| 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) | 01-487-5296 (014875296) |
| NCB Code | USA (01) |
| Manufacturer | The Boeing Company |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 5HW82821-135 | the boeing company | panel structural aircraft | 81205 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | Special Features | WIND SWEPT SURFACE CRITICAL ITEM; OPPOSITE -136; C/O: 5HW82822-147 ACCESS PANEL, STUD BOLT (4); DIM. ARE STOCK MATERIAL; M/O 6AL-4V (AD-1) ANN TITANIUM PLATE |
| ABMK | Overall Width | 6.000 INCHES NOMINAL |
| AGAV | End Item Identification | F-22 RAPTOR |
| CZEK | Aircraft Mission Design Series | F-22A |
| ABHP | Overall Length | 11.000 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| CZDJ | Aircraft Location | PANEL ASSEMBLY - ACCESS, RIB 4 AND 6 |
| MDCL | Material Document And Classification | AMS-T-9046 ASSN STD SINGLE MATERIAL RESPONSE |
| MATT | Material | TITANIUM |
| CXCY | Part Name Assigned By Controlling Agency | PANEL ASSEMBLY, AFT |
| Relevant Components for NSN - 1560-01-487-5296, 1560014875296 | ||||
| 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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