Part Details | AIRCRAFT STRUCTURAL PANEL
1560-00-007-8991 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.
Alternate Parts: 6720041071, 6720-04107-1, 1560-00-007-8991, 00-007-8991, 1560000078991, 000078991
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | JUL 21, 1972 | 00-007-8991 | 35987 ( PANEL, STRUCTURAL, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1560-00-007-8991
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6720-04107-1 | 14590 | VERIDIAN ENGINEERING INC |
Technical Data | NSN 1560-00-007-8991
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | HONEYCOMB |
| AIRCRAFT MISSION DESIGN SERIES | C-130 |
| OVERALL LENGTH | 27.920 INCHES NOMINAL |
| OVERALL WIDTH | 22.950 INCHES NOMINAL |