|
MIL C 6781 : B
|
CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED |
|
MIL G 23081 : C
|
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 : C
|
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 : B
|
INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
|
MIL A 6271 : C
|
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 : E
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
MIL G 23083 : C
|
GYROSCOPE, RATE SWITCHING MS 17399 |
|
MIL A 26336 : 0
|
ANTENNA AT-84O/ARC |
|
MIL P 81655 : 0
|
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 : D
|
ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS-3793/A |
|
JSGS 87231 : A
|
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 : 0
|
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 : 0
|
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 : 0
|
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 : C
|
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 : A
|
MICROPHONE, LINEAR M-162/AIC GENERAL SPECIFICATIONS FOR |
|
MIL T 5483 : D
|
TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
|
MIL T 38473 : A
|
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 : A
|
INDICATOR, AZIMUTH, ID 307/ARN [ASG] |
|
MIL G 25597 : D
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
|
MIL I 29589 : 0
|
INTERROGATOR SET, AN/UPX-24(V) |
|
MIL S 25879 : C
|
SWITCH, RADIO FREQUENCY TRANSMISSION LINE SA-521A/A |
|
MIL T 21208 : 0
|
TEST SET, RADIO AN/ARM-32 |
|
MIL A 23595 : D
|
AMPLIFIER, AUDIO FREQUENCY |
|
MIL STD 2124 : A
|
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 : B
|
SELECTOR, ANTENNA C 4808 ARC |
|
MIL C 7135 : F
|
COMPRESSOR, PNEUMATIC, 3000 PSI 2 SCFM AERO 2A AERO 2A-1 AERO 2B AND AERO 2B-1 |
|
MIL A 83162 : A
|
AMPLIFIER, SYNCHRO, SIGNAL AM-6015/A |
|
MIL I 81186 : 0
|
INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360 |
|
MIL R 81046 : 0
|
RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
|
MIL C 23697 : 0
|
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 : 0
|
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 : D
|
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 : 0
|
ASSEMBLY, STATION TRANSFER 65A132F7 |
|
MIL C 23367 : 0
|
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 C 85521 : 0
|
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 : 0
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM |
|
MIL G 19053 : C
|
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 : 0
|
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 : 0
|
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 : 0
|
ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
|
MIL A 81918 : 0
|
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 : 0
|
INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
|
MIL D 81358 : B
|
DISPLAY GROUP, TACTICAL DATA AN/ASA-66 |
|
MIL T 23733 : A
|
TRANSMITTER, RATE GYROSCOPE T-751 (/AJB-3) |
|
MIL T 63534 : 0
|
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 : A
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
|
MIL T 19576 : A
|
TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED) |
|
MIL A 81258 : 0
|
AMPLIFIER, RESOLVER, GENERAL SPECIFICATION FOR |
|
MIL C 17858 : C
|
COMPASS SYSTEM, MAGNETIC SLAVED, DIRECTIONAL GYRO STABILIZED, 4 DEG/HR TYPE MA-1 |
|
MIL J 5251 : A
|
JACK U-82/U |
|
MIL C 22764 : C
|
CODER RECEIVER TRANSMITTER K & Y532A ASQ |
|
MIL A 25546 : C
|
AMPLIFIER, AUDIO FREQUENCY, AM944/AIC-L 3 |
|
MIL S 85377 : A
|
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 : B
|
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 : 0
|
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 : 0
|
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 : B
|
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 : D
|
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 : A
|
ENCODERS SHAFT ANGLE TO DIGITAL |
|
ISA 37.6 : 1982
|
SPECIFICATIONS AND TESTS FOR POTENTIOMETRIC PRESSURE TRANSDUCERS |
|
MIL PRF 55359 : A
|
ANTENNA AS-1304()/ARN-30 |
|
MIL H 15362 : B
|
HARNESSES, TEST BENCH, AVIONIC EQUIPMENT GENERAL SPECIFICATION FOR |
|
MIL R 21073 : A
|
RECORDER, MAGNETIC DISTORTION, RO-32/ASQ |
|
MIL I 81454 : 0
|
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 : 0
|
GAGE SYSTEM, FUEL QUANTITY, CAPACITOR TYPE NONVACUUM TUBE, INTEGRALLY LIGHTED GENERAL SPECIFICATION FOR |
|
MIL S 23535 : 0
|
SYSTEM, INTEGRATED FLIGHT INSTRUMENTATION |
|
MIL I 21203 : A
|
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 : A
|
AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM TRANSMITTERS |
|
MIL A 19940 : 0
|
AMPLIFIER, CONTROL SINGLE CHANNEL, S-2 COMPASS |
|
MIL G 22169 : 0
