SeaMax M-22 | |
---|---|
SeaMax M-22 | |
Role | Light amphibious light-sport aircraft and FAI microlight |
National origin | Brazil |
Manufacturer | Airmax Construções Aeronáuticas Seamax Brasil |
Designer | Miguel Rosario |
First flight | 2000 |
Status | In production |
Unit cost |
- Seamax M22 Specs
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The AirMax SeaMax is a Brazilian single-engine, amphibiouslight sport aircraft (LSA) and Fédération Aéronautique Internationale microlight originally manufactured by AirMax Construções Aeronáuticas of Jacarepaguá.[1]
- In this same page, just click above in 'Technical Publications'. Choose your aircraft version manual and click 'download'. SEAMAX keep all documents updated and at your disposal at anytime. Www.seamaxaircraft.com Support Technical publications.
- Sep 04, 2020 This thing has only a total of 60 hours on the aircraft and engine and prop. Everything Is practically new! Give me, Danny a shout for any and all questions you may have. Don't let this new Searey get away. Contact me,Danny, at 931-473-5401 days, or 931-808-5401 evenings till 10 CST. Can't buy the kit for that price!
By 2015 the manufacturer was Seamax Brasil of Sao Paulo.[2]
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SeaMax in Linnasalmi, Hämeenlinna
Design and development[edit]
Plane and Pilot builds on more than 50 years of serving pilots and owners of aircraft with the goal of empowering our readers to improve their knowledge and enthusiasm for aviation. Plane and Pilot expands upon the vast base of knowledge and experience from aviation’s most reputable influencers to inspire, educate, entertain and inform. Product User Manuals Seamax Inflatable Boat Manual Seamax Electric Air Pump (80D / 80DB) Manual Seamax Electric Air Pump (SUP20S) Manual Seamax Electric Air Pump (SUP20D) Manual Seamax Deluxe Launching Wheels Manual Seamax Standard Boat Launching Wheels Manual Seamax Inflatable Boat Cover Manual Seamax Bimini Solution.
The SeaMax was designed in 1999. A prototype was flown in 2000 and the first production aircraft left the factory in 2001. The SeaMax is constructed using composite materials and metal components. It has a two-seat, side-by-side configuration cabin with a bubble canopy which is hydraulically raised for access. The high-wing is strut-braced and the tail is a cruciform tail. The aircraft's tricycle landing gear is retractable for landing on water. It is powered by a 100 hp (75 kW) Rotax 912ULSpusher configuration engine mounted above the wing to avoid water ingestion.[1][2]
Versions can be constructed to meet the requirements of both the European microlight and US LSA categories.[2]
Specifications[edit]
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 8.75 m (28 ft 8 in)
- Wing area: 12.24 m2 (131.8 sq ft)
- Empty weight: 300 kg (661 lb)
- Gross weight: 520 kg (1,146 lb)
- Fuel capacity: 96 litres (21 imp gal; 25 US gal)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)
Performance
- Maximum speed: 210 km/h (130 mph, 110 kn)
- Cruise speed: 195 km/h (121 mph, 105 kn)
- Stall speed: 58 km/h (36 mph, 31 kn)
- Rate of climb: 5 m/s (980 ft/min)
See also[edit]
Aircraft of comparable role, configuration, and era
Related lists
References[edit]
Wikimedia Commons has media related to AirMax SeaMax. |
- ^ abcBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 23. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ abcTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 79. Flying Pages Europe SARL, 2015. ISSN1368-485X
Retrieved from 'https://en.wikipedia.org/w/index.php?title=AirMax_SeaMax&oldid=897906183'
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