|
SAE AS 5372 : 2015
|
FUSE, CURRENT LIMITER TYPE, AIRCRAFT |
|
MIL G 23081 : C
|
GYROSCOPE INDICATOR SYSTEM VERTICAL. |
|
MIL P 0081653 : C
|
POWER CONTROLLER, SOLID STATE, GENERAL SPECIFICATION FOR |
|
MIL C 83166 : LATEST
|
CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
|
AFGS 87213 : B
|
DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
|
MIL C 38240 : C
|
COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
|
MIL A 85802 : 0
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
|
MIL M 8609 : B
|
MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE AIR 4004 : 2015
|
GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
|
MIL T 5842 : B
|
TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
|
MIL R 38370 : B
|
RECORDING SET, FLIGHT DATA A/A24U-10 |
|
MIL I 18856 : B
|
INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
|
MIL T 38034 : E
|
TIMER, FIRE CONTROL, BOMBING, DUAL |
|
SAE AIR 6114 : 2016
|
INTERFACE FOR MICRO MUNITION (IMM) HANDBOOK |
|
SAE AIR 5451 : 2017
|
A GUIDE TO LANDING GEAR SYSTEM INTEGRATION |
|
MIL P 81655 : 0
|
PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
|
MIL C 87979 : 0
|
CLOCK, AIRCRAFT, ELECTRONIC |
|
MIL T 81998 : 0
|
TEST SET, RADIO SET AN/ARM-165 |
|
MIL R 29583 : 0
|
RADIO SET |
|
MIL S 85018 : A
|
SECOND ORDER ATTITUDE REFERENCE SYSTEM (SOARS) AN/ASN-116 |
|
MIL PRF 83287 : G
|
INDICATORS, FAULT LOCATING, GENERAL SPECIFICATION FOR |
|
MIL R 83726/24 : M
|
RELAYS, SOLID STATE, TIME DELAY (ON OPERATE), TRACK MOUNTED, TYPE 1, CLASS C, SPST, 150 MILLIAMPERES, FIXED TIME, 50 MILLISECONDS TO 500 SECONDS |
|
MIL S 24711 : 0
|
SWITCH, PROXIMITY, SOLID-STATE |
|
SAE AS 6129 : 2012
|
INTERFACE STANDARD, AIRBORNE EO/IR SYSTEMS, ELECTRICAL |
|
DEFSTAN 66-31(PT3)/1(2007) : 2007
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 3: CONTRACTOR REQUIREMENTS - AIR USE APPLICATION |
|
MIL PRF 29595 : A
|
BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 5809 : G
|
CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL R 38435 : B
|
RECORDING SET, SIGNAL DATA A/A 24U-6 |
|
MIL E 23001 : B
|
ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
JSGS 87231 : A
|
ENGINES, AIRCRAFT, TURBINE |
|
MIL M 8555 : C
|
MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
|
MIL T 83460 : 0
|
TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
|
MIL F 87154 : 0
|
FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
|
MIL I 7627 : F
|
INDICATOR, TURN AND SLIP 28V DC |
|
MIL L 6503 : H
|
LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
|
MIL I 38121 : C
|
INDICATOR, PRESSURE, EGU-9/A |
|
MIL A 85055 : 0
|
AVIONICS SYSTEM PERFORMANCE SPECIFICATION FOR A-4M/AV-8 BOMBING SET, ANGLE RATE AN/ASB-19(V) |
|
MIL A 22145 : C
|
ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
|
MIL STD 7080 : 0
|
SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
|
MIL PRF 32272 : A
|
INTEGRATED POWER MANAGEMENT CENTER (IPMC) |
|
MIL T 38473 : A
|
TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
|
MIL PRF 83383 : F
|
CIRCUIT BREAKERS, REMOTE CONTROL, THERMAL, TRIP FREE, GENERAL SPECIFICATION FOR |
|
MIL F 5373 : D
|
FUSEHOLDER, BLOCK TYPE, AIRCRAFT |
|
MIL PRF 8565 : K
|
BATTERY STORAGE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL H 81014 : A NOTICE 1
|
HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
|
MIL I 5949 : G
|
INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF |
|
MIL G 25597 : D
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1 |
|
MIL B 28873 : 0
|
BLOWERS, ELECTRONICALLY COMMUTATED BRUSHLESS, DIRECT CURRENT, (ECDC) MOTOR DRIVEN, FOR COOLING ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
|
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR |
|
MIL T 27305 : C
|
TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
|
MIL T 85350 : B
|
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 A 85072 : A
|
ACTUATOR, ELECTROMECHANICAL, LINEAR |
|
MIL I 21206 : B
|
INDICATOR, RATE OF FLOW, FUEL; EFU-7/A (300-5000-15000 PPH) |
|
MIL I 27709 : A
|
INDICATOR, ATTITUDE ARU-14/A, REMOTE |
|
MIL R 81046 : 0
|
RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
|
MIL HDBK 704/1 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS (PART 1 OF 8 PARTS) |
|
MIL HDBK 704/5 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS THREE PHASE, VARIABLE FREQUENCY, 115 VOLT (PART 5 OF 8 PARTS) |
|
MIL PRF 6106/15 : E
|
RELAY, ELECTROMAGNETIC, 50 AMPERES, DC, SPDT, HERMETICALLY SEALED |
|
MIL A 22669 : 0
|
