AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Plate 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) | 01-495-2549 (014952549) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| MMS1420CONDT7451 | boeing company the | plate metal | RFQ |
| MMS1420CONDT7451-2.75X48X144 | boeing company the | plate metal | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 48.000 INCHES NOMINAL |
| ABRY | LENGTH | 144.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 2.7500 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | F/A-18E/F HORNET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 73000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 63000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | T-7451 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7050 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7050 ALLOY AND T7451 CONDITION |
| Relevant Components for NSN - 9535-01-495-2549, 9535014952549 | ||||
| 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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