MIL-C-6781 Revision B:1960
|
CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED |
MIL-G-23081 Revision C:1972
|
GYROSCOPE INDICATOR SYSTEM VERTICAL. |
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL A 85670 : 0
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
AFGS-87213 Revision B:1993
|
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
MIL C 83166 : LATEST
|
CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
MIL-I-27674 Revision C:1994
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE MULTIFUNCTION, MINUS 5O DEG TO PLUS 2OO DEG C |
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
MIL-I-8580 Revision B:1965
|
INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
MIL-A-6271 Revision C:1976
|
ANTENNA, SUBSYSTEM FOR VHF AIRBORNE COMMUNICATION EQUIPMENT GENERAL SPECIFICATION FOR |
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
MIL-R-38370 Revision B:1972
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
MIL-T-38034 Revision E:1970
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
MIL-G-23083 Revision C:1972
|
GYROSCOPE, RATE SWITCHING MS 17399 |
MIL-A-26336 Base Document:1958
|
Antenna AT-840-ARC |
MIL-P-81655 Base Document:1970
|
PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
SAE AS 1145 : 2016
|
AIRCRAFT BRAKE TEMPERATURE MONITOR SYSTEMS (BTMS) |
MIL-E-23001 Revision B:1976
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-DTL-85670 Revision D:2012
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS-3793/A |
JSGS-87231 Revision A:1995
|
ENGINES, AIRCRAFT, TURBINE |
DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL A 5815 : E
|
ANTENNA, AIRBORNE, UHF - BAND GENERAL SPECIFICATION FOR |
MIL-T-83460 Base Document:1975
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
MIL I 7627 : F
|
INDICATOR, TURN AND SLIP 28V DC |
MIL A 87136 : NOTICE 1
|
ANTENNAS, AIRBORNE GENERAL SPECIFICATION FOR |
MIL-STD-2218 Base Document:1992
|
THERMAL DESIGN, ANALYSIS & TEST PROCEDURES FOR AIRBORNE ELECTRONIC EQUIPMENT |
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
MIL-A-85055 Base Document:1979
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL-A-22145 Revision C:1992
|
ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
SAE ARP 6001 : 2012
|
AEROSPACE - PASSIVE SIDE STICK UNIT, GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS |
MIL-M-49199 Revision A:1985
|
MICROPHONE, LINEAR M-162/AIC GENERAL SPECIFICATIONS FOR |
MIL-T-5483 Revision D:1964
|
TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
MIL-T-38473 Revision A:1972
|
TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
MIL A 18357 : 0
|
ANTENNA AT-145B/A |
MIL E 85726 : A
|
ENCLOSURE, STANDARD AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
MIL-I-8691 Revision A:1955
|
INDICATOR, AZIMUTH, ID 307/ARN [ASG] |
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
MIL-I-29589 Base Document:1991
|
INTERROGATOR SET, AN/UPX-24(V) |
MIL S 25879 : C
|
SWITCH, RADIO FREQUENCY TRANSMISSION LINE SA-521A/A |
MIL-T-21208 Base Document:1958
|
TEST SET, RADIO AN/ARM-32 |
MIL-A-23595 Revision D:1995
|
AMPLIFIER, AUDIO FREQUENCY |
MIL-STD-2124 Revision A:1984
|
FLIGHT INCIDENT RECORDER/CRASH POSITION LOCATOR, MINIMUM PERFORMANCE STANDARDS FOR |
MIL-T-85350 Revision B:1990
|
TRANSMITTER, BEACON, LOCATOR T-1438/D |
MIL-S-38160 Revision B:1968
|
Selector, Antenna C-4808/ARC |
MIL-C-7135 Revision F:1967
|
Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
MIL-A-83162 Revision A:1989
|
AMPLIFIER, SYNCHRO, SIGNAL AM-6015/A |
MIL-I-81186 Base Document:1966
|
INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360 |
MIL-R-81046 Base Document:1964
|
RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
MIL-C-23697 Base Document:1963
|
COMPUTER SET, NAVIGATIONAL AN/ASN-42(*) |
MIL BULL 400 : 0
|
AIRBORNE ELECTRONIC AND ASSOCIATED EQUIPMENT, APPLICABLE DOCUMENTS |
MIL S 81746 : 0
|
SERVTORQ, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
MIL-T-22067 Base Document:1959
|
TEST KIT, MK-91(*)/APM-66 |
MIL-D-8684 Revision B:1959
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
MIL-I-38338 Revision D:1991
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
MIL D 87213 : 0
|
DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-A-81371 Base Document:1970
|
ASSEMBLY, STATION TRANSFER 65A132F7 |
MIL-C-23367 Base Document:1963
|
COMPUTER, FLIGHT DIRECTOR, AIRCRAFT |
DSCC 89112 : B
|
POWER DIVIDER, 4-WAY, 0 DEGREE, CONNECTORS |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/17(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/15(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/16(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-18793 Revision B:2011
|
ANTENNA AS-333/AP |
MIL F 9490 : D
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-85521 Base Document:1983
|
CONCENTRATOR, OXYGEN, GGU-7/A |
ISA 37.8 : 1982
|
SPECIFICATIONS AND TESTS FOR STRAIN GAGE FORCE TRANSDUCERS |
MIL A 7291 : A
|
ANTENNA AT-191B/AP |
MIL-E-29581 Base Document:1991
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM |
MIL-G-19053 Revision C:1957
|
GAGE - AIRCRAFT, CAPACITANCE, LIQUID OXYGEN CONVERTER, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL-B-25084 Base Document:1955
|
BEACON, RADIO AN-APN 69 |
MIL C 87104 : 0
|
COAXIAL ASSEMBLIES, GENERAL SPECIFICATION FOR |
MIL I 38120 : A (3)
|
INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
MIL-J-23013 Base Document:1961
|
JUNCTION BOX JEU-25 (*)/A |
DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
MIL-R-38435 Revision B:1968
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
MIL STD 1763 : A
|
AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL-A-81621 Base Document:1969
|
ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
MIL-A-81918 Base Document:1976
|
ADAPTER, LAUNCHER, AIRCRAFT, ADU-299A/A |
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
MIL-I-85671 Base Document:1987
|
INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
MIL-D-81358 Revision B:1970
|
DISPLAY GROUP, TACTICAL DATA AN/ASA-66 |
MIL-T-23733 Revision A:1968
|
TRANSMITTER, RATE GYROSCOPE T-751 (/AJB-3) |
MIL-T-63534 Base Document:1981
|
TURRET SUBSYSTEM, UNIVERSAL, (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, TURRET CONTROL UNIT FOR |
MIL-DTL-25895 Revision A:2007
|
ANTENNA AT-505/AP |
MIL H 83511 : 0
|
HEADSET-MICROPHONE AND HEADSET-ELECTRICAL (MEDIUM NOISE ATTENUATION, HEARING PROTECTIVE), GENERAL SPECIFICATIONS FOR |
MIL-A-23670 Revision A:1965
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
MIL-T-19576 Revision A:1961
|
TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED) |
MIL-A-81258 Base Document:1965
|
AMPLIFIER, RESOLVER, GENERAL SPECIFICATION FOR |
MIL-C-17858 Revision C:1966
|
COMPASS SYSTEM, MAGNETIC SLAVED, DIRECTIONAL GYRO STABILIZED, 4 DEG/HR TYPE MA-1 |
MIL-J-5251 Revision A:1952
|
JACK U-82/U |
MIL-C-22764 Revision C:1964
|
CODER RECEIVER TRANSMITTER K & Y532A ASQ |
MIL-A-25546 Revision C:1970
|
Amplifier, Audio Frequency AM-944/AIC-13 |
MIL-S-85377 Revision A:1983
|
SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
MIL-M-81850 Revision A:1974
|
MAGNETIC TAPE TRANSPORT RD-319/AYA-8 |
MIL E 18239 : D
|
EARPHONE H-87B/U |
MIL-P-83927 Revision B:1981
|
POWER SUPPLIES, GUIDED MISSILE LAUNCHERS, SINGLE TYPES PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, AND COMPOSITE TYPE PP-4506/A AND PS-1037 |
MIL-A-85652 Base Document:1984
|
AMPLIFIER-MIXER AM-7157/DKT-59 |
MIL A 18793 : 0
|
ANTENNA AS-333/AP |
MIL C 22442 : D
|
CABLE ASSEMBLIES, RADIO FREQUENCY (AIRCRAFT AUDIO), GENERAL SPECIFICATION FOR |
MIL-A-85648 Base Document:1983
|
AMPLIFIER, TRAVELING WAVE TUBE |
MIL A 55359 : 0
|
ANTENNA AS-1304 ( ) /ARN-30 |
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
MIL-D-8685 Revision B:1967
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
DSCC 87065 : C#CAN
|
SWITCH (COAXIAL L-BAND) RF TRANSMISSION LINE (1P2T REMOTE) FAILSAFE |
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-R-81876 Revision B:1988
