  
USA Distributor:
Magni USA, L.L.C.
Greg Gremminger
17225 Pleasant View Dr.
Ste. Genevieve, MO 63670
e-mail
(314) 540-0367
(573) 883-2866 (fax)
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M-22 VOYAGER
2-Seater, Partially Enclosed, Optimized for Cross-Country |
 Magni 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.
 The 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. |
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click on photos for expanded view |
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WEIGHT |
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| 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 |
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| 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 |
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| 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 |
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| 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
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OPTIONS:
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- Electric trim control
- Removable Rear Seat Windscreen
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