NSN 1560-01-587-2292 of Panel Structural Aircraft - Parts Details
| Alternative NSN: 1560015872292 |
| Item Name: Panel Structural Aircraft |
| FSG: 15 Aircraft and Airframe Structural Components |
| Federal Supply Class (FSC): 1560 Airframe Structural Components |
| NIIN: 015872292 |
| NCB Code: USA (01) |
| Manufacturers: Society Of Automotive Engineers Inc , Sae International |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers AMS-C-7438-3.1-1 8-4400-5056PAA, AMS C 7438 3 1 1 8 4400 5056PAA under NSN 1560-01-587-2292 of Panel Structural Aircraft manufactured by Society Of Automotive Engineers Inc, Sae International.
Federal Supply Class of NSN 1560-01-587-2292 is FSC 1560 contains part details of Airframe Structural Components. Quote for your desired part numbers.
Part Number's List for NSN 1560-01-587-2292, 1560015872292
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Part No Manufacturer Item Name QTY RFQ AMS-C-7438-3.1-1 8-4400-5056PAA Society Of Automotive Engineers Inc panel structural aircraft Avl RFQ AMS C 7438 3 1 1 8 4400 5056PAA Sae International panel structural aircraft Avl RFQ
Characteristics Data of NSN 1560015872292MRC Criteria Characteristic ABHP OVERALL LENGTH 96.000 INCHES NOMINAL" ABMK OVERALL WIDTH 48.000 INCHES NOMINAL" AGAV END ITEM IDENTIFICATION C-5 ACFT" CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY ALUM HONEYCOMB" CZDJ AIRCRAFT LOCATION AIRFRAME STRUCTURAL" CZEK AIRCRAFT MISSION DESIGN SERIES C-5A" FEAT SPECIAL FEATURES U/O SIDE COWLS, MISC. PANELS, FLAPS, SLATS; 3.1 NOM. CORE DENSITY, 1/8 CELL SIZE, 4.40 THK" MATT III MATERIAL ALUMINUM ALLOY 5056" MDCL MATERIAL DOCUMENT AND CLASSIFICATION MIL-C-7438 MIL SPEC SINGLE MATERIAL RESPONSE" ABHP OVERALL LENGTH 96.000 INCHES NOMINAL" ABMK OVERALL WIDTH 48.000 INCHES NOMINAL" AGAV END ITEM IDENTIFICATION C-5 ACFT" CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY ALUM HONEYCOMB" CZDJ AIRCRAFT LOCATION AIRFRAME STRUCTURAL" CZEK AIRCRAFT MISSION DESIGN SERIES C-5A" FEAT SPECIAL FEATURES U/O SIDE COWLS, MISC. PANELS, FLAPS, SLATS; 3.1 NOM. CORE DENSITY, 1/8 CELL SIZE, 4.40 THK" MATT III MATERIAL ALUMINUM ALLOY 5056" MDCL MATERIAL DOCUMENT AND CLASSIFICATION MIL-C-7438 MIL SPEC SINGLE MATERIAL RESPONSE"
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 96.000 INCHES NOMINAL" |
| ABMK | OVERALL WIDTH | 48.000 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | C-5 ACFT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ALUM HONEYCOMB" |
| CZDJ | AIRCRAFT LOCATION | AIRFRAME STRUCTURAL" |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5A" |
| FEAT | SPECIAL FEATURES | U/O SIDE COWLS, MISC. PANELS, FLAPS, SLATS; 3.1 NOM. CORE DENSITY, 1/8 CELL SIZE, 4.40 THK" |
| MATT | III MATERIAL | ALUMINUM ALLOY 5056" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-C-7438 MIL SPEC SINGLE MATERIAL RESPONSE" |
| ABHP | OVERALL LENGTH | 96.000 INCHES NOMINAL" |
| ABMK | OVERALL WIDTH | 48.000 INCHES NOMINAL" |
| AGAV | END ITEM IDENTIFICATION | C-5 ACFT" |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ALUM HONEYCOMB" |
| CZDJ | AIRCRAFT LOCATION | AIRFRAME STRUCTURAL" |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5A" |
| FEAT | SPECIAL FEATURES | U/O SIDE COWLS, MISC. PANELS, FLAPS, SLATS; 3.1 NOM. CORE DENSITY, 1/8 CELL SIZE, 4.40 THK" |
| MATT | III MATERIAL | ALUMINUM ALLOY 5056" |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-C-7438 MIL SPEC SINGLE MATERIAL RESPONSE" |