magnigactory

Dealers

Insurance

photos_dvd



PinkLadies


magnisday


Used Magnis

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


GAITROS AVIATION
Rotax Independent
Repair Center
Annuals - Maintenance
LSA, Experimental
& Standard Aircraft

PRA  stlclub
RotorcraftForum
PSF Magazine

tshirts
T-shirts, etc.


M-16 TANDEM TRAINER
2-Seater, Partially Enclosed

Magni trainingNew to the millennium model of the M-16 are longer and wider cockpit areas, a larger windscreen, an optional removable rear seat windscreen, a larger instrument panel, a larger seat tank (19 gal), standard electric trim, fuel gauge, Flydat or EIS engine monitor, airspeed indicator, altimeter, rotor tachometer, prerotator, rotor brake, wheel brakes, landing light and wheel pants. See the extensive list of standard equipment listed below.
 
Two different engines are available: Rotax 914 turbo (115 HP) or Rotax 912 ULS (100 HP). With the Rotax 912 ULS, carburetor heat and temperature gauge is standard.
 
The M16 Tandem Trainer affords many ways to share and enjoy the passion of un-restrained gyroplane freedom in the unprecedented safety and aerodynamic stability the Magni gyros are famous