1560-12-317-5982
Wing Landing Flap
1560123175982 123175982 VG95211-ML-123175982 A11B162000N3
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 Germany
NSN Created on 20 Apr 1989
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 1560-12-317-5982
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Related Documents 1560-12-317-5982 1+ Documents (More...)
VG95211-ML-123175982 A11B162000N3 A movable airfoil, whether hinged, pivoted or mounted on tracks, forming
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Germany (DE) 4. 1560-12-317-5982 Marketplace Restrictions Approved Sources Datasheet Management Open
RQST NE Updated Every Day 1560-12-317-5982 RQST Updated Every Day 1560-12-317-5982 RQST NE Restrictions
Restrictions 1560-12-317-5982
End Users 1560-12-317-5982
- Portugal (ZP)
Approved Sources 1560-12-317-5982
- Part Number
- Manufacturer
- Status
- VG95211-ML-123175982
- Manufacturer
- D3030 - Wehrtechnische Dienststelle Fur (Active)
- Definitive Standard
- Definitive Standard
- A11B162000N3
- D0216 - General Atomics Aerotec Systems Gmbh (Active)
- Primary Buy
- Primary Buy
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