Part Details | AIRCRAFT STRUCTURAL PLATE
1560-00-004-5582 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: 3888011, 388801-1, 1560-00-004-5582, 00-004-5582, 1560000045582, 000045582
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | JUN 09, 1972 | 00-004-5582 | 31495 ( PLATE, STRUCTURAL, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-004-5582
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 388801-1 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 1560-00-004-5582
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 5,COND T3 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | MOUNTING |
| AIRCRAFT MISSION DESIGN SERIES | C130 |
| OVERALL LENGTH | 2.610 INCHES MINIMUM AND 2.625 INCHES MAXIMUM |
| OVERALL WIDTH | 1.843 INCHES MINIMUM AND 1.853 INCHES MAXIMUM |