AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Part Number AMS C 7438 3 1 1 8 4400 5056PAA described as Panel Structural Aircraft with NSN 1560-01-587-2292 with FSC 1560 Airframe Structural Components by Manufacture Sae International is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1560-01-587-2292 Item Description: 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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