AMPLIFIER-POWER SUPPLY-RECEIVER AM-2310(*)/ASQ AND ANTENNA AS-909(*)/ARA-48 |
|
MIL PRF 83419 : F
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL A 55503 : 0
|
ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
|
MIL D 8684 : B
|
DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
|
MIL I 38338 : D
|
INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
|
MIL A 25546 : C
|
AMPLIFIER, AUDIO FREQUENCY, AM944/AIC-L 3 |
|
MIL R 85669 : 0
|
REPEATER SET, RADIO, POD AN/ARQ-49 |
|
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 B 83424 : 0
|
BATTERY SYSTEMS, SEALED CELL, NICKEL CADMIUM, INTEGRAL CHARGE CONTROL, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL DTL 27193 : D
|
INDICATOR, ATTITUDE ARU-2B/A |
|
MIL R 83726/22 : F
|
RELAYS, SOLID STATE, REPEAT CYCLE TIMER, TYPE 4, CLASS C, SPST, 250 MILLIAMPERES |
|
MIL C 23367 : 0
|
COMPUTER, FLIGHT DIRECTOR, AIRCRAFT |
|
MIL PRF 83726/13 : L
|
RELAYS, SOLID STATE, TIME DELAY, (ON OPERATE), TYPE 1 CLASS C, SPST-NO, 300 MILLIAMPERES, FIXED TIME, 0.05 TO 600 SECONDS, HERMETICALLY SEALED |
|
SAE AS 6858 : 2017
|
INSTALLATION OF FUEL CELL SYSTEMS IN LARGE CIVIL AIRCRAFT |
|
SAE ARP 5120 : 2016
|
AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE |
|
SAE AS 58091 : 2012
|
CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
BS EN 13718-1:2014
|
MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
MIL DTL 6162 : C
|
GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
|
DEFSTAN 66-31(PT3)/2(2008) : 2008
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 3: CONTRACTOR REQUIREMENTS - AIR USE APPLICATION |
|
MIL C 85521 : 0
|
CONCENTRATOR, OXYGEN, GGU-7/A |
|
MIL E 29581 : 0
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM |
|
ARINC 609 : 1987
|
DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS |
|
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 F 5372 : D
|
FUSE, CURRENT LIMITER TYPE, AIRCRAFT |
|
AFGS 87219 : B
|
ELECTRICAL POWER SYSTEMS, AIRCRAFT |
|
MIL HDBK 244 : A
|
GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
|
MIL R 23016 : A
|
RADIO SET AN/ARC-94 |
|
MIL PRF 28750/9 : G
|
RELAY, SOLID-STATE, HERMETICALLY SEALED, CLASS 2, OPTICALLY ISOLATED, ZERO VOLTAGE TURN-ON, 1 AMPERE (2 AMPERES WITH HEAT SINK), 400 HZ, POWER SWITCHING, SPST (N.O.) |
|
MIL I 85506 : 0
|
INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
|
MIL G 83872 : A
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
|
MIL T 38049 : A
|
TRANSMITTER, PRESSURE TRU 60A |
|
DOD STD 35/82 : A
|
AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM CONVERTERS AND INVERTERS |
|
MIL I 38120 : A (3)
|
INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
|
MIL T 23539 : 0
|
TEST SET, DOPPLER RADAR AN/APM-148(*) |
|
MIL J 23013 : 0
|
JUNCTION BOX JEU-25 (*)/A |
|
MIL STD 35/96 : 0
|
AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, REGULATORS, CURRENT AND VOLTAGE AC, AND DC |
|
MIL A 19736 : A
|
AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
|
MIL HDBK 258 : 0
|
INTERFACE CONTROL DOCUMENT FOR INFRARED DETECTING SET AN/AAS-36 |
|
MIL A 81621 : 0
|
ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
|
MIL STD 2120 : 0
|
CONNECTORS, ELECTROMAGNETIC INTERFERENCE (EMI) FILTER CONTACT |
|
MIL D 83029 : A
|
DRIVE ASSEMBLY, CONSTANT SPEED, GENERAL SPECIFICATION FOR |
|
MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
|
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 PRF 83726/35 : D
|
RELAYS, HYBRID, TIME DELAY (ON OPERATE), CLASS B, TYPE 1, HERMETICALLY SEALED, 4DPT, 10 AMPERES, FIXED TIME DELAY, 0.1 TO 600 SECONDS |
|
MIL HDBK 704/7 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS 270 VDC (PART 7 OF 8 PARTS) |
|
MIL T 21205 : B
|
TRANSMITTER, RATE OF FLOW, FUEL; TRU-12/A (300 - 5000 -15000 PPH) |
|
MIL R 83726/14 : E
|
RELAYS, HYBRID, TIME DELAY, (ON OPERATE), TYPE 1, CLASS B, 10 AMPERES, 4PDT, HERMETICALLY SEALED, FIXED TIME, 0.100 TO 300 SECONDS |
|
MIL PRF 83726/31 : K
|
RELAY, HYBRID, TIME DELAY (ON RELEASE), CLASS B, TYPE 2A, HERMETICALLY SEALED, DPDT, 10 AMPERES, ADJUSTABLE TIME DELAY (EXTERNAL RESISTOR), 0.1 TO 500 SECONDS |
|
MIL T 63534 : 0
|
TURRET SUBSYSTEM, UNIVERSAL, (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, TURRET CONTROL UNIT FOR |
|
MIL P 26517 : A
|
POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
13/30276231 DC : 0
|
BS EN 13718-1 - MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
MIL A 23670 : A
|
ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
|
MIL PRF 83287/1 : D
