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We have a large inventory from top manufacturers such as Sae International, Society Of Automotiv, Society Of Automotive Engineers Inc with top products such as AMS-QQ-A-250 5, AMS-QQ-A-250 5-O-0.032X6X36, AMS-QQ-A-250-5, AMS-QQ-A-250-5-CD0-0 032X6X36, AMS-QQ-A-250-5-CD0-0 032X6X36 for NSN 9535-01-532-0297 Sheet Metal Parts. We pride ourselves on serving the U.S. and her allies while maintaining our No China Sourcing Policy. We invite you to explore our NSN parts at your leisure, and our team of industry experts are on standby to assist you through the purchasing process as needed. Fill out the request for quote form below and hear from a dedicated account representative in fifteen minutes.
Part Information of NSN 9535015320297
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | sae international | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-O-0.032X6X36 | sae international | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5 | society of automotiv | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-CD0-0 032X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-CD0-0 032X6X36 | society of automotiv | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-O-0 032X6X36 | society of automotiv | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-O-0-032X6X36 | society of automotive engineers inc | sheet metal | Avl | RFQ |
Product Details of NSN 9535015320297
| MRC | Criteria | Characteristic |
|---|---|---|
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET 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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
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