| Item Name | Panel Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-454-0033 (014540033) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 68A325304-2241 | boeing company the | panel structural aircraft | 76301 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 14.940 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 9.860 INCHES NOMINAL |
| ABNM | THICKNESS | 0.040 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | COVER,COMPARTMENT-AIRCRAFT MOUNTED AUX DRIVE |
| CZEJ | AIRCRAFT STATION NUMBER | FS595.900 TO FS626.900 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-15S/I/E |
| FEAT | SPECIAL FEATURES | USED ON NEXT ASSY P/N 68A325304-2185 ON F-15S CUM50 AND UP,F-15I CUM20 AND UP AND F-15E CUM210 AND UP |
| MATT | III MATERIAL | TITANIUM |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046.TYPE I,COMP B MIL SPEC SINGLE MATERIAL RESPONSE |
| Relevant Components for NSN - 1560-01-454-0033, 1560014540033 | ||||
| 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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