AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| 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) | 01-467-3657 (014673657) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 68A332107-2010 | boeing company the | stiffener aircraft | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | Material Thickness | 0.045 INCHES NOMINAL |
| MDCL | Material Document And Classification | MIL-T-9046,TYPE 3,COMP C,ANL MIL SPEC SINGLE MATERIAL RESPONSE |
| FEAT | Special Features | DIM. STOCK MATERIAL; NEXT HIGHER ASSY 68A332001 U/O F-15A,B CUM1-BLK11 |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | TITANIUM ALLOY |
| ABHP | Overall Length | 6.570 INCHES NOMINAL |
| CZEJ | Aircraft Station Number | FS840.59 |
| CZEK | Aircraft Mission Design Series | F-15A,B |
| CZDJ | Aircraft Location | LOWER,AFT CLOSURE BEAM |
| ABMK | Overall Width | 1.880 INCHES NOMINAL |
| BWJF | Side For Which Designed | RIGHT SIDE |
| Relevant Components for NSN - 1560-01-467-3657, 1560014673657 | ||||
| 1560-00-527-0503 (1560005270503) | 1560-14-369-1469 (1560143691469) | 1560-01-103-1503 (1560011031503) | 1560-01-557-1242 (1560015571242) | |
| 1560-01-045-8786 (1560010458786) | 1560-01-684-4250 (1560016844250) | 1560-01-670-3002 (1560016703002) | 1560-01-489-5868 (1560014895868) | |
| 1560-00-040-8570 (1560000408570) | 1560-00-128-2551 (1560001282551) | 1560-01-191-1837 (1560011911837) | 1560-00-682-6014 (1560006826014) | |
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