MIL L 7808 : K (1)
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
MIL-P-5315 Revision B:1964
|
PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT |
MIL-STD-130 Revision N:2007
|
IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
QQ-P-35 Revision C:1988
|
PASSIVATION TREATMENTS FOR CORROSION-RESISTANT STEEL |
MIL L 23699 : E
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
SAE ARP 868 : 2013
|
METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL H 25579 : E
|
HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
MIL R 25897 : LATEST
|
|
MS8000 Revision E:2016
|
HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, REUSABLE FITTINGS, HIGH TEMPERATURE, MEDIUM PRESSURE, FLARE-TO-FLARE |
MIL-STD-889 Revision C:2016
|
DISSIMILAR METALS |
MS33656 Revision J:1987
|
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
|
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-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 |
MIL-STD-1247 Revision D:2009
|
MARKINGS, FUNCTIONS AND HAZARDS DESIGNATIONS OF HOSE, PIPE, AND TUBE LINES FOR AIRCRAFT MISSILE, AND SPACE SYSTEMS |
MS28741 Revision K:2010
|
HOSE ASSEMBLY, DETACHABLE END FITTING, MEDIUM PRESSURE |