SAE ARP 699 : 2015
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HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT
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MIL-R-83372 Base Document:1972
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RELAY, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR
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MIL C 27536 : B
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COUPLING, CLAMP, GROOVED, V-BAND
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MIL H 81014 : A NOTICE 1
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HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C
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SAE AS 1472 : 2013
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HOSE ASSEMBLY, LOW PRESSURE, POTABLE WATER
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MIL-D-82687 Base Document:1980
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DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O
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MIL F 85406 : 0
|
FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B
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MIL-A-81973 Base Document:1974
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AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR
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MIL-R-85880 Base Document:1988
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ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
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MIL-F-29419 Base Document:1985
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FRAME, SHIPPING [SIXCON]
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MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A
|
GG-R-1971 Base Document:1976
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RETRACTOR, RIB, HARKEN
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MIL-A-45940 Base Document:1971
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ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M24 (LESS M60D MACHINE GUN)
|
MIL-S-8512 Revision D:1974
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SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
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MIL-S-83427 Base Document:1974
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SURVIVAL KIT CONTAINERS, CNU-129(V)/P AND CNU-130/P
|
NEMA XR 14-1990 (R1995, R2000)
|
RECOMMENDED PRACTICES FOR LOAD-BEARING MECHANICAL ASSEMBLIES USED IN DIAGNOSTIC IMAGING
|
MIL-F-85596 Base Document:1983
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FIN, RETARDER, AIR INFLATABLE BSU-85/B
|
MIL-STD-1261 Revision C:1988
|
ARC WELDING PROCEDURES FOR CONSTRUCTIONAL STEELS
|
MIL-B-48008 Base Document:1972
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BATTERY, THERMAL, XM97
|
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
|
MIL F 83296 : 0
|
FITTING, TETRAFLUOROETHYLENE HOSE, HIGH TEMPERATURE, HIGH PRESSURE (3,000 PSI HYDRAULIC AND PNEUMATIC)
|
MIL-S-58095 Revision A:1986
|
SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
|
SAE ARP 907 : 2013
|
MISSILE & ROCKET APPLICATIONS - HOSE ASSEMBLIES, FLEXIBLE METAL, HIGH PRESSURE AND HIGH TEMPERATURE
|
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
|
MIL-S-13119 Revision E:1984
|
SPREADER, SLING, PLATE TYPE, NONADJUSTABLE
|
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook
|
GGG-S-62 Revision D:1986
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SAW, CHAIN, PORTABLE, POWER
|
MIL W 46244 : B
|
WARHEAD, GUIDED MISSILE, HE M17A1 PARTS FOR
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MIL-A-45941 Base Document:1971
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M23 (LESS M60D MACHINE GUN)
|
MIL-R-46509 Revision A:1982
|
ROCKET MOTOR, XM30, METAL PARTS FOR
|
MIL-A-45947 Base Document:1972
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: RAMP MOUNTED, LIGHT WEIGHT, M41 (LESS M60D MACHINE GUN)
|
SAE AS 1960 : 2013
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COUPLING ASSEMBLY, V-BAND, SHEET METAL FLANGE, PNEUMATIC TUBE
|
SAE MA 2100 : 2015
|
HOSE ASSEMBLIES, METAL MEDIUM PRESSURE, HIGH TEMPERATURE, METRIC
|
MIL-T-81821 Base Document:1969
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TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR
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