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National Stock Number:
1560-01-544-5889
Federal Supply Class:
1560
National Item Identification Number:
015445889
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:
| 24-1617-3 | 06DM5 | INFINITY FABRICATION, INC. | | 24-1617-3 | 0C7H8 | D-J ENGINEERING INC | | 24-1617-3 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 24-1617-3 | 1P642 | VOLUMATIC INC | | 24-1617-3 | 1QJK4 | FMW, INC. | | 24-1617-3 | 29957 | NORDAM GROUP LLC, THE | | 24-1617-3 | 2V045 | MALONES CNC MACHINING INC | | 24-1617-3 | 59213 | AERO COMPONENTS, LLC | | 24-1617-3 | 81205 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | AERODYNAMIC BALANCE RUDDER | | AIRCRAFT MISSION DESIGN SERIES | B-52G | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE | | III MATERIAL | ALUMINUM ALLOY 2024 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | PANEL ASSY | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 10.500 INCHES NOMINAL | | OVERALL WIDTH | 6.400 INCHES NOMINAL | | SPECIAL FEATURES | SERIAL NO. 57-6468 & ON; USED ON 25-3187; FINISH F-2.115; HEAT TREAT T4; O TEMP SHT | | THICKNESS | 0.032 INCHES NOMINAL |
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