MIL-STD-2175 Revision A:1993
|
CASTING, CLASSIFICATION AND INSPECTION OF |
MIL-A-83577 Revision B:1988
|
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
SAE MAM 4131 : 1996
|
ALUMINUM ALLOY, DIE AND HAND FORGINGS 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T74) SOLUTION HEAT TREATED AND AGED |
MIL-C-47269 Revision A:1992
|
CASTINGS, INSPECTION OF (FOR GUIDED MISSILE AND ROCKET MATERIAL) |
NASA MSFC SPEC 560 : 1988
|
THE FUSION WELDING OF STEEL, CORROSION AND HEAT RESISTANT ALLOYS |
MIL-B-85667 Revision A:1991
|
BOLT, SLEEVE, STRAIGHT SHANK, PROTRUDING AND FLUSH HEAD GENERAL SPECIFICATION FOR |
MIL-P-87988 Base Document:1989
|
PIN-RIVET, THREADED WITH HEX SOCKET |
SAE MAM 5401 : 2003
|
NICKEL ALLOY, CORROSION AND HEAT RESISTANT, INVESTMENT CASTINGS 62NI - 21.5CR - 9.0MO - 3.6CB VACUUM MELTED, VACUUM CAST AS CAST |
MIL-B-87114 Revision A:1978
|
BOLTS, RECESS DRIVE, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/9(2012) : 2012
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-S-21472 Revision C:1988
|
SCREW, SHOULDER, HEXAGON SOCKET-HEAD AND SLOTTED-HEAD GENERAL SPECIFICATION FOR |
MIL-S-45909 Revision C:1989
|
STUD, LOCKED IN - RING LOCKED SERRATED |
MIL-B-23964 Revision D:1981
|
BOLT, SELF-RETAINING, POSITIVE LOCKING |
DEFSTAN 00-970(PT0)/14(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-B-85604 Revision A:1988
|
BOLT, NICKEL ALLOY 718, TENSION, HIGH STRENGTH, (125 KSI FSU & 220 KSI FTU) HIGH TEMPERATURE, SPLINE DRIVE, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/12(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-N-85730 Base Document:1988
|
NUT, SELF-LOCKING, SPLINE DRIVE, ASSEMBLED WASHER, NICKEL ALLOY 718, 220 KSI FTU, 900 DEGREES F, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/8(2011) : 2011
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013
|
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-S-45915 Revision A:1967
|
STUD, LOCKED IN - KEY LOCKED - GENERAL SPECIFICATION FOR |
MIL-N-7873 Revision B:1994
|
NUT, SELF-LOCKING 1,200 DEG F |
MIL-P-71012 Revision A:1994
|
PISTOL, SEMIAUTOMATIC, COMPACT, 9MM: M11 |
MIL-F-60445 Revision C:1991
|
FIN AND NOZZLE ASSEMBLY, FOR ROCKET MOTOR 2.75 INCH MARK 4 AND MARK 40 PARTS FOR |
SAE AMS 2680 : 2010
|
ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS |
MIL-B-85598 Base Document:1988
|
BEARINGS, ELASTOMERIC GENERAL SPECIFICATION FOR |
MIL-STD-1261 Revision C:1988
|
ARC WELDING PROCEDURES FOR CONSTRUCTIONAL STEELS |
SAE MA 2060 : 2015
|
FITTINGS, WELDED, HYDRAULIC, TITANIUM AND CORROSION RESISTANT STEEL, 21 000 KPA, METRIC |
NEMA XR 14-1990 (R1995, R2000)
|
RECOMMENDED PRACTICES FOR LOAD-BEARING MECHANICAL ASSEMBLIES USED IN DIAGNOSTIC IMAGING |
SAE AMS 5340 : 2018
|
STEEL, CORROSION RESISTANT, INVESTMENT CASTINGS, 14CR - 4.25NI - 2.25MO - 0.25CB - 3.25CU, HOMOGENIZATION AND SOLUTION HEAT TREATED |
SAE AMS F 7190 : 2016
|
FORGING, STEEL, FOR AIRCRAFT/AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
NASA KSC SPEC Z 0005 : 1995
|
BRAZING - STEEL, COPPER, ALUMINIUM, NICKEL, AND MAGNESIUM ALLOYS, SPECIFICATION FOR |
MIL-I-45914 Revision A:1991
|
INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
NASA MSFC SPEC 504 : 1990
|
WELDING, ALUMINIUM ALLOYS |
MIL-S-58112 Base Document:1989
|
SLING, MULTI LEG, HELICOPTER, EXTERNAL CARGO |
FF-N-836 Revision E:1994
|
Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
SAE AS 7100/1 : 2008
|
NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) SURVEY CHECKLISTS FOR THE NDT SUPPLIERS ACCREDITATION PROGRAM |
MIL-F-18280 Revision F:1995
|
FITTING, FLARELESS TUBE, FLUID CONNECTION |
MIL-A-11356 Revision F:1987
|
ARMOR, STEEL, CAST, HOMOGENEOUS, COMBAT-VEHICLE TYPE (1/4 TO 8 INCHES, INCLUSIVE) |
MIL-C-14613 Revision A:1972
|
CHARGER, BOLT, CALIBER .50 BROWNING MACHINE GUN, M10 |
MIL-STD-1891 Base Document:1992
|
BOLTS AND SCREWS, INSPECTION OF |
NAVSEA T9074 AS GIB 010/271 : 0
|
REQUIREMENTS FOR NONDESTRUCTIVE TESTING METHODS |
MIL-N-85729 Base Document:1988
|
NUT, SELF-LOCKING, A-286, 160 KSI FTU, 450 DEGREES F, GENERAL SPECIFICATION FOR |
SAE AMS T 81915 : 2016
|
TITANIUM AND TITANIUM-ALLOY CASTINGS, INVESTMENT |
SAE AIR 4728 : 2013
|
REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS) |
MIL A 5503 : E
|
ACTUATOR, AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
MIL-G-63343 Base Document:1980
|
GRENADE XM74, HEMISPHERES FOR |
SAE AS 4488 : 2013
|
TUBULAR ASSEMBLIES, FUSION WELDED, INSPECTION PROCESSES AND ACCEPTANCE STANDARDS FOR |
MIL-F-7190 Revision B:1985
|
FORGING, STEEL, FOR AIRCRAFT AND AEROSPACE EQUIPMENT AND SPECIAL ORDNANCE APPLICATIONS |
NASA STD 6002 : 2008
|
APPLYING DATA MATRIX IDENTIFICATION SYMBOLS ON AEROSPACE PARTS |
MIL-S-70335 Revision A:1990
|
SCREW THREADS, INTERNAL COLD FORMED, GENERAL SPECIFICATION FOR |
MIL-W-5013 Revision L:1991
|
WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-I-25135 Revision E:1984
|
INSPECTION MATERIALS, PENETRANTS |
MIL-STD-40002 Base Document:1991
|
HEAT TREATMENT CODING SYSTEM, GENERAL |
SAE AS 13572 : 2014
|
SPRINGS, HELICAL, COMPRESSION AND EXTENSION |
SAE AMS STD 2175 : 2003
|
CASTINGS, CLASSIFICATION AND INSPECTION OF |
PREN 6052 : 200P1
|
AEROSPACE SERIES - RIVETS - COLLAR - SYSTEM IN ALUMINIUM ALLOY SHEAR TYPE INCH SERIES - TECHNICAL SPECIFICATION |