Are you in need of part numbers AMS-QQ-A-250-5, AMS-QQ-A-250-5-CDT3-0-071X6X36, AMS-QQ-A-250 5-T3-0.071X6X36, AMS-QQ-A-250-5-T3-0.071X6X36 from Society Of Automotive Engineers Inc, Sae International manufacturers of NSN 9535015317786? ASAP Parts Online has the part number in stock and ready to be shipped. Along with NSN 9535015317786 corresponding part numbers, we have access to billions of premium parts such as Sheet Metal for the aviation, defense, and military industries. We are here to help streamline the process.
Alternative NSN: 9535-01-531-7786 |
Item Name:Sheet Metal |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NIIN: 015317786 |
NCB Code: USA (01) |
Manufacturers: Sae International , Society Of Automotive Engineers Inc |
Part No Part No
|
Item Name Item Name
|
Manufacturer Manufacturer
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS-QQ-A-250-5 | sheet metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250-5 | sheet metal | Sae International | Avl |
|
AMS-QQ-A-250-5-CDT3-0-071X6X36 | sheet metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250 5-T3-0.071X6X36 | sheet metal | Society Of Automotive Engineers Inc | Avl |
|
AMS-QQ-A-250-5-T3-0.071X6X36 | sheet metal | Sae International | Avl |
|
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0710 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
ALBY | USAGE DESIGN | AIRCRAFT |
CQBC | MINIMUM TENSILE STRENGTH | 61000 POUNDS PER SQUARE INCH |
CQHQ | MINIMUM YIELD STRENGTH | 40000 POUNDS PER SQUARE INCH |
FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
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