| 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) | 01-568-1095 (015681095) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| L3226402-022 | boeing company the | panel structural aircraft | 43999 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 38.900 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 18.800 INCHES NOMINAL |
| ABNM | THICKNESS | 0.032 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | B-1B ACFT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSY |
| CZDJ | AIRCRAFT LOCATION | FWD NACELLE DUCT VANE |
| CZEJ | AIRCRAFT STATION NUMBER | YN99.75 TO YN143.00 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT |
| FEAT | SPECIAL FEATURES | N/A L3226401; U/O Q AND SUB; -21 OPPOSITE; T3; CORE BIAS WEAVE GLASS REINFORCED PHENOLIC; C/O ALLOY SH, CORE, CHANNEL, CLIPS, RIVETS, PLUGS |
| MATT | III MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| Relevant Components for NSN - 1560-01-568-1095, 1560015681095 | ||||
| 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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