MIL-I-18802 Revision A:1962
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT
Available format(s)
PDF
Withdrawn date
18-03-1998
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes installation of oil and fuel lines in aircraft.
| DocumentType |
Standard
|
| Pages |
14
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
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| 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 |
| MIL-D-8685 Revision B:1967 | DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| MIL-T-8606 Revision C:1973 | TUBING, STEEL, CORROSION RESISTANT (18-8 STABILIZED AND EXTRA LOW CARBON) |
| MS33786 Revision B:2013 | Fitting, Installation, Flared Tube and Hose, Swivel |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL H 8794 : D | HOSE, RUBBER, HYDRAULIC, FUEL AND OIL RESISTANT |
| MS33515 Revision J:1973 | FITTING END, STANDARD DIMENSIONS FOR BULKHEAD FLARELESS TUBE CONNECTIONS |
| AND10104 : REV 5 | TUBING, STEEL, CORROSION RESISTANT, ROUND, STANDARD DIMENSIONS FOR |
| MS21919 Revision E:1981 | CLAMP, LOOP TYPE, CUSHIONED, SUPPORT |
| MS33656 Revision J:1987 | FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MS33583 Revision C:1993 | TUBING END, DOUBLE FLARE, STANDARD DIMENSIONS FOR |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MS33584 Revision C:1990 | TUBING END, STANDARD DIMENSIONS FOR FLARED |
| MS33611 Revision A:1983 | TUBE BEND RADII |
| MIL H 8795 : D | HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT |
| MIL T 5579 : 0 | TANK, SELF-SEALING OIL, AIRCRAFT |
| MS33514 Revision G:1990 | FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG) |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MS28741 Revision K:2010 | HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE |
| MIL C 22263 : B | COUPLING FUEL LINE, FLEXIBLE, 125 PSI, GENERAL SPECIFICATION FOR |
| MS33790 Base Document:1958 | BEND DATA, MINIMUM, HYDRAULIC, PNEUMATIC, FUEL AND OIL HOSE |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
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