Aerospace Performance Parts is pleased to offer immediate purchasing options for Society Of Automotive Engineers Inc part number AMS-QQ-A-250 5-T3-0.040X6X36, which you have taken interest in. This Sheet Metal item is listed alongside the NSN 9535-01-531-7789 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number AMS-QQ-A-250 5-T3-0.040X6X36 or any other FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal components we carry from Society Of Automotive Engineers Inc under CAGE Code 81343, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 9535-01-531-7789 part number AMS-QQ-A-250 5-T3-0.040X6X36 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7789 Item PartTypeName: SHEET,METAL | 9535 | 015317789 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-CDT3-0,04X6X36 | 5 | 9 | 5 |
| 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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