MIL E 5400 : T
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Withdrawn date
31-01-2024
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.NO CONTENTS SECTION
Describes airborne electronic equipment for piloted aircraft. Coverage includes classification, applicable documents, relays, resistors, tapped resistor, soldering, mechanical assemblies, springs, switches, materials, terminals, mounting, toggle switches, semiconductor devices, bearings, adhesives, electrical filter, mechanised production, and circuit approval. Also gives diagrams and tables.
| Committee |
AREA GDRQ
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| DevelopmentNote |
INACTIVE FOR NEW DESIGN
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| DocumentType |
Standard
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| Pages |
87
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Withdrawn
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| 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 Specification 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 HEADING 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 KY-532A/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-1013(*)/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 | Amplifiers, 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 Group 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 |
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