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National Stock Number:
1560-01-152-6591
Federal Supply Class:
1560
National Item Identification Number:
011526591
Description:
STRINGER,AIRCRAFT
Detail:
AN AUXILIARY LONGITUDINAL MEMBER OF THE STRUCTURAL FRAMEWORK OF A FUSELAGE, NACELLE, EMPENNAGE, WING, AND THE LIKE. IT IS DESIGNED TO STIFFEN AND/OR SUPPORT THE SKIN BY ATTACHMENT OF BULKHEADS, FORMERS, FRAMES, RIBS, AND THE LIKE.
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Manufacturer Information:
| 35-10703-533 | 06DM5 | INFINITY FABRICATION, INC. | | 35-10703-533 | 0C7H8 | D-J ENGINEERING INC | | 35-10703-533 | 0P657 | CAMNETICS MANUFACTURING CORPORATION | | 35-10703-533 | 1P642 | VOLUMATIC INC | | 35-10703-533 | 1QJK4 | FMW, INC. | | 35-10703-533 | 29957 | NORDAM GROUP LLC, THE | | 35-10703-533 | 2V045 | MALONES CNC MACHINING INC | | 35-10703-533 | 59213 | AERO COMPONENTS, LLC | | 35-10703-533 | 81205 | THE BOEING COMPANY |
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Techincal Specification:
| AIRCRAFT LOCATION | PANEL-ENGINE WRAP COWL, UPPER, ASSY | | AIRCRAFT MISSION DESIGN SERIES | B-52 | | OVERALL LENGTH | 39.000 INCHES NOMINAL | | OVERALL WIDTH | 3.200 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-287 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL THICKNESS | 0.040 INCHES NOMINAL | | MATERIAL | ALUMINUM ALLOY 7075 | | SPECIAL FEATURES | MATL; CLAD ALUM SHT, 0 TEMPER; OPPOSITE -534 |
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