|
INDICATORS, FAULT LOCATING, FLAG INDICATING, MECHANICAL RESET |
|
SAE ARP 1148 : 2013
|
GROUND ELECTRICAL POWER UNIT, TRANSPORTABLE 115/200 VOLT AC (NOMINAL) 400 HERTZ, 3-PHASE 4-WIRE (GROUNDED NEUTRAL) Y-CONNECTED SYSTEM |
|
DEFSTAN 66-31(PT2)/2(2008) : 2008
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 2: CONTRACTOR GENERAL REQUIREMENTS |
|
MIL C 22764 : C
|
CODER RECEIVER TRANSMITTER K & Y532A ASQ |
|
MIL R 85895 : 0
|
RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
|
MIL T 23913 : 0
|
TEST SET, INTERCOMMUNICATION SET AN/A1M AND 3A |
|
MIL I 5133 : C
|
INDICATOR, ATTITUDE TYPE J 8 |
|
MIL B 81365 : 0
|
BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
|
MIL STD 461 : G
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
|
MIL S 8512 : D
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
|
MIL S 85377 : A
|
SWITCH, STEPPING, DIRECT CURRENT AIRCRAFT DISPENSER |
|
MIL M 81850 : A
|
MAGNETIC TAPE TRANSPORT RD-319/AYA-8 |
|
SAE AS 4764 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760 AIRCRAFT STATION INTERFACES |
|
MIL R 83726/20 : C (2)
|
RELAY, SOLID STATE, TIME DELAY (ON OPERATE) TYPE 1, CLASS C, SPST, 250 MILLIAMPERES, FIXED TIME, .05 TO 500 SECONDS |
|
MIL A 85652 : 0
|
AMPLIFIER-MIXER AM-7157/DKT-59 |
|
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 85648 : 0
|
AMPLIFIER, TRAVELING WAVE TUBE |
|
DEFSTAN 66-31(PT6)/2(2008) : 2008
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 6: REQUIREMENTS FOR GENERAL PURPOSE TME APPLICATIONS |
|
MIL STD 2131 : A
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
|
MIL L 58085 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
|
SAE ARP 5311 : 2016
|
AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
|
MIL P 8564 : D
|
PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG] |
|
MIL B 8075 : D
|
BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
|
MIL PRF 8565/6 : B
|
BATTERY, STORAGE, AIRCRAFT, MAINTENANCE-FREE, 24-VOLT, 1.5-AMPERE-HOUR |
|
MIL HDBK 87244 : 0
|
AVIONICS/ELECTRONICS INTEGRITY |
|
MIL D 8685 : B
|
DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
|
STANAG 3456 : 0
|
AIRCRAFT ELECTRICAL POWER SYSTEM CHARACTERISTICS |
|
STANAG 7117 : 2008
|
RECHARGEABLE PNEUMATIC ENERGY SOURCE FOR AIRCRAFT STORES RELEASE |
|
SAE ARP 94910 : 2012
|
AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
|
SAE ARP 4945 : 2013
|
AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING |
|
ASTM F 2318 : 2015
|
Standard Specification for Rotary Wing Basic Life Support, Advanced Life Support, and Specialized Medical Support Air Ambulances |
|
UNI EN 13718-1 : 2014
|
MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
MIL HDBK 516 : C
|
AIRWORTHINESS CERTIFICATION CRITERIA |
|
MIL STD 464 : C
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
|
MIL S 8812 : D
|
STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
|
10/30203853 DC : 0
|
BS ISO 22072 - AEROSPACE - ELECTROHYDROSTATIC ACTUATOR (EHA) - CHARACTERISTICS TO BE DEFINED IN PROCUREMENT SPECIFICATIONS |
|
DIN 29576-1:1992-05
|
AEROSPACE - AIRCRAFT ELECTRICAL SYSTEMS - CHARACTERISTICS |
|
MIL E 7016 : F
|
ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
|
DEFSTAN 66-31(PT1)/2(2008) : 2008
|
BASIC REQUIREMENTS AND TESTS FOR ELECTRONIC AND ELECTRICAL TEST AND MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
|
MIL A 38331 : 0
|
AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
|
MIL R 21073 : A
|
RECORDER, MAGNETIC DISTORTION, RO-32/ASQ |
|
MIL I 27273 : A
|
INVERTER, POWER, STATIC, GENERAL SPECIFICATION FOR |
|
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 HDBK 1760 : A
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
|
MIL A 23887 : A
|
ALTIMETER SET, ELECTRONIC AN/APN-141 (V) |
|
MIL M 85522 : A
|
MONITOR, OXYGEN CRU-91/A |
|
MIL C 85518 : 0
|
COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
|
MIL P 87210 : 0
|
PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
|
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 I 87216 : 0
|
INSTRUMENT SYSTEMS, 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 C 85629 : A (1)
|
CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
|
MIL I 81454 : 0
|
INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
|
MIL D 81641 : 0
|
DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
|
MIL C 19941 : A
|
CONTROLLER, S-2 COMPASS, TYPE |
|
MIL T 81760 : A
|
TEST SET, PROGRAMMER AN/USM-299A |
|
MIL A 81359 : 0
|
AIRCRAFT WEAPONS RELEASE SET AN/AWE-1 |
|
