| Part Number: 4F42000-123A | Manufacturer: Triumph Group Inc |
| NSN : 1560-01-530-7239 (1560015307239) | Item Name : skin aircraft |
| CAGE Code: 7S551 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 4F42000123A |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-530-7239 Item Description: Skin Aircraft | 1560 | 015307239 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4f42000-123a | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 187.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 65.000 INCHES NOMINAL |
| ABNM | THICKNESS | 0.100 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| CZDJ | AIRCRAFT LOCATION | UPPER LOBE |
| CZEJ | AIRCRAFT STATION NUMBER | FS1964.0 THRU FS2273.0 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 |
| FEAT | SPECIAL FEATURES | REPLACES -105A SKINS; DIM. ARE STOCK MATL; CLAD; HEAT TREAT COND-T761 |
| MATT | III MATERIAL | ALUMINUM ALLOY 7475 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST-07-120 ASSN STD SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 187.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 65.000 INCHES NOMINAL |
| ABNM | THICKNESS | 0.100 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| CZDJ | AIRCRAFT LOCATION | UPPER LOBE |
| CZEJ | AIRCRAFT STATION NUMBER | FS1964.0 THRU FS2273.0 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 |
| FEAT | SPECIAL FEATURES | REPLACES -105A SKINS; DIM. ARE STOCK MATL; CLAD; HEAT TREAT COND-T761 |
| MATT | III MATERIAL | ALUMINUM ALLOY 7475 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST-07-120 ASSN STD SINGLE MATERIAL RESPONSE |
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