| 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) | 01-453-6217 (014536217) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The, Warner Robins Air Logistics Center |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 68A250471-2005 | boeing company the | stiffener aircraft | 76301 | RFQ |
| 68A250471-2005 | warner robins air logistics center | stiffener aircraft | 98752 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | Overall Width | 3.610 INCHES NOMINAL |
| SFTT | Surface Treatment | ANODIZE |
| ABPX | Material Thickness | 1.500 INCHES NOMINAL |
| MATT | Material | ALUMINUM ALLOY 7075 |
| CZDJ | Aircraft Location | CONFORMAL FUEL TANK |
| MDCL | Material Document And Classification | MMS 159 PLATE,CONDITION-T7351 MFR REF SINGLE MATERIAL RESPONSE |
| STDC | Surface Treatment Document And Classification | PS13201,TYPE II,CLASS 1 MFR REF SINGLE TREATMENT RESPONSE |
| MRC | Decoded Requirement | Clear Text Reply |
| ABHP | Overall Length | 11.410 INCHES NOMINAL |
| CZEK | Aircraft Mission Design Series | F-15E |
| FEAT | Special Features | USED ON LCT-4 CUM91-93,96-112;P/N 68A250471-2006 IS THE OPPOSITE CONFIGURATION |
| Components Related to NSN - 1560-01-453-6217, 1560014536217 | ||||
| 1560-01-622-1614 (1560016221614) | 1560-00-473-9499 (1560004739499) | 1560-00-022-8695 (1560000228695) | 1560-01-656-2338 (1560016562338) | |
| 1560-00-102-9097 (1560001029097) | 1560-01-653-0161 (1560016530161) | 1560-14-390-1434 (1560143901434) | 1560-01-432-6504 (1560014326504) | |
| 1560-01-146-9243 (1560011469243) | 1560-01-256-2449 (1560012562449) | 1560-01-438-8198 (1560014388198) | 1560-00-808-0140 (1560008080140) | |
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