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1560-01-514-9825
Wing Landing Flap
1560015149825 015149825 113N2003-45SP
A movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading or trailing edge of a wing of an aircraft. It is designed for the specific purpose of lowering the landing speed by varying the effective camber and may be used in accelerated takeoffs and improved climbs. Excludes leading edge devices that prevent stalls by ducting air over the top of a wing through extended slats. Excludes SLAT,AIRCRAFT. View more Wing Landing Flap
January 2023
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Restrictions 1560-01-514-9825
1560-01-514-9825 is a Wing Landing Flap that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. This item does not contain a precious metal.
Import and Export 1560-01-514-9825
- Schedule B
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- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-514-9825
- New Zealand (ZE01)
- Effective Date:
- 1 Nov 2003
Approved Sources 1560-01-514-9825
- Part Number
- Manufacturer
- Status
- 113N2003-45SP
- Manufacturer
- 81205 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 1560-01-514-9825
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- End Item Identification [AGAV]
- B757 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Flap Assembly Main
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Freight Information 1560-01-514-9825
1560-01-514-9825 has freight characteristics managed by New Zealand.. 1560-01-514-9825 has a variance between NMFC and UFC when transported by rail and the description should be consulted.