Part Details | AIRCRAFT STRUCTURAL PLATE
1560-00-011-1334 A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes PLATE, MENDING; SHIM; and SPACER, PLATE.
Alternate Parts: 3C13075105, 3C13075-105, 1560-00-011-1334, 00-011-1334, 1560000111334, 000111334
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | JAN 01, 1963 | 00-011-1334 | 31495 ( PLATE, STRUCTURAL, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-011-1334
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3C13075-105 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 1560-00-011-1334
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 4 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | COVER,RUDDER PEDAL |
| AIRCRAFT MISSION DESIGN SERIES | C-141 |
| OVERALL LENGTH | 28.970 INCHES NOMINAL |
| OVERALL WIDTH | 9.000 INCHES NOMINAL |
| MATERIAL THICKNESS | 5.250 INCHES NOMINAL |