Part Details | AIRCRAFT STRUCTURAL COMPONENT SUPPORT
1560-00-007-0496 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; BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT; and RADIUS BLOCK.
Alternate Parts: 4F51131101C, 4F51131-101C, 1560-00-007-0496, 00-007-0496, 1560000070496, 000070496
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
15 | JUL 06, 1972 | 00-007-0496 | 32243 ( SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-007-0496
Part Number | Cage Code | Manufacturer |
---|---|---|
4F51131-101C | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 1560-00-007-0496
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-367 FED SPEC SINGLE MATERIAL RESPONSE |
OVERALL LENGTH | 22.710 INCHES NOMINAL |
OVERALL WIDTH | 3.840 INCHES NOMINAL |
MATERIAL THICKNESS | 2.900 INCHES NOMINAL |
END ITEM IDENTIFICATION | C-5A AIRCRAFT |