| Alternative NSN: 9535-01-531-7787 |
| 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: 015317787 |
| NCB Code: USA (01) |
| Manufacturers: Sae International, Society Of Automotive Engineers Inc |
Browse NSN parts of NSN 9535-01-531-7787 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9535-01-531-7787 like AMS QQ A 250 5 CDT3 0 025X6X36, AMS QQ A 250 5 T3 0 025X6X36, AMS-QQ-A-250 5, AMS-QQ-A-250 5, AMS-QQ-A-250 5-T3-0.025X6X36 described as Sheet Metal from industry leading manufactures such as Society Of Automotive Engineers Inc, Sae International. We are proud to offer an inventory of over 2 billion ready-to-ship parts, 24/7 availability, and key locations in the U.S./abroad. These attributes allow us to meet all aircraft on ground (AOG) requirements with ease.
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS QQ A 250 5 CDT3 0 025X6X36 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS QQ A 250 5 T3 0 025X6X36 | Sae International | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5 | Sae International | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-T3-0.025X6X36 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0250 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 59000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 39000 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 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
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9505-00-056-1762 (9505000561762) |
9505-00-056-1763 (9505000561763) |
9505-00-057-2157 (9505000572157) |
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9505-00-057-9449 (9505000579449) |
9505-00-059-6171 (9505000596171) |
9505-00-059-6172 (9505000596172) |
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9505-00-059-6174 (9505000596174) |
9505-00-059-6175 (9505000596175) |
9505-00-059-6176 (9505000596176) |
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9505-00-061-1592 (9505000611592) |
9505-00-061-1593 (9505000611593) |
9505-00-061-1594 (9505000611594) |
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