|
RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
DEFSTAN 00-69(PT2)/1(1998) : 1998
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL-S-8812 Revision D:1975
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
SAE AIR 5271 : 2009
|
A GUIDELINE FOR APPLICATION OF HIGH-DENSITY FIBER OPTIC INTERCONNECTS TO AEROSPACE PLATFORMS |
MIL-HDBK-231 Revision A:1991
|
ENCODERS SHAFT ANGLE TO DIGITAL |
ISA 37.6 : 1982
|
SPECIFICATIONS AND TESTS FOR POTENTIOMETRIC PRESSURE TRANSDUCERS |
MIL-PRF-55359 Revision A:1997
|
ANTENNA AS-1304()/ARN-30 |
MIL-H-15362 Revision B:1958
|
HARNESSES, TEST BENCH, AVIONIC EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-R-21073 Revision A:1960
|
RECORDER, MAGNETIC DISTORTION, RO-32/ASQ |
MIL-I-81454 Base Document:1967
|
INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL A 25895 : 0
|
ANTENNA AT-505/AP |
MIL-G-8798 Base Document:1956
|
GAGE SYSTEM, FUEL QUANTITY, CAPACITOR TYPE NONVACUUM TUBE, INTEGRALLY LIGHTED GENERAL SPECIFICATION FOR |
MIL-S-23535 Base Document:1963
|
SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION |
MIL-I-21203 Revision A:1962
|
INDICATOR, ATTITUDE, SPHERICAL, DIRECT READING, FAST ERECTING, ELECTRIC GYRO |
MIL F 26685 : B NOTICE 1
|
FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
MIL-STD-35-108 Revision A:1993
|
AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM TRANSMITTERS |
MIL-A-19940 Base Document:1957
|
AMPLIFIER, CONTROL SINGLE CHANNEL, S-2 COMPASS |
MIL-G-22169 Base Document:1959
|
GYRO, VERTICAL AND MOUNT |
MIL-A-23887 Revision A:1965
|
ALTIMETER SET, ELECTRONIC AN/APN-141 (V) |
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-85518 Base Document:1984
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
MIL-M-85522 Revision A:1991
|
MONITOR, OXYGEN CRU-91/A |
MIL-M-22179 Base Document:1961
|
MICROPHONE, DYNAMIC M 96 |
MIL-I-27304 Revision E:1977
|
INDICATOR, RATE OF FLOW |
MIL-R-87245 Base Document:1986
|
RADIO COMMUNICATION SYSTEM, AIRBORNE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA: ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-D-23222 Revision A:1971
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
MIL-STD-1378 Revision E:1989
|
REQUIREMENTS FOR EMPLOYING STANDARD ELECTRONIC MODULES |
MIL C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
MIL-I-8673 Base Document:1955
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
MIL-A-81359 Base Document:1970
|
AIRCRAFT WEAPONS RELEASE SET AN/AWE-1 |
MIL-M-21734 Revision C:1971
|
MICROPHONE, DYNAMIC, OXYGEN MASK M-94B/A |
MIL-T-81760 Revision A:1970
|
TEST SET, PROGRAMMER AN/USM-299A |
MIL-D-81641 Base Document:1972
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
MIL I 85581 : 0
|
INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
MIL-HDBK-338 Revision B:1998
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
MIL-HDBK-2124 Base Document:2000
|
FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
MIL-A-81852 Revision A:1986
|
ALTIMETER-ENCODER AAU-32/A |
MIL-I-22075 Revision C:1984
|
Indicator, Bearing-Distance-Heading ID-663D/U |
MIL-H-49225 Base Document:1980
|
HEADSET MICROPHONE KIT MK-896A/AIC (COMPONENTS OF) |
MIL-F-25562 Revision B:1964
|
FILTER, RADIO INTERFERENCE F AND 245-APX AND 25 |
MIL-I-85832 Base Document:1989
|
INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
MIL-T-85530 Base Document:1982
|
TEST SET, TOW TARGET, A/E24T-143 |
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-85248 Revision A:1984
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
MIL S 0081619 : C
|
SWITCH, SOLID STATE TRANSDUCER, (ANALOG AND DIGITAL) GENERAL SPECIFICATION FOR |
MIL STD 2096 : A NOTICE 1
|
MICROCIRCUIT DATA REQUIREMENTS |
MIL-A-81369 Base Document:1970
|
ASSEMBLY, LEFT-RIGHT STATION 65A132F5 |
MIL-P-83763 Base Document:1969
|
POWER SUPPLY, TRANSISTORIZED |
MIL-A-6224 Revision E:1976
|
ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR |
MIL-R-24011 Revision A:1965
|
RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
MIL-C-18277 Revision B:1961
|
COUPLER, ANTENNA CU-351/AR AND COUPLER, ANTENNA CU-509/AR |
MIL H 49198 : A
|
HEADSET-MICROPHONE KIT, MK-1564( )/AIC |
MIL T 25439 : A (1)
|
TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
DSCC 81022 : D
|
FILTER, LINE, 400 HERTZ |
MIL C 81125 : NOTICE 1
|
COUPLER, ANTENNA CU-1304 (*)/ARC AND MOUNTING MT-3261 (*)/ARC |
MIL-A-22424 Revision A:1967
|
ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
MIL-B-38401 Revision A:1973
|
BEACON SET, RADIO AN/URT-33 |
MIL-A-81851 Revision B:1986
|
ALTIMETER AAU-31/A |
MIL-I-8700 Revision A:1970
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-A-27328 Base Document:1960
|
AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-7 |
MIL-I-5482 Revision C:1960
|
INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE |
MIL-A-25487 Revision B:1987
|
ANTENNA AT-172()/ARN-14 |
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
MIL-A-22212 Base Document:1959
|
ANTENNAS, AT-500(*)/AP AND AT-929(*)/AP; AND ANTENNA BASE AB-117(*)/AP |
MIL-DTL-9490 Revision E:2008
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
NASA MSFC SPEC 250 : 1963
|
PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-G-81665 Base Document:1971
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
MIL-I-18804 Revision B:1964
|
INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
MIL-A-5999 Revision B:1973
|
ANTENNA SUBSYSTEM FOR AIRCRAFT MARKER BEACON EQUIPMENT GENERAL SPECIFICATION FOR |
MIL-G-26988 Revision C:1971
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
MIL-A-7292 Revision A:1952
|
ANTENNA AT-190B/AP |
MIL-A-25081 Base Document:1955
|
AMPLIFIER, ELECTRONIC CONTROL, 2 CHANNEL, APPROACH AND NAVIGATIONAL, TYPE MB-4 |
MIL-B-19906 Revision A:1961
|
BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
MIL-M-5793 Revision A:1954
|
MICROPHONE M-3A/A |
MIL-I-26689 Revision C:1981
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
MIL-T-81587 Revision A:1971
|
TIMER ASSEMBLY RAIN REPELLENT |
MIL-A-25367 Revision B:1988
|
ANTENNA AT-536/ARN |
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
MIL-C-26485 Revision D:1968
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
MIL-R-23761 Revision B:1975
|
Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
MIL-I-22126 Revision B:1972
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
MIL-N-49098 Revision A:1990
|
NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
MIL-I-23366 Revision B:1987
|
INDICATOR, HORIZONTAL SITUATION ID-1O13(*)/A |
MIL A 25088 : C
|
|
MIL-C-19941 Revision A:1966
|
CONTROLLER, S-2 COMPASS, TYPE |
MIL-DTL-7627 Revision G:2010
|
INDICATOR, TURN AND SLIP, 28 V DC |
MIL-I-81453 Revision A:1977
|
INTERROGATOR SET AN APX 76B(V) |
MIL-H-27269 Revision A:1977
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
MIL-G-23723 Base Document:1964
|
GYROSCOPE, RATE SWITCHING CN-495/AJB-3 |
MIL-H-27186 Base Document:1959
|
HEADSET-MICROPHONE, SOUND POWERED H-159/GIC-1O |
MIL-STD-2164 Base Document:1985
|
ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
DOD-HDBK-791 Base Document:1988
|
MAINTAINABILITY DESIGN TECHNIQUES |
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
MIL G 23701 : 0
|
MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
MIL S 38039 : B
|
SYSTEM, ILLUMINATED, WARNING, CAUTION, AND ADVISORY, GENERAL SPECIFICATION FOR |
MIL-V-85830 Base Document:1989
|
VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
MIL A 9331 : A
|
ANTENNA AT-440A/U |
MIL-D-8181 Revision B:1965
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
MIL T 18497 : 0
|
TEST SET, RADIO AN/ARM-25 |
MIL M 21393 : A
|
MICROPHONE, DYNAMIC M-92C/U |
MIL-T-5422 Revision F:1971
|
TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT |
MIL-I-27665 Revision B:1984
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
MIL-W-17247 Revision B:1974
|
WIND MEASURING SET AN/UMQ-5 (COMPONENTS OF) |
MIL-I-8671 Revision D:1994
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
