MIL-STD-704 Revision F:2004
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AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
CONCLUDING MATERIAL
Sets up the requirements and characteristics of aircraft electric power provided at the input terminals of electric utilization equipment.
| Committee |
AREA SESS
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| DevelopmentNote |
F NOTICE 1 - Notice of Validation. (01/2009) F NOTICE 2 - Notice of Validation. (11/2013) Supersedes SAE AS 5625. (06/2014) New child NOT 3 2021 is now added.
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| DocumentType |
Standard
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| Pages |
41
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| ProductNote |
New child NOT 3 2021 is now added.
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| Supersedes |
| SAE AS 5372 : 2015 | FUSE, CURRENT LIMITER TYPE, AIRCRAFT |
| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| MIL-P-0081653 Revision C:1987 | POWER CONTROLLER, SOLID STATE, GENERAL SPECIFICATION FOR |
| MIL C 83166 : LATEST | CONVERTER MULTIPLEXER, SIGNAL DATA, GENERAL SPECIFICATION FOR |
| AFGS-87213 Revision B:1993 | 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 Base Document:1986 | ACTUATOR, ELECTROMECHANICAL, LINEAR |
| MIL-M-8609 Revision B:1965 | 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 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-R-38370 Revision B:1972 | RECORDING SET, FLIGHT DATA A/A24U-10 |
| MIL-I-18856 Revision B:1969 | INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
| MIL-T-38034 Revision E:1970 | 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 Base Document:1970 | PITOT STATIC TUBE, L-SHAPED, COMPENSATED, ELECTRICALLY HEATED, GENERAL SPECIFICATION FOR |
| MIL-C-87979 Base Document:1987 | CLOCK, AIRCRAFT, ELECTRONIC |
| MIL-T-81998 Base Document:1975 | TEST SET, RADIO SET AN/ARM-165 |
| MIL-R-29583 Base Document:1992 | RADIO SET |
| MIL-S-85018 Revision A:1978 | Second Order Attitude Reference System (Soars) AN/ASN-116 |
| MIL-PRF-83287 Revision G:2007 | INDICATORS, FAULT LOCATING, GENERAL SPECIFICATION FOR |
| MIL-R-83726-24 Revision M:2016 | 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 Revision A:2011 | BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-5809 Revision G:1987 | CIRCUIT BREAKERS, TRIP-FREE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-R-38435 Revision B:1968 | RECORDING SET, SIGNAL DATA A/A 24U-6 |
| MIL-E-23001 Revision B:1976 | ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
| JSGS-87231 Revision A:1995 | ENGINES, AIRCRAFT, TURBINE |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-T-83460 Base Document:1975 | TRANSDUCER, MOTIONAL PICKUP TRU-164/A |
| MIL-F-87154 Base Document:1980 | 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 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
| MIL-I-38121 Revision C:1989 | INDICATOR, PRESSURE, EGU-9/A |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-A-22145 Revision C:1992 | ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL-PRF-32272 Revision A:2016 | INTEGRATED POWER MANAGEMENT CENTER (IPMC) |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL-PRF-83383 Revision F:2017 | Circuit Breakers, Remote Control, Thermal, Trip Free General Specification For |
| MIL F 5373 : D | FUSEHOLDER, BLOCK TYPE, AIRCRAFT |
| MIL-PRF-8565 Revision K:2001 | 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 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MIL-B-28873 Base Document:1983 | 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 Revision C:1987 | TRANSFORMER AND INDUCTORS [AUDIO, POWER AND HIGH POWER PULSE] INDUCTOR, POWER TF5S04ZZ |
| 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-A-85072 Revision A:1987 | ACTUATOR, ELECTROMECHANICAL, LINEAR |
| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-I-27709 Revision A:1962 | INDICATOR, ATTITUDE ARU-14/A, REMOTE |
| MIL-R-81046 Base Document:1964 | RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
| MIL-HDBK-704-1 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics (Part 1 of 8 Parts) |
| MIL-HDBK-704-5 Base Document:2004 | 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 Revision E:2011 | RELAY, ELECTROMAGNETIC, 50 AMPERES, DC, SPDT, HERMETICALLY SEALED |
| MIL-A-22669 Base Document:1960 | Amplifier-Power Supply-Receiver AM-2310(*)/ASQ and Antenna AS-909(*)/ARA-48 |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-55503 Base Document:1966 | ATTITUDE HEADING REFERENCE SET AN/ASN-76 |
| 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-A-25546 Revision C:1970 | Amplifier, Audio Frequency AM-944/AIC-13 |
| MIL-R-85669 Base Document:1988 | 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 Base Document:1970 | ASSEMBLY, STATION TRANSFER 65A132F7 |
| MIL B 83424 : 0 | BATTERY SYSTEMS, SEALED CELL, NICKEL CADMIUM, INTEGRAL CHARGE CONTROL, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-27193 Revision D:2017 | INDICATOR, ATTITUDE ARU-2B/A |