|
GYRO, VERTICAL AND MOUNT |
|
MIL A 23887 : A
|
ALTIMETER SET, ELECTRONIC AN/APN-141 (V) |
|
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 85518 : 0
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
|
MIL M 85522 : A
|
MONITOR, OXYGEN CRU-91/A |
|
MIL M 22179 : 0
|
MICROPHONE, DYNAMIC M 96 |
|
MIL I 27304 : E
|
INDICATOR, RATE OF FLOW |
|
MIL R 87245 : 0
|
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 : A
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
|
MIL STD 1378 : E
|
REQUIREMENTS FOR EMPLOYING STANDARD ELECTRONIC MODULES |
|
MIL C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
|
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
|
MIL A 81359 : 0
|
AIRCRAFT WEAPONS RELEASE SET AN/AWE-1 |
|
MIL M 21734 : C
|
MICROPHONE, DYNAMIC, OXYGEN MASK M-94B/A |
|
MIL-T-81760 Revision A:1970
|
TEST SET, PROGRAMMER AN/USM-299A |
|
MIL D 81641 : 0
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
|
MIL I 85581 : 0
|
INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
|
MIL HDBK 338 : B
|
ELECTRONIC RELIABILITY DESIGN HANDBOOK |
|
MIL HDBK 2124 : 0
|
FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
|
MIL A 81852 : A
|
ALTIMETER-ENCODER AAU-32/A |
|
MIL I 22075 : C
|
INDICATOR, BEARING DISTANCE-HEADING; ID - 663D/U |
|
MIL H 49225 : 0
|
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 : 0
|
INTERCOM, HELICOPTER AIRCREWMAN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE SET |
|
MIL T 85530 : 0
|
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 : 0
|
ASSEMBLY, LEFT-RIGHT STATION 65A132F5 |
|
MIL P 83763 : 0
|
POWER SUPPLY, TRANSISTORIZED |
|
MIL A 6224 : E
|
ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR |
|
MIL R 24011 : A
|
RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
|
MIL C 18277 : B
|
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 : A
|
ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
|
MIL B 38401 : A
|
BEACON SET, RADIO AN/URT-33 |
|
MIL A 81851 : B
|
ALTIMETER AAU-31/A |
|
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL A 27328 : 0
|
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 : B
|
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 : 0
|
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 : 0
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
|
MIL I 18804 : B
|
INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
|
MIL A 5999 : B
|
ANTENNA SUBSYSTEM FOR AIRCRAFT MARKER BEACON EQUIPMENT GENERAL SPECIFICATION FOR |
|
MIL G 26988 : C
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MIL A 7292 : A
|
ANTENNA AT-190B/AP |
|
MIL A 25081 : 0
|
AMPLIFIER, ELECTRONIC CONTROL, 2 CHANNEL, APPROACH AND NAVIGATIONAL, TYPE MB-4 |
|
MIL B 19906 : A
|
BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
|
MIL M 5793 : A
|
MICROPHONE M-3A/A |
|
MIL I 26689 : C
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
|
MIL T 81587 : A
|
TIMER ASSEMBLY RAIN REPELLENT |
|
MIL A 25367 : B
|
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 : D
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
|
MIL R 23761 : B
|
REGULATORS, VOLTAGE, AND CONTROL PANELS AIRCRAFT DIRECT CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
|
MIL I 22126 : B
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
|
MIL-N-49098 Revision A:1990
|
NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
|
MIL I 23366 : B
|
INDICATOR, HORIZONTAL SITUATION ID-1O13(*)/A |
|
MIL A 25088 : C
|
|
|
MIL C 19941 : A
|
CONTROLLER, S-2 COMPASS, TYPE |
|
MIL-DTL-7627 Revision G:2010
|
INDICATOR, TURN AND SLIP, 28 V DC |
|
MIL I 81453 : A
|
INTERROGATOR SET AN APX 76B(V) |
|
MIL H 27269 : A
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
|
MIL G 23723 : 0
|
GYROSCOPE, RATE SWITCHING CN-495/AJB-3 |
|
MIL H 27186 : 0
|
HEADSET-MICROPHONE, SOUND POWERED H-159/GIC-1O |
|
MIL STD 2164 : 0
|
ENVIRONMENTAL STRESS SCREENING PROCESS FOR ELECTRONIC EQUIPMENT |
|
DOD HDBK 791 : 0
|
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 : 0
|
VENTILATOR, TACTICAL, HELICOPTER AIRCREWMEN, CHEMICAL, BIOLOGICAL, RADIOLOGICAL PROTECTIVE |
|
MIL A 9331 : A
|
ANTENNA AT-440A/U |
|
MIL D 8181 : B
|
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 : F
|
TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT |
|
MIL I 27665 : B
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C |
|
MIL W 17247 : B
|
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 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
|
MIL A 6348 : D
|
AMPLIFIER AM-203/ARA-19 |
|
MIL M 22001 : 0
|
MICROPHONE, CARBON, OXYGEN MASK, ANB-M-C1 |
|
MIL HDBK 1763 : 0
|
AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
