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1560-01-476-4107
Wing Landing Flap
1560014764107 014764107 17P6P5603-27
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 1560-01-476-4107
IUID Required
1560-01-476-4107 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. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). 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 1560-01-476-4107
- Schedule B
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- HTS Code
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End Users 1560-01-476-4107
- US Air Force (FBB4)
- Effective Date:
- 1 Jul 2000
Approved Sources 1560-01-476-4107
- Part Number
- Manufacturer
- Status
- 17P6P5603-27
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Management Data 1560-01-476-4107
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Aug 2005
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
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Freight Information 1560-01-476-4107
1560-01-476-4107 has freight characteristics.. 1560-01-476-4107 has a variance between NMFC and UFC when transported by rail and the description should be consulted.