|
|
National Stock Number: 1560-01-108-1295
Federal Supply Class: 1560
National Item Identification Number: 011081295
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.
|
Manufacturer Information:
204-70011-20 | 06DM5 | INFINITY FABRICATION, INC. | 204-70011-20 | 0C7H8 | D-J ENGINEERING INC | 204-70011-20 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | 204-70011-20 | 1P642 | VOLUMATIC INC | 204-70011-20 | 1QJK4 | FMW, INC. | 204-70011-20 | 29957 | NORDAM GROUP LLC, THE | 204-70011-20 | 2V045 | MALONES CNC MACHINING INC | 204-70011-20 | 32821 | H & R PARTS CO INC | 204-70011-20 | 59213 | AERO COMPONENTS, LLC | 204-70011-20 | 81205 | THE BOEING COMPANY |
|
Techincal Specification:
AIRCRAFT LOCATION | FORWARD FAIRING STRUT ASSY | AIRCRAFT MISSION DESIGN SERIES | E-3A | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL THICKNESS | 0.063 INCHES NOMINAL | MATERIAL | ALUMINUM ALLOY 2024 | OVERALL LENGTH | 8.500 INCHES NOMINAL | OVERALL WIDTH | 3.500 INCHES NOMINAL | SPECIAL FEATURES | FINISH F02.30;HEAT TREAT T42 |
|
|