|
MIL T 18232 : B
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
|
MIL A 81307 : 0
|
AMPLIFIER, SERVOMOTOR GENERAL SPECIFICATION |
|
MIL A 38187 : A
|
ANTENNA AT-983/ARN AND ANTENNA AT-983A/ARN |
|
ISA 37.3 : 1982
|
SPECIFICATIONS AND TESTS FOR STRAIN GAGE PRESSURE TRANSDUCERS |
|
MIL I 27247 : C
|
INDICATOR, TEMPERATURE, SYNCHRO |
|
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL D 7106 : C
|
DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
|
MIL A 22165 : 0
|
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 : 0
|
ALTIMETER-ENCODER, AAU-21/A |
|
MIL N 81207 : A
|
NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
|
MIL I 81400 : 0
|
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 : 0
|
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 : C
|
RECEIVING-DECODING GROUP AN/ARA-63 |
|
MIL A 81372 : 0
|
ASSEMBLY, PRIORITY LOGIC 65A132F8 |
|
SAE ARP 4729 : 2017
|
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
|
MIL I 25479 : A
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
|
MIL I 27552 : C
|
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 : A
|
DISPLAY GROUP, TACTICAL DATA AN ASA 70 |
|
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
|
MIL R 29583 : 0
|
RADIO SET |
|
MIL S 8932 : A
|
SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL H 58108 : 0
|
HEADSET-MICROPHONE KIT MK-2193/AIC |
|
MIL A 85505 : 0
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
|
MIL A 27670 : D
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
|
MIL A 83212 : A
|
ALTIMETER, PRESSURE AAU-27/A |
|
MIL A 85672 : 0
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
|
MIL A 81605 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
|
MIL A 19939 : A
|
AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
|
MIL W 87105 : 0
|
WAVEGUIDE ASSEMBLIES, GENERAL SPECIFICATION FOR |
|
MIL I 27680 : C
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
|
MIL I 83262 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL A 81370 : 0
|
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 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
MIL C 25601 : C
|
COUPLER, ANTENNA CU-308D/U |
|
MIL-I-27623 Revision C:1972
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
|
MIL T 85678 : 0
|
TRANSPONDER, RADAR TRACKING |
|
MIL A 81296 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
|
MIL I 83117 : B
|
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 : 0
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
|
MIL G 27693 : A
|
GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
|
MIL I 25645 : D
|
INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
|
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
|
MIL I 27848 : B
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
|
MIL A 81423 : 0
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-73 |
|
MIL G 25591 : E
|
GYROSCOPE, RATE, SWITCHING, TYPE MC-1 |
|
MIL A 27671 : B
|
AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
|
MIL I 38258 : 0
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
|
MIL E 81512 : 0
|
ENCODER, SHAFT POSITION TO DIGITAL, CONTACT TYPE, ALTITUDE REPORTING, GENERAL SPECIFICATION FOR |
|
MIL I 27619 : G
|
INDICATORS, ATTITUDE DIRECTOR |
|
MIL HDBK 246 : A
|
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 : 0
|
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 : D
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
|
MIL A 55368 : 0
|
AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
|
MIL A 9286 : C
|
AF AMPLIFIER AM-476()/AIC-10 |
|
MIL C 18266 : A
|
CORD, P/O 87B/U |
|
MIL I 27667 : C
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
|
MIL I 23524 : A
|
INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
|
DOD C 85050 : 0
|
CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 81883 : 0
|
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 : A
|
INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
|
MIL A 81373 : 0
|
ASSEMBLY, QUANTITY SELECT 65A132F9 |
|
MIL I 81049 : A
|
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 : B
|
RADAR TRANSPONDER AN/DPN-77(*) |
|
MIL C 85373 : A
|
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 : A
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
|
MIL P 85576 : B
|
POWER SUPPLY PP-2581C/A |
|
MIL-DTL-27193 Revision D:2017
|
INDICATOR, ATTITUDE ARU-2B/A |
|
MIL A 9080 : 0
|
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 : A
|
CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL P 18987 : A
|
PLOTTING BOARD, TACTICAL DISPLAY PT-396/AS |
|
MIL P 19461 : A
|
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 |