| Item Name | Stiffener Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-467-2912 (014672912) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 68A332107-2008 | boeing company the | stiffener aircraft | 76301 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | Material Thickness | 0.045 INCHES NOMINAL |
| MDCL | Material Document And Classification | MIL-T-9046,COMP C,TYPE 3,ANL MIL SPEC SINGLE MATERIAL RESPONSE |
| FEAT | Special Features | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332001, U/O F-15A,B CUM1-BLK11 |
| MATT | Material | TITANIUM ALLOY |
| CZEJ | Aircraft Station Number | FS833.28 |
| CZEK | Aircraft Mission Design Series | F-15A,B |
| ABHP | Overall Length | 8.450 INCHES NOMINAL |
| CZDJ | Aircraft Location | LOWER,AFT CLOSURE BEAM |
| ABMK | Overall Width | 1.880 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| BWJF | Side For Which Designed | RIGHT SIDE |
| Relevant Components for NSN - 1560-01-467-2912, 1560014672912 | ||||
| 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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