MIL T 6396 : E
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING
Available format(s)
PDF
Superseded date
28-07-2008
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Requirements for three types of non-self-sealing internal removable, propulsion fluid system tanks, including fittings for aircraft use.
| Committee |
FSC 1560
|
| DevelopmentNote |
E NOTICE 1 - Notice of Inactivation for New Design. E NOTICE 2 - Notice of Reactivation. (08/2006)
|
| DocumentType |
Standard
|
| Pages |
43
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| 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 T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
| 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)/7(2011) : 2011 | 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)/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 |
| 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 |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| SAE AIR 1664 : 2013 | AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS |
| MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| MIL-P-46111 Revision C:1978 | PLASTIC FOAM, POLYURETHANE (FOR USE IN AIRCRAFT) |
| MIL-D-43699 Revision C:1987 | DRUMS, FABRIC, COLLAPSIBLE, (DRINKING WATER, 55-,250- & 500 GALLON CAPACITIES) |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL-HDBK-806 Base Document:1996 | INSPECTION AND ACCEPTANCE STANDARDS FOR PROPULSION FLUID CELLS AND FITTINGS |
| MIL-P-8045 Revision B:1964 | PLASTIC SELF-SEALING AND NON SELF-SEALING TANK BACKING MATERIAL |
| MIL-R-83309 Base Document:1971 | REPAIR MATERIAL, NITRILE, FUEL, BLADDER, AIRCRAFT |
| MIL-STD-1606 Revision A:1983 | TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS |
| MS29563 Revision B:1974 | FITTING, ATTACHMENT, MOLDED, TANK, FLUSH "O" RING, RECTANGULAR, 10 X 16 |
| MS29559 Revision C:1974 | Fitting, (O) Ring, Circular, Thru Bolt Type, Single Groove, Tank |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
| MIL I 27686 : F | INHIBITOR, ICING, FUEL SYSTEM |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| FED-STD-601 Base Document:1955 | RUBBER, SAMPLING AND TESTING |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MS33786 Revision B:2013 | Fitting, Installation, Flared Tube and Hose, Swivel |
| MS29560 Revision C:1974 | Fitting, (O) Ring, Circular, Threaded Insert Type, Single Groove, Tank |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MS29564 Revision B:1974 | Fitting, Attachment, Molded Tank, Thru Hole, Flush (O) Ring, Rectangular, 12 X 18 |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MIL-P-8045 Revision B:1964 | PLASTIC SELF-SEALING AND NON SELF-SEALING TANK BACKING MATERIAL |
| MS20470 Revision H:1993 | RIVET, SOLID UNIVERSAL HEAD, ALUMINUM ALLOY AND TITANIUM COLUMBIUM ALLOY |
| MS29565 Revision B:1974 | FITTING, ATTACHMENT, MOLDED TANK, FLUSH, "O" RING, RECTANGULAR, 12 X 18 |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MS29558 Revision C:1974 | FITTING, "O" RING, CIRCULAR, COMPRESSION TYPE, SINGLE GROOVE, TANK |
| MS29566 Revision B:1974 | FITTING, ATTACHMENT, MOLDED TANK, THRU HOLE, FLUSH, "O" RING, OVAL, 8 X 12 |
| TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON |
| MS24665 Revision F:1986 | PIN, COTTER (SPLIT) |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MS33581 Revision D:1987 | FITTING O RING GENERAL FEATURES OF CONSTRUCTION |
| FED-STD-191 Revision A:1978 | TEXTILE TEST METHODS |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-S-8879 Revision C:1991 | SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-L-22851 Revision D:1990 | LUBRICATING OIL, AIRCRAFT PISTON ENGINE, (ASHLESS DISPERSANT) |
| MS29568 Revision B:1974 | FITTING, ATTACHMENT, MOLDED TANK, FLUSH, "O" RING, OVAL |
| MIL-L-6082 Revision E:1990 | LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL) |
| MS29567 Revision B:1974 | FITTING, ATTACHMENT, MOLDED TANK, THRU HOLE, FLUSH, "O" RING, RECTANGULAR, 10 X 16 |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| QQ-P-416 Revision F:1991 | PLATING, CADMIUM (ELECTRODEPOSITED) |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| MIL-P-25621 Revision B:1974 | PRESERVATION, PACKAGING AND PACKING OF RUBBER AND NYLON FUEL, OIL AND WATER PLUS ALCOHOL CELLS |
| MIL C 6021 : H NOTICE 1 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| MIL-STD-801 Revision E:2017 | INSPECTION AND ACCEPTANCE STANDARDS FOR FLEXIBLE FUEL CELLS AND FITTINGS |
| O-E-760 Revision D:1987 | ETHYL ALCOHOL (ETHANOL), DENATURED ALCOHOL, PROPRIETARY SOLVENTS & SPECIAL INDUSTRIAL SOLVENTS |
| MS29562 Revision B:1974 | Fitting, Attachment, Molded, Tank, Thru Hole, Flush, (O) Ring, Rectangular, 10 X 16 |
| 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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