . . . . . . . . . . . . . . . .WATERIWASTEELECTRICAL/ELEC;RON;C-Components ‘ . “ “ - -

AWE MULTIFUNCTION UNITS . . . . . . . . .STANDARD PRACTICES - INTEGRATED AVIONICS . .WATER BALLAST . . . . . . . . . . . . . . .INTEGRATED AVIONICS ARCHITECTURE . . . . . .COMMUNICATIONS - STAFF . . . . . . . . . . .IN-FLIGHT REFUELING - TANKER . . . . . . . .CENTRAL MAINTENANCE SYSTEM (CMS) . . . . . .SYSTEM INTEGRATION ~ DISPLAY “.. . . . . .LIQUID/GZiSEOUS NITROGEN . . .COMMUNICATION/NAVIGATION/;D;N+I;I;A&~N. . .AIRBORNE AUXILXARY POWER . . . .RESERVED. . . . . . . . . . . .STANDARD PRACTICES - STRUCTURESDOORS . . . . . . . . . . .FUSELAGE: . . . . . . . . . . .NACELLES/PYLONS . . . . . . . .STABILIZERS . . . . . . . .WINDOWS AND C&JbPIES . . . . . .

57 WINGS . .58 AND 59 RESERVE;: : : : : : ~ : : : . .60 STANDARD PRACTICES - PROPELLER .61626364

. . . . . .

. . . . . .

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. . . . . .

. . . . . .

. . . . . .

. . . . . .

. . . . . .

. . . . . .

. . . . . .PROPELLERS/PROPULSORS . . . . . . . . . . .ROTOR(S) . . . . . . . . . . . . . . . . . .ROTOR DRIVE(S) . . . J. . . . . . . . . . .TAIL ROTOR. . . . . . . . . . . . . . . . .

~

45474952535658596163656769707172

73757677788082848586878889919395979899

101102103105106107

Supersedes page iv ofMIL-STD-1808 (USAF) iv


MIL-STD-1808 (USAF)

CONTENTS

PARAGRAPH

65666’768 AND 6970717272 (1)72 (2)73747576777879808182838485 THRU 90919293949596979899

6. NOTES

TAILROTORDRIVE . . . . . . . . . . . - - .FOLDING BLADES/PYLON . . . . . . . . . . . .ROTORS FLIGHT CONTROLS . . . . . . . . . . .RESERVED. . . . . . . . . . .STANDARD PRACTICES - ENGINE . . . . . . . .POWER PLANT . . . . . . .- . . - . . . . .ENGINE. . . . . . . . . . . .- . - . . .-ENGINE - TURBINE/TURBOPROP . . . . . . . . .ENGINE - RECIPROCATING . . . . . . . - . . .ENGINE FUEL AND CONTROL . . . . . . - . . -ENGINE IGNITION . . . . . . - . - . . - . .ENGINE AIR. . . . . . . . . . . - . - . . -ENGINE CONTROLS . . . . . - . . . . - . . .ENGINE INDICATING . . . . . . - . - . . . .ENGINE EXHAUST. . . . . . . . . . . . . - -ENGINE OIL. . . . . . . . . .- . . . . . .ENGINE STARTING . . . . . . . . . . - . - .TURBINES. . . . . . . . . - . . . . . . . .WATER INJECTION . . . . . . . - . . . . . .ACCESSORY GEARBOXES . . . . . . . - . . . -PROPULSION AUGMENTATION . . . . . . - . . .RESERVED. . . . . . . . . . . . - . . . . .CHARTS/DIAGRJ+MS . . - . . . . - . . . . . .ELECTRICAL POWER MULTIPLEXING . . . . . - .SURVEILLANCE. . . . . . . - . . - . - . . .WEAPON SYSTEM . . . . . . . . - . - . . - -CREW ESCAPE AND SAFETY . . . . . . . - . . .MISSILES, DRONES AND TELEMETRY . . . . . . .IMAGE RECORDING . . . . . . . . . . . . . -METEOROLOGICAL AND ATMOSPHERIC RESEARCH . .ELECTRONIC WARFARE.. . . . . . . . . . . .

