MIL-A-19736 Revision A:1960
Current
Current
The latest, up-to-date edition.
Air Refueling Systems, General Specification for
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Published date
05-08-1960
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€16.67
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1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
Describes the general requirements for design, installation and test of probe and drogue air refueling systems for fixed wing aircraft.
| DocumentType |
Standard
|
| Pages |
17
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the general requirements for design, installation and test of probe and drogue air refueling systems for fixed wing aircraft. Detail requirements necessary to completely define specific equipment will be set forth in a detail specification or drawing provided by the procuring activity or contractor.
| ATP 3.3.4.6 : 2016 | AIR-TO-AIR (AERIAL) REFUELING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 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 |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | 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)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| SAE ARP694C | Aerial Refueling Lights - Design Criteria |
| STANAG 3447 : 2016 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-A-8865 Revision B:1987 | Airplane Strength and Rigidity Miscellaneous Loads |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR (S/S BY NASM33540) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-P-5315 Revision B:1964 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT (S/S BY SAE-AMS-P-5315) |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MS 33633 : LATEST | |
| MIL S 6744 : LATEST | |
| MIL-A-8591 Revision H:1990 | Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase); General Design Criteria for (S/S by MIL-STD-8591) |
| MIL R 6855 : E | RUBBER, SYNTHETIC, SHEETS, STRIPS, MOLDED OR EXTRUDED SHAPES |
| MS29513 Revision C:1966 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, \"O\" RING (S/S BY SAE-AS29513) |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MS33588 Revision E:1984 | Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588) |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK (S/S BY NASM20995) |
| MIL-F-17874 Revision B:1965 | Fuel Systems, Aircraft, Installation and Test of |
| MIL P 7936 : LATEST | PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL R 6106 : J | RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES |
| MIL-S-4040 Revision G:2012 | Solenoid, Electrical General Specification for (No S/S Document) |
| MIL-P-6906 Revision B:1969 | Plates, Identification, Aircraft |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL-T-7928 Revision G:1976 | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification for (S/S BY SAE-AS7928) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL-L-19537 Revision C:1965 | Lacquer: Acrylic-Nitrocellulose Gloss (for Aircraft use) (S/S by MIL-L-81352) |
| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-I-18802 Revision A:1962 | Installation of Fuel and Oil Lines, Aircraft (S/S by SAE-AS18802) |
| MIL C 26482 : G | CONNECTOR, ELECTRICAL (CIRCULAR, MINIATURE, QUICK DISCONNECT, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
| MIL-C-5501 Revision G:1989 | Caps and Plugs, Protective, Dust and Moisture Seal, General Specification for (S/S by NAS847) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-P-7962 Revision D:1980 | PRIMER COATING, CELLULOSE-NITRATE MODIFIED ALKYD TYPE, CORROSION-INHIBITING, FAST-DRYING (FOR SPRAY APPLICATION OVER PRETREATMENT COATING) (NO S/S DOCUMENT) |
| MIL-H-4495 Revision D:1985 | Hose Assembly, Rubber, Aerial Refueling |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MS33547 Revision C:1957 | PINS, SPRING, FUNCTIONAL LIMITATIONS OF (S/S BY NASM33547) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
| MIL N 25027 : G | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
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