| 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) | 01-498-6152 (014986152) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| L3226424-031 | boeing company the | plate structural aircraft | 43999 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.120 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 1.500 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.620 INCHES MINIMUM AND 0.750 INCHES MAXIMUM |
| CZDJ | AIRCRAFT LOCATION | AFT VANE BALL ATTACH |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| FEAT | SPECIAL FEATURES | DIM. ARE STOCK MATERIAL; U/O B-1B 1&SUBQ; NHA L3316421; NUCLEAR HARDNESSCRITICAL ITEM |
| MATT | III MATERIAL | STEEL CORROSION RESISTING |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST0160LB0013,COND A,CRES BAR ASSN STD SINGLE MATERIAL RESPONSE |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| Relevant Components for NSN - 1560-01-498-6152, 1560014986152 | ||||
| 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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