NSN 1560-01-370-4087
Frame Installation
Datasheet
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Product description
Aircraft Structural Panel NSN 1560-01-370-4087.
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MPN or Model
17P2A6011-5
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Schedule B
8803.90.9060 (Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)) -
NMF (National Motor Freight)
013120 - Aluminum Article NOI Sub 6 -
Unit Weight (Est.)
276 lb
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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.
Pricing and Availability
Get a quote for 1560-01-370-4087 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |
17P2A6011-5 | Boeing Company, The |
17P2A6011-215 | Boeing Company, The |