| MIL-R-83726-22 Revision F:2008 | Relays, Solid State, Repeat Cycle Timer, Type IV, Class C, SPST, 250 Milliamperes (No S/S Document) |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| MIL-PRF-83726-13 Revision L:2016 | 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 Requirements for medical devices used in air ambulances |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL C 55629 : B | CIRCUIT BREAKERS, MAGNETIC, UNSEALED, TRIP-FREE, SINGLE POLE, FRONT MOUNTED, AUXILIARY CONTACTS (1 TO 100 AMPERES) |
| MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-35-72 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTROMECHANICAL, ROTARY |
| 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)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-STD-35-73 Base Document:1974 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, ACTUATORS, ELECTROMECHANICAL, LINEAR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| 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)/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 |
| MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-PRF-55629 Revision E:2011 | CIRCUIT BREAKERS, MAGNETIC, UNSEALED OR PANEL SEAL, TRIP-FREE, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-DTL-6162 Revision C:2000 | 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 Base Document:1983 | Concentrator, Oxygen, GGU-7/A |
| MIL-E-29581 Base Document:1991 | 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 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL-PRF-28750-9 Revision G:2015 | 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 Base Document:1983 | INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
| MIL-G-83872 Revision A:1977 | GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU 60A |
| DOD-STD-35-82 Revision A:1979 | 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 Base Document:1963 | TEST SET, DOPPLER RADAR AN/APM-148(*) |
| MIL-J-23013 Base Document:1961 | JUNCTION BOX JEU-25 (*)/A |
| MIL-STD-35-96 Base Document:1976 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM, REGULATORS, CURRENT AND VOLTAGE AC, AND DC |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-HDBK-258 Base Document:1979 | INTERFACE CONTROL DOCUMENT FOR INFRARED DETECTING SET AN/AAS-36 |
| MIL-A-81621 Base Document:1969 | ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
| MIL-STD-2120 Base Document:1984 | CONNECTORS, ELECTROMAGNETIC INTERFERENCE (EMI) FILTER CONTACT |
| MIL-D-83029 Revision A:1968 | DRIVE ASSEMBLY, CONSTANT SPEED, GENERAL SPECIFICATION FOR |
| MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
| 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-PRF-83726-35 Revision D:2013 | 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 Base Document:2004 | 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 Revision B:1960 | TRANSMITTER, RATE OF FLOW, FUEL; TRU-12/A (300 - 5000 -15000 PPH) |
| MIL-R-83726-14 Revision E:2016 | 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 Revision K:2018 | 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 Base Document:1981 | 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 Revision A:1965 | Attitude Heading Reference System HEADING AN/ASN-50(*) |
| MIL-PRF-83287-1 Revision D:2007 | INDICATORS, FAULT LOCATING, FLAG INDICATING, MECHANICAL RESET |
| SAE ARP1148B | 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 Revision C:1964 | Coder Receiver Transmitter KY-532A/ASQ |
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL T 23913 : 0 | TEST SET, INTERCOMMUNICATION SET AN/A1M AND 3A |
| MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| 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 |
| 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 Base Document:1984 | AMPLIFIER-MIXER AM-7157/DKT-59 |
| 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-85648 Base Document:1983 | 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 Revision A:1991 | 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 Revision D:1970 | 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 Revision B:2012 | BATTERY, STORAGE, AIRCRAFT, MAINTENANCE-FREE, 24-VOLT, 1.5-AMPERE-HOUR |
| MIL-HDBK-87244 Base Document:1995 | AVIONICS/ELECTRONICS INTEGRITY |
| MIL-D-8685 Revision B:1967 | 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 (Withdrawn 2024) |
| 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 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| MIL-S-8812 Revision D:1975 | 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 Revision F:1976 | 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 Base Document:1964 | AMPLIFIER-POWER SUPPLY AM-4080/ASN-55, LEVELLING |
| MIL-R-21073 Revision A:1960 | Recorder, Magnetic Distortion, RO-32/ASQ |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| 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-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-A-23887 Revision A:1965 | Altimeter Set, Electronic AN/APN-141(V) |
| MIL-M-85522 Revision A:1991 | MONITOR, OXYGEN CRU-91/A |
| MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
| MIL-P-87210 Base Document:1984 | PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
