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  • MIL-STD-704 Revision F:2004

    Current The latest, up-to-date edition.

    AIRCRAFT ELECTRIC POWER CHARACTERISTICS

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    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    FOREWORD
    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. DEFINITIONS
    4. GENERAL REQUIREMENTS
    5. DETAILED REQUIREMENTS
    6. NOTES
    CONCLUDING MATERIAL

    Abstract - (Show below) - (Hide below)

    Sets up the requirements and characteristics of aircraft electric power provided at the input terminals of electric utilization equipment.

    General Product Information - (Show below) - (Hide below)

    Committee AREA SESS
    Development Note 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.
    Document Type Standard
    Product Note New child NOT 3 2021 is now added.
    Publisher US Military Specs/Standards/Handbooks
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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 AN/ASN-50(*)
    MIL-PRF-83287-1 Revision D:2007 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 Revision C:1964 CODER RECEIVER TRANSMITTER K & Y532A 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
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    MIL O 38338 : C (1) OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR
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    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
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    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
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    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 GROUPS 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
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    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
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    SAE AS 4941 : 2015 AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS
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    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
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    SAE ARP 1940 : 1993 SOLID-STATE FREQUENCY CONVERTER 400 HERTZ, 3-PHASE OUTPUT
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    Standards Referencing This Book - (Show below) - (Hide below)

    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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