SAE ARP 699 : 2015
|
HIGH TEMPERATURE PNEUMATIC DUCT SYSTEMS FOR AIRCRAFT |
MIL-R-83372 Base Document:1972
|
RELAY, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR |
MIL C 27536 : B
|
COUPLING, CLAMP, GROOVED, V-BAND |
MIL H 81014 : A NOTICE 1
|
HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
SAE AS 1472 : 2013
|
HOSE ASSEMBLY, LOW PRESSURE, POTABLE WATER |
MIL-D-82687 Base Document:1980
|
DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
MIL F 85406 : 0
|
FUSE SYSTEM, JOINT SERVICE ELECTRONIC BOMB FMU-139/B |
MIL-A-81973 Base Document:1974
|
AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
MIL-R-85880 Base Document:1988
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ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-F-29419 Base Document:1985
|
FRAME, SHIPPING [SIXCON] |
MIL H 81529 : 0
|
HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
GG-R-1971 Base Document:1976
|
RETRACTOR, RIB, HARKEN |
MIL-A-45940 Base Document:1971
|
ARMAMENT SUBSYSTEM, HELICOPTER, 7.62 MM MACHINE GUN: DOOR MOUNTED, LIGHT WEIGHT, M24 (LESS M60D MACHINE GUN) |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-S-83427 Base Document:1974
|
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
|
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
|
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
|
SAW, CHAIN, PORTABLE, POWER |
MIL W 46244 : B
|
WARHEAD, GUIDED MISSILE, HE M17A1 PARTS FOR |
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
|
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
|
TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |