|
|
|
National Stock Number:
1560-01-370-3639
Federal Supply Class:
1560
National Item Identification Number:
013703639
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:
| 17P2A6027-5 | 88277 | THE BOEING COMPANY |
|
Techincal Specification:
| AIRCRAFT LOCATION | CENTER FUSELAGE FILLET,LWR WING | | AIRCRAFT MISSION DESIGN SERIES | C-17A | | AIRCRAFT STATION NUMBER | STA 910.500 TO STA 981.500 | | FABRICATION METHOD | LAMINATED AND COMPOSITE | | MATERIAL DOCUMENT AND CLASSIFICATION | DMS1974 MFR REF 1ST MATERIAL RESPONSE AND DMS2288 MFR REF 2ND MATERIAL RESPONSE | | III MATERIAL | PLASTIC POLYAMIDE AND PLASTIC ARAMID | | PROPRIETARY CHARACTERISTICS | NPAC | | SIDE FOR WHICH DESIGNED | LEFT SIDE | | SPECIAL FEATURES | NHA 17P2A6027-3;PANEL INSTL-FILLET,UNDERWING Y=910.500 TO Y=981.500 | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-23377 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-F-18264 MIL SPEC 2ND TREATMENT RESPONSE | | SURFACE TREATMENT | PRIMER EPOXY |
|
|