NSN 1560-01-414-7040
Frame Installation
0.062 inches thickness, aft crew station aircraft location, f-16a/b/c/d aircraft mission design series, material: glass fiber.
Manufacturer part number 16F2191-19 for national stock number 1560014147040.
Datasheet
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Product description
Aircraft Structural Panel NSN 1560-01-414-7040.
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MPN or Model
16F2191-19
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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.)
1.2 lb -
Overall Length
17.000 inches -
Overall Width
14.800 inches -
Thickness
0.062 inches -
End Application
F-16a/b/c/d aircraft -
Aircraft Location
Aft crew station -
Aircraft Mission Design Series
F-16a/b/c/d -
Material
Glass fiber -
Material Specification
Fms-1029, type 2. Color b mfr ref 1st 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.
Pricing and Availability
Get a quote for 1560-01-414-7040 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
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16F2191-19 | Lockheed Martin Corporation |
16F2191-19 | Triumph Fabrications-hot Springs, |
16F2191-19 | Aero Components, Inc. |