MIL I 85581 : 0
|
INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
|
MIL D 8804 : B
|
DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL C 85300 : 0
|
COOLER, CRYOGENIC DETECTOR |
|
MIL PRF 83726/29 : J
|
RELAY, HYBRID, TIME DELAY (ON RELEASE), CLASS B, TYPE 2A, HERMETICALLY SEALED, DPDT, 10 AMPERES, FIXED TIME, 0.1 TO 500 SECONDS |
|
MIL A 81852 : A
|
ALTIMETER-ENCODER AAU-32/A |
|
MIL I 22075 : C
|
INDICATOR, BEARING DISTANCE-HEADING; ID - 663D/U |
|
MIL G 45279 : 0
|
GYRO, DIRECTIONAL CN-998( )/ASN-43 |
|
DEFSTAN 66-31(PT1)/1(2007) : 2007
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
|
SAE AS 47641 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760B AIRCRAFT STATION INTERFACES |
|
MIL C 85248 : A
|
CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
|
SAE AS 5716 : 2012
|
STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
|
MIL A 81369 : 0
|
ASSEMBLY, LEFT-RIGHT STATION 65A132F5 |
|
MIL R 83726/12 : F
|
RELAYS, HYBRID, TIME DELAY (ON RELEASE), TYPE 2A, CLASS B, 10 AMPERES, 4PDT, HERMETICALLY SEALED, FIXED TIME, 0.100 TO 300 SECONDS |
|
MIL R 24011 : A
|
RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
|
MIL PRF 83174 : E
|
TRANSMITTER, ACCELEROMETER, AXIAL |
|
MIL C 18277 : B
|
COUPLER, ANTENNA CU-351/AR AND COUPLER, ANTENNA CU-509/AR |
|
MIL T 81832 : 0
|
TEST SET, ALTIMETER SET AN/APM-348 |
|
MIL PRF 83726/28 : K
|
RELAYS, HYBRID, TIME DELAY (ON OPERATE), CLASS B, TYPE 1, HERMETICALLY SEALED, DPDT, 10 AMPERES, FIXED TIME, 0.1 TO 500 SECONDS |
|
MIL C 81125 : NOTICE 1
|
COUPLER, ANTENNA CU-1304 (*)/ARC AND MOUNTING MT-3261 (*)/ARC |
|
MIL C 85642 : 0
|
COMMUNICATIONS CENTRAL AN/ASC-26 |
|
MIL A 81851 : B
|
ALTIMETER AAU-31/A |
|
MIL T 27200 : C
|
TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
|
MIL R 83726/23 : E
|
RELAYS, HYBRID, TIME DELAY (ON RELEASE), TYPE 2B, CLASS B, 10 AMPERES, 4PDT, HERMETICALLY SEALED |
|
MIL G 85468 : 0
|
GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
|
MIL T 85601 : 0
|
TEST SET, INDICATOR AN/APM-433 |
|
SAE ARP 1281 : 2002
|
ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
|
SAE ARP 4404 : 2013 : R2019
|
AIRCRAFT ELECTRICAL INSTALLATIONS |
|
MIL HDBK 704/2 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, 400 HZ, 115 VOLT (PART 2 OF 8 PARTS) |
|
MIL HDBK 704/3 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS THREE PHASE, 400 HZ, 115 VOLT (PART 3 OF 8 PARTS) |
|
DEFSTAN 66-31(PT6)/1(2007) : 2007
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 6: REQUIREMENTS FOR GENERAL PURPOSE TME APPLICATIONS |
|
SAE ARP 1595 : 2013(R2019)
|
DESIGN AND VERIFICATION OF AIRCRAFT NOSE WHEEL STEERING SYSTEMS |
|
SAE AS 5725 : 2015
|
INTERFACE STANDARD, MINIATURE MISSION STORE INTERFACE |
|
SAE AS 22145 : 2012
|
ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
|
IEEE 127-1963
|
IEEE Standard for Aerospace Equipment Voltage and Frequency Ratings |
|
SAE AIR 6234 : 2016
|
HANDBOOK: STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
|
MIL STD 810 : G
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
|
SAE ARP 5015 : 2011
|
GROUND EQUIPMENT - 400 HERTZ GROUND POWER PERFORMANCE REQUIREMENTS |
|
DIN EN 13718-1:2014-12
|
MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
MIL PRF 21480 : B
|
GENERATOR SYSTEM, ELECTRIC POWER, 400 HERTZ, ALTERNATING CURRENT, AIRCRAFT - GENERAL SPECIFICATION FOR |
|
MIL DTL 83361 : B
|
INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
|
MIL DTL 27715 : C
|
CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL G 6162 : B
|
GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
|
SAE AS 1188 : 2014
|
AIRCRAFT TIRE INFLATION-DEFLATION EQUIPMENT |
|
MIL PRF 15733/59 : B
|
FILTERS, RADIO FREQUENCY INTERFERENCE, HERMETICALLY SEALED, STYLE FL64 |
|
MIL DTL 9490 : E
|
FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL G 81665 : 0
|
GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
|
MIL A 23622 : 0
|
ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
|
MIL R 83726/13 : K
|
RELAYS, SOLID STATE, TIME DELAY, (ON OPERATE), TYPE 1 CLASS C, SPST-NO, 300 MILLIAMPERES, FIXED TIME, 0.05 TO 600 SECONDS, HERMETICALLY SEALED |
|
MIL DTL 9320 : E
|
SIGNAL, WARNING, AUDIBLE, FOR HEADSET, TYPE MA-1 |
|
MIL PRF 83287/2 : E
|
INDICATORS, FAULT LOCATING, FLAG INDICATING, ELECTRICAL RESET |
|
MIL DTL 38394 : E
|
TRANSMITTER, PRESSURE TRU-81/A, OIL, 0-500 PSI |
|
MIL B 19906 : A
|
BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
|
MIL L 21652 : A
|
