Part Details | AIRCRAFT STRUCTURAL PLATE
1560-00-020-6251 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: 32312767, 32-31276-7, 1560-00-020-6251, 00-020-6251, 1560000206251, 000206251
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | APR 25, 1967 | 00-020-6251 | 31495 ( PLATE, STRUCTURAL, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-020-6251
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 32-31276-7 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 1560-00-020-6251
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7178 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 TO 15 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | LOWER LONGERON |
| AIRCRAFT STATION NUMBER | FS 249.65 |
| SIDE FOR WHICH DESIGNED | LEFT SIDE |
| AIRCRAFT MISSION DESIGN SERIES | F-4 |
| OVERALL LENGTH | 9.100 INCHES NOMINAL |
| OVERALL WIDTH | 4.700 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.125 INCHES NOMINAL |
| SPECIAL FEATURES | TEMP CONDITION T6 |
| END ITEM IDENTIFICATION | F-4 PHANTOM |