MIL-S-83030 Revision A:1968
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STEEL ALLOY, CARBURIZING, BARS AND BILLETS, STEEL NICKEL-CHROMIUM (3310, 3316, AND 9310), PREMIUM QUALITY
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SAE MA 4070 : 2013
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PINS, PROCUREMENT SPECIFICATION FOR, METRIC
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SAE AS 1177 : 2018
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NONDESTRUCTIVE INSPECTION STANDARDS FOR BOLTS AND SCREWS
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MIL BULL 343 : A
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DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
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MIL-T-81364 Base Document:1966
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T-BOLT, 180,000 PSI TYPE 431 STAINLESS STEEL, MANUFACTURING PROCESS REQUIREMENTS
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SAE AMS 2680 : 2010
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ELECTRON-BEAM WELDING, FOR FATIGUE CRITICAL APPLICATIONS
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SAE AMS 5351 : 2017
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STEEL CASTINGS, SAND, CORROSION AND MODERATE HEAT RESISTANT, 13CR, NORMALIZED AND TEMPERED
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SAE MA 1784 : 2012
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SPACERS AND WASHERS, PROCUREMENT SPECIFICATION FOR, METRIC
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SAE MA 1937 : 2018
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NUT, HEX, FREE RUNNING, PROCUREMENT SPECIFICATION FOR, METRIC
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SAE AMS5328E:1987(S2017)
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STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.28 - 0.36C) (SAE 4330 MODIFIED), ANNEALED
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SAE AMS 5412 : 2012R(2018)
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STEEL CASTINGS, VACUUM MELTED, VACUUM CAST, INVESTMENT, CORROSION RESISTANT 13CR - 8.0NI - 2.2MO - 1.1AI (195,000 PSI (1344 MPA) TENSILE STRENGTH (CONDITION H1000) HOMOGENIZED, SOLUTION, AND PRECIPITATION HEAT TREATED
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MS172236THRUMS172270 Revision B:1974
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NUT, SPANNER, BEARING RETAINING, AERONAUTICAL (ASG)
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SAE J 420 : 2018
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MAGNETIC PARTICLE INSPECTION
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MIL-Q-22631 Revision B:1964
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QUALITY CONTROL OF METAL WROUGHT PRODUCTS EXCEPT FORGINGS PROCURED TO NON-GOVERNMENTAL SPECIFICATIONS
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SAE AMS 5348 : 2017
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STEEL CASTINGS, TUBULAR, CENTRIFUGAL, CORROSION RESISTANT, 15CR - 4.6NI - 0.22 (CB+TA) - 2.8CU, SOLUTION HEAT TREATED
|
SAE AMS 7304 : 2015
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SPRINGS, STEEL, 0.85 - 1.05C, HARDENED AND TEMPERED AFTER FORMING
|
SAE AMS S 6098 : 1999
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STEEL, CHROME-NICKEL-MOLYBDENUM (8735) BARS AND REFORGING STOCK (AIRCRAFT QUALITY)
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SAE AMS T 5066 : 2015
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TUBING, CARBON STEEL (1025), (AIRCRAFT QUALITY)
|
SAE AMS 5115 : 2017
|
Wire, Carbon Steel 0.60 - 0.75C Hardened and Tempered
|
MIL-S-8503 Revision B:1978
|
STEEL BARS, CHROME-VANADIUM (6150) AIRCRAFT QUALITY
|
MIL-S-18729 Revision C:1965
|
STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY
|
SAE AMS 5330 : 2015
|
STEEL CASTINGS, INVESTMENT, 0.80CR - 1.8NI - 0.35MO (0.38 - 0.46C) (SAE 4340 MODIFIED), ANNEALED
|
MIL-S-8690 Revision B:1978
|
STEEL, CHROME NICKEL MOLYBDENUM 8620, BARS AIRCRAFT QUALITY
|
AN103901THRUAN104000 Revision 3:1986
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BOLT - DRILLED HEX HEAD, 6 HOLES, .3125-24
|
MIL R 25532 : A
|
ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR
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SAE AMS 3046 : 2014
|
MAGNETIC PARTICLES, FLUORESCENT, WET METHOD, OIL VEHICLE, AEROSOL PACKAGED
|
SAE AMS S 6050 : 1998
|
STEEL, CHROME-NICKEL-MOLYBDENUM (8630) BARS AND REFORGING STOCK (AIRCRAFT QUALITY)
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