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1560-00-392-2569
Wing Landing Flap
1560003922569 003922569 14-27200-508
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 1560-00-392-2569
1560-00-392-2569 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 is a US Munitions List Item and must be mutilated to scrap. 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 1560-00-392-2569
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 1560-00-392-2569
- Brazil (YA01)
- Effective Date:
- 1 Aug 2000
- Republic of Korea (ZH01)
- Effective Date:
- 1 Apr 1991
Approved Sources 1560-00-392-2569
- Part Number
- Manufacturer
- Status
- 14-27200-508
- Manufacturer
- 79U29 - Northrop Grumman Systems Corporation (Active)
- Primary Buy
- Primary Buy
- 14-27200-508
- 76823 - Northrop Grumman Systems Corporation (Active)
- Original Design
- Original Design
Datasheet 1560-00-392-2569
- Characteristic
- Specifications
- FIIG
- Specifications
- A11500
- End Item Identification [AGAV]
- Aircraft Model F5e
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Freight Information 1560-00-392-2569
1560-00-392-2569 has freight characteristics.. 1560-00-392-2569 has a variance between NMFC and UFC when transported by rail and the description should be consulted.