|
|
|
National Stock Number:
1560-01-523-6684
Federal Supply Class:
1560
National Item Identification Number:
015236684
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:
| 204-70045-114 | 0C7H8 | D-J ENGINEERING INC | | 204-70045-114 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 204-70045-114 | 1QJK4 | FMW, INC. | | 204-70045-114 | 81205 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | SIDE COWL PANEL ASSY-ENG. NACELLE | | AIRCRAFT MISSION DESIGN SERIES | E-3A | | OVERALL LENGTH | 5.000 INCHES NOMINAL | | OVERALL WIDTH | 2.200 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9046 MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.050 INCHES NOMINAL | | MATERIAL | TITANIUM | | SIDE FOR WHICH DESIGNED | LEFT SIDE | | SPECIAL FEATURES | USED 0N -1, -401, -447, -460; FINISH SRF 12.205; DIMENSIONS ARE STOCKSIZE; LH ONLY |
|
|