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National Stock Number:
1560-01-561-1830
Federal Supply Class:
1560
National Item Identification Number:
015611830
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:
| 5-96284-801 | 06DM5 | INFINITY FABRICATION, INC. | | 5-96284-801 | 0BT76 | PRO-FAB, LLC | | 5-96284-801 | 0C7H8 | D-J ENGINEERING INC | | 5-96284-801 | 0JXZ1 | MERRILL CORPORATION | | 5-96284-801 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 5-96284-801 | 14248 | HARLOW AEROSTRUCTURES, LLC | | 5-96284-801 | 1P642 | VOLUMATIC INC | | 5-96284-801 | 29957 | NORDAM GROUP LLC, THE | | 5-96284-801 | 2V045 | MALONES CNC MACHINING INC | | 5-96284-801 | 32821 | H & R PARTS CO INC | | 5-96284-801 | 34336 | TECT HYPERVELOCITY, INC. | | 5-96284-801 | 3L665 | C. E. MACHINE CO., INC. | | 5-96284-801 | 59213 | AERO COMPONENTS, LLC | | 5-96284-801 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | RIB INSTL CLOSURE ELEVATOR TRAILING EDGE | | AIRCRAFT MISSION DESIGN SERIES | KC-135 ACFT | | OVERALL LENGTH | 2.300 INCHES NOMINAL | | OVERALL WIDTH | 1.770 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.510 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 2024 | | SPECIAL FEATURES | OPPOSITE -7; USED ON -10 AND -2 RIB INSTALLATION; BAC1489; T4 CLAD STRIP; T4 TEMP; FINISH F-2.115; DIM. ARE STOCKSIZE MATL. |
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