| Item Name | Plate Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-498-6154 (014986154) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| L3226424-072 | boeing company the | plate structural aircraft | 43999 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | Overall Length | 5.120 INCHES NOMINAL |
| ABPX | Material Thickness | 0.620 INCHES MINIMUM AND 1.250 INCHES MAXIMUM |
| CZDJ | Aircraft Location | AFT VANE BALL ATTACH |
| FEAT | Special Features | DIM. ARE STOCK MATERIAL; NHA L3326421; M/O PH13-8M0 CRES BAR; U/O B-1B 1 AND SUBQ; NUCLEAR HARDNESS CRITICAL ITEM |
| MDCL | Material Document And Classification | ST0160LB0013, COND A ASSN STD SINGLE MATERIAL RESPONSE |
| MRC | Decoded Requirement | Clear Text Reply |
| ABMK | Overall Width | 1.500 INCHES NOMINAL |
| CZEK | Aircraft Mission Design Series | B-1B |
| MATT | Material | STEEL CORROSION RESISTING |
| NHCF | Nuclear Hardness Critical Feature | HARDENED |
| Relevant Components for NSN - 1560-01-498-6154, 1560014986154 | ||||
| 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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