| 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) | 01-466-5613 (014665613) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 17P3A1623-513 | boeing company the | plate structural aircraft | 88277 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | Material Thickness | 0.071 INCHES NOMINAL |
| SR-5 | Design Control Reference Or Manufacturers Code | 88277 |
| MATT | Material | ALUMINUM ALLOY 6061 |
| CZDJ | Aircraft Location | CENTER FUSELAGE |
| MDCL | Material Document And Classification | QQ-A-250/11,TEMP T6 FED SPEC SINGLE MATERIAL RESPONSE |
| MRC | Decoded Requirement | Clear Text Reply |
| SR-5 | Design Control Reference Or Manufacturers Code | |
| FEAT | Special Features | MANUFACTURER SUGGESTED NAME - PLATE,STRUCTUREAL-RAMP TOE,FWD;NHA 17P3A1601 |
| SR-5 | Design Control Reference Or Manufacturers Code | 17P3A1623-513 |
| ABHP | Overall Length | 3.000 INCHES NOMINAL |
| CZEK | Aircraft Mission Design Series | C-17A |
| ABMK | Overall Width | 3.000 INCHES NOMINAL |
| Relevant Components for NSN - 1560-01-466-5613, 1560014665613 | ||||
| 1560-01-141-9838 (1560011419838) | 1560-00-588-2363 (1560005882363) | 1560-01-252-8219 (1560012528219) | 1560-01-388-6401 (1560013886401) | |
| 1560-01-008-7294 (1560010087294) | 1560-00-366-9982 (1560003669982) | 1560-00-536-7361 (1560005367361) | 1560-01-027-6767 (1560010276767) | |
| 1560-01-287-5477 (1560012875477) | 1560-01-605-0677 (1560016050677) | 1560-01-237-9622 (1560012379622) | 1560-01-533-6724 (1560015336724) | |
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