| 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) | 01-495-2547 (014952547) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| MMS1420CONDT7451 | boeing company the | plate metal | 76301 | RFQ |
| MMS1420CONDT7451-0.312X48X144 | boeing company the | plate metal | 76301 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 48.000 INCHES NOMINAL |
| ABRY | LENGTH | 144.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.3120 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 - 9535-01-495-2547, 9535014952547 | ||||
| 9515-01-536-3375 (9515015363375) | 9515-00-814-7221 (9515008147221) | 9530-00-237-0734 (9530002370734) | 9540-00-197-9847 (9540001979847) | |
| 9520-01-274-4554 (9520012744554) | 9515-00-061-4892 (9515000614892) | 9530-01-135-8297 (9530011358297) | 9535-01-581-6877 (9535015816877) | |
| 9510-00-541-9207 (9510005419207) | 9540-01-071-2142 (9540010712142) | 9530-00-060-5585 (9530000605585) | 9530-00-233-1340 (9530002331340) | |
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