|
|
|
National Stock Number:
1560-01-545-4950
Federal Supply Class:
1560
National Item Identification Number:
015454950
Description:
BRACKET,STRUCTURAL COMPONENT,AIR
Detail:
An item of various configuration that is an integral member of the airframe structure. It is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. It may include holes for mounting purposes or to form an assembly.
|
Manufacturer Information:
| 35-10404-38 | 81205 | THE BOEING COMPANY | | 35-10704-38 | 06DM5 | INFINITY FABRICATION, INC. | | 35-10704-38 | 0C7H8 | D-J ENGINEERING INC | | 35-10704-38 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 35-10704-38 | 1P642 | VOLUMATIC INC | | 35-10704-38 | 1QJK4 | FMW, INC. | | 35-10704-38 | 29957 | NORDAM GROUP LLC, THE | | 35-10704-38 | 2V045 | MALONES CNC MACHINING INC | | 35-10704-38 | 59213 | AERO COMPONENTS, LLC | | 35-10704-38 | 81205 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | PANEL-ENGINE WRAP | | AIRCRAFT MISSION DESIGN SERIES | B-52 | | OVERALL LENGTH | 70.000 INCHES NOMINAL | | OVERALL WIDTH | 0.700 INCHES NOMINAL | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE-FRAME CAP, PANEL-ENGINE WRAP COWL, LOWER, ASSY OF | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-362 FED SPEC 1ST MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.040 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 2024 | | SPECIAL FEATURES | OPPOSITE 35-10704-37 |
|
|