MIL-STD-2156 Base Document:1983
|
LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
SAE AS 8662 : 1999
|
KNIFE, HUNTING, SHEATHED, SURVIVAL, PILOTS |
SAE AS 4060 : 2013
|
TUBE FITTINGS SWAGED JOINT, ROLLER EXPANDER, MANUAL PROCESS, REQUIREMENTS FOR |
FF-R-556 Revision D:1981
|
RIVET, SOLID, SMALL, RIVET, SPLIT, SMALL, RIVET TUBULAR SMALL, FLAT WASHER (BURR) AND CAP RIVET, GENERAL PURPOSE |
MIL-A-83577 Revision B:1988
|
ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
DIN 65570:1990-12
|
AEROSPACE; HEAT TREATMENT FACILITIES; GENERAL REQUIREMENTS |
SAE AMS 4240 : 1982
|
CASTINGS, SAND - 10MG, SOLUTION HEAT TREATED & NATURALLY AGED |
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 |
UNI EN ISO 11846 : 2008
|
CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
MIL-F-71131 Base Document:1992
|
FIN, MORTAR CARTRIDGE: M32 |
BS EN ISO 11846:2008
|
Corrosion of metals and alloys. Determination of resistance to intergranular corrosion of solution heat- treatable aluminium alloys |
QQ-A-200 Revision E:1980
|
ALUMINUM ALLOY, BAR, ROD, SHAPES, STRUCTURAL SHAPES, TUBE AND WIRE, EXTRUDED, GENERAL SPECIFICATION FOR |
MIL-A-22771 Revision D:1984
|
ALUMINUM ALLOY FORGINGS, HEAT TREATED |
MIL-F-48076 Revision A:1984
|
FIN, ASSEMBLY, M158 |
QQ-A-225 Revision G:1990
|
ALUMINUM AND ALUMINUM ALLOY BAR, ROD, WIRE, OR SPECIAL SHAPES, ROLLED, DRAWN, OR COLD FINISHED, GENERAL SPECIFICATION FOR |
ASTM G 110 : 1992 : R2009
|
Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
MIL A 46192 : B
|
ALUMINUM ALLOY ARMOR ROLLED PLATE (1/2 TO 4 INCHES THICK), WELDABLE (ALLOY 2519) |
FF-B-584 Revision F:1989
|
BOLTS, FINNED NECK, KEY HEAD, MACHINE, RIBBED NECK, SQUARE NECK, TEE HEAD |
MIL-STD-1892 Base Document:1985
|
WELDING, ARC AND OXYFUEL GAS, PROCESS AND REQUIREMENTS FOR |
MIL-C-8603 Revision B:1984
|
CLAMPS, LOOP TYPE, AND STRAPS, SUPPORT |
MIL T 8878 : D
|
TURNBUCKLE, POSITIVE SAFETYING |
MIL R 007885 : C SUPP 1
|
RIVETS; BLIND, STRUCTURAL, LOCKED AND FRICTION RETAINED SPINDLE, GENERAL SPECIFICATION FOR |
DOD-E-83578 Revision A:1987
|
EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
MIL-C-7438 Revision G:1985
|
CORE MATERIAL, ALUMINUM, FOR SANDWICH CONSTRUCTION |
SAE AMS WW T 700B :2001(S2018)
|
TUBE, ALUMINIUM AND ALUMINIUM ALLOY, DRAWN, SEAMLESS, GENERAL SPECIFICATION FOR |
SAE AMS 4318 : 1994
|
ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS AND RODS 12.2SI - 1.0MG - 0.90CU - 0.90NI (4032-T86) SOLUTION HEAT TREATED, COLD WORKED, AND ARTIFICIALLY AGED |
MIL-A-23121 Revision C:1970
|
AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
MIL-HDBK-1587 Base Document:1996
|
MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
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-S-7839 Revision B:1973
|
SCREW, STRUCTURAL, AIRCRAFT |
MIL-A-21180 Revision D:1984
|
ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
MIL-R-27384 Revision B:1970
|
RIVET, BLIND, DRIVE TYPE |
MIL-R-5674 Revision F:1994
|
RIVETS, STRUCTURAL, ALUMINIUM ALLOY, TITANIUM COLUMBIUM ALLOY GENERAL SPECIFICATION FOR |
MIL-R-85880 Base Document:1988
|
ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
I.S. EN 14101:2002
|
SPACE PRODUCT ASSURANCE - MATERIAL SELECTION FOR CONTROLLING STRESS-CORROSION CRACKING |
SAE AS 4444 : 2013
|
FITTINGS, 24 DEGREE CONE FLARELESS, FLUID CONNECTION, 5000 PSI |
MIL-H-9890 Revision E:1988
|
HARDWARE, INDIVIDUAL LOAD CARRYING EQUIPMENT: AND HARDWARE, MISCELLANEOUS |
MIL-W-22248 Revision A:1971