. . . . . . . . . . . . . . . --- . . . -

6.1 Intended use. . . . . . . . . . . . - . - . . .6.2 IssueofDODISS . . . . . . . - . . . . - . . .6.3 Supersession data . . . . . - . . - . . . . . -

~

108109110112113114116117119121123124126127129131132133134135136137138139141143144145146147148

149149149149

Supersedes page v[vi ofMIL-STD-1808 (USAF) vlvi


MIL-STD-1808 (USAF)

subject of the JG manual and shall be numbered as provided inMIL-M-83495. For example: All operational checkouts of systems,subsystems, sub–subsystems or a subject nuniber identified itemwould be identified as “-001”.

5.1.5.2 VP ical functions. The following typical functions maybe used as guide for development of the function numbers and maybe expanded[changed to suit equipment requirements:

001 -002 -003 -004 -005 -006 -007 -008 -009 -010 -

5.1.6shall

Operational CheckoutAccessRemoveRepairInstallInspectCleanLubricateServiceAlign and Adjust

011 - Calibrate012 - Operate013 - Troubleshoot014 - Disassemble015 - Assemble016 - Test017 - Non Destructive Inspection018 - Corrosion Prevention019 - Follow-On Maintenance020 - Shipping/Handling/Packaging

Text development. The definitions of the system numberingbe used as a basis for seauencinq/developing the text of

the manuals/view packages.

5.2 Definition of aircraft aroups, systems and subsystems.

GROUP DEFINITION

AIRCRAFT The complete operational unit.Includes dimensions and areas,lifting and shoring, levelingand weighing, towing andtaxing, parking and shoring,required placards, servicing.

5.3 System number index. The following index is a compilationof the Systems that will be found on the subsequent pages of thisdocument and has been added for quick reference purposes.

SYSTEM TITLE

00 AIRCRAFT - GENERAL

01 THRU 04 RESERVED

05 TIME LIMITS/MAINTENANCE CHECKS

06 DIMENSIONS ANE AREAS

REPRINTED WITHOUT CHANGE 9


07

08

09

10

11

12

13

14

15

16

17

18

I 19

20

21

22

23

24

25

26

27

28

29

30

Supersedes page 10MIL-STD-1808 (USAF)

MIL-sTD-1808 (USAF)

LIFTING, SHORING, RECOVERING AND TRANSPORTING

LEVELING AWE WEIGHING

TOWING AND TAXIING

PARKING AND MOORING

PLACARDS AND MARKINGS

SERVICING

EQUIPMENT STORAGE

AIRCRAFT LOADING AND OFF-LOADING

SUPPORT EQUIPMENT

SITING INSTALLATION

PREPARATION FOR USE AND SHIPMENT

WEAPONS INSTRUMENTATION

TRAINING EQUIPMENT

ST~ARD PRACTICES - AIRFRAME SYSTEMS

AIR CONDITIONING

AUTO FLIGHT

COM$IUNICATIONS

ELECTRICAL POWER

EQUIPMENT/FURNISHINGS

FIRE PROTECTION

FLIGHT CONTROLS

FUEL

HYDRAULIC POWER ‘

ICE ANE RAIN PROTECTION

of10


MIL-sTD-1808 (USAF)

31 INDICATING/RECORDING SYSTEMS

32 LANDING GEAR”

33 LIGHTS

34 NAVIGATION

35

36

37

38

39

40

41

42

43

44

45

46

47

I 48

49

50

51

52

OXYGEN

PNEUMATIC

VACUUM

WAT?3R/WASTE

ELECTRICAL/ELECTRONIC COMPONENTS AWEMULTIFUNCTION UNITS

STANDARD PRACTICES - INTEGRATED AVIONICS

WATER BALLAST

INTEGRATED AVIONICS ARCHITECTURE

COMMUNICATIONS - STAFF

IN-FLIGHT REFUELING - TANKER

CENTRAL MAINTENANCE SYSTEM (CMS)

SYSTEM INTEGRATION AWE DISPLAY

LIQUID/GASEOUS NITROGEN

COMMUNICATION/NAVIGATION/IDENTIFICATION

AIRBORNE AUXILIARY POWER

RESERVED

STANDARD PRACTICES - STRUCTURES

DOORS

53 FUSELAGE

54 NACELLES/PYLONS

Supersedes page 11 ofMIL-sTD-1808 (USAF) 11


MIL-STD-1808 (uSAF)

