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1560-01-449-2059
Wing Landing Flap
1560014492059 014492059 17N6P0639-516 17N6P0639-502
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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Related Documents 1560-01-449-2059 1+ Documents (More...)
United States (US) 4. 1560-01-449-2059 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1560-01-449-2059 RQST Updated Every Day 1560-01-449-2059 RQST NE Related Documents
Restrictions 1560-01-449-2059
IUID Required
1560-01-449-2059 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 1560-01-449-2059
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-01-449-2059
- US Air Force (FBB4)
- Effective Date:
- 1 Oct 1999
- Former MOE Rule:
- FEE4
Approved Sources 1560-01-449-2059
- Part Number
- Manufacturer
- Status
- 17N6P0639-516
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
- 17N6P0639-502
- 88277 - The Boeing Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 1560-01-449-2059
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- Aircraft Location [CZDJ]
- Wing
- Aircraft Mission Design Series [CZEK]
- C-17A
- Special Features [FEAT]
- Manufacturer Suggested Name - Structural Assembly,Outboard Flap;Nha 17N6p0637
- Design Control Reference Or Manufacturers Code [SR-5]
- Design Control Reference Or Manufacturers Code [SR-5]
- 88277
- Design Control Reference Or Manufacturers Code [SR-5]
- 17N6p0639-516
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Freight Information 1560-01-449-2059
1560-01-449-2059 has freight characteristics.. 1560-01-449-2059 has a variance between NMFC and UFC when transported by rail and the description should be consulted.