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National Stock Number:
1560-01-557-8181
Federal Supply Class:
1560
National Item Identification Number:
015578181
Description:
PANEL,STRUCTURAL,AIRCRAFT
Detail:
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.
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Manufacturer Information:
| 2344M0007-01 | 0YCM5 | BAE SYSTEMS TECHNOLOGY SOLUTIONS & SERVICES INC |
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Techincal Specification:
| AIRCRAFT LOCATION | AQ-36 LPCR | | AIRCRAFT MISSION DESIGN SERIES | C-130 | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/AA ASSN STD SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 6061 | | OVERALL LENGTH | 6.375 INCHES MINIMUM AND 6.405 INCHES MAXIMUM | | OVERALL WIDTH | 5.750 INCHES MINIMUM AND 5.770 INCHES MAXIMUM | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-53022 TY I MIL SPEC 1ST TREATMENT RESPONSE AND MIL-C-46168 COLOR 37038 MIL SPEC 2ND TREATMENT RESPONSE | | SURFACE TREATMENT | PRIMER AND PAINT | | THICKNESS | 0.063 INCHES NOMINAL |
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