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USA Distributor: 
 Magni USA, L.L.C.
 Greg Gremminger
e-mail
 (314) 540-0367
(573) 883-2866 (fax)


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M-22 VOYAGER
2-Seater, Partially Enclosed, Optimized for Cross-Country

m22_1Magni Gyro has announced the June, 2005 availability of a new gyroplane model. The M-22 Voyager is a new design gyroplane based on the popular M-16 Trainer model. The model sports large and stylish baggage strakes on each side of the tandem enclosure. Baggage space includes available space under both seats. The M-22, with its new rakish strakes presents a new and very attractive look to the already stylish line of Magni gyroplanes. 
The M-22 Voyager eliminates the rear seat flight and engine controls to allow full utilization of available spaces for baggage. (rear controls cannot be added to the M-22. The M-16 is not adaptable to M-22 modifications.) 

The M-22 Voyager is the same performance and price as the dual control 914, M-16 Trainer. The M-22 is available only with the Rotax 914UL engine. All appropriate M-16 options are available on the M-22, such as the rear seat windscreen shown in the photos. 
m22_2The M-16 Trainer has always been a popular cross-country gyroplane. Around Europe and Africa, flights of M-16s regularly fly thousands of kilometer adventure tours. In the U.S., Magni Gyros have regularly made long trips – for several years now I have flown my M-16 Trainer from Missouri to PRA and EAA conventions in Indiana and Texas. Baggage storage for longer trips has always been a bit wanting. Now, the M22 provides approximately 150 liters (over 5 cubic feet) of available storage space. External compartment doors provide easy access.
click on photos for expanded view
   
WEIGHT
 
Empty weight (914) 270 Kg (595 lb.)
Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
Useful Load - USA 277 Kg (612 lb.)
PERFORMANCE
 
Maximum speed 115 mph
Cruising speed 90 mph
Absolute ceiling 4000 m (13,000 ft)
Service ceiling 3500 m (11,400 ft)
Take-off roll 70 m (230 ft)
Landing roll from 0 to 30 m (0 to 100 ft)
Rate of climb 5 m/s (950 ft/min)
Fuel tank capacity 72 lt (19 gal)
Endurance 3.4 h
Range (no reserve) 300 miles
DIMENSIONS
 
Rotor diameter 8535 mm (28 ft)
Propeller diameter 1700 mm (67 inch)
Overall width 1800 mm (71 inch)
Overall lenght 4655 mm (184 inch)
Overall height 2600 mm (103 inch)
DESCRIPTION
 
Airframe: Chrome-alloy aeronautical 4130 steel, tig welded. Fiberglass fuselage canopy. Fiberglass wheel pants. Fiberglass instrument panel.
Seat: With integral fuel-tank manufactured in epoxy resin reinforced with fiberglass.
Baggage Capacity 150 Liters
Instruments: Rotor Tach, Altimeter, Airspeed Indicator, Flydat or EIS engine monitor
Engine: 914 Rotax Turbo, 4 cylinders, 4-stroke, water-cooled, 115 hp with electric starter and mechanical prerotator.
Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
Rotor: two-blade, composite materials.
Controls: Single - Front Seat
Trim Electric
STANDARD EQUIPMENT
  • Electric Starter
  • Airpeed Indicator
  • Altimeter
  • Flydat or EIS Instrument Monitor
  • Cockpit partial enclosure
  • Prerotator
  • Rotor Brake
  • Wheel Brakes and Wheel Pants
  • Landing Light
  • Electric Trim - Front
  • 19 gallon Fuel Tank
  • Arplast Propeller
  • Magni Rotor
OPTIONS:


  • Electric trim control
  • Removable Rear Seat Windscreen