LIGHT, BEACON, ANTI COLLISION AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL PRF 22885/113 : A
|
SWITCHES, PUSHBUTTON, ILLUMINATED, 1.17 BY .96, LIGHT EMITTING DIODE (LED), SUNLIGHT READABLE, VOLTAGE DIMMABLE, NIGHT VISION GOGGLE COMPATIBLE, EMC COMPLIANT, COMMON TERMINATION SYSTEM (CTS), SPDT, DPDT, 4PDT, LOGIC LEVEL TO 7.5 AMPERES, DRIPPROOF, WATERTIGHT, SPLASHPROOF, HIGH IMPACT SHOCK RESISTANT |
|
MIL I 26689 : C
|
INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
|
MIL R 28894 : 0
|
RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
|
MIL T 81587 : A
|
TIMER ASSEMBLY RAIN REPELLENT |
|
MIL C 49175 : B
|
COOLER, CRYOGENIC, MECHANICAL HD-1033B/UA AND HD-1033C/UA |
|
MIL E 29581/1 : 0
|
EARCUP, UNIT ACTIVE NOISE REDUCTION SYSTEM, MH-53E AIRCRAFT |
|
SAE ARP 6154 : 2017
|
AEROSPACE FLUID POWER ELECTROHYDROSTATIC MODULE, DESIGN, PERFORMANCE AND TEST RECOMMENDATIONS |
|
MIL PRF 32144 : B
|
CLOCK, AIRCRAFT, ELECTRONIC |
|
MIL A 19939 : A
|
AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
|
MIL M 7793 : F
|
METER, TIME TOTALIZING |
|
MIL PRF 83726/30 : K
|
RELAY, HYBRID, TIME DELAY (ON OPERATE), CLASS B, TYPE 1, HERMETICALLY SEALED, DPDT, 10 AMPERES, ADJUSTABLE TIME DELAY (EXTERNAL RESISTOR), 0.1 TO 500 SECONDS |
|
MIL C 27889 : D
|
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
|
JSSG 2009 : A
|
AIR VEHICLE SUBSYSTEMS (JOINT SERVICE SPECIFICATION GUIDE) |
|
MIL C 85247 : 0
|
COMPUTER, AIR DATA CP-1005A/A |
|
SAE AS 53731 : 2014
|
FUSE HOLDER, BLOCK TYPE, AIRCRAFT |
|
MIL T 81578 : NOTICE 1
|
TEST SET, RADAR BEACON AN/APM-230A |
|
MIL C 81991 : 0
|
CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
|
MIL T 63520 : 0
|
TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, GUN CONTROL ASSEMBLY FOR |
|
MIL STD 1760 : E
|
AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
|
MIL C 26485 : D
|
CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
|
MIL I 22126 : B
|
INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
|
MIL N 49098 : A
|
NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
|
MIL I 23366 : B
|
INDICATOR, HORIZONTAL SITUATION ID-1O13(*)/A |
|
MIL T 85026 : D
|
TEST SET AN/ASM-475 FOR THE AN/ASX-2 RECOGNITION SET |
|
MIL I 83452 : LATEST
|
INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
|
MIL PRF 83726/36 : D
|
RELAY, HYBRID, TIME DELAY (ON RELEASE), CLASS B, TYPE 2A, HERMETICALLY SEALED, 4PDT, 10 AMPERES, FIXED TIME DELAY, 0.1 TO 600 SECONDS |
|
MIL I 83287 : E
|
INDICATOR, FAULT LOCATING GENERAL SPECIFICATION FOR |
|
MIL STD 1539 : 0
|
ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS |
|
MIL C 27715 : 0
|
CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL PRF 22885/108 : H
|
SWITCHES, PUSHBUTTON, ILLUMINATED, 4-LAMP REPLACEABLE INCANDESCENT OR NON-REPLACEABLE LIGHT EMITTING DIODE (LED), 0.750 SQUARE, SPDT, DPDT, 4PDT SILVER CONTACTS - 2 CIRCUIT (5 AMPERES) OR SPDT (7.5 AMPERES); GOLD CONTACTS - LOW LEVEL TO 1 AMPERE, OPTIONAL ELECTRONIC COMPONENTS, SUNLIGHT READABLE DISPLAY (DRIPPROOF, WATERTIGHT, SPLASHPROOF, EMI/RFI SHIELDING, HIGH IMPACT SHOCK |
|
MIL C 5026 : F
|
CUTOUT RELAY, ENGINE GENERATOR |
|
MIL O 38338 : C (1)
|
OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
|
MIL H 27269 : A
|
HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
|
MIL PRF 24711 : B
|
SWITCH, PROXIMITY, SOLID-STATE |
|
MIL G 23723 : 0
|
GYROSCOPE, RATE SWITCHING CN-495/AJB-3 |
|
DSCC 88062 : G
|
RELAY, SOLID STATE, HERMETICALLY SEALED, OPTICALLY ISOLATED, 2.1 AMPERES, 60 V DC, ANALOG SIGNAL SWITCHING, SPST (N.O.), TTL/CMOS CONTROL INPUTS, SHORT CIRCUIT PROTECTED, OUTPUT SWITCH STATUS |
|
MIL R 22679 : 0
|
RECEIVER-TRANSMITTER RADIO RT-559/ASQ-58 AND RT-559A/ASQ-58 |
|
MIL G 23701 : 0
|
MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
|
MIL PRF 83726/21 : H
|
RELAY, SOLID-STATE, TIME DELAY (ON OPERATE), TYPE 1, CLASS C, SPST, 250 MILLIAMPERES, VARIABLE TIME, 0.05 TO 500 SECONDS |
|
MIL I 83287/2 : C
|
INDICATOR, FAULT LOCATING, FLAG INDICATING, ELECTRICAL RESET |
|
MIL DTL 25627 : D
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
|
MIL PRF 25435 : D
|
TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL R 7051 : A
|
RELAY BANK, BOMB SALVO CIRCUIT 3 UNIT, 28 VOLT DC TYPE A 1 |
|
SAE AS 4073 : 2013(R2018)
|
AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
|
MIL HDBK 1028/3 : 0
|
MAINTENANCE FACILITIES FOR AMMUNITION, EXPLOSIVES AND TOXINS |
|
MIL D 8181 : B
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
|
