NSN 1560-01-528-1016 · NIIN 015281016 · FSC 1560
NO DASHES 1560015281016
In Stock
PANEL,STRUCTURAL,AIRCRAFT
Airframe Structural Components
Application: C-2A AND E-2A
Technical characteristics
14 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABNM | THICKNESS | INCHES NOMINAL 0.250 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 6.000 |
| ABHP | OVERALL LENGTH | INCHES NOMINAL 46.000 |
| SFTT | SURFACE TREATMENT | PRIMER EPOXY |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL STD SINGLE TREATMENT RESPONSE -IL-STD-130 |
| RTSE | RELATIONSHIP TO SIMILAR EQUIPMENT | 71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-2A |
| FEAT | SPECIAL FEATURES | SURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409. |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASSN STD SINGLE MATERIAL RESPONSE QQ-A-250 TO 5 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY:STRIP |
| CZDJ | AIRCRAFT LOCATION | WING CENTER SECTION TRAILING EDGE |
| AGAV | END ITEM IDENTIFICATION | C-2A AND E-2A |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |