Thank you for your interest in part number AMS-QQ-A-250 8, a component manufactured by Society Of Automotive Engineers Inc that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 9535-01-532-0513 and features the description “Sheet Metal.” To request a quote for part number AMS-QQ-A-250 8, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 9535-01-532-0513 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Society Of Automotive Engineers Inc, which is associated with the CAGECode 81343. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal part number AMS-QQ-A-250 8.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-532-0513 Item PartTypeName: SHEET,METAL | 9535 | 015320513 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/8-H34-0.040X12X48 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
| MATT | Material | ALUMINUM ALLOY 5052 |
| HEAT | Heat Treatment | H-34 STRAIN HARDENED |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
| CQBC | Minimum Tensile Strength | 34000 POUNDS PER SQUARE INCH |
| MDCL | Material Document And Classification | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |
| ALBY | Usage Design | AIRCRAFT |
| MRC | Decoded Requirement | Clear Text Reply |
| FEAT | Special Features | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
| AARN | Fabrication Method | ROLLED |
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