|
MIL R 85895 : 0
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
|
MIL C 6781 : B
|
CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED |
|
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
|
MIL L 85762 : A
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
|
MIL R 83372 : 0
|
RELAY, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR |
|
MIL I 83294 : 0
|
INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, 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 |
|
MIL R 29583 : 0
|
RADIO SET |
|
MIL S 24317 : 0
|
SWITCH, MULTI-STATION, PUSHBUTTON (ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL E 23001 : B
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL I 7627 : F
|
INDICATOR, TURN AND SLIP 28V DC |
|
MIL L 6503 : H
|
LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
|
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
|
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 |
|
MIL I 85071 : A
|
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
|
MIL STD 7080 : 0
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
|
MIL HDBK 83575 : 0
|
GENERAL HANDBOOK FOR SPACE VEHICLE WIRING HARNESS DESIGN AND TESTING |
|
MIL T 81714 : E
|
TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR |
|
MIL C 7135 : F
|
COMPRESSOR, PNEUMATIC, 3000 PSI 2 SCFM AERO 2A AERO 2A-1 AERO 2B AND AERO 2B-1 |
|
MIL R 81046 : 0
|
RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
|
MIL C 23697 : 0
|
COMPUTER SET, NAVIGATIONAL AN/ASN-42(*) |
|
DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
|
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)/11(2013) : 2013
|
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)/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 R 81876 : B
|
RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
|
MIL W 8777 : C
|
WIRE, ELECTRICAL, SILICONE-INSULATED COPPER 600-VOLT, 200 DEGREE C |
|
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 |
|
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 H 8891 : A
|
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
|
MIL R 23016 : A
|
RADIO SET AN/ARC-94 |
|
MIL STD 2156 : 0
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
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 H 5440 : H
|
HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
|
MIL E 45782 : C
|
ELECTRICAL WIRING, PROCEDURES FOR |
|
MIL A 81621 : 0
|
ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
|
MIL DTL 8777 : F
|
WIRE, ELECTRICAL, SILICONE-INSULATED, COPPER, 600-VOLT, 200 DEGREES C |
|
MIL A 26624 : B
|
AIR CONDITIONER, A/M32C-5, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC MOTOR DRIVEN |
|
MIL M 25047 : C
|
MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
|
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 A 23670 : A
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
|
MIL M 87158 : A
|
MANUALS, TECHNICAL, AIRCRAFT BATTLE DAMAGE ASSESSMENT AND REPAIR |
|
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
|
MIL C 22764 : C
|
CODER RECEIVER TRANSMITTER K & Y532A ASQ |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL E 7080 : B
|
ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
|
MIL STD 2131 : A
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL S 5594 : B
|
SWITCH, TOGGLE, ELECTRICALLY HELD SEALED GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
MIL S 83129 : A
|
SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
|
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
|
SAE AS 8700 : 1999
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL HDBK 516 : C
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
MIL M 9397 : E
|
FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
|
MIL S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
MIL S 8710 : B
|
STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
|
MIL S 8805/48 : F
|
SWITCH, SENSITIVE, ROLLER LEVER, SELF RETURN, RESILIENT SEAL, FLUID RESISTANT |
|
SAE AIR 5271 : 2009
|
A GUIDELINE FOR APPLICATION OF HIGH-DENSITY FIBER OPTIC INTERCONNECTS TO AEROSPACE PLATFORMS |
|
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
|
MIL R 21073 : A
|
RECORDER, MAGNETIC DISTORTION, RO-32/ASQ |
|
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL F 26685 : B NOTICE 1
|
FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
|
MIL DTL 26126 : C
|
RELAYS, ELECTRICAL, OVERVOLTAGE, DC, GENERAL SPECIFICATION FOR |
|
MIL A 23887 : A
|
ALTIMETER SET, ELECTRONIC AN/APN-141 (V) |
|
MIL C 85518 : 0
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
|
MIL D 23222 : A
|
DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
|
MIL I 8673 : 0
|
INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
|
MIL D 81641 : 0
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
|
MIL I 81454 : 0
|
INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
|
MIL A 81359 : 0
|
AIRCRAFT WEAPONS RELEASE SET AN/AWE-1 |
|
MIL C 19941 : A
|
CONTROLLER, S-2 COMPASS, TYPE |
|
MIL T 25920 : C
|
TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
|
MIL D 8804 : B
