2995-01-370-9807 HOUSING,OIL PUMP ASSEMBLY,ENGINE Index 1560-01-370-9809 PANEL,STRUCTURAL,AIRCRAFT

National Stock Number:
1560-01-370-9808

Federal Supply Class:
1560

National Item Identification Number:
013709808

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:
17P2A6022-588277THE BOEING COMPANY


Techincal Specification:
AIRCRAFT LOCATIONCENTER FUSELAGE,WING FILLET,CLOSEOUT
AIRCRAFT STATION NUMBERFS 981.500 TO FS 1045.75
AIRCRAFT MISSION DESIGN SERIESC-17A
FABRICATION METHODLAMINATED AND COMPOSITE
MATERIAL DOCUMENT AND CLASSIFICATIONDMS1974 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 MFR REF 2ND MATERIAL RESPONSE
III MATERIALPLASTIC POLYAMIDE AND PLASTIC ARAMID
PROPRIETARY CHARACTERISTICSNPAC
SIDE FOR WHICH DESIGNEDLEFT SIDE
SPECIAL FEATURESNHA 17P2A6022-3;PANEL INSTL,FILLET CLOSEOUT-Y=981.50 TO Y=1045.75
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONMIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE
SURFACE TREATMENTPRIMER EPOXY


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