NSN 1560-01-152-1468
Frame Installation
Tc/o honeycomb core 0.526 in. Thk;inner skin; ring 0.250 in. Dia. Gas relief holes; skin 0.012 in. Thk; 2 doublers 0.250 in. Dia. Gas relief holes; 1 doubler 0.020 in. Thk and 1 doubler 0.040 in. Thk; 9 rivets,blind; and 1 guard.
Manufacturer part number 25-2371-4 for national stock number 1560011521468.
Datasheet
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Product description
Aircraft Structural Panel NSN 1560-01-152-1468.
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MPN or Model
25-2371-4
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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)
106280 - Plates Structural I/s NOI -
End Application
B-52 -
Side For Which Designed
Left side -
Material
Aluminum alloy 2024 -
Material Specification
Qq-a-362 t4 federal specification single material response
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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.
![Mechanic Bill explains Frame Installation](/public/images/billy-thinking.png)
Pricing and Availability
Get a quote for 1560-01-152-1468 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
25-2371-4 | The Boeing Company |
25-2371-4 | The Boeing Company |
25-2371-4 | The Boeing Company |
25-2371-4 | The Boeing Company |
Stock Check
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