1560-14-548-4201
Aircraft Structural Panel
1560145484201 145484201 MCF1128133-502
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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Restrictions 1560-14-548-4201
End Users 1560-14-548-4201
- France (ZF)
Approved Sources 1560-14-548-4201
- Part Number
- Manufacturer
- Status
- MCF1128133-502
- Manufacturer
- SG408 - Iai/Malat (Replaced)
- Primary Buy
- Primary Buy
- MCF1128133-502
- SD661 - Israel Aircraft Industries Ltdmalat (Replaced)
- Secondary Buy
- Secondary Buy