Thank you for taking an interest in the Panel Structural Aircraft NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number AMS C 7438 3 1 1 8 4400 5056PAA, an item that traces back to the manufacturer Sae International. Listed with NSN 1560015872292, this listing is available for purchase from our website at any time. If you are interested in part number AMS C 7438 3 1 1 8 4400 5056PAA and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1560-01-587-2292 Item PartTypeName: PANEL,STRUCTURAL,AIRCRAFT | 1560 | 015872292 | 0 | P | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-C-7438-3.1-1/8-4400-5056PAA | 5 | 2 | 3 |
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" |
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