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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-0.125X12X48, AMS-QQ-A-250-5, AMS-QQ-A-250-5-CD0-0 125X12X48, AMS-QQ-A-250-5-CD0-0-125X12X48 for NSN 9535-01-532-0311 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 9535015320311
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 5 | sae international | sheet metal | Avl | RFQ |
| AMS-QQ-A-250 5-O-0.125X12X48 | 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 125X12X48 | society of automotive engineers inc | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-CD0-0-125X12X48 | society of automotiv | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-O-0-125X12X48 | society of automotiv | sheet metal | Avl | RFQ |
| AMS-QQ-A-250-5-O-0-125X12X48 | society of automotive engineers inc | sheet metal | Avl | RFQ |
Product Details of NSN 9535015320311
| MRC | Criteria | Characteristic |
|---|---|---|
| AGTA | BASIC SHAPE STYLE | SOLID |
| ABRY | LENGTH | 48.000 INCHES NOMINAL |
| ALBY | USAGE DESIGN | AIRCRAFT |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| ABGL | WIDTH | 12.000 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AARN | FABRICATION METHOD | ROLLED |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.1250 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS; |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
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| 9505-00-067-3875(9505000673875) | 9505-00-067-7589(9505000677589) | 9505-00-069-1469(9505000691469) | 9505-00-069-1471(9505000691471) |