MIL HDBK 704/4 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, VARIABLE FREQUENCY, 115 VOLT (PART 4 OF 8 PARTS) |
|
PREN 13718-1 : DRAFT 2013
|
MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
DEFSTAN 66-31(PT2)/1(2007) : 2007
|
BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 2: CONTRACTOR GENERAL REQUIREMENTS |
|
MIL I 26359 : B
|
INDICATOR, ATTITUDE, REMOTE ARU-4/A |
|
MIL DTL 58085 : C
|
LIGHT, BEACON, ANTI-COLLISION, AIRCRAFT |
|
MIL E 85583 : A
|
ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL E 25499 : C
|
ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
|
MIL HDBK 87213 : A
|
ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
|
MIL B 85584 : B
|
BATTERY RELAY CONTROL UNIT, AIRCRAFT |
|
MIL F 23447 : 0
|
FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
|
MIL T 38306 : 0
|
TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
|
MIL T 81921 : 0
|
TEST SET, RADAR BEACON AN/APM-230B |
|
MIL R 83726 : B
|
RELAY, HYBRID, TIME DELAY (ON RELEASE), CLASS B, TYPE LIA, HERMETICALLY SEALED, DPDT, 10 AMPERES, ADJUSTABLE TIME DELAY (EXTERNAL RESISTOR)O.1 TO 500 SECONDS |
|
MIL DTL 38449 : D
|
SIGNAL AND SIGNAL/INTERCOMMUNICATION AMPLIFIERS, UNIVERSAL, AERIAL REFUELING |
|
MIL DTL 81014 : B
|
HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
|
MIL T 18232 : B
|
TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
|
MIL HDBK 704/8 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS 28 VDC (PART 8 OF 8 PARTS) |
|
MIL E 38453 : A
|
ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL S 38399 : A
|
STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
|
SAE AS 47643 : 2017
|
VERIFICATION METHODS FOR MIL-STD-1760E AIRCRAFT STATION INTERFACES |
|
MIL B 23072 : 0
|
BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR |
|
MIL I 27247 : C
|
INDICATOR, TEMPERATURE, SYNCHRO |
|
MIL PRF 83726/20 : G
|
RELAY, SOLID-STATE, TIME DELAY (ON OPERATE), TYPE 1, CLASS C, SPST, 250 MILLIAMPERES, FIXED TIME, 0.05 TO 500 SECONDS |
|
MIL A 83419 : C
|
ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
|
MIL A 85046 : 0
|
ACTUATOR, LINEAR ELECTROMECHANICAL |
|
MIL G 83163 : 0
|
GYRO, DIRECTIONAL CN-1251/ASN-89(V) |
|
MIL T 81943 : 0
|
TEST SET, RADIO, AN/ARM-156 |
|
MIL P 85573 : 0
|
POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
|
BS ISO 22072:2011
|
Aerospace. Electrohydrostatic actuator (EHA). Characteristics to be defined in procurement specifications |
|
MIL D 81544 : A
|
DISPENSER, PARACHUTE FLARE, SUU-44/A |
|
FAA AC 33.28-2 : 2003
|
GUIDANCE MATERIAL FOR 14 CFR SECTION 33.28, RECIPROCATING ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS |
|
MIL F 38363 : B (3)
|
FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL N 81207 : A
|
NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
|
MIL HDBK 704/6 : 0
|
GUIDANCE FOR TEST PROCEDURES FOR DEMONSTRATION OF UTILIZATION EQUIPMENT COMPLIANCE TO AIRCRAFT ELECTRICAL POWER CHARACTERISTICS SINGLE PHASE, 60 HZ, 115 VOLT (PART 6 OF 8 PARTS) |
|
MIL E 18927 : E
|
ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
|
MIL A 81403 : 0
|
ALTIMETER-ENCODER, AAU-21/A |
|
MIL T 63536 : 0
|
TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, LOGIC CONTROL UNIT ASSEMBLY FOR |
|
MIL I 81400 : 0
|
INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL A 22424 : A
|
ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
|
SAE ARP 4404 : 2013
|
AIRCRAFT ELECTRICAL INSTALLATIONS |
|
IEEE 45.1 : 2017
|
IEEE Recommended Practice for Electrical Installations on Shipboard--Design |
|
SAE AS 4270 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES |
|
SAE AS 50881 : 2015
|
WIRING AEROSPACE VEHICLE |
|
SAE ARP 1070 : 2014
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
SAE AS 6019 : 2012
|
ARC FAULT CIRCUIT BREAKER (AFCB), AIRCRAFT, TRIP-FREE 28 VDC |
|
SAE AS 47642 : 2017
|
VALIDATION METHODS FOR MIL-STD-1760C AIRCRAFT STATION INTERFACES |
|
EIA EMCB1-1 : 1993
|
HISTORICAL RATIONALE FOR MILITARY EMI LIMITS |
|
AECTP-250 : 2014
|
ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
|
SAE AS 94900 : 2007
|
AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
|
ASTM F 2319 : 2004
|
Standard Specification for Fixed Wing Basic Life Support, Advanced Life Support, and Specialized Medical Support Air Ambulances (Withdrawn 2013) |
|
EN 13718-1:2014
|
Medical vehicles and their equipment - Air ambulances - Part 1: Requirements for medical devices used in air ambulances |
|
I.S. EN 13718-1:2014
|
