MIL-S-18729 Revision C:1965
|
STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY |
MIL L 7808 : K (1)
|
LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
SAE AS 1502 : 1986
|
HOSE, AIR DUCT, FLEXIBLE, HELICAL, METALLIC WIRE SUPPORTED (EXPOSED), SELF EXTINGUISHING |
MIL-STD-129 Revision R:2014
|
Military Marking for Shipment and Storage |
SAE AS 1503 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, HELICAL, METALLIC WIRE SUPPORTED (COVERED), SELF EXTINGUISHING |
SAE AMS 1541 : 1991
|
CLEANER, FUEL DROP TANK, WATER-SOLUBLE |
SAE AS 1505 : 2013
|
HOSE, AIR DUCT FLEXIBLE, ANNULAR CONVOLUTED, SELF EXTINGUISHING |
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 AS 4774 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, SILICONE-COATED FABRIC, 1 PSI, EXTERNAL NYLON HELIX, SELF-EXTINGUISHING |
MIL-STD-810 Revision G:2008
|
ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL T 5624 : R
|
TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
SAE AS 1591 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, POLYURETHANE-COATED FABRIC, 1 psi, EXTERNAL NYLON HELIX, SELF-EXTINGUISHING |
TT-S-735 Revision A:1988
|
STANDARD TEST FLUIDS, HYDROCARBON |
MIL-Y-1140 Revision H:1972
|
YARN, CORD, SLEEVING CLOTH, AND TAPE GLASS |
SAE AS 1506 : 2013
|
HOSE, AIR DUCT, SEMIFLEXIBLE, SLEEVE SECTION, UNREINFORCED, SELF EXTINGUISHING |
SAE AS 4804 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, SILICONE-COATED FABRIC, EXTERNAL NYLON HELIX, LOW-NOISE |
SAE AS 1544 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, HELICAL, NONMETALLIC WIRE SUPPORTED (COVERED), SILICONE RUBBER, SELF EXTINGUISHING |
MS35842 Revision E:1969
|
CLAMP, HOSE, LOW PRESSURE TYPE, F. |
SAE AS 1543 : 2013
|
HOSE, AIR DUCT, SEMIFLEXIBLE, SLEEVE SECTION UNREINFORCED, SELF EXTINGUISHING, NOMEX |
SAE AS 1542 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, HELICAL CONVOLUTED, SELF EXTINGUISHING |
SAE AS 1504 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, HELICAL, NONMETALLIC WIRE SUPPORTED (EXPOSED), SELF EXTINGUISHING |
MIL-STD-100 Revision G:1997
|
ENGINEERING DRAWINGS |
ASTM B 194 : 2015 : REDLINE
|
Standard Specification for Copper-Beryllium Alloy Plate, Sheet, Strip, and Rolled Bar |
SAE AS 1241 : 2016
|
FIRE RESISTANT PHOSPHATE ESTER HYDRAULIC FLUID FOR AIRCRAFT |
MIL-L-6082 Revision E:1990
|
LUBRICATING OIL, AIRCRAFT PISTON ENGINE (NONDISPERSANT MINERAL OIL) |
NAS1922:2016
|
CLAMP, HOSE, BAND, TANGENTIAL WORM, LIGHT WEIGHT |
TT-I-735 Revision A:1963
|
ISOPROPYL ALCOHOL |
MIL H 5606 : G
|
HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
QQ-P-416 Revision F:1991
|
PLATING, CADMIUM (ELECTRODEPOSITED) |
MS33660 Revision D:1999
|
TUBING END HOSE CONNECTION, STANDARD DIMENSIONS FOR |
MIL P 5425 : D
|
PLASTIC, SHEET, ACRYLIC, HEAT RESISTANT |
MIL L 6085 : C
|
LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY |
SAE AS 4546 : 2013
|
HOSE, AIR DUCT, FLEXIBLE, SILICONE-COATED FABRIC, 1 TO -.5 PSI, EXTERNAL NYLON HELIX, SELF-EXTINGUISHING |