55

56

57

58 AND 59

60

61

62

63

64

65

66

67

68 AND 69

70

71

7272 (1)72 (2)

73

74

75

76

77

78

-?9

STABILIZERS

WINDOWS ANI”CANOPIES

WINGS

RESERVED

STANDARD PRACTICES - PROPELLER

PROPELLERSIPROPULSORS

ROTOR(S)

ROTQR DRIVE(S),

TAIL ROTOR

TAIL ROTOR DRIVE

FOLDING BLADES/PYLON

ROTORS FLIGHT CONTROLS

RESERVED

STANDARD P~CTICES - ENGINE

POW~R PLANY

ENG;NEENGINE - TURBINE/TURBOPROPENGINE - RECIPROCATING

ENGINE FUEL AND CONTROL

ENGINE IGNITION

ENGINE AIR

ENGINE CONTROLS

ENGINE INDICATING

ENGINE EXHAUST ‘

ENGINE OIL



MIL-STD-1808 (USAF)

80

81

82

83

84

85 THRU 90

91

92

1 93

94

95

96

97

98

I 99

Supersedes page 13 ofMIL-sTD-1808 (USAF)

ENGINE STARTING

TURBINES

WATER INJECTION

ACCESSORY GEARBOXES

PROPULSION AUGMENTATION

RESERVED

CHARTS/DIAGRAMS

ELECTRICAL POWER MULTIPLEXING

SURVEILLANCE

WEAPON SYSTEM

CREW ESCAPE AND SAFETY

MISSILES, DRONES AND TELEMETRY

IMAGE RECORDING

METEOROLOGICAL AND ATMOSPHERIC RESEARCH

ELECTRONIC WARFARE

13


~SYSTEM SYSTEM TITLE

00 AIRCRAFTGENERAL

00 AIRCRAFTDESCRIPTION

MIL-STD-1808 (USAF)

DEFINITION

General information for thecomplete aircraft, proceduresaircraft safety and generalaircraft maintenance, use of

10 AIRCRAFTGENERALMAINTENANCE

20 AIRCRAFTSAFETY

30 SAFETY ANDPROTECTIVEDEVICES’

aircraft safety and protectivedevices, and fatigue lifecalculations ~

for

General description of the aircraftand it’s systems, including type ofaircraft, it’s roles, accommoda–tion5 i salient constructionfeatures, power unit installation,systems and operational equipment.

I

Those instructions necessaqf foraircraft maintenance condition,cockpit ent~, electrical (static)grounding, external power andcooling removal and installation,proximity switch control hookup andremoval, ground communications;.connecting and disconnecting,util+ty power connection, radomeopening and closing, landing geardoor:opening and closing, soloflight configuration, engine oilanalysis, electrical bonding andsealing, and stress frameinstallation and removal.

Those specific or vehicle peculiarinstructions’ necessary to make safeand prepare’ the aircraft formaintenance action. Includesinstructions for returning theaircraft to its serviceable state.

Tho”se instructions necessary foruse OE operation of devices, suchas; ejection control safety lever,safety pins, safety locks, safetypin flag assemblies, safety strutextensions and other requiredsafety devices. Includes

REPRINTED WITROUT CHANGE 14



07 50 - Continued

MIL-STD-1808 (USAF)


DEFINITION

manufacture of transportationsledges or pallets. For removalprocedures and maintenanceinformation, refer to appropriatesystem/subsystem.


~SYSTEM sYSTEM TITLE

08 LEVELINGANDWEIGHING

00 GENERAL

10 WEIGHTANDBALANCE

20 LEVELING

30 WEIGHING

MIL-STD-1808 (USAF)

DEFINITION

That material necessa~ to properlylevel the aircraft for any of thevarious maintenance, overhaul or majorrepairs which might become necessaryduring the life of the aircraft.Includes those units or componentswhich are specifically dedicated torecord, store or compute weight andbalance data. Also includes thosemaintenance practices necessary toprepare the aircraft for weighing andthe procedures to weigh the aircraft.Includes weight and Center of Gravity(CG) data. This system shall be usedfor reference. Actual procedures forleveling, weighing and computing CGshall be included in the -5 seriesmanuals.

Those units or components on theaircraft dedicated to the specificfunction of recording, storing orcomputing weight and balance data.