| 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-I-87216 Base Document:1984 | INSTRUMENT SYSTEMS, 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 C 85629 : A (1) | CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
| MIL-I-81454 Base Document:1967 | INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
| MIL-D-81641 Base Document:1972 | Display, Head-up, General Specification for |
| MIL-C-19941 Revision A:1966 | CONTROLLER, S-2 COMPASS, TYPE |
| MIL-T-81760 Revision A:1970 | TEST SET, PROGRAMMER AN/USM-299A |
| MIL-A-81359 Base Document:1970 | Aircraft Weapons Release Set AN/AWE-1 |
| MIL I 85581 : 0 | INTERVALOMETER, ROCKET LAUNCHER, REUSABLE |
| MIL-D-8804 Revision B:1993 | DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-85300 Base Document:1982 | COOLER, CRYOGENIC DETECTOR |
| MIL-PRF-83726-29 Revision J:2013 | 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 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-G-45279 Base Document:1975 | 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 Revision A:1984 | CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
| SAE AS 5716 : 2012 | STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
| MIL-A-81369 Base Document:1970 | Assembly, Left-Right Station 65A132F5 |
| MIL-R-83726-12 Revision F:2016 | 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 Revision A:1965 | RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
| MIL-PRF-83174 Revision E:2012 | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL-C-18277 Revision B:1961 | COUPLER, ANTENNA CU-351/AR AND COUPLER, ANTENNA CU-509/AR |
| MIL-T-81832 Base Document:1971 | TEST SET, ALTIMETER SET AN/APM-348 |
| MIL-PRF-83726-28 Revision K:2013 | Relays, Hybrid, Time Delay (on Operate), Class B, Type I, 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 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| MIL-T-27200 Revision C:1975 | TRANSMITTER, RATE GYROSCOPE TRU-2A/A |
| MIL-R-83726-23 Revision E:2015 | RELAYS, HYBRID, TIME DELAY (ON RELEASE), TYPE 2B, CLASS B, 10 AMPERES, 4PDT, HERMETICALLY SEALED |
| MIL-G-85468 Base Document:1981 | GENERATOR CONTROL INDICATOR SG-118/AST-4(V) |
| MIL-T-85601 Base Document:1983 | 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 Base Document:2004 | 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 Base Document:2004 | 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 Revision G:2008 | 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 Revision B:2010 | Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for |
| MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| MIL-DTL-27715 Revision C:2014 | 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 Revision B:2009 | FILTERS, RADIO FREQUENCY INTERFERENCE, HERMETICALLY SEALED, STYLE FL64 |
| MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-G-81665 Base Document:1971 | GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
| MIL-A-23622 Base Document:1963 | 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 Revision E:2010 | Signal, Warning, Audible, for Headset, Type MA-1 |
| MIL-PRF-83287-2 Revision E:2007 | INDICATORS, FAULT LOCATING, FLAG INDICATING, ELECTRICAL RESET |
| MIL-DTL-38394 Revision E:2009 | Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI |
| MIL-B-19906 Revision A:1961 | BOMB RACK AND ROCKET LAUNCHER, COMBINATION, AERO 15 SERIES |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL-PRF-22885-113 Revision A:2010 | 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 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-R-28894 Base Document:1986 | RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-T-81587 Revision A:1971 | TIMER ASSEMBLY RAIN REPELLENT |
| MIL C 49175 : B | COOLER, CRYOGENIC, MECHANICAL HD-1033B/UA AND HD-1033C/UA |
| MIL-E-29581-1 Base Document:1991 | 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 Revision B:2012 | CLOCK, AIRCRAFT, ELECTRONIC |
| MIL-A-19939 Revision A:1966 | AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| MIL-PRF-83726-30 Revision K:2018 | 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 Revision A:2013 | Air Vehicle Subsystems |
| MIL-C-85247 Base Document:1982 | 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 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL-T-63520 Base Document:1981 | TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, GUN CONTROL ASSEMBLY FOR |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-C-26485 Revision D:1968 | CONTROL ASSEMBLY, ATTITUDE, GYROSCOPIC AF/A24G-1A |
| 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-T-85026 Revision D:1988 | 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 Revision D:2013 | 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 Base Document:1973 | 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 Revision H:2017 | 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 Revision F:1984 | CUTOUT RELAY, ENGINE GENERATOR |
| MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
| MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
