NSN 1560-00-225-5542
Aircraft Structural Panel
Datasheet
-
Product description
Aircraft Structural Panel NSN 1560-00-225-5542.
-
MPN or Model
4-5019-2
-
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
More from these suppliers
- 1560-01-646-8255 MPN 25-8851-15Aircraft Stiffener Rib
- 5320-00-062-5561 MPN BACB30NW10K8Pin-rivet
- 4820-00-071-4235 MPN 35-17611-504Butterfly Valve
- 5935-00-224-3745 MPN 25-30105-70Electrical Receptacle Connector
- 5306-00-297-2888 MPN 6-52642Shoulder Bolt
- 1560-00-332-2649 MPN 5-87839-32Aircraft Access Cover
- 1560-00-419-6850 MPN 65-48140-4Drain Assembly
- 1560-00-436-0295 MPN 39-23293-2Air Structural Component Support
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 1560-00-225-5542 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
4-5019-2 | Boeing Company, The |
4-5019-2 | The Boeing Company |
4-5019-24 | Boeing Company, The |
4-5019-24 | The Boeing Company |
4-5019-24 | Infinity Fabrication Inc |
4-5019-24 | Malone's Cnc Machining, Inc. |
4-5019-24 | H & R Parts Co., Inc. |
4-5019-24 | Honeycomb Company Of America, Inc. |
Stock Check
