| 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) | 01-378-4034 (013784034) |
| NCB Code | USA (01) |
| Manufacturer | Lockheed Martin Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| CZEJ | AIRCRAFT STATION NUMBER | FS212.33 TO FS228.66 |
| FEAT | SPECIAL FEATURES | C/O 1 PANEL 3337135-3,1 STIFFENER 3337135-7,1 STIFFENER 3337135-9,1 STIFFENER 3337135-13,1 SUPPORT 3337137-15,1 SUPPORT 3337144-3,6 ANCHOR NUT MS21059-3,2 PIN HLT114-5-6,2 NUT KFN618-5,HEAT REAT PER T6,MATERIAL; CLAD |
| BWJF | SIDE FOR WHICH DESIGNED | LEFT SIDE |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-Q-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
| AGAV | END ITEM IDENTIFICATION | C-130 HERCULES AIRPLANE. |
| CZDJ | AIRCRAFT LOCATION | FUSELAGE LOWER SERFACE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-130H |
| Relevant Components for NSN - 1560-01-378-4034, 1560013784034 | ||||
| 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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