1560-14-540-9770
Aircraft Structural Panel
1560145409770 145409770 EA1M141
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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www.nsnlookup.com /fsg-31/fsc-3120/fr 3120-14-338-1993 https//www.nsnlookup.com /fsg-15/fsc-1560/fr 1560-14-540-9770
Aircraft Structural Panel 1560145409770 Self-Aligning Plain Bearing 3120143464662 EA1M141 https
A detachable assembly in or on which a journal https//www.nsnlookup.com /fsg-15/fsc-1560/fr 1560-14-540-9770
Aircraft Structural Panel 1560145409770 8083Aircraft Leading Edge1560143428083 143428083 EA1M141
Restrictions 1560-14-540-9770
End Users 1560-14-540-9770
- France (ZF)
Approved Sources 1560-14-540-9770
- Part Number
- Manufacturer
- Status
- EA1M141
- Manufacturer
- F6117 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
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