| Item Name | Panel Structural Ai |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-358-6993 (013586993) |
| NCB Code | USA (01) |
| Manufacturer | Northrop Grumman Systems Corporation |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 9123962-10 | northrop grumman systems corporation | panel structural ai | 26512 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | COMPOSITE |
| ABHP | OVERALL LENGTH | 16.000 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | A-10A |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-R-9300B MIL SPEC SINGLE MATERIAL RESPONSE |
| ABMK | OVERALL WIDTH | 24.000 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | ENGINE NACELLE LOWER INNER PANEL |
| ABNM | THICKNESS | 0.050 INCHES NOMINAL |
| MATT | MATERIAL | GLASS FIBER |
| SFTT | SURFACE TREATMENT | PRIMER EPOXY-POLYAMIDE AND PAINT POLYURETHANE |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |
| CZEJ | AIRCRAFT STATION NUMBER | NS158.245 TO NS171.500 |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-C-83286 MIL SPEC 2ND TREATMENT RESPONSE |
| Relevant Components for NSN - 1560-01-358-6993, 1560013586993 | ||||
| 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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