Those instructions necessary to pre-pare the aircraft for leveling and theleveling procedure. Includes infor-mation on the leveling equipment used.

Those instructions necessary toprepare the aircraft for weighing andthe weighing procedure. Includesinformation on the weighing equipmentused. Also includes limits ofvariation allowed between physicalrecorded weight and calculated weightbas”ed ’on specific ’aircraft record.

40 WEIGHT AND Weight and moment or index informationCG DATA characteristic of the aircraft, limi-

tations, datum points and lines, CGrange, weight and balance managementof the fuel and other expendable loads



MIL-STD-1808 (USAF)


13 EQUIPMENTSTORAGE

00 GENERAL

10 TEMPORARYSTORAGE

20 EXTENDEDSTORAGE

30 STORAGEINSPECTIONSANTETREATMENTS

40 REMOVAL FROMSTORAGE

50 MOVING/FLYING

TO OVERHAUL/MAINTENANCEFACILITY

DEFINITION

Shall contain those procedures andillustrations requir>d fortemporary and extended storage,inspections and treatments duringstorage, removal from storage, etc.

T“nose instructions necessary toprepare the equipment for tempora~storage (under ninety days) .Includes special servicing,location of protective covers,tie-down points, drains, etc.

Those instructions necessary toprepare the equipment for extendedstorage (over ninety days) .Includes special servicing,sealing, venting, protection fromsun, preservatives or protectionrequired, protective covers,tie-down points, drains, etc.

Those instructions necessary toperform the required inspectionsand apply the required treatmentsduring storage.

Those instructions necessary toremove the equipment from storageand prepare it for use.

Those instructions necessary to

prepare the equipment to be movedor flown to an overhaul/maintenancefacility.



MIL-


14 AIRCRAFTLOADINGANDOFF-LOADING

00 GENERAL

10 SUPPORTEQUIPMENT

20 CARGO

30 INTERNAL ANDEXTERNALSTORES

40 NONNUCLEARMUNITIONS

Supersedes page 32 ofMIL-sTD-1808 (U5AF)

-STD-1808(USAF)

DEFINITION

Shall contain those procedures andillustrations necessary to load andoff–load internal and external stores,munitions and cargo. Includes infor-mation on the equipment and specialtools required. Cross references shallbe made to the applicable systems forinformation on the aircraft attachmentpoints, pylons and carriers. Thissystem shall be used for reference.Actual procedures for loading and off-loading shall be included in applic-able cargo/munitions loading manuals.

A list of all support equipment andspecial tools, information andillustrations, as necessary, on thoseitems not covered in other manualsshall be included.

Examples of loading and off-loadingtechniques, interior layout, floorloadings, location and strength oflashing points, methods of stowing andsecuring, capacities and dimensions ofcompartments and doors shall beincluded.

A list of stores such as external fueltanks, reconnaissance pods, chaffdispensers, air/sea rescue equipment,etc. carried. Includes the carrier/adapter on which they are fitted.Data on the throttles of the ejectorrelease units shall be included.Loading and off-loading procedures andillustrations shall be included.

A list of nonnuclear munitions suchas rofkets, missiles, bombs,ammunition, etc, and the carrier/adapter on which they are mountedshall be included. Data on thethrottles of the ejector release

32,



MIL-STD-1808 (USAF)

18 WEAPONSINSTRUMENTATION

00 GENERAL

10thru90

DEFINITION

That information necessav toexplain and describe theinstrumentation used for test, dataacquisition and flight terminationof airborne weapons. Includesinstrumentation for testing weaponspayload, telemetry, etc.

Subsystems 10 thru 90 shall be usedto describe weapons instrumenta-tion. The manufacturer may assignthe subsystem numbers to suit therequired types of instrumentation.



MIL-STD-1808 (USAF)


19 TRAININGEQUIPMENT

00 GENERAL

10thru90


DEFINITION

Shall contain that unique equipmentrequired to support trainingsystems. Does not include aircraftcomponents, commercial suppOrt ortest equipment.

Subsystems 10 thru 90 shall be usedto describe either individualtrainers or groupings of trainers.The nianufacturer may assign thesubsystem numbers to suit therequired types of trainers.

