1560-14-428-4074
Wing Landing Flap
1560144284074 144284074 PM1A161
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 8 Dec 1988
Data Last Changed
July 2023
July 2023
NATO Update Count
1
1
NATO Data Quality

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PM1A161 A movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading
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in your web browser . 1560-13-110-1552Main Flap With Vane1560131101552 131101552 A10-16-300-00-1M3 PM1A161
| RNVC: 2 | DAC: 6 7 Mar 2012 1560-13-110-1552 https//www.nsnlookup.com /fsg-15/fsc-1560/fr 1560-14-428-4074
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| RNVC: 2 | DAC: 6 7 Mar 2012 1560-13-110-1552 https//www.nsnlookup.com /fsg-15/fsc-1560/fr 1560-14-428-4074
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Restrictions 1560-14-428-4074
End Users 1560-14-428-4074
- France (ZF)
Approved Sources 1560-14-428-4074
- Part Number
- Manufacturer
- Status
- PM1A161
- Manufacturer
- F6117 - Dassault Aviation (Active)
- Primary Buy
- Primary Buy
- PM1A161
- F2312 - Ste Euro Construc Avion Breguet (Active)
- Secondary Buy
- Secondary Buy
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