| Item Name | Panel Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-575-7037 (015757037) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The, Nordam Group Inc |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| L2100164 023 | boeing company the | panel structural aircraft | 43999 | RFQ |
| L2100164-023 | nordam group inc | panel structural aircraft | 29957 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 48.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 140.000 INCHES NOMINAL |
| ABNM | THICKNESS | 8.000 INCHES NOMINAL |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CORE |
| CZDJ | AIRCRAFT LOCATION | TRAILING EDGE-HORIZONTAL STABILIZER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B |
| FEAT | SPECIAL FEATURES | DIM. ARE STOCK MATERIAL |
| MATT | III MATERIAL | ALUMINUM ALLOY 5056 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST0170LB0020 ASSN STD SINGLE MATERIAL RESPONSE |
| Components Related to NSN - 1560-01-575-7037, 1560015757037 | ||||
| 1560-01-075-9616 (1560010759616) | 1560-00-018-5178 (1560000185178) | 1560-01-118-6968 (1560011186968) | 1560-01-038-1887 (1560010381887) | |
| 1560-00-536-6448 (1560005366448) | 1560-00-692-1155 (1560006921155) | 1560-01-548-1248 (1560015481248) | 1560-01-524-2900 (1560015242900) | |
| 1560-00-476-2712 (1560004762712) | 1560-01-614-2100 (1560016142100) | 1560-00-253-9600 (1560002539600) | 1560-00-329-2786 (1560003292786) | |
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