38


MIL-STD-1808 (USAF)


33 LIGHTS

00 GENERAL

10 FLIGHT

DEFINITION

Those units and components whichprovide for external and internalillumination, such as landinglights, taxi lights, positionlights, rotating lights, icelights, master warning lights,passenger reading and cabin domelights, etc. Includes lightfixtures, switches and wiring. ,Shall not include warning lightsfor individual systems. Shall notinclude lamps/bulbs which arecovered in System 39, ELECTRICAL/ELECTRONIC COMPONENTSANEMULTIFUNCTION UNITS.

That Dortion of the svstem in theCOMPARTMENT/ compartment above the’floor andCOCKPIT between the forward passenger

partition and the forward pressuredome. Does not include cargocompartment. Includes direct andindirect illumination of workareas, panels and instruments.Includes the master warning lightsystem and the warning lightdimming systems where notintegrated with a central audio orvisual system under System 31-50.

20 PASSENGER That portion of the system in theCOMPARTMENTS areas in which the passengers are

seated and in buffet/galley,lavatories, lounges and coatrooms . Includes items such asdirect and indirect illumination,passenger call system, lightedsigns, etc.

NOTE : For those aircraft whicli do not contain passengercompartments, and the flight compartment(s) can bereasonably divided, subsystem 20 may be used to aid indefining such division.




MIL-STD-1808 (USAF)

I33 30 CARGO, SERVICE

COMPARTMENT SAND WEAPONSBAYS

40 EXTERIOR

50 ENERGENCYLIGHTING

Supersedes page 66 ofMIL-STD-1808 (USAF)

DEFINITION

That portion of the system in thecompartments for stowage ofcargo and the housing of variouscomponents, accessories or weapons.

That portion of the system usedprovide illumination outside ofaircraft. Includes lights suchlandina, navigation, Dosition

totheas

.<.indicating, w~ng illumination,rotat+ng, courtesy, taxi, etc.

That portion of the system usedDrovide illumination in case of

to

~rimary electrical power failure.Includes items such as inertiaflashlights, lanterns, etc.

66


MIL-STD-1808 (USAF)

~SYSTEM SYSTEM TITLE DEFINITION

45 NOTE : Subsystem Code is selected to match applicableI system interface. For example, 45-21-XX would identify

all Air Conditioning system monitoring and testingprovided by the CMS and would provide directions forusing the CMS to execute those maintenance functions.

I Detailed testing not capable of coverage in System 45would be appropriately cross referenced and would be

I provided in System 21. Similarly, 45-32-XX wouldidentify landing gear monitoring and testing provided

I by the CMS. 45-45-XX would identify the CMS itself.



MIL-STD-1808 (USAF)


46 SYSTEMINTEGRATIONAND DISPLAY

00 GENERAL

10 ACQUISITION

20 PROCESSING ANDINTEGRATION

30 DISPLAY

40 SYSTEMSthru INTEGRATION70 SOFTWARE

PACKAGES

REPRINTED WITHOUT CHANGE

DEFINITION

The primary aircraft system used toprovide central acquisition,processing and display of datafrom multiple sources, such asflight controls, navigationcomputation, air data computation,warnings, engine parameters, etc.

Those units and components used toacquire data for integration andprocessing. Excludes componentswhich are covered”by the applicablesystem.

Those units and components used tointegrate and process dataacquired from a variety of sourcesand output signals to displays orwarning devices. Includes itemssuch as interfaces, centralprocessing units, data buscontrols, e~c.

Those units which display data orprovide warn;ngs. Items includedare not related to specificsystems. Includes multifunctiondisplays, integrated control andwarning units, remote displays,etc.

These subsystems shall be used toprovide information about thosesoftware packages which are appli–cable to more than one system ofthe aircraft and can be classifiedas multisystem applicable software.This includes software for compu-ters which, in the event of failureof the computer(s) in” another sys-tem, assume management of that sys-tem.

84



MIL-STD-1808 (USAF)

47 LIQUID/GASEOUSNITROGEN

00 GENERAL

10 GENERATION/STORAGE

20 DISTRIBUTION

30 CONTROLLING

40 INDICATING

DEFINITION

Those units and components used togenerate, store, deliver andregulate liquid/gaseous nitrogen totwo or more using systems.Includes regulators, lines,manifolds, etc. Does not includeliquid nitrogen handling componentsof the using system.

