NSN 1560-00-162-7219
Aircraft Structural Panel
Datasheet
-
Product description
Aircraft Structural Panel NSN 1560-00-162-7219.
-
MPN or Model
5-86512-3
-
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.)
12 lb
More from these suppliers
- 1560-00-411-7971 MPN 40-1302-8Aircraft Structural Panel
- 1560-00-766-1559 MPN 5-96298-4Aircraft Skin
- 1560-01-551-5654 MPN 5-86893-74Aircraf Structural Component Web
- 1560-01-552-2933 MPN 65-5893-5Air Structural Component Support
- 1560-00-766-1560 MPN 5-96299-1Aircraft Structural Panel
- 1560-00-798-5098 MPN 35-8221-538Aircraft Skin
- 1560-00-979-5218 MPN 65-28207-3Aircraft Structural Panel
- 1560-01-174-0768 MPN 4F11052-113AAircraft 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.
Pricing and Availability
Get a quote for 1560-00-162-7219 aircraft structural panelManufacturer Part Numbers and Alternates
| MPN manufacturer part number | Registrant or Supplier |
|---|---|
| 5-86512-3 | Boeing Company, The |
| 5-86512-3 | Ices Corporation |
| 5-86512-3 | Craft Manufacturing And Tooling, |
| 5-86512-3 | Handy Tool & Mfg. Co., Inc., The |
| 5-86512-3 | Nordam Group, Inc., The |
| 5-86512-3 | Morris, Mark A |
Stock Check
