NSN 1560-01-174-0775
Frame Installation
C/o doubler 4f11051-179a; panel assy p/n 4f11056-101a; doubler matl al alloy qq-a-250/12,7075-t6 bare; used as panel assy,floor,relief crew compartment.
Manufacturer part number 4F11051-105A for national stock number 1560011740775.
Datasheet
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Product description
Aircraft Structural Panel NSN 1560-01-174-0775.
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MPN or Model
4F11051-105A
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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)
011790 - Aircraft Parts NOI -
Unit Weight (Est.)
95.1 lb -
End Application
C-5b acft
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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 1560-01-174-0775 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
4F11051-105A | Lockheed Martin Corporation |
4F11051-105A | Triumph Airborne Structures, Inc. |
4F11051-105A | Applied Aerospace Structures, Corp. |
4F11051-105A | Nordam Group, Inc., The |
4F11051-105A | Lbz, L.l.c. |
4F11051-105A | Ki Ho Military Acquisition |
4F11051-105A | Top Flight Aerostructures, Inc. |
4F11051-105A | Cascade Composites, Llc |
4F11051-105A | Aero Components, Inc. |
4F11051-105A | Cpi Aerostructures, Inc. |
4F11051-105A | Honeycomb Company Of America, Inc. |