| Item Name | Sheet Metal |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 01-531-2522 (015312522) |
| NCB Code | USA (01) |
| Manufacturer | Society Of Automotive Engineers Inc, Sae International |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-250 1-CD0-0 032X8X36 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
| QQ-A-250 1-0-0.32X8X36 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
| QQ-A-250 1-0-0.32X8X36 | sae international | sheet metal | 0u583 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 8.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 11000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 3500 POUNDS PER SQUARE INCH |
| MATT | MATERIAL | ALUMINUM ALLOY 1100 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/1 FED SPEC 1ST MATERIAL RESPONSE |
| Components Related to NSN - 9535-01-531-2522, 9535015312522 | ||||
| 9520-00-961-8953 (9520009618953) | 9540-00-006-8552 (9540000068552) | 9540-00-805-5993 (9540008055993) | 9515-00-267-0921 (9515002670921) | |
| 9515-01-483-6261 (9515014836261) | 9505-00-228-6209 (9505002286209) | 9510-00-951-0312 (9510009510312) | 9535-01-012-2385 (9535010122385) | |
| 9530-00-512-2347 (9530005122347) | 9510-00-982-6102 (9510009826102) | 9540-01-176-5974 (9540011765974) | 9510-00-056-1921 (9510000561921) | |
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