AMF-S14 Maranda | |
---|---|
Role | Utility aircraft |
Manufacturer |
Falconar Avia Manna Aviation |
Designer | Chris Falconar |
First flight | 1961 |
Number built | 95 (2011) |
Developed from | Adam RA-14 Loisirs |
Variants | Falconar AMF-14H Maranda |
The Falconar AMF-S14 Maranda is a two-seat, light aircraft first flown in Canada in 1961 and originally marketed for amateur construction by Falconar Avia. [1]
Since the winding up of business by Falconar Avia in 2019, the plans are now sold by Manna Aviation. [2]
Based on the Adam RA-14 Loisirs, it is a conventional high-wing strut-braced monoplane with fixed, tailwheel undercarriage. The fuselage is wood construction with fabric covering with a folding wing. [3] The pilot and single passenger sit side-by-side in a fully enclosed cabin. One example has been built as a floatplane with fiberglass covered wooden floats using Falconar plans. [4] [5] The airfoil employed is a NACA 23012. [6]
Acceptable installed engine power ranges from 85 to 150 hp (63 to 112 kW). [7]
Data from Air Trails
General characteristics
Performance
Related development
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AMF-S14 Maranda | |
---|---|
Role | Utility aircraft |
Manufacturer |
Falconar Avia Manna Aviation |
Designer | Chris Falconar |
First flight | 1961 |
Number built | 95 (2011) |
Developed from | Adam RA-14 Loisirs |
Variants | Falconar AMF-14H Maranda |
The Falconar AMF-S14 Maranda is a two-seat, light aircraft first flown in Canada in 1961 and originally marketed for amateur construction by Falconar Avia. [1]
Since the winding up of business by Falconar Avia in 2019, the plans are now sold by Manna Aviation. [2]
Based on the Adam RA-14 Loisirs, it is a conventional high-wing strut-braced monoplane with fixed, tailwheel undercarriage. The fuselage is wood construction with fabric covering with a folding wing. [3] The pilot and single passenger sit side-by-side in a fully enclosed cabin. One example has been built as a floatplane with fiberglass covered wooden floats using Falconar plans. [4] [5] The airfoil employed is a NACA 23012. [6]
Acceptable installed engine power ranges from 85 to 150 hp (63 to 112 kW). [7]
Data from Air Trails
General characteristics
Performance
Related development
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cite journal}}
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help)
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help)
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