Part Details | AIRCRAFT STRUCTURAL PLATE
1560-00-015-2146 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: 69267584, 69-26758-4, 1560-00-015-2146, 00-015-2146, 1560000152146, 000152146
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | JAN 01, 1961 | 00-015-2146 | 31495 ( PLATE, STRUCTURAL, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-015-2146
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 69-26758-4 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 1560-00-015-2146
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 11 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT MISSION DESIGN SERIES | KC-135 |
| MATERIAL THICKNESS | 0.065 INCHES NOMINAL |
| END ITEM IDENTIFICATION | KC-135 TANKER AIRPLANE |