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MIL P 7936 : LATEST

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY

Superseded date

23-07-2013

Published date

12-01-2013

DocumentType
Standard
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy

MIL-I-8580 Revision B:1965 INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1
MIL-A-26442 Base Document:1959 ADAPTERS, WAVEGUIDE TO COAXIAL
MIL I 25688 : A INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE
MIL-T-5483 Revision D:1964 TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT
MIL H 81014 : A NOTICE 1 HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C
SAE AS 8181 : 1997 DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR
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-E-5627 Revision B:1965 EXTINGUISHERS, FIRE, CARBON DIOXIDE, PORTABLE
MIL-P-5431 Revision A:1967 Plastic, Phenolic, Graphited Sheets, Rods, Tubes and Shapes
MIL-C-23367 Base Document:1963 Computer, Flight Director, Aircraft
MIL-C-19179 Revision B:1963 COUPLING ASSEMBLY, QUICK-DISCONNECT, FUEL
MIL BULL 343 : A DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
MIL L 21910 : NOTICE 1 LAUNCHER, ROCKET LAU-10/A
MIL I 38120 : A (3) INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A
MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
MIL B 38608 : A BOMB, FIRE, BLU-23/B
MIL-G-23337 Base Document:1962 GAGE - PRESSURE, DIAL INDICATING
MIL-T-21205 Revision B:1960 TRANSMITTER, RATE OF FLOW, FUEL; TRU-12/A (300 - 5000 -15000 PPH)
MIL-T-19576 Revision A:1961 TRANSMITTER, REMOTE COMPASS, THIN WING TYPE ML-1 (UNSTABILIZED)
MIL-C-5604 Revision B:1962 COMPASS, MAGNETIC, PILOTS STANDBY
MIL-I-23870 Base Document:1963 INDICATOR, FUEL RATE OF FLOW, 0 TO 15 GPM
MIL F 5508 : B FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC
MIL-S-6330 Revision H:1965 SURVIVAL KIT, LIFE RAFT
MIL-T-25193 Revision B:1961 Transmitter, Remote Compass, Type C-2 (Unstabilized)
MIL-I-5418 Revision B:1963 INDICATOR: AIRSPEED, PITOT STATIC, SENSITIVE, 50-650 KNOTS
MIL-T-22030 Base Document:1959 TRANSMITTER, RATE OF FLOW, FUEL; TRU 26/A (300 TO 10,000 PPH)
L-P-383 Base Document:1967 PLASTIC MATERIAL, POLYESTER RESIN, GLASS FIBER BASE, LOW PRESSURE LAMINATED
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-G-22169 Base Document:1959 GYRO, VERTICAL AND MOUNT
MIL-C-18053 Revision A:1958 CONTROL AMPLIFIER, ALTITUDE (P-1 AUTOMATIC PILOT RADAR SET, AN/APN-22)
MIL-P-3584 Revision A:1963 PLASTIC SHEET, POLYVINYL CHLORIDE, PLASTICIZED, ELASTOMERIC
MIL-V-8712 Revision A:1965 VALVE, AIR RELIEF, LOW PRESSURE
MIL-G-23676 Base Document:1963 GAGE, PRESSURE, DIAL INDICATING, OXYGEN, HIGH PRESSURE
MIL-P-25726 Revision B:1959 PROBE, TOTAL TEMPERATURE, TYPE MA-1
MIL-R-5520 Revision C:1964 RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE
MIL T 25439 : A (1) TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3
MIL-A-27328 Base Document:1960 AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-7
MIL-I-5482 Revision C:1960 INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE
MIL-A-23622 Base Document:1963 ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT
MIL-I-18804 Revision B:1964 INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH
MIL-I-21718 Base Document:1958 Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots
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-P-25632 Revision B:1960 PITOT STATIC TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED, 115 VOLT, 4OO HZ, TYPE MA-1
