| Part Number: 4F22033-121A | Manufacturer: Triumph Group Inc |
| NSN : 1560-01-530-4023 (1560015304023) | Item Name : skin aircraft |
| CAGE Code: 7S551 | FSC : 1560 Airframe Structural Components |
| Alternate P/N : 4F22033121A | INC Code: 61081 |
| NIIN : 01-530-4023 (015304023) | FSG : 15 Aircraft and Airframe Structural Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-530-4023 Item Description: Skin Aircraft | 1560 | 015304023 | 0 | P | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4f22033-121a | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 144.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 75.000 INCHES NOMINAL |
| ABNM | THICKNESS | 0.090 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SKIN,UPPER LOBE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 AIRCRAFT |
| FEAT | SPECIAL FEATURES | REPLACES -119A; CLAD(1)SIDE; DIM.ARE STOCK MATL.; ECN 2005C0001; NEW P/N FOR CROWN SKINS FOR MORE CORROSION STRESS RESISTANT |
| MATT | III MATERIAL | ALUMINUM ALLOY 7475 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST-07-118 ASSN STD SINGLE MATERIAL RESPONSE |
| ABHP | OVERALL LENGTH | 144.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 75.000 INCHES NOMINAL |
| ABNM | THICKNESS | 0.090 INCHES NOMINAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SKIN,UPPER LOBE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 AIRCRAFT |
| FEAT | SPECIAL FEATURES | REPLACES -119A; CLAD(1)SIDE; DIM.ARE STOCK MATL.; ECN 2005C0001; NEW P/N FOR CROWN SKINS FOR MORE CORROSION STRESS RESISTANT |
| MATT | III MATERIAL | ALUMINUM ALLOY 7475 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ST-07-118 ASSN STD SINGLE MATERIAL RESPONSE |
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