5306-01-528-1015 BOLT,MACHINE Index 6150-01-528-1017 CABLE ASSEMBLY,SPECIAL PURPOSE,E

National Stock Number:
1560-01-528-1016

Federal Supply Class:
1560

National Item Identification Number:
015281016

Description:
PANEL,STRUCTURAL,AIRCRAFT

Detail:
A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. It is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. It may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. It may be mounted by means of fasteners, bonding or welding. Excludes PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.


Manufacturer Information:
7109191145FLEET READINESS CENTER SOUTHWEST
71091-1391145FLEET READINESS CENTER SOUTHWEST


Techincal Specification:
AIRCRAFT LOCATIONWING CENTER SECTION TRAILING EDGE
AIRCRAFT MISSION DESIGN SERIESC-2A
OVERALL LENGTH46.000 INCHES NOMINAL
OVERALL WIDTH6.000 INCHES NOMINAL
PART NAME ASSIGNED BY CONTROLLING AGENCYINAVY:STRIP
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNEDBOTH SIDES
RELATIONSHIP TO SIMILAR EQUIPMENT71091-11 CAP STRIP REPAIR, FOR WING CENTER SECTION TRAILING EDGE
SPECIAL FEATURESSURFACE TREATMENT SPECIFICATION ALSO INCLUDES LPS-409.
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-STD-130 MIL STD SINGLE TREATMENT RESPONSE
SURFACE TREATMENTPRIMER EPOXY
THICKNESS0.250 INCHES NOMINAL


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