You have arrived on the Request for Quote (RFQ) page for part number AMS QQ A 250 5 CD0 0 032X12X36, a Society Of Automotive Engineers Inc component that is listed with the product description “Sheet Metal” and NSN 9535-01-532-0294 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Society Of Automotive Engineers Inc part number AMS QQ A 250 5 CD0 0 032X12X36, you can seamlessly search for more items from this manufacturer or CAGECode 81343 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal, which this component falls under having the NSN 9535-01-532-0294. Whether you desire part number AMS QQ A 250 5 CD0 0 032X12X36 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| 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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