|
|
|
National Stock Number:
1560-01-587-1240
Federal Supply Class:
1560
National Item Identification Number:
015871240
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:
| 2.6 5/32 .411 5056 | 51344 | NORTHROP GRUMMAN CORP MILITARY AIRCRAFT SYSTEMS DIV CHANDLER SITE | | AMS-C-7438-2.6-5/32-0.411PAA5056 | 51344 | NORTHROP GRUMMAN CORP MILITARY AIRCRAFT SYSTEMS DIV CHANDLER SITE | | AMSC-7438-2.6-5/32-4110-5056-PAA | 0U583 | SAE INTERNATIONAL | | AMSC-7438-2.6-5/32-4110-5056-PAA | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AMS-C-7438-2.6-5/32-411-5056-PAA | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | MIL-C-7438G | 81349 | MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M |
|
Techincal Specification:
| AIRCRAFT LOCATION | AIRFRAME STRUCTURAL | | AIRCRAFT MISSION DESIGN SERIES | C-5A | | PART NAME ASSIGNED BY CONTROLLING AGENCY | ALUM HONEYCOMB | | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-C-7438G MIL SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 5056 | | SPECIAL FEATURES | U/O SIDE COWLS, SLATS, FLAPS, MISC PANELS; 5/32 CELL SIZE, .411 THK |
|
|