That portion of the system whichgenerates andlor stores nitrogen.Includes tanks, cells, reservoirs,accumulators, etc. Shall notinclude plumbing, pumps, valves,controls, etc.

That portion of the system whichis used to distribute nitrogen tothe using systems. Includesplumbing, pumps, valves,regulators, etc.

The nitrogen controls which meterthe nitrogen to the distributioncomponents and into the usingsystems. Includes items such aslevers, switches, cables, etc.

That portion of the system whichis used to indicate the flow rate,temperature and pressure of thenitrogen. Includes items such astransmitters, indicators, etc.



SYSTEM~SYSTEM TITLE

COMMUNICATION/NAVIGATION/IDENTIFICATION(CNI )

00 GENERAL

10 ANTENNAS /APERTURES /ARRAYS

20 PROCESSING ANDINTEGRATION

30 CONTROLS/DISPLAYS


DEFINITION

Those units and components whichfurnish a means of ~ommunicatingwith{n the aircraft, between theaircraft and other aircraft,between the aircraft and groundstations, between’ the aircraft andground crew, navigating, andproviding emergency locationsignals. ~ncludes voice, datacontinuous wave communicatingcomponents, intercom, taperecorder-record player, andemergency s+gnal transmitters.This’ system shall be used when thecommunication, navigation andidentification systems areintegrated.

That portion of the system which isused for transmission and receptionof signals. Includes items such asantennas, apertures, arrays,antenna couplers, transmissionlines, etc.

That portion of the system which isused for navigation and emergencytransmission, communication withground crew, between aircraft,between flight crew personnel andwith ground stations. Includesitems such as enc~ption devices,decoders, processors, transmitters,receivers, amplifiers, powersupplies, recorders, etc.

That portion of the system whichprovides control and display of CNIfunctions. Includes items such asfunct?on selection devices, modeselection, signal’power levels,control panels, frequency controland’display, signal volume, etc.

86


MIL-STD-1808 (uSAF)


193 SURVEILLANCE

00 GENERAL

10 DATAPROCESSING

20 DATADISPLAY

30 RECORDING

40 IDENTIFICATION

50 INFRAREDSENSORS

60 LASERSENSORS

70 SURVEILLANCERADAR

80 MAGNETICSENSORS


DEFINITION

Those units and components whichfurnish a means of sensing thesurrounding environment andprocess, display and record theresulting information.

That portion of the system thatprovides computation, switchingand storage of signals acquired.

That portion of the system thatprovides the data display ofinformation acquired by sensors.

That portion of the system thatprovides the recording ofinformation acquired by sensors.

That portion of the system thatprovides identification ofinformation acquired by sensors.

That portion of the system thatuses heat sensing devices, suchas infrared scanners, infraredimage and detection to acquireinformation.

That portion of the system thatuses laser devices to acquireinformation for distance measuring,identification, etc.

That portion of the system thatuses radar for surveillance ormapping purposes. Includes devicessuch as antennas, receivers,transmitters, indicators, etc.

That portion of the system thatsenses magnetic anomalies.Includes devices such as

141


MIL-STD-1808 (USAF)


I 93 80 - Continued magnetometers, amplifiers,computers, indicators, etc.

90 SONAR That portion of the system thatSENSORS senses objects underwater. This

includes devices such asmodulators, computers, transducers, “’indicators, etc.



MIL-sTD-1808 (USAF)


94 WEAPON Those units and components whichSYSTEM furnish a means of acquiring a

target, performing releasecalculations based on ballistics,winds, air and ground speed,altitude, attitude, etc, andreleasing stores eitherautomatically or manually.

00 GENERAL

10 WEAPONSRELEASE

20 UNASSIGNED

30 WEAPONSSUSPENSION

40 UNASSIGNED

50 GUNNERY

60 UNASSIGNED

70 WEAPONSCONTROL


The weapon release system consistsof all equipment required torelease, fire and/or jettisonstores. Includes computers,displays, controls, storesmanagement, etc.

The weapons suspension systemprovides interconnecting equipmentto transport and release/fireweapons. Includes multipurposepylons if used for any weaponmounting role, special pylons,ejection racks, launchers, etc.

The gunnery system consists of allguns and equipment necessary tofire stores.

