NSN 1560-00-898-8579
Aircraft Structural Panel
Datasheet
-
Product description
Aircraft Structural Panel NSN 1560-00-898-8579.
-
MPN or Model
65-4034
-
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.)
14 lb
More from these suppliers
- 1560-00-898-8586 MPN 65-4041-1Aircraft Structural Panel
- 1560-01-004-8754 MPN 35-33251-8Aircraft Access Door
- 1560-00-652-7617 MPN 90-4577-51Aircraft Trailing Edge
- 1560-00-788-4998 MPN 35-8679-19Aircraft Access Door
- 1560-01-444-4961 MPN 40-1080-506Aircraft Structural Panel
- 1560-00-035-1257 MPN 6-54199Follow Arm Assembly
- 5305-00-045-3180 MPN BACB30LR4-6Machine Screw
- 5306-00-097-9425 MPN 26-10171-1Externally Relieved Body Bolt
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 1560-00-898-8579 aircraft structural panelManufacturer Part Numbers and Alternates
| MPN manufacturer part number | Registrant or Supplier |
|---|---|
| 65-4034 | The Boeing Company |
| 65-4034 | Craft Manufacturing And Tooling, |
| 65-4034 | Handy Tool & Mfg. Co., Inc., The |
| 65-4034 | Ices Corporation |
| 65-4034 | Boeing Company, The |
| 65-4034 | Nordam Group, Inc., The |
| 65-4034 | Morris, Mark A |
Stock Check
