Part Details | AIRCRAFT STRUCTURAL COMPONENT SUPPORT
1560-00-018-0674 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: CV155205183, CV15-520518-3, 1560-00-018-0674, 00-018-0674, 1560000180674, 000180674
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | MAY 08, 1968 | 00-018-0674 | 32243 ( SUPPORT, STRUCTURAL COMPONENT, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-018-0674
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CV15-520518-3 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 1560-00-018-0674
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CONSISTS OF 1 FITTING,ALUMINUM ALLOY,QQ-A-200/11 7075-T6,2.620 IN. LG,1.880 IN. W,0.120 IN. THK MATL,4 HOLES 0.191 IN. DIA,2 HOLES 0.625 IN. DIA,2 BUSHINGS |
| END ITEM IDENTIFICATION | AIRCRAFT MODEL A7A |