Those units and components whichfurnish a means of designating andacquiring a target. Includesradar, computers, displays, etc,necessary to provide weaponsrelea<e decision (aiming cues) .

143


MIL-STD-1808 (USAF)


95 CREWESCAPEANDSAFETY

Those units and components whichfurnish a means of ejecting orjettisoning personnel, capsulesor equipment from the airframe.

00

10

GENERAL

EJECTIONSEATS

That portion of the system which isused to eject flight crew orpassenger seats individually fromthe airframe.

That portion of the systeminvolving hatches and canopiesincluding rn$niature detonatingcord ! Does not include the canopyand it’s actuating mechanisms whichare covered in System 56, WINDOWSAND CANOPIES:

That portion of the system whichprovides a protective environment

20 ESCAPEHATCHESICANOPIES

30 CAPSULEEJECTION

for the flight crewseparation from the

afterairframe.

40

50

UNASSIGNED

GLOBALSURVIVALKITS

That portion of theinsures flight crew

system thatsurvivability

after unplanned separation and/o;landing.

60 IMPACTPROTECTIONANDFLOTATION

That portion of the systemproviding protection and/orflotation for personnel/equipmentafter impact.

70 CAPSULEFLIGHT

That portion of the system used tocontrol attitude and direction ofthe capsule or container afterejecting or jettisoning from theairframe.

Supersedes page 144 ofMIL-STD-1808 (USAF) 144


MIL-STD-1808 (USAF)

~SYSTEM sYSTEM TITLE

96 MISSILES,DRONESANDTELEMETRY

00 GENERAL

10 SURFACE TOSURFACEMISSILES

20 SURFACE TOAIR MISSILES

30 DRONES

40 TELEMETRY


DEFINITION

Those units and components whichfurnish a means of launching andcontrolling drones and groundlaunched missiles.

That portion of the system whichis used for launching andcontrolling surface to surfacemissiles.

That portion of the system whichis used for launching andcontrolling surface to airmissiles.

That portion of the system whichis used for launching andcontrolling drones.

That portion of the system whichis used for telemetry forapplications other than missile,drone or decoy usage.

145


MIL-STD-1808 (USAF)


97 IMAGERECORDING

00

10

20

30

40

50

GENERAL

STRIKE

OFFENSIVEWEAPONSSYSTEM

FIRECONTROLSYSTEM

INSTRUMENTA-TION SYSTEM

RANGESYSTEM


DEFINITION

Those units and components whichfurnish a means of recording onfilm, video, disc, tape, etc. Doesnot include recording systems whichare part of any other system.

That portion of the system which isused for recording the results ofan air strike.

That portion of the system which isused for recording instruments andthe dropping of bombs.

That portion of the system which isused for recording rockets andgunfire.

That portion of the system whichis used for recording meters,dials, displays, etc.

That portion of the system whichis u~ed for range recording.Includes installations such asforward and oblique recordingsystems.

146


MIL-sTD-1808 (USAF)


98 METEOROLOGICALANDATMOSPHERICRESEARCH

00 GENERAL

10 WEATHER

20 CLE+RAIRTURBULENCE

30 POLLUTANTS

40 MAGNETIC/GRAVITATIONAL


DEFINITION

Those units and components whichfurnish a means of providing andrecording measurement of natural orman–made atmospheric phenomena,gravitation and magnetic.

That portion of the system whichis used to measure and recordmoisture, temperature, cloudiness,wind, etc.

That portion of the system whichis used to detect, measure andrecord clear air turbulence.

That portion of the system whichis used to detect, measure andrecord contaminated particles.

That portion of the system whichis used to detect, measure andrecord the earth’s magnetic andgravitational force.

147



MIL-sTD-1808 (USAF)

199

00

10

20

30

ELECTRONICWARFARE

GENERAL

ACTIVE

PASSIVE

ELINT(ElectronicIntelligence)


DEFINITION

Those units and components whichfurnish a means of detecting,jamming or nullifying theeffectiveness of defensivedetection devices.

That portion of the systemconsisting of receivers,transmitters, repeaters, blankingand modulating devices, etc.

That portion of the system thatcontains no active elements. Forexample: chaff.

That portion of the systemconsisting of electronicintelligence systems, such asreceivers, monitors, recorders andanalysis devices.

148


i not measurement sensitive eeel -...

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