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National Stock Number: 1560-01-570-1801
Federal Supply Class: 1560
National Item Identification Number: 015701801
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:
6-74870-2 | 06DM5 | INFINITY FABRICATION, INC. | 6-74870-2 | 0C7H8 | D-J ENGINEERING INC | 6-74870-2 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | 6-74870-2 | 1P642 | VOLUMATIC INC | 6-74870-2 | 1QJK4 | FMW, INC. | 6-74870-2 | 29957 | NORDAM GROUP LLC, THE | 6-74870-2 | 2V045 | MALONES CNC MACHINING INC | 6-74870-2 | 59213 | AERO COMPONENTS, LLC | 6-74870-2 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
AIRCRAFT LOCATION | SKIN SPLICE, FORE FLAP | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT | OVERALL LENGTH | 6.400 INCHES NOMINAL | OVERALL WIDTH | 2.100 INCHES NOMINAL | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL THICKNESS | 0.051 INCHES NOMINAL | MATERIAL | ALUMINUM ALLOY 7075 | SPECIAL FEATURES | OPPOSITE -1; HEAT TREAT T6; FINISH F-2.115; DIM. ARE STOCKSIZE MATL; USED ON 5-88142 OR 65-7360 DEMENDING ON SERIAL NUMBER; AL SHT; 0 TEMPER |
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