| 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) | 01-621-8533 (016218533) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| L2300331-013 | boeing company the | panel structural aircraft | 43999 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| CXCY | Part Name Assigned By Controlling Agency | CLOSURE |
| MDCL | Material Document And Classification | QQ-A-250L4 ASSN STD SINGLE MATERIAL RESPONSE |
| FEAT | Special Features | LEADING EDGE,UPPER VERTICAL STABALIZER ASSEMBLY |
| ABMK | Overall Width | 8.00 INCHES NOMINAL |
| ABHP | Overall Length | 20.25 INCHES NOMINAL |
| AGAV | End Item Identification | B1-B ACFT |
| CZDJ | Aircraft Location | LEADING EDGE UPPER |
| CZEK | Aircraft Mission Design Series | B1-1ACFT |
| MATT | Material | ALUMINUM ALLOY 2024 |
| ABNM | Thickness | 0.050 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| Relevant Components for NSN - 1560-01-621-8533, 1560016218533 | ||||
| 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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