| Item Name | Plate Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-488-1770 (014881770) |
| NCB Code | USA (01) |
| Manufacturer | The Boeing Company |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 5HF74230-101 | the boeing company | plate structural aircraft | 81205 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 10.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.500 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | F-22 RAPTOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CLOSURE PLATE |
| CZDJ | AIRCRAFT LOCATION | AFT BOOM |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
| FEAT | SPECIAL FEATURES | WIND SWEPT SURFACE CRITICAL ITEM; OPPOSITE -102; DIM. ARE STOCK MATERIAL; M/O: 6AL-4V (AB-1) ANN TITANIUM PLATE, FINAL COND A |
| MATT | III MATERIAL | TITANIUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 ASSN STD SINGLE MATERIAL RESPONSE |
| Components Related to NSN - 1560-01-488-1770, 1560014881770 | ||||
| 1560-01-222-3045 (1560012223045) | 1560-00-704-6805 (1560007046805) | 1560-01-022-7230 (1560010227230) | 1560-01-187-8221 (1560011878221) | |
| 1560-00-431-9978 (1560004319978) | 1560-01-162-5479 (1560011625479) | 1560-01-643-4675 (1560016434675) | 1560-01-461-8303 (1560014618303) | |
| 1560-01-245-2559 (1560012452559) | 1560-00-617-9811 (1560006179811) | 1560-00-118-7606 (1560001187606) | 1560-00-885-0736 (1560008850736) | |
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