| MIL-PRF-24711 Revision B:2008 | Switch, Proximity, Solid-State |
| MIL-G-23723 Base Document:1964 | 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 Base Document:1960 | 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 Revision H:2015 | 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 Revision D:2008 | TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-R-7051 Revision A:1966 | 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 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-HDBK-704-4 Base Document:2004 | 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 Revision C:2012 | Light, Beacon, Anti-Collision, Aircraft |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-E-25499 Revision C:1970 | ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
| MIL-HDBK-87213 Revision A:2005 | ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
| MIL-B-85584 Revision B:1995 | BATTERY RELAY CONTROL UNIT, AIRCRAFT |
| MIL-F-23447 Base Document:1962 | FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
| MIL-T-38306 Base Document:1964 | TRANSMITTER, RATE GYROSCOPE T 970/AJB - 7 |
| MIL-T-81921 Base Document:1973 | 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 Revision D:2010 | SIGNAL AND SIGNAL/INTERCOMMUNICATION AMPLIFIERS, UNIVERSAL, AERIAL REFUELING |
| MIL-DTL-81014 Revision B:2001 | HOOK, HELICOPTER EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| MIL-HDBK-704-8 Base Document:2004 | 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 Revision A:1971 | ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-S-38399 Revision A:1975 | STARTER, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR |
| SAE AS 47643 : 2017 | VERIFICATION METHODS FOR MIL-STD-1760E AIRCRAFT STATION INTERFACES |
| MIL-B-23072 Base Document:1961 | BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR |
| MIL-I-27247 Revision C:1985 | INDICATOR, TEMPERATURE, SYNCHRO |
| MIL-PRF-83726-20 Revision G:2015 | 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 Base Document:1973 | TEST SET, RADIO, AN/ARM-156 |
| MIL-P-85573 Base Document:1983 | 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 Revision A:1973 | Navigational Set, TACAN AN/ARN-84 (V) |
| MIL-HDBK-704-6 Base Document:2004 | 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 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| MIL-A-81403 Base Document:1967 | ALTIMETER-ENCODER, AAU-21/A |
| MIL-T-63536 Base Document:1981 | TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, LOGIC CONTROL UNIT ASSEMBLY FOR |
| MIL-I-81400 Base Document:1966 | INSTRUMENT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-22424 Revision A:1967 | 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 ARP1070D | 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 Revision H:2014 | 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 Revision C:1979 | RECEIVING-DECODING GROUP AN/ARA-63 |
| MIL-A-81372 Base Document:1970 | ASSEMBLY, PRIORITY LOGIC 65A132F8 |
| MIL-A-49079 Revision A:1986 | ALTIMETER SET, ELECTRONIC AN/APN-209(V) (UNITS OF) |
| DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
| MIL-G-23083 Revision C:1972 | Gyroscope, Rate Switching MS 17399 |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-B-23431 Revision B:1993 | BEACON, RADAR AN/APN-154(V) |
| MIL-G-45280 Base Document:1975 | GYROMAGNETIC COMPASS SET AN/ASN-430 |
| 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 T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
| MIL-D-81357 Revision A:1970 | Display Group, Tactical Data AN/ASA-70 |
| MIL-T-81831 Base Document:1971 | TEST SET, ALTIMETER SET AN/APM-347 |
| ISO 22072:2011 | Aerospace — Electrohydrostatic actuator (EHA) — Characteristics to be defined in procurement specifications |
| MIL-T-85472 Revision A:1987 | TEST SET, GROUP OQ-169A/DSM-96A |
| MIL S 8932 : A | SWITCH, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-B-85099 Base Document:1978 | BATTERY, WET PRIMARY FOR AN/DKT-37(V) TELEMETRY PACKAGE |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| SAE AIR 4094 : 2016 | AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS |
| MIL-A-27670 Revision D:1994 | AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-A-85672 Base Document:1987 | AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
| MIL-I-83262 Revision B:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
| MIL-I-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
| SAE ARP 4729 : 2017 | DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
| MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
| MIL-A-81370 Base Document:1970 | Assembly, Center Station 65A132F6 |
| SAE AS 85075 : 2000 | TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR |
| SAE ARP731C | GENERAL REQUIREMENTS FOR APPLICATION OF VAPOR CYCLE REFRIGERATION SYSTEMS FOR AIRCRAFT |
| MIL-PRF-15733-58 Revision D:2015 | FILTERS AND CAPACITORS, RADIO FREQUENCY INTERFERENCE, HERMETICALLY SEALED, STYLE FL63 |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL T 25502 : C | TRUE HEADING COMPUTER GROUP AN/AJA-I |
| MIL-PRF-83726 Revision H:2017 | Relays, Hybrid and Solid State, Time Delay, General Specification for |
