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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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Superseded date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
Superseded by
Published date
12-01-2013
Publisher
| 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Superseded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 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, 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 AS8712 | 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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