|
|
|
National Stock Number:
1560-01-469-7126
Federal Supply Class:
1560
National Item Identification Number:
014697126
Description:
PLATE,STRUCTURAL,AIRCRAFT
Detail:
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.
|
Manufacturer Information:
| 17P3A2408-503 | 88277 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | AFT FUSELAGE | | AIRCRAFT MISSION DESIGN SERIES | C-17A | | MATERIAL DOCUMENT AND CLASSIFICATION | DMS1592 MFR REF SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.163 INCHES MINIMUM AND 0.173 INCHES MAXIMUM | | III MATERIAL | TITANIUM | | PROPRIETARY CHARACTERISTICS | NPAC | | OVERALL LENGTH | 7.370 INCHES MINIMUM AND 7.430 INCHES MAXIMUM | | OVERALL WIDTH | 5.460 INCHES MINIMUM AND 5.520 INCHES MAXIMUM | | SPECIAL FEATURES | MANUFACTURER SUGGESTED NAME - PLATE,STRUCTURAL,LATCH NO. 10 TO NO. 11, RAMP;NHA 17P3A2400 | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | DPS4.50-36 MFR REF SINGLE TREATMENT RESPONSE | | SURFACE TREATMENT | PAINT EPOXY |
|
|