NSN 1560-01-425-6410
Aircraft Structural Panel
Datasheet
-
Product description
Aircraft Structural Panel NSN 1560-01-425-6410.
-
MPN or Model
DAA3121D052-008
-
Schedule B
8803.90.9060 (Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites))
More from these suppliers
- 4820-01-263-0340 MPN DAA3284P001-324Check Valve
- 5306-01-349-6103 MPN DAA3252D006-011Shoulder Bolt
- 5985-01-387-7926 MPN DAA3394P420-117Waveguide Assembly
- 1560-01-390-6924 MPN DAA3510A350-007Aircraft Structural Plate
- 5320-01-391-9148 MPN 03A073-8-4APin-rivet
- 1680-01-411-9452 MPN DAA3255P027-119Push-pull Control Assembly
- 1560-01-423-9294 MPN DAA3420D129-339Aircraft Thermal Insulation
- 1560-01-423-9291 MPN DAA3420D129-315Aircraft Thermal Insulation
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 1560-01-425-6410 aircraft structural panelManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
DAA3121D052-008 | Northrop Grumman Systems Corporation |
DAA3121D052-008 | Triumph Aerostructures, Llc |