NSN 1560-01-163-1678 Frame Installation

About this product

Al honeycomb core perforated 0.1875 in.Hex and 0.0015 in.Nominal foil thickness type 3-15d per bms-4-3a type 2c,substitute material,al honeycomb core per 4/4,3-15n,mil-c-7438b.

Manufacturer part number 25-2371-17 for national stock number 1560011631678.

Datasheet

Product description

Aircraft Structural Panel NSN 1560-01-163-1678.
MPN or Model

25-2371-17
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
Overall Length
88.000 inches
Overall Width
43.000 inches
Thickness
0.526 inches
End Application
B-52
Side For Which Designed
Left side
Aircraft Location
Trailing edge, outboard strut

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Aircraft Structural Panel

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

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Manufacturer Part Numbers and Alternates

MPN manufacturer part number	Registrant or Supplier
25-2371-17	The Boeing Company

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