|
WELDMENTS, ALUMINUM AND ALUMINUM ALLOY |
MIL F 70546 : 0
|
FIN ASSEMBLIES, MORTAR CARTRIDGE, 81MM, M28, M29 |
SAE AMS 4148 : 2017
|
ALUMINUM ALLOY DIE FORGINGS (7175-T66) SOLUTION AND PRECIPITATION HEAT TREATED |
MIL-F-71153 Base Document:1993
|
FIN, MORTAR CARTRIDGE: M33 |
QQ-A-596 Revision E:1981
|
ALUMINUM ALLOY PERMANENT AND SEMI-PERMANENT MOLD CASTINGS |
MIL-S-8512 Revision D:1974
|
SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-F-80188 Revision B:1985
|
FURNACE, HEAT TREATING, ELECTRIC, METAL LINED, BOX DESIGN |
MIL-STD-2131 Revision A:1991
|
LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL R 46963 : A
|
ROCKET MOTOR, M42A1, BOOSTER |
MIL-F-14888 Revision A:1981
|
FIN ASSEMBLY, XM170 |
PREN 6071 : 200P1
|
AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE |
SAE ARP 1675 : 2014
|
STRUCTURAL WELDBONDING OF ALUMINUM STRUCTURES |
QQ-A-200-16 Revision A:1974
|
ALUMINUM ALLOY STRUCTURAL SHAPES, EXTRUDED, 6061 |
MIL-W-8604 Revision A:1982
|
WELDING, FUSION, ALUMINUM ALLOYS, PROCESSING AND PERFORMANCE OF |
MIL-K-8662 Revision E:1974
|
KNIFE, HUNTING, SHEATHED, SURVIVAL PILOT S |
SAE MAM 4247 : 1994
|
ALUMINUM ALLOY, HAND FORGINGS 7.7ZN - 2.4MG - 1.6CU - 0.16CR (7049-T7352) SOLUTION HEAT TREATED, STRESS RELIEVED BY COMPRESSION, AND PRECIPITATION HEAT TREATED |
MIL-S-85510 Base Document:1981
|
|
MIL A 46118 : D
|
ALUMINUM ALLOY ARMOR, 2219, ROLLED PLATE AND DIE FORGED SHAPES |
SAE AMS 2772 : 2016
|
HEAT TREATMENT OF ALUMINUM ALLOY RAW MATERIALS |
MIL-F-85731 Base Document:1986
|
FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
BS ISO 11846 : 1995
|
CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
MIL-T-7081 Revision D:1965
|
TUBE, ALUMINUM ALLOY, SEAMLESS, ROUND, DRAWN, 6061, AIRCRAFT HYDRAULIC QUALITY |
MIL A 38726 : 0
|
ADAPTER ASSEMBLY, REUSABLE, FLEXIBLE HOSE, LOW PRESSURE |
MIL-Q-22631 Revision B:1964
|
QUALITY CONTROL OF METAL WROUGHT PRODUCTS EXCEPT FORGINGS PROCURED TO NON-GOVERNMENTAL SPECIFICATIONS |
MIL-F-5509 Revision D:1978
|
FITTING, FLARED TUBE, FLUID CONNECTION |
NASA MSFC SPEC 504 : 1990
|
WELDING, ALUMINIUM ALLOYS |
MIL S 25073 : 0
|
|
SAE AMS 4051 : 1985
|
ALUMINUM ALLOY SHEET AND PLATE, ALCLAD 6.8ZN - 2.8MG - 2.0CU - 0.23CR (ALCLAD 7178-0) ANNEALED |
MIL P 25995 : B
|
PIPE, ALUMINUM ALLOY, DRAWN OR EXTRUDED |
MIL F 71037 : NOTICE 2
|
FIN ASSEMBLY, MORTAR CARTRIDGE |
FF-N-836 Revision E:1994
|
Nut: Square, Hexagon, Cap, Slotted, Castle, Knurled, Welding and Single Ball Seat |
SAE MA 2150 : 2015
|
CLAMPS, LOOP OR P STYLE, SINGLE POINT MOUNT, MULTIPLE SHAPES, METRIC |
SAE AMS 4023 : 2015
|
ALUMINUM ALLOY SHEET AND PLATE, ALCLAD, 1.0MG - 0.60SI - 0.28CU - 0.20CR (ALCLAD 6061; -T6 SHEET, -T651 PLATE) |
SAE MAM 4323 : 1997
|
ALUMINUM ALLOY, HAND FORGINGS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T7452) SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED |
I.S. EN ISO 11846:2008
|
CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |
ISO 11846:1995
|
Corrosion of metals and alloys Determination of resistance to intergranular corrosion of solution heat-treatable aluminium alloys |
EN 14101:2001
|
Space product assurance - Material selection for controlling stress-corrosion cracking |
DIN 50900-3:1985-09
|
CORROSION OF METALS; TERMS; TERMS OF CORROSION TESTING |
DOD C 63976 : 0
|
CASE, CARTRIDGE, 30MM, AMMUNITION FOR M788 M789 AND M799 SERIES OF 30 MM, AMMUNITION |
MIL-F-18280 Revision F:1995
|
FITTING, FLARELESS TUBE, FLUID CONNECTION |
MIL-B-543 Revision G:1990
|
BUCKLE, TONGUELESS AND WEB STRAP |
MIL-I-85889 Base Document:1988
|
IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL S 9479 : C
|
|
MIL-F-13926 Revision B:1984
|
FIRE CONTROL MATERIAL MANUFACTURE AND INSPECTION, GENERAL SPECIFICATION FOR |
MIL-C-8956 Revision A:1970
|
CLAMP, LOOP TUBE SUPPORT |
QQ-A-200-8 Revision F:1983
|
ALUMINUM ALLOY 6061, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED |
MIL-S-81771 Revision A:1975
|
SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR |
MIL-P-83126 Revision A:1980
|
PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
ADS-13F-HDBK : 1997
|
AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL-A-63547 Base Document:1982
|
ALUMINUM ALLOY 7475, ROD |
JSSG-2010-12 Base Document:1998
|
Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL-P-63137 Revision B:1981
|
PROJECTILE, 8-INCH HE, RA, M650 WARHEAD SECTION FORWARD |
MIL-R-7885 Revision D:1988
|
RIVET, BLIND, STRUCTURAL, MECHANICALLY LOCKED SPINDLE AND FRICTION LOCKED SPINDLE, GENERAL SPECIFICATION FOR |
SAE AS 85731 : 2015
|
FASTENER, POSITIVE LOCKING, ELECTRONIC EQUIPMENT, GENERAL SPECIFICATION FOR |
ASTM G 110 : 1992 : R2015
|
Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
ASTM B 313M : 1988
|
Specification for Aluminum and Aluminum-Alloy Round Welded Tubes (Metric) (Withdrawn 1990) |
EN ISO 11846:2008
|
Corrosion of metals and alloys - Determination of resistance to intergranular corrosion of solution heat-treatable aluminium alloys (ISO 11846:1995) |
SAE MAM 4141 : 1990
|
ALUMINUM ALLOY, DIE FORGINGS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T73) SOLUTION AND PRECIPITATION HEAT TREATED |
MIL-I-43684 Revision B:1989
|
INTRENCHING TOOL, HAND, FOLDING, LIGHTWEIGHT, AND CARRIER |
MIL-R-51344 Revision B:1982
|
ROCKET, INCENDIARY, 66 MM TPA 4 ROUND CLIP, M74 OR M74A1 |
SAE AMS 4021 : 2017
|
ALUMINUM ALLOY, ALCLAD SHEET AND PLATE, 1.0MG - 0.60SI - 0.28CU - 0.20CR (ALCLAD 6061-0) ANNEALED |
MIL A 81596 : A
|
ALUMINUM FOIL FOR SANDWICH CONSTRUCTION |
MIL-STD-645 Revision B:1981
|
DIP BRAZING OF ALUMINUM ALLOYS |
MIL-B-21902 Revision A:1963
|
|
NASA MSFC STD 506 : 1988
|
MATERIALS AND PROCESSES CONTROL |
QQ-A-601 Revision F:1981
|
ALUMINUM ALLOY SAND CASTINGS |
SAE MA 2151 : 2015
|
CLAMP ASSEMBLIES, SADDLE OR OMEGA STYLE, TWO POINT MOUNT, MULTIPLE SHAPES, METRIC |
MIL-STD-40002 Base Document:1991
|
HEAT TREATMENT CODING SYSTEM, GENERAL |
SAE AMS 4321 : 2016
|
ALUMINUM ALLOY FORGINGS, 7.7ZN - 2.5MG - 1.5CU - 0.16CR (7049-01), HIGH TEMPERATURE ANNEALED |
ASTM G 110 : 1992 : R2003 : EDT 1
|
Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
SAE MAM 4248 : 1993
|
ALUMINUM ALLOY, HAND FORGINGS AND ROLLED RINGS 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061-T652) SOLUTION HEAT TREATED, STRESS RELIEVED BY COMPRESSION, AND PRECIPITATION HEAT TREATED |
ASTM G 110 : 1992 : R1997
|
Standard Practice for Evaluating Intergranular Corrosion Resistance of Heat Treatable Aluminum Alloys by Immersion in Sodium Chloride + Hydrogen Peroxide Solution |
ASTM B 308M : 1988
|
Specification for Aluminum-Alloy 6061-T6 Standard Structural Shapes, Rolled or Extruded (Metric) (Withdrawn 1990) |
BS EN 14101:2001
|
SPACE PRODUCT ASSURANCE - MATERIAL SELECTION FOR CONTROLLING STRESS-CORROSION CRACKING |
DIN EN ISO 11846:2008-08
|
CORROSION OF METALS AND ALLOYS - DETERMINATION OF RESISTANCE TO INTERGRANULAR CORROSION OF SOLUTION HEAT-TREATABLE ALUMINIUM ALLOYS |