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MIL-STD-704 Revision F:2004

Current
Current

The latest, up-to-date edition.

AIRCRAFT ELECTRIC POWER CHARACTERISTICS
Available format(s)

PDF

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
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.
DocumentType
Standard
Pages
41
ProductNote
New child NOT 3 2021 is now added.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
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 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
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, ANTI COLLISION 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-1O13(*)/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 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 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 ARP 731 : 2015 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 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
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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