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) | 01-531-5843 (015315843) |
| NCB Code | USA (01) |
| Manufacturer | Society Of Automotive Engineers Inc, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMSQQA250 4AT3-0060X0360X0.0630 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250/4 | sae international | sheet metal | RFQ |
| AMSQQA250 4A T3 36 0X6 0X0 063 | sae international | sheet metal | RFQ |
| AMSQQA250 4A-T3-36.0X6.0X0.063 | society of automotive engineers inc | sheet metal | RFQ |
| AMS-QQ-A-250/4 | society of automotive engineers inc | sheet metal | RFQ |
| AMSQQA250 4AT3 0060X0360X0 0630 | sae international | sheet metal | RFQ |
| AMS QQ A 250 4 T3 0 063X6X36 | society of automotive engineers inc | sheet metal | RFQ |
| AMS QQ A 250 4 T3 0 063X6X36 | sae international | sheet metal | RFQ |
| AMS-QQ-A-250 4-CDT3-0 063X6X36 | society of automotive engineers inc | sheet metal | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 6.000 INCHES NOMINAL |
| ABRY | LENGTH | 36.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| ALBY | USAGE DESIGN | AIRCRAFT |
| CQBC | MINIMUM TENSILE STRENGTH | 63000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 42000 POUNDS PER SQUARE INCH |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/4 |
| Relevant Components for NSN - 9535-01-531-5843, 9535015315843 | ||||
| 9510-00-224-1673 (9510002241673) | 9505-00-541-9654 (9505005419654) | 9540-01-353-5127 (9540013535127) | 9515-66-151-1706 (9515661511706) | |
| 9515-00-153-3357 (9515001533357) | 9535-01-012-2441 (9535010122441) | 9520-01-694-5689 (9520016945689) | 9510-01-484-4625 (9510014844625) | |
| 9530-00-993-4137 (9530009934137) | 9515-00-153-3227 (9515001533227) | 9515-01-555-3938 (9515015553938) | 9530-00-060-5594 (9530000605594) | |
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