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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY
Published date
12-01-2013
Publisher
Superseded date
23-07-2013
Superseded by
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| 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Superseded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 (No S/S Document) |
| MIL-A-26442 Base Document:1959 | Adapters, Waveguide-to-Coaxial (No S/S Document) |
| 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 (No S/S Document) |
| MIL H 81014 : A NOTICE 1 | HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
| SAE AS8181A | 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, Altitude, ARU-14/A, Remote (No S/S Document) |
| MIL-E-5627 Revision B:1965 | Extinguishers, Fire, Carbon Dioxide, Portable (No S/S Document) |
| 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 (S/S by MIL-C-24788) |
| 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 Refueling Systems, General Specification for |
| MIL B 38608 : A | BOMB, FIRE, BLU-23/B |
| MIL-G-23337 Base Document:1962 | Gages, 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) (NO S/S DOCUMENT) |
| MIL-C-5604 Revision B:1962 | Compass, Magnetic, Pilot\'s Standby (S/S by SAE-AS5604) |
| MIL-I-23870 Base Document:1963 | Indicator, Fuel Rate of Flow, 0 to 15 GPM (No S/S Document) |
| MIL F 5508 : B | FUSE, AIRCRAFT AUTOMATIC QUANTITY MEASURING HYDRAULIC |
| MIL-S-6330 Revision H:1965 | SURVIVAL KITS, LIFE RAFT (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| MIL-C-18053 Revision A:1958 | Control Amplifier, Altitude (P-1 Automatic Pilot Radar Set, AN/APN-22) (No S/S Document) |
| MIL-P-3584 Revision A:1963 | PLASTIC SHEET, POLYVINYL CHLORIDE, PLASTICIZED, ELASTOMERIC (NO S/S DOCUMENT) |
| MIL-V-8712 Revision A:1965 | VALVE, AIR RELIEF, LOW PRESSURE8(ASG) (S/S BY SAE-AS8712) |
| MIL-G-23676 Base Document:1963 | Gage, Pressure, Dial Indicating Oxygen, High Pressure (No S/S Document) |
| MIL-P-25726 Revision B:1959 | Probe, Total Temperature, Type MA-1 |
| MIL-R-5520 Revision C:1964 | RESERVOIRS, AIRCRAFT, HYDRAULIC, NON-SEPARATED TYPE (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| MIL-I-5482 Revision C:1960 | Indicator, Pressure, Synchro, Aircraft, 165 Degree Scale (No S/S Document) |
| 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 (No S/S Document) |
| 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, 400 HZ, TYPE MA-1 (NO S/S DOCUMENT) |
| MIL-I-25931 Revision B:1964 | Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No S/S Document) |
| MIL-R-25535 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, PRELIMINARY FLIGHT RATING TEST FOR (NO S/S DOCUMENT) |
| MIL-C-81003 Base Document:1964 | Clinometer, Elevation ML-591/U |
| MIL-I-7723 Revision B:1965 | Indicator, Temperature, Electrical Resistance, Multifunction, -70 Degrees (No S/S Document) |
| 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 (No S/S Document) |
| 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 (S/S by SAE-AS8181) |
| 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 (No S/S Document) |
| 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 AS8712 | Valve; Air Relief, Low Pressure |
| MIL-H-23799 Base Document:1963 | Hose Assembly, Metal, Transfer, Liquid Oxygen (No S/S Document) |
| MIL-I-27552 Revision C:1995 | Indicator, Temperature, Thermocouple EHU-15A/A, Potentiometer Type, White Lighted |
| MIL-S-21277 Revision A:1958 | SWITCHES, LIQUID LEVEL, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| MIL-G-5678 Revision C:1964 | Gage, Pressure, Dial Indicating, Manifold Pressure (No S/S Document) |
| 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 (No S/S Document) |
| MIL-C-6092 Revision A:1960 | Computer, Aircraft Load Balancing (No S/S Document) |
| 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 (S/S by SAE-AS8791) |
| 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, MS28088, 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 (S/S BY SAE-AS6302) |
| 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 and ID-798/ARN (No S/S Document) |
| MIL-S-7886 Revision B:1962 | Spark Plug, Shielded, Aircraft Reciprocating Engine, General Specification For |
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