1560-01-587-1219 PANEL,STRUCTURAL,AIRCRAFT Index 1560-01-587-1398 CLIP,AIRCRAFT

National Stock Number:
1560-01-587-1242

Federal Supply Class:
1560

National Item Identification Number:
015871242

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:
3.11/81.4765056PAA51344NORTHROP GRUMMAN CORP MILITARY AIRCRAFT SYSTEMS DIV CHANDLER SITE
AMS-C-7438-3.1-1/8-1.476PAA505651344NORTHROP GRUMMAN CORP MILITARY AIRCRAFT SYSTEMS DIV CHANDLER SITE
AMS-C-7438-3.1-1/8-1476-5056PAA0U583SAE INTERNATIONAL
AMS-C-7438-3.1-1/8-1476-5056PAA81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
MIL-C-7438G81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M


Techincal Specification:
AIRCRAFT LOCATIONAIRFRAME STRUCTURAL
AIRCRAFT MISSION DESIGN SERIESC-5A
PART NAME ASSIGNED BY CONTROLLING AGENCYALUM HONEYCOMB
MATERIALALUMINUM ALLOY 5056
SPECIAL FEATURESU/O SIDE COWLS, MISC PANELS, SLATS, FLAPS; 3.1 NOM CORE DENSITY, 1/8 CELL SIZE, 1.476 THK


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