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National Stock Number:
1560-01-110-6510
Federal Supply Class:
1560
National Item Identification Number:
011106510
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.
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Manufacturer Information:
| 204-70045-398 | 06DM5 | INFINITY FABRICATION, INC. | | 204-70045-398 | 0C7H8 | D-J ENGINEERING INC | | 204-70045-398 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 204-70045-398 | 1P642 | VOLUMATIC INC | | 204-70045-398 | 1QJK4 | FMW, INC. | | 204-70045-398 | 29957 | NORDAM GROUP LLC, THE | | 204-70045-398 | 2V045 | MALONES CNC MACHINING INC | | 204-70045-398 | 59213 | AERO COMPONENTS, LLC | | 204-70045-398 | 81205 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | FWD SIDE COWL ENGINE NACELLE PANEL | | AIRCRAFT MISSION DESIGN SERIES | E-3A | | OVERALL LENGTH | 70.000 INCHES NOMINAL | | OVERALL WIDTH | 57.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.040 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 2024 | | SIDE FOR WHICH DESIGNED | LEFT SIDE | | SPECIAL FEATURES | HEAT TREAT T62;FINISH F-8.05 |
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