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 kilometres. In the U.S., Magni Gyros have
regularly made long trips - for several years now our US agent
has flown his 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 litres (over 5 cubic feet) of available storage space.
External compartment doors provide easy access.
See more photos of the M-22 Voyager
|
TECHNICAL SPECIFICATIONS
| WEIGHT |
|
| Empty
weight (914) |
272
Kg (600 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 (185 kms/hr) |
| Cruising
speed |
90
mph (145 kms/hr) |
| 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. Fibreglass fuselage canopy.
Fibreglass wheel pants. Fibreglass instrument panel. |
| Seat: |
With
integral fuel-tank manufactured in epoxy resin reinforced
with fibreglass. |
| Baggage
Capacity: |
150
Litres |
| 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 fibre with ground adjustable pitch. |
| Rotor: |
two-blade,
composite materials. |
| Controls: |
Single
- Front Seat. |
| Trim |
Electric |
|
|
| STANDARD
EQUIPMENT |
Electric Starter |
|
Airspeed Indicator |
|
Altimeter |
|
Flydat or EIS Instrument Monitor |
|
Cockpit partial enclosure |
|
Prerotator |
|
Rotor Brake |
|
Carburettor Heat and Temperature Gauge - 912
(non-turbo) only |
|
Wheel Brakes and Wheel Pants |
|
Landing Light |
|
Electric Trim - Front |
|
19 gallon Fuel Tank |
|
Arplast Propeller |
|
Magni Rotor |
|
|
| OPTIONS: |
Electric
trim control - rear seat |
|
Removable Rear Seat Windscreen |
For further particulars, please call Michael Richardson, Magni
Gyro Australia ph (08) 97556243 mob 0418 946796
|
