MIL-I-18802 Revision A:1962
Withdrawn
Withdrawn
Installation of Fuel and Oil Lines, Aircraft (S/S by SAE-AS18802)
Available format(s)
PDF
Published date
03-13-1962
Publisher
Withdrawn date
03-18-1998
US$20.00
Excluding Tax where applicable
Describes installation of oil and fuel lines in aircraft.
| DocumentType |
Standard
|
| Pages |
14
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
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| 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 (S/S BY SAE-AS4395) |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
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| MS33584 Revision C:1990 | TUBING END STANDARD DIMENSIONS FOR FLARED (S/S BY SAE-AS4330) |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
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| MS28741 Revision K:2010 | Hose Assembly, Detachable End Fitting, Medium Pressure |
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| MS33790 Base Document:1958 | BEND DATA, MINIMUM, HYDRAULIC, PNEUMATIC, FUEL AND OIL HOSE (NO S/S DOCUMENT) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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