NSN 1560-01-305-2233
Frame Installation
Nuclear hardness critical item & smoothness critical item; core material: nomex honeycomb per bms8-124, cl iv, ty v, gr 3, thk tolerance plus or minus .006; opposite -005.
Manufacturer part number DAA3132D903-006 for national stock number 1560013052233.
Datasheet
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Product description
Aircraft Structural Panel NSN 1560-01-305-2233.
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MPN or Model
DAA3132D903-006
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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 -
Unit Weight (Est.)
35.9 lb -
Overall Length
37.000 inches -
Overall Width
23.000 inches -
Thickness
0.600 inches -
End Application
Pacer special -
Criticality Code Justification
Feat -
Aircraft Location
Outboard trailing edge upper panel assembly -
Aircraft Mission Design Series
B-2 -
Material
Plastic aramid -
Nuclear Hardness Critical Feature
Hardened
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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 1560-01-305-2233 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
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DAA3132D903-006 | The Boeing Company |