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 5898 : D
|
CORD, ELECTRICAL [WF 5/U, WF 14/U,WD 34/U, WM 53/U, WM 85/U] |
|
MIL R 26895 : 0
|
RELAY, FIELD CONTROL, GENERATOR 28 VOLT DC, TYPE MD AND 1 |
|
MIL I 18373 : B
|
INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
|
MIL C 85248 : A
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
|
MIL R 24011 : A
|
RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
|
MIL R 6463 : A
|
RELAY, GENERATOR EQUALIZER BUS, TYPE A1 |
|
MIL C 18277 : B
|
COUPLER, ANTENNA CU-351/AR AND COUPLER, ANTENNA CU-509/AR |
|
MIL C 85642 : 0
|
COMMUNICATIONS CENTRAL AN/ASC-26 |
|
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 |
|
DOD STD 863 : B
|
WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
|
MIL I 8700 : A
|
INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL P 5238 : C
|
PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE ARP 1897 : 2013
|
CLAMP SELECTION AND INSTALLATION GUIDE |
|
SAE AIR 5575 : 2017
|
HOT STAMP WIRE MARKING CONCERNS FOR AEROSPACE VEHICLE APPLICATIONS |
|
MIL G 81665 : 0
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
|
MIL A 23622 : 0
|
ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
|
MIL STD 681 : F
|
IDENTIFICATION CODING AND APPLICATION OF HOOKUP AND LEAD WIRE |
|
MIL R 28894 : 0
|
RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
|
MIL S 8805/43 : G
|
SWITCH, SENSITIVE, PLUNGER, 7 AMPERES RESILIENT SEAL, FLUID RESISTANT |
|
MIL A 19939 : A
|
AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
|
MIL W 22759 : E
|
WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
|
MIL C 81991 : 0
|
CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
|
MIL R 26126 : B
|
RELAY, ELECTRICAL, OVERVOLTAGE DC, GENERAL SPECIFICATION FOR |
|
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL I 23366 : B
|
INDICATOR, HORIZONTAL SITUATION ID-1O13(*)/A |
|
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
|
MIL DTL 25561 : B
|
GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE MC-2 |
|
MIL R 9221 : 0
|
RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC TYPE M AND 2 |
|
MIL E 85583 : A
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL G 83380 : 0
|
GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
|
MIL E 25499 : C
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
|
MIL I 8671 : D
|
INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
|
MIL F 23447 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
|
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
|
MIL W 26217 : B
|
WINCH, DRUM, POWER OPERATED AF E24H 1, CARGO LOADING, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE |
|
MIL N 81207 : A
|
NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
|
SAE AS 55941 : 2013
|
SWITCHES, TOGGLE, ELECTRICALLY HELD, SEALED, GENERAL SPECIFICATION FOR |
|
SAE ARP 1070E : 2019
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
SAE ARP 1070 : 2014
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
MIL G 23081 : C
|
GYROSCOPE INDICATOR SYSTEM VERTICAL. |
|
MIL D 19326 : H
|
DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL R 81498 : C
|
RECEIVING-DECODING GROUP AN/ARA-63 |
|
MIL G 23083 : C
|
GYROSCOPE, RATE SWITCHING MS 17399 |
|
MIL B 23431 : B
|
BEACON, RADAR AN/APN-154(V) |
|
MIL F 8615 : D
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
|
MIL I 85112 : 0
|
INDICATOR SET, VERTICAL SCALE |
|
MIL A 85505 : 0
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
|
MIL A 85672 : 0
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
|
MIL W 18326 : A
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
|
MIL A 81605 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
|
SAE AS 22145 : 2012
|
ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
|
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
MIL I 81453 : A
|
INTERROGATOR SET AN APX 76B(V) |
|
MIL T 85678 : 0
|
TRANSPONDER, RADAR TRACKING |
|
MIL A 81296 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
|
MIL M 4803 : D
|
MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
|
MIL L 85314 : A
|
LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
|
MIL A 81423 : 0
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-73 |
|
MIL D 83753 : NOTICE 2
|
DISPENSER, BOMB, TYPE SUU-21/A |
|
MIL I 8672 : B
|
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 C 7115 : F
|
CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 81883 : 0
|
CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
|
MIL I 7802 : A
|
INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
|
MIL C 85283 : B
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9 |
|
MIL L 5667 : B
|
LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
|
MIL M 23888 : NOTICE 1
|
MONITOR, RADIO FREQUENCY ID AND 9O2A/AR |
|
MIL S 9419 : E
|
SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
|
MIL C 85373 : A
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A |
|
MIL T 81821 : 0
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
|
MIL D 5025 : C
|
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 |