1560-14-368-5014
Wing Landing Flap
1560143685014 143685014 F10A162A1 85-691-0238
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
Managed by France
NSN Created on 20 Feb 1981
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality
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F10A162A1 85-691-0238 A movable airfoil, whether hinged, pivoted or mounted on tracks, forming part
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Restrictions 1560-14-368-5014
End Users 1560-14-368-5014
- France (ZF)
Approved Sources 1560-14-368-5014
- Part Number
- Manufacturer
- Status
- F10A162A1
- Manufacturer
- F6117 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
- 85-691-0238
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference
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