| MIL-I-81453 Revision A:1977 | INTERROGATOR SET AN APX 76B(V) |
| MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
| MIL-T-85678 Base Document:1974 | TRANSPONDER, RADAR TRACKING |
| MIL-DTL-7627 Revision G:2010 | INDICATOR, TURN AND SLIP, 28 V DC |
| MIL-T-81436 Base Document:1966 | TEST SET, ELECTRONIC CIRCUIT PLUG IN UNIT AN/USM-146 |
| MIL-PRF-85676 Revision A:2006 | LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY |
| MIL-A-81296 Revision D:1985 | ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
| MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
| MIL S 9320 : C | SIGNAL, WARNING, AUDIBLE, FOR HEADSET |
| MIL-PRF-15733-34 Revision T:2015 | Filters and Capacitors, Radio Frequency Interference, Hermetically Sealed, Style FL90 |
| MIL-T-25485 Revision C:1974 | TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-A-81423 Base Document:1966 | ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-73 |
| MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
| MIL T 25435 : B | TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR |
| MIL-A-27671 Revision B:1965 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-11 |
| MIL-S-6904 Revision B:1965 | Signal, Emergency Warning, General Specification For |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MIL-T-81223 Base Document:1965 | 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 Revision G:2015 | RELAYS, HYBRID, TIME DELAY, ON PICKUP, TYPE 1, CLASS A, 2 AMPERES, 2PDT, FIXED TIME, 0.06 TO 300 SECONDS |
| MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
| MIL-C-27505 Revision B:1967 | Cartridge, Engine Starter MXU-4A/A |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-HDBK-845 Base Document:1992 | STANDARD POWER SUPPLY APPLICATIONS HANDBOOK |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL-A-55368 Base Document:1972 | AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
| MIL-C-85392 Base Document:1987 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
| MIL-T-85298 Base Document:1979 | TEST SET, WEAPON CONTROL, AIRCRAFT AN/ASM 184B (V)1 AND AN/ASM 184B (V) 2 |
| MIL-T-25307 Revision D:1985 | TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1 |
| MIL-C-38418 Revision E:1981 | Control Assembly, Gyroscope, Attitude A/A24G-39 |
| MIL-A-9286 Revision C:1969 | AF AMPLIFIER AM-476()/AIC-10 |
| MIL-STD-1818 Revision A:1993 | ELECTROMAGNETIC EFFECTS REQUIREMENTS FOR SYSTEMS |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL-PRF-15733-41 Revision H:2004 | 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 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-T-81134 Base Document:1976 | TEST SET AN/ASM-184 (V) 1 AIRCRAFT WEAPON CONTROL TEST SET AN/ASM-184 |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-A-81373 Base Document:1970 | ASSEMBLY, QUANTITY SELECT 65A132F9 |
| MIL-I-7802 Revision A:1967 | INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
| 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 R 6466 : B NOTICE 1 | RELAY, ARMATURE, EXCITER PROTECTION, TYPE A-1 |
| MIL-T-7743 Revision F:1993 | TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-C-85283 Revision B:1994 | 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 Revision B:2000 | Power Supply, Transformer-Rectifier, Aircraft, General Specification for |
| MIL-PRF-85046 Revision A:2015 | ACTUATOR, LINEAR, ELECTROMECHANICAL |
| 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-T-81821 Base Document:1969 | TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
| MIL-A-85434 Revision A:1983 | AMPLIFIER, TRAVELING WAVE TUBE AM-6937/DLQ-3B |
| MIL-PRF-32085 Base Document:2001 | RELAYS, ELECTROMAGNETIC, 270 V DC, ESTABLISHED RELIABILITY, GENERAL SPECIFICATION FOR |
| MIL-C-7079 Revision A:1965 | CIRCUIT BREAKERS, NON TRIP-FREE GENERAL SPECIFICATION FOR |
| MIL-P-85576 Revision B:1987 | POWER SUPPLY PP-2581C/A |
| MIL-D-5025 Revision C:1961 | Direction Finder Group AN/APA-69A and AN/APA-69C |
| MIL-R-83726-8 Revision F:2015 | 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 Revision A:1962 | 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 Revision A:1962 | 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 | IEEE Standard for 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 |
| MIL-HDBK-704-6 Base Document:2004 | 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-HDBK-704-1 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics (Part 1 of 8 Parts) |
| MIL-HDBK-704-5 Base Document:2004 | 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-HDBK-704-8 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 28 VDC (Part 8 of 8 Parts) |
| MIL-HDBK-704-2 Base Document:2004 | 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-704-4 Base Document:2004 | 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) |
| MIL-HDBK-704-7 Base Document:2004 | Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 270 VDC (Part 7 of 8 Parts) |
| MIL-HDBK-704-3 Base Document:2004 | 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) |
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