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National Stock Number:
1560-01-512-6162
Federal Supply Class:
1560
National Item Identification Number:
015126162
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:
| 527-14799-18 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | SPLICE FITTING PRODUCTION BREAK | | AIRCRAFT MISSION DESIGN SERIES | C-135 AIRCRAFT | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 2.400 INCHES NOMINAL | | III MATERIAL | ALUMINUM ALLOY 7075 | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ADAPTER | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 34.200 INCHES NOMINAL | | OVERALL WIDTH | 2.500 INCHES NOMINAL | | SPECIAL FEATURES | 6OPPOSITE -17, FINISH F-2.20 PLUS F-2.68; ULTRASONIC INSPECT MATERIAL PRIOR TO MACHINING PER MIL-STD-2154, CLASS A (BAC5439, CLASS A MANADATORY FOR INTERNAL USE BY BOEING AND THEIR CONTRACTORS)7075-T73511 ALUMINUM EXTRUSION BAR PER AMS-QQ-A-200/11 |
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