| Part Number: L2400014-006 | Manufacturer: Kamp Systems Inc |
| NSN : 1560-01-437-7260 (1560014377260) | Item Name : plate structural aircraft |
| CAGE Code: 02SF5 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : L2400014006 | INC Code: 31495 |
| NIIN : 01-437-7260 (014377260) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-437-7260 Item Description: Plate Structural Aircraft | 1560 | 014377260 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L2400014-006 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 37.210 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 6.750 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.100 INCHES NOMINAL |
| CZDJ | AIRCRAFT LOCATION | VERTICAL STABILIZER LWR RUDDER SEAL LAND |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | B-1B ACFT |
| FEAT | SPECIAL FEATURES | NHA L2400001;OPPOSITE -005 |
| MATT | III MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE |
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