| Alternative NSN: 9535-01-532-0294 |
| 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: 015320294 |
| NCB Code: USA (01) |
| Manufacturers: Sae International, Society Of Automotive Engineers Inc |
Browse NSN parts of NSN 9535-01-532-0294 and get lowest price for your requested parts in 15 minutes. Just ordered part of NSN 9535-01-532-0294 like AMS QQ A 250 5, AMS QQ A 250 5 CD0 0 032X12X36, AMS-QQ-A-250 5, AMS-QQ-A-250 5-O-0.032X12X36, AMS-QQ-A-250 5-O-0.032X12X36 described as Sheet Metal from industry leading manufactures such as Sae International, Society Of Automotive Engineers Inc. 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 | Sae International | sheet metal | Avl | RFQ |
| AMS QQ A 250 5 CD0 0 032X12X36 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-O-0.032X12X36 | Society Of Automotive Engineers Inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-O-0.032X12X36 | Sae International | sheet metal | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| HEAT | Heat Treatment | O-ANNEALED |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ALBY | Usage Design | AIRCRAFT |
| MRC | Decoded Requirement | Clear Text Reply |
| 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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
| MATT | Material | ALUMINUM ALLOY 2024 |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |
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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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