1560-21-820-4186
Aircraft Structural Panel
1560218204186 218204186 41A20004-808
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. View more Aircraft Structural Panel
January 2023
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Aircraft Structural Panel 1560218204186 1560-21-820-4186 1560218204186 218204186 is a preformed
Restrictions 1560-21-820-4186
End Users 1560-21-820-4186
- Canada (ZC)
Approved Sources 1560-21-820-4186
- Part Number
- Manufacturer
- Status
- 41A20004-808
- Manufacturer
- 88308 - Bombardier Inccanadair (Active)
- Primary Buy
- Primary Buy