MEDICAL VEHICLES AND THEIR EQUIPMENT - AIR AMBULANCES - PART 1: REQUIREMENTS FOR MEDICAL DEVICES USED IN AIR AMBULANCES |
|
MIL F 26301 : H
|
FLASHER, SOLID STATE, AIRCRAFT NAVIGATIONAL LIGHT, GENERAL SPECIFICATION FOR |
|
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 |
|
MIL A 49079 : A
|
ALTIMETER SET, ELECTRONIC AN/APN-209(V) (UNITS OF) |
|
DOD STD 1788 : LATEST
|
AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
|
MIL G 23083 : C
|
GYROSCOPE, RATE SWITCHING MS 17399 |
|
MIL F 8378 : B
|
FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
|
MIL F 8615 : D
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
|
MIL I 85112 : 0
|
INDICATOR SET, VERTICAL SCALE |
|
MIL B 23431 : B
|
BEACON, RADAR AN/APN-154(V) |
|
MIL G 45280 : 0
|
GYROMAGNETIC COMPASS SET AN/ASN-430 |
|
MIL I 27552 : C
|
INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED |
|
MIL S 21277 : A
|
SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
|
MIL T 83174 : B (3)
|
TRANSMITTER, ACCELEROMETER, AXIAL |
|
MIL D 81357 : A
|
DISPLAY GROUP, TACTICAL DATA AN ASA 70 |
|
MIL T 81831 : 0
|
TEST SET, ALTIMETER SET AN/APM-347 |
|
ISO 22072:2011
|
Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications |
|
MIL T 85472 : A
|
TEST SET, GROUP OQ-169A/DSM-96A |
|
MIL S 8932 : A
|
SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL B 85099 : 0
|
BATTERY, WET PRIMARY FOR AN/DKT-37(V) TELEMETRY PACKAGE |
|
MIL A 85505 : 0
|
ALTIMETER, STANDBY, TYPES 1 AND 2 |
|
SAE AIR 4094 : 2016
|
AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS |
|
MIL A 27670 : D
|
AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
|
MIL L 85762 : A
|
LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
|
MIL A 83212 : A
|
ALTIMETER, PRESSURE AAU-27/A |
|
MIL A 85672 : 0
|
AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
|
MIL G 26988 : C
|
GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
|
MIL A 81605 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
|
MIL I 83262 : B
|
INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
|
MIL I 83245 : A
|
INDICATOR SET, OIL PRESSURE A/A24J-17 |
|
SAE ARP 4729 : 2017
|
DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
|
MIL I 27680 : C
|
INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
|
MIL A 81370 : 0
|
ASSEMBLY, CENTER STATION 65A132F6 |
|
SAE AS 85075 : 2000
|
TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
|
SAE ARP 731 : 2015
|
GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT |
|
MIL-PRF-15733 /58D:2015
|
FILTERS AND CAPACITORS, RADIO FREQUENCY INTERFERENCE, HERMETICALLY SEALED, STYLE FL63 |
|
MIL D 8708 : C
|
DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
|
MIL T 25502 : C
|
TRUE HEADING COMPUTER GROUP AN/AJA-I |
|
MIL PRF 83726 : H
|
RELAYS, HYBRID AND SOLID STATE, TIME DELAY, GENERAL SPECIFICATION FOR |
|
MIL I 81453 : A
|
INTERROGATOR SET AN APX 76B(V) |
|
MIL I 27623 : C
|
INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
|
MIL T 85678 : 0
|
TRANSPONDER, RADAR TRACKING |
|
MIL DTL 7627 : G
|
INDICATOR, TURN AND SLIP, 28 V DC |
|
MIL T 81436 : 0
|
TEST SET, ELECTRONIC CIRCUIT PLUG IN UNIT AN/USM-146 |
|
MIL PRF 85676 : A
|
LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
|
MIL A 81296 : D
|
ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
|
MIL I 83117 : B
|
INDICATOR, ANGLE OF ATTACK |
|
MIL S 9320 : C
|
SIGNAL, WARNING, AUDIBLE, FOR HEADSET |
|
MIL PRF 15733/34 : T
|
FILTERS AND CAPACITORS, RADIO FREQUENCY INTERFERENCE, HERMETICALLY SEALED, STYLE FL90 |
|
MIL T 25485 : C
|
TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
|
MIL C 87970 : 0
|
CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
|
MIL I 27848 : B
|
INDICATOR, HORIZONTAL SITUATION AQU-4/A |
|
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 I 38258 : 0
|
INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
|
MIL T 25435 : B
|
TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
|
MIL A 27671 : B
|
AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
|
MIL S 6904 : B
|
SIGNAL, EMERGENCY WARNING, GENERAL SPECIFICATION FOR |
|
MIL E 6051 : D
|
ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
|
MIL T 81223 : 0
|
TEST SET, PNEUMATIC PRESSURE AN/PSM-15C |
|
MIL R 83726/28 : C
|
RELAY, TIME DELAY ON OPERATE, CLASS B, TYPE 1, HERMETICALLY SEALED, DPDT, 10 AMPERES, FIXED TIME, 0.1 TO 500 SECONDS |
|
MIL R 83726/7 : G
|
RELAYS, HYBRID, TIME DELAY, ON PICKUP, TYPE 1, CLASS A, 2 AMPERES, 2PDT, FIXED TIME, 0.06 TO 300 SECONDS |
|
MIL I 27619 : G
|
INDICATORS, ATTITUDE DIRECTOR |
