Alternative NSN: 9535-01-531-7789 |
Item Name: Sheet Metal |
CAGE Code : 0U583 , 81343 |
NIIN: 015317789 |
FSG: 95 Metal Bars Sheets and Shapes |
FSC Name: 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
NCB Code: USA (01) |
Manufacturers: sae international , society of automotive engineers inc |
Part No Part No
|
Manufacturer |
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS-QQ-A-250-5 | sae international | sheet metal | Avl | |
AMS-QQ-A-250-5-T3-0.040X6X36 | sae international | sheet metal | Avl | |
AMS-QQ-A-250-5 | society of automotive engineers inc | sheet metal | Avl | |
AMS-QQ-A-250 5-CDT3-0 04X6X36 | society of automotive engineers inc | sheet metal | Avl | |
AMS-QQ-A-250 5-T3-0.040X6X36 | society of automotive engineers inc | sheet metal | Avl |
MRC | Criteria | Characteristic |
---|---|---|
MATT | Material | ALUMINUM ALLOY 2024 |
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ABGL | Width | 6.000 INCHES NOMINAL |
CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
MRC | Decoded Requirement | Clear Text Reply |
ALBY | Usage Design | AIRCRAFT |
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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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