| Item Name | Rib Stiffener Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-486-9865 (014869865) |
| NCB Code | USA (01) |
| Manufacturer | The Boeing Company |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 5HW83123-104 | the boeing company | rib stiffener aircraft | 81205 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMK | Overall Width | 4.000 INCHES NOMINAL |
| MDCL | Material Document And Classification | 5PT-7B02 ASSN STD SINGLE MATERIAL RESPONSE |
| AGAV | End Item Identification | F-22 RAPTOR |
| CZEK | Aircraft Mission Design Series | F-22A |
| MRC | Decoded Requirement | Clear Text Reply |
| CZDJ | Aircraft Location | PANEL SUPPORT, NO. 3 FIXED LEADING EDGE |
| MATT | Material | ALUMINUM ALLOY 7075 |
| CXCY | Part Name Assigned By Controlling Agency | RIB |
| FEAT | Special Features | OVERALL WIDTH DIM. IS STOCK MATERIAL; OPPOSITE -103; M/O: 7075-T7451 ALUMINUM PLATE |
| ABHP | Overall Length | 4.992 INCHES NOMINAL |
| Components Related to NSN - 1560-01-486-9865, 1560014869865 | ||||
| 1560-01-143-1243 (1560011431243) | 1560-01-613-3072 (1560016133072) | 1560-01-666-2431 (1560016662431) | 1560-00-111-1600 (1560001111600) | |
| 1560-01-166-7249 (1560011667249) | 1560-00-432-5686 (1560004325686) | 1560-00-409-4988 (1560004094988) | 1560-01-595-4206 (1560015954206) | |
| 1560-00-047-1833 (1560000471833) | 1560-01-567-5768 (1560015675768) | 1560-01-685-3942 (1560016853942) | 1560-01-521-0544 (1560015210544) | |
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