AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| 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) | 01-524-2401 (015242401) |
| NCB Code | USA (01) |
| Manufacturer | Society Of Automotive Engineers Inc, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMS-QQ-A-250 14 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250 14-CD0-0 100X12X48 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250 14-CD0-0 100X12X48 | sae international | sheet metal | RFQ |
| AMS QQ A 250 14 | sae international | sheet metal | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| CQHQ | Minimum Yield Strength | 21000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 48.000 INCHES NOMINAL |
| ABGL | Width | 12.000 INCHES NOMINAL |
| AGAV | End Item Identification | FIXED WING AIRCRAFT, MCDONNEL DOUGLAS F-4F PHANTOM |
| CQBC | Minimum Tensile Strength | 40000 POUNDS PER SQUARE INCH |
| MATT | Material | ALUMINUM ALLOY, QQ-A-250/14 |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.100 INCHES NOMINAL |
| Relevant Components for NSN - 9535-01-524-2401, 9535015242401 | ||||
| 9510-00-265-1694 (9510002651694) | 9510-00-294-0987 (9510002940987) | 9540-01-030-4751 (9540010304751) | 9540-01-071-4705 (9540010714705) | |
| 9540-01-392-8966 (9540013928966) | 9530-01-376-7085 (9530013767085) | 9530-00-249-7450 (9530002497450) | 9515-00-580-6208 (9515005806208) | |
| 9510-01-574-0210 (9510015740210) | 9540-01-071-2151 (9540010712151) | 9540-01-071-6543 (9540010716543) | 9515-01-681-2261 (9515016812261) | |
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