|
MIL C 27505 : B
|
CARTRIDGE, ENGINE STARTER MXU-4A/A |
|
MIL T 5583 : C
|
TRANSMITTER, POSITION, 28 VOLTS DC |
|
MIL HDBK 845 : 1992
|
STANDARD POWER SUPPLY APPLICATIONS HANDBOOK |
|
MIL M 7969 : C
|
MOTOR, ALTERNATING CURRENT, 400 CYCLE, 115/200 VOLT SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
|
MIL A 55368 : 0
|
AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
|
MIL C 85392 : 0
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
|
MIL T 85298 : 0
|
TEST SET, WEAPON CONTROL, AIRCRAFT AN/ASM 184B (V)1 AND AN/ASM 184B (V) 2 |
|
MIL T 25307 : D
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
|
MIL C 38418 : E
|
CONTROL ASSEMBLY, GYROSCOPE, ATTITUDE A/A24G-39 |
|
MIL A 9286 : C
|
AF AMPLIFIER AM-476()/AIC-10 |
|
MIL STD 1818 : A
|
ELECTROMAGNETIC EFFECTS REQUIREMENTS FOR SYSTEMS |
|
MIL I 23524 : A
|
INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
|
MIL PRF 15733/41 : H
|
FILTERS, RADIO FREQUENCY INTERFERENCE, STYLE FL84 |
|
ADS-65-HDBK : 2004
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
|
AECTP-500 : 2016
|
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
|
MIL R 5149 : B
|
ROCKET ENGINE, LIQUID PROPELLANT GENERAL SPECIFICATION FOR |
|
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 T 81134 : 0
|
TEST SET AN/ASM-184 (V) 1 AIRCRAFT WEAPON CONTROL TEST SET AN/ASM-184 |
|
MIL I 26299 : G
|
INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
|
MIL A 81373 : 0
|
ASSEMBLY, QUANTITY SELECT 65A132F9 |
|
MIL I 7802 : A
|
INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
|
MIL I 81049 : A
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
|
MIL C 38333 : 0
|
CONTROLLER, COMPASS SYSTEM C-6448/ASN-55 |
|
MIL R 6466 : B NOTICE 1
|
RELAY, ARMATURE, EXCITER PROTECTION, TYPE A-1 |
|
MIL T 7743 : F
|
TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR |
|
MIL C 85283 : B
|
CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9 |
|
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
|
MIL M 23888 : NOTICE 1
|
MONITOR, RADIO FREQUENCY ID AND 9O2A/AR |
|
MIL DTL 26517 : B
|
POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT GENERAL SPECIFICATION FOR |
|
MIL PRF 85046 : A
|
ACTUATOR, LINEAR, ELECTROMECHANICAL |
|
MIL R 23864 : B
|
RADAR TRANSPONDER AN/DPN-77(*) |
|
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 A 85434 : A
|
AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
|
MIL PRF 32085 : 0
|
RELAYS, ELECTROMAGNETIC, 270 V DC, ESTABLISHED RELIABILITY, GENERAL SPECIFICATION FOR |
|
MIL C 7079 : A
|
CIRCUIT BREAKERS, NON TRIP-FREE GENERAL SPECIFICATION FOR |
|
MIL P 85576 : B
|
POWER SUPPLY PP-2581C/A |
|
MIL D 5025 : C
|
DIRECTION FINDER GROUPS AN/APA-69A AND AN/APA 69C |
|
MIL R 83726/8 : F
|
RELAYS, HYBRID, TIME DELAY, (ON RELEASE), TYPE 2A, CLASS A, 2 AMPERES, 2PDT, FIXED TIME, 0.100 TO 300 SECONDS |
|
MIL T 25627 : C
|
TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
|
MIL C 18244 : A
|
CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
|
SAE AIR 1810 : 2013
|
DESIGN, DEVELOPMENT AND TEST CRITERIA - SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS |
|
SAE AIR 5937 : 2012
|
INFORMATION ON ELECTRIC BRAKES |
|
MIL P 18987 : A
|
PLOTTING BOARD, TACTICAL DISPLAY PT-396/AS |
|
SAE ARP 60493 : 2017
|
GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC) |
|
SAE ARP 5794 : 2014
|
CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
|
SAE ARP 1070E : 2019
|
DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
|
SAE ARP 5584 : 2011
|
DOCUMENT FOR ELECTRIC POWER MANAGEMENT |
|
SAE AS 4941 : 2015
|
AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
|
AEDP-6 : 2014
|
NATO ADVANCED DATA STORAGE INTERFACE REQUIREMENTS AND IMPLEMENTATION GUIDE |
|
SAE AIR 4367 : 2012
|
AIRCRAFT INFLIGHT ICE DETECTORS AND ICING RATE MEASURING INSTRUMENTS |
|
ARINC 575 : 68 SUPP 3
|
MARK 3 SUBSONIC AIR DATA SYSTEM (DIGITAL) DADS |
|
DSCC 90091 : G
|
RELAY, SOLID STATE, HERMETICALLY SEALED, OPTICALLY ISOLATED, 1 OR 2 A, WITH OR WITHOUT CIRCUIT-BREAKER ACTION OR STATUS INDICATION, 6-PIN CERAMIC DUAL-IN-LINE PACKAGE |
|
IEEE 1826 : 2012
|
POWER ELECTRONICS OPEN SYSTEM INTERFACES IN ZONAL ELECTRICAL DISTRIBUTION SYSTEMS RATED ABOVE 100 KW |
|
SAE ARP 1940 : 1993
|
SOLID-STATE FREQUENCY CONVERTER 400 HERTZ, 3-PHASE OUTPUT |
|
EIA IS 647 : 1996
|
REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE EMISSIONS AND SUSCEPTIBILITY CHARACTERISTICS OF EQUIPMENT INTENDED TO OPERATE IN SEVERE ELECTROMAGNETIC ENVIRONMENTS |