Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number AMS QQ A 250 5, which is a Sheet Metal item from Sae International that is listed with the NSN 9535-01-532-0294 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
Note : We Will Not Share Your Information To Any Third Parties.
To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number AMS QQ A 250 5 was specifically produced by Sae International under the CAGE Code 0U583, providing traceability. Furthermore, with the NSN 9535-01-532-0294, one can also determine that this listing falls under Federal Supply Class (FSC) 9535 Plate Sheet Strip and Foil Nonferrous Base Metal. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number AMS QQ A 250 5, and we will be in touch.
| 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote
