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National Stock Number:
1560-01-554-2684
Federal Supply Class:
1560
National Item Identification Number:
015542684
Description:
SUPPORT,STRUCTURAL COMPONENT,AIR
Detail:
A device of various shapes to be permanently attached to the structure of an aircraft. It is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. It may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. Excludes items which are primarily designed for dampening shock and/or vibration. Excludes BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; and BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
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Manufacturer Information:
| 65-5872-43 | 06DM5 | INFINITY FABRICATION, INC. | | 65-5872-43 | 0C7H8 | D-J ENGINEERING INC | | 65-5872-43 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 65-5872-43 | 1P642 | VOLUMATIC INC | | 65-5872-43 | 1QJK4 | FMW, INC. | | 65-5872-43 | 29957 | NORDAM GROUP LLC, THE | | 65-5872-43 | 2V045 | MALONES CNC MACHINING INC | | 65-5872-43 | 59213 | AERO COMPONENTS, LLC | | 65-5872-43 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | RIB INSTAL. LEADING EDGE,INBD FLAP | | AIRCRAFT MISSION DESIGN SERIES | KC-135 | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.040 INCHES NOMINAL | | III MATERIAL | ALUMINUM ALLOY 2024 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | CHORD | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 11.000 INCHES NOMINAL | | OVERALL WIDTH | 3.800 INCHES NOMINAL | | SPECIAL FEATURES | OPPOSITE -44; USED ON -59; 0 SHT,0TEMP; T4 HEAT TREAT; FINISH F-2.115; DIM. ARE STOCKSIZE |
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