MIL-F-23447 Base Document:1962
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
MIL-A-6348 Revision D:1956
|
AMPLIFIER AM-203/ARA-19 |
MIL-M-22001 Base Document:1959
|
MICROPHONE, CARBON, OXYGEN MASK, ANB-M-C1 |
MIL-HDBK-1763 Base Document:1998
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
MIL-T-18232 Revision B:1968
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
MIL-A-81307 Base Document:1965
|
AMPLIFIER, SERVOMOTOR GENERAL SPECIFICATION |
MIL-A-38187 Revision A:1972
|
ANTENNA AT-983/ARN AND ANTENNA AT-983A/ARN |
ISA 37.3 : 1982
|
SPECIFICATIONS AND TESTS FOR STRAIN GAGE PRESSURE TRANSDUCERS |
MIL-I-27247 Revision C:1985
|
INDICATOR, TEMPERATURE, SYNCHRO |
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
MIL-D-7106 Revision C:1987
|
DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
MIL-A-22165 Base Document:1959
|
AMPLIFIER, COMPASS, SERVO (TYPE MF-1 COMPASS) |
MIL G 83163 : 0
|
GYRO, DIRECTIONAL CN-1251/ASN-89(V) |
MIL S 21317 : 0
|
SIMULATOR, ATTITUDE SM-111/APS-67 |
MIL I 7491 : B
|
INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
MIL-A-81403 Base Document:1967
|
ALTIMETER-ENCODER, AAU-21/A |
MIL-N-81207 Revision A:1973
|
NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
MIL-I-81400 Base Document:1966
|
INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-D-19326 Revision H:1990
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-STD-1512 Base Document:1972
|
ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
MIL A 87211 : NOTICE 1
|
AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
MIL-R-81498 Revision C:1979
|
RECEIVING-DECODING GROUP AN/ARA-63 |
MIL-A-81372 Base Document:1970
|
ASSEMBLY, PRIORITY LOGIC 65A132F8 |
SAE ARP 4729 : 2017
|
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
MIL-I-25479 Revision A:1987
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
MIL-I-27552 Revision C:1995
|
INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED |
MIL-S-21277 Revision A:1958
|
SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
MIL A 83366 : 0
|
ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
MIL-D-81357 Revision A:1970
|
DISPLAY GROUP, TACTICAL DATA AN ASA 70 |
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-R-29583 Base Document:1992
|
RADIO SET |
MIL S 8932 : A
|
SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-H-58108 Base Document:1986
|
HEADSET-MICROPHONE KIT MK-2193/AIC |
MIL-A-85505 Base Document:1983
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
MIL-A-27670 Revision D:1994
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
MIL-A-83212 Revision A:1976
|
ALTIMETER, PRESSURE AAU-27/A |
MIL-A-85672 Base Document:1987
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
MIL-A-81605 Revision D:1984
|
ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
MIL-A-19939 Revision A:1966
|
AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
MIL-W-87105 Base Document:1977
|
WAVEGUIDE ASSEMBLIES, GENERAL SPECIFICATION FOR |
MIL-I-27680 Revision C:1973
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
MIL-I-83262 Revision B:1977
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-A-81370 Base Document:1970
|
ASSEMBLY, CENTER STATION 65A132F6 |
SAE AS 22145 : 2012
|
ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL-D-18300 Revision H:1993
|
DESIGN EXAMINATIONS, ENGINEERING AVIONIC SYSTEMS/EQUIPMENT GENERAL REQUIREMENTS FOR |
MIL T 25502 : C
|
TRUE HEADING COMPUTER GROUP AN/AJA-I |
MIL-D-8708 Revision C:1991
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-C-25601 Revision C:1969
|
COUPLER, ANTENNA CU-308D/U |
MIL-I-27623 Revision C:1972
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-T-85678 Base Document:1974
|
TRANSPONDER, RADAR TRACKING |
MIL-A-81296 Revision D:1985
|
ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
MIL-I-83117 Revision B:1975
|
INDICATOR, ANGLE OF ATTACK |
MIL A 7965 : C SUPP 1
|
ANTENNA COMPONENTS, ANTIPRECIPITATION STATIC |
MIL C 26518 : B
|