MIL-I-25931 Revision B:1964 INDICATOR, POSITION, LANDING GEAR, SYMBOL-INDICATING, INTEGRALLY LIGHTED
MIL-R-25535 Revision A:1959 ROCKET MOTOR, AERONAUTICAL, PRELIMINARY FLIGHT RATING TEST FOR
MIL-C-81003 Base Document:1964 Clinometer, Elevation ML-591/U
MIL-I-7723 Revision B:1965 INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION 70 DEG TO PLUS 150 DEG.C DUAL
MIL I 25137 : A INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED, TYPE ME-4
MIL-I-27280 Revision A:1960 INDICATOR, INDICATED AIRSPEED AVU-10/A
MIL-R-23057 Base Document:1961 Regulator, Compressed Air, High Pressure (3500 PSI)
MIL-G-23723 Base Document:1964 Gyroscope, Rate Switching CN-495/AJB-3
MIL G 23701 : 0 MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52
MIL I 7069 : A NOTICE 1 INDICATORS, TACHOMETER, ELECTRIC, PERCENT SPEED TYPE, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL P 6074 : A PRESERVATION, PACKAGING AND PACKING OF PROPELLERS, PROPELLER SPARES AND PROPELLER ACCESSORIES
MIL-D-8181 Revision B:1965 DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR
MIL-B-38977 Base Document:1968 Bomb, Practice BDU-38/B
MIL I 6424 : A NOTICE 1 INDICATOR, INDUCTION COMPASS, TYPE V 8
MIL-F-23447 Base Document:1962 FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF
MIL-A-81307 Base Document:1965 Amplifiers, Servomotor, General Specification
MIL A 8897 : A ACCUMULATORS, HYDRAULIC CYLINDRICAL, 3,000 PSI AIRCRAFT TYPE 11 SYSTEMS
MIL-A-22165 Base Document:1959 Amplifier, Compass, Servo (Type MF-1 Compass)
MIL-I-21685 Base Document:1958 INDICATOR, COMPASS REPEATER, ROTATING DIAL, TYPE MW-2
SAE AS 8712 : 2013 VALVE; AIR RELIEF, LOW PRESSURE
MIL-H-23799 Base Document:1963 HOSE ASSEMBLY, METAL, TRANSFER, LIQUID OXYGEN
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-P-8045 Revision B:1964 PLASTIC SELF-SEALING AND NON SELF-SEALING TANK BACKING MATERIAL
MIL R 25534 : A NOTICE 1 ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
MIL-G-27693 Revision A:1962 GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH
MIL-G-5678 Revision C:1964 GAGE PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE
MIL G 5413 : D NOTICE 1 GENERATOR, TACHOMETER, FOUR POLE
MIL-E-81512 Base Document:1968 ENCODER, SHAFT POSITION TO DIGITAL, CONTACT TYPE, ALTITUDE REPORTING, GENERAL SPECIFICATION FOR
MIL-C-6092 Revision A:1960 COMPUTER, AIRCRAFT LOAD BALANCING
MIL-I-7075 Revision A:1965 INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE
MIL-R-8791 Revision D:1982 RETAINER, PACKING, HYDRAULIC, AND PNEUMATIC, TETRAFLUOROETHYLENE RESIN
MIL-I-5416 Revision B:1962 INDICATOR, INDICATED AIRSPEED 10-150 KNOTS
MIL B 38634 : LATEST BOMB, FIRE, BLU 32A B
MIL-I-23524 Revision A:1986 INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V)
MIL G 9398 : C GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT
MIL R 25532 : A ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
MIL-I-7802 Revision A:1967 INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE]
MIL-I-7906 Revision A:1961 INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB 1
MIL-T-6302 Revision B:1964 TRANSMITTER, PRESSURE, FUEL 0-600 PSI
MIL-C-7942 Revision B:1966 CONNECTORS, HOSE, QUICK-DISCONNECT, ANTI "G" SUIT
MIL-I-25992 Revision A:1959 INDICATOR, BEARING DISTANCE HEADING ID 526A ARN
MIL-S-7886 Revision B:1962 SPARK PLUG, SHIELDED, AIRCRAFT RECIPROCATING ENGINE, GENERAL SPECIFICATION FOR

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