MIL L 7808 : K (1)
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LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
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MIL-P-5315 Revision B:1964
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PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT
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MIL-STD-130 Revision N:2007
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IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
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QQ-P-35 Revision C:1988
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PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL
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MIL L 23699 : E
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LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE
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SAE ARP 868 : 2013
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METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
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MIL-STD-810 Revision G:2008
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ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
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MIL H 25579 : E
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
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MIL R 25897 : LATEST
|
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MS8000 Revision E:2016
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HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE
|
MIL-STD-889 Revision C:2016
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DISSIMILAR METALS
|
MS33656 Revision J:1987
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FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
|
QQ-C-320 Revision B:1974
|
CHROMIUM PLATING (ELECTRODEPOSITED)
|
MIL-STD-143 Revision B:1969
|
STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF
|
MS8001 Revision E:2016
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARELESS-TO-FLARELESS
|
MIL-S-8879 Revision C:1991
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SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
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MIL A 8625 : F
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ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
|
MIL-L-6082 Revision E:1990
|
LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL)
|
MIL-F-8615 Revision D:1976
|
FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG]
|
MIL H 8795 : D
|
HOSE ASSEMBLY, RUBBER HYDRAULIC, FUEL AND OIL RESISTANT
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MIL-STD-1247 Revision D:2009
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MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS
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MS28741 Revision K:2010
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HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE
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