Aerospace Engineering Solutions is proud to offer immediate purchasing options on Society Of Automotive Engineers Inc part number AMS QQ A 250 5 CD0 0 032X12X36, a Sheet Metal product we carry that is listed with the NSN 9535-01-532-0294 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Society Of Automotive Engineers Inc through the CAGE Code 81343, as well as categorized under FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal based on the first four digits of the NSN 9535-01-532-0294. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number AMS QQ A 250 5 CD0 0 032X12X36 and other NSN items of need.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-532-0294 Item PartTypeName: SHEET,METAL | 9535 | 015320294 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-O-0.032X12X36 | 5 | 9 | 5 |
| 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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