|
|
|
National Stock Number:
1560-01-375-8709
Federal Supply Class:
1560
National Item Identification Number:
013758709
Description:
FRAME,AIRCRAFT
Detail:
A principal transverse structural member of the fuselage, hull, nacelle, pod, and the like. It follows the periphery and provides shape and support by attachment to the longitudinal members or skin.
|
Manufacturer Information:
| 35-10702-2056 | 06DM5 | INFINITY FABRICATION, INC. | | 35-10702-2056 | 0C7H8 | D-J ENGINEERING INC | | 35-10702-2056 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 35-10702-2056 | 1P642 | VOLUMATIC INC | | 35-10702-2056 | 1QJK4 | FMW, INC. | | 35-10702-2056 | 29957 | NORDAM GROUP LLC, THE | | 35-10702-2056 | 2V045 | MALONES CNC MACHINING INC | | 35-10702-2056 | 59213 | AERO COMPONENTS, LLC | | 35-10702-2056 | 81205 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | LOWER COWL PANEL ASSEMBLY | | AIRCRAFT MISSION DESIGN SERIES | B-52H | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-355 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.500 INCHES NOMINAL | | III MATERIAL | ALUMINUM ALLOY 2024 | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL LENGTH | 14.800 INCHES NOMINAL | | OVERALL WIDTH | 1.500 INCHES NOMINAL | | SPECIAL FEATURES | U/A: SKIN SUPPORT INBD ANGLE; OPPOSITE -2055; HT T4; FIN F-2.30 |
|
|