CONNECTOR, ELECTRICAL, MINIATURE, RACK AND PANEL, ENVIRONMENT RESISTING, 2OO DEGREES C AMBIENT TEMPERATURE |
MIL T 18460 : 0
|
TEST SET, INDICATOR, AN/APM-74 |
MIL-C-87970 Base Document:1982
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
MIL-G-27693 Revision A:1962
|
GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
MIL-I-25645 Revision D:1970
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
MIL-L-85314 Revision A:1983
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
MIL-I-27848 Revision B:1994
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
MIL-A-81423 Base Document:1966
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-73 |
MIL-G-25591 Revision E:1981
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
MIL-A-27671 Revision B:1965
|
AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
MIL-I-38258 Base Document:1965
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
MIL-E-81512 Base Document:1968
|
ENCODER, SHAFT POSITION TO DIGITAL, CONTACT TYPE, ALTITUDE REPORTING, GENERAL SPECIFICATION FOR |
MIL-I-27619 Revision G:1974
|
INDICATORS, ATTITUDE DIRECTOR |
MIL-HDBK-246 Revision A:1982
|
PROGRAM MANAGERS GUIDE FOR THE STANDARD ELECTRONIC MODULES PROGRAM |
MIL-I-8672 Revision B:1969
|
INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
MIL-C-85392 Base Document:1987
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
MIL G 21480 : A
|
GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
MIL-T-25307 Revision D:1985
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
MIL-A-55368 Base Document:1972
|
AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
MIL-A-9286 Revision C:1969
|
AF AMPLIFIER AM-476()/AIC-10 |
MIL C 18266 : A
|
CORD, P/O 87B/U |
MIL-I-27667 Revision C:1990
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
MIL-I-23524 Revision A:1986
|
INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
DOD-C-85050 Base Document:1982
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-C-81883 Base Document:1976
|
CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
MIL-I-26299 Revision G:1990
|
INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
MIL-I-7802 Revision A:1967
|
INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
MIL-A-81373 Base Document:1970
|
ASSEMBLY, QUANTITY SELECT 65A132F9 |
MIL-I-81049 Revision A:1972
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
MIL C 38333 : 0
|
CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
MIL B 83771 : A
|
BATTERY, REMOTELY ACTIVATED SUBMINIATURE RESERVE PRIMARY |
SAE ARD 50020 : A2003
|
FIBER-OPTIC INTERCONNECTION HARDWARE FOR AEROSPACE APPLICATIONS |
MIL M 23888 : NOTICE 1
|
MONITOR, RADIO FREQUENCY ID AND 9O2A/AR |
MIL R 85725 : 0
|
RACK, INTEGRATED AVIONICS, FORCED AIR COOLED, GENERAL SPECIFICATION FOR |
MIL-R-23864 Revision B:1972
|
RADAR TRANSPONDER AN/DPN-77(*) |
MIL-C-85373 Revision A:1987
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A |
MIL-F-25880 Revision B:1972
|
FILTER, BAND PASS, BAND SUPPRESSION F -339/A |
MIL-I-25992 Revision A:1959
|
INDICATOR, BEARING DISTANCE HEADING ID 526A ARN |
MIL-T-23103 Revision A:1971
|
THERMAL PERFORMANCE EVALUATION, AIRBORNE ELECTRONIC EQUIPMENT AND SYSTEMS, GENERAL REQUIREMENTS FOR |
MIL-A-85434 Revision A:1983
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
MIL-P-85576 Revision B:1987
|
POWER SUPPLY PP-2581C/A |
MIL-DTL-27193 Revision D:2017
|
INDICATOR, ATTITUDE ARU-2B/A |
MIL-A-9080 Base Document:1954
|
ANTENNA, LIAISON COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF |
MIL-D-5025 Revision C:1961
|
DIRECTION FINDER GROUPS AN/APA-69A AND AN/APA 69C |
MIL-C-18244 Revision A:1962
|
CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-P-18987 Revision A:1962
|
PLOTTING BOARD, TACTICAL DISPLAY PT-396/AS |
MIL-P-19461 Revision A:1959
|
PLOTTING BOARD, TACTICAL DISPLAY, PT-429/A |
MIL-C-81452 Revision B:1972
|
CABLE ASSEMBLY W-1 OF AN/AQS-13 |
SAE AIR 4922A : 2015
|
PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION |