DIN 65035:1993-11
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AEROSPACE; STEEL, NICKEL- AND COBALT-ALLOY STOCK, FORGINGS AND RINGS; TECHNICAL SPECIFICATION |
QQ-A-200-13 Revision C:1983
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ALUMINUM ALLOY BAR, ROD, SHAPES, TUBE, AND WIRE, EXTRUDED, 7178 |
SAE AMS T 81556 : 2001
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TITANIUM AND TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
DIN 65038-1:1989-08
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AEROSPACE; STEEL, NICKEL- AND COBALT-ALLOYS BARS; TECHNICAL SPECIFICATION |
MIL-A-22771 Revision D:1984
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ALUMINUM ALLOY FORGINGS, HEAT TREATED |
QQ-A-225 Revision G:1990
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ALUMINUM AND ALUMINUM ALLOY BAR, ROD, WIRE, OR SPECIAL SHAPES, ROLLED, DRAWN, OR COLD FINISHED, GENERAL SPECIFICATION FOR |
NASA MSFC STD 1249 : 1985
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NDE GUIDELINES AND REQUIREMENTS FOR FRACTURE CONTROL PROGRAMS |
MIL-T-81556 Revision A:1983
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TITANIUM & TITANIUM ALLOYS, EXTRUDED BARS AND SHAPES, AIRCRAFT QUALITY |
MIL-S-8844 Revision D:1987
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STEEL BAR, REFORGING STOCK AND MECHANICAL TUBING LOW ALLOY PREMIUM QUALITY |
DEFSTAN 00-970(PT0)/9(2012) : 2012
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
94/712749 DC : 0
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PREN 4050-4 - AEROSPACE SERIES - TEST METHOD FOR METALLIC MATERIALS - ULTRASONIC INSPECTION OF BARS, PLATES, FORGING STOCK AND FORGINGS - PART 4: ACCEPTANCE CRITERIA |
PREN 6071 : 200P1
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AEROSPACE SERIES - ALUMINIUM AND ALUMINIUM ALLOY WROUGHT PRODUCTS - TECHNICAL SPECIFICATION - PLATE |
BS 5S 100:1993
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Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube) |
SAE AS 7114/3 : 2008
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NADCAP REQUIREMENTS FOR NONDESTRUCTIVE TESTING FACILITY ULTRASONIC SURVEY |
SAE AS 7100/1 : 2008
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NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) SURVEY CHECKLISTS FOR THE NDT SUPPLIERS ACCREDITATION PROGRAM |
NASA STD 5006 : 2015
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GENERAL FUSION WELDING REQUIREMENTS FOR AEROSPACE MATERIALS |
DIN 29546:1990-10
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Aerospace; wrought aluminium alloys sheet, plate and strip; technical specification; inactive for new design |
QQ-A-200-3 Revision F:1983
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ALUMINUM ALLOY 2024, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED |
QQ-A-200-14 Revision B:1984
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ALUMINUM ALLOY BAR, ROD, SHAPES, AND WIRE, EXTRUDED, 7178-T76, (IMPROVED EXFOLIATION RESISTANT) |
DIN 65021:1986-11
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AEROSPACE; SHEET, PLATE AND STRIP OF STEEL, NICKEL ALLOYS AND COBALT ALLOYS; TECHNICAL SPECIFICATION |
MIL-W-5013 Revision L:1991
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WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
QQ-A-200-11 Revision E:1983
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ALUMINUM ALLOY 7075, BAR, ROD, SHAPES, TUBE AND WIRE, EXTRUDED |
SAE MAM 4141 : 1990
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ALUMINUM ALLOY, DIE FORGINGS, 5.6ZN - 2.5MG - 1.6CU - 0.23CR (7075-T73) SOLUTION AND PRECIPITATION HEAT TREATED |
MIL-T-82856 Base Document:1983
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TUNGSTEN, THORIATED, TWO PERCENT, FORGED |
MIL-T-24766 Base Document:1992
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TITANIUM FORGINGS & FORGING STOCK, HIGH QUALITY FOR SHIPS SERVICE |
MIL T 82833 : NOTICE 1
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TUNGSTEN, THORIATED, TWO PERCENT, FORGED & CUPPED |