| Item Name | Plate Structural Aircraft |
| Federal Supply Group (FSG) | Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC) | 1560 Airframe Structural Components |
| National Item Identification Number (NIIN) | 01-543-2898 (015432898) |
| NCB Code | USA (01) |
| Manufacturer | The Boeing Company |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | Material Thickness | 0.040 INCHES NOMINAL |
| CXCY | Part Name Assigned By Controlling Agency | DOUBLER |
| FEAT | Special Features | -2 OPPOSITE; TEMP 0; SH CLAD; HEAT TREAT T4; FINISH F-2.115; DIMENSIONS ARE STOCKSIZE |
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
| AGAV | End Item Identification | KC-135 |
| CZDJ | Aircraft Location | LE, OUTBOARD AILERON |
| CZEJ | Aircraft Station Number | 779.96 |
| MRC | Decoded Requirement | Clear Text Reply |
| ABHP | Overall Length | 3.500 INCHES NOMINAL |
| ABMK | Overall Width | 1.500 INCHES NOMINAL |
| CZEK | Aircraft Mission Design Series | KC-135 |
| MATT | Material | ALUMINUM ALLOY 2024 |
| Relevant Components for NSN - 1560-01-543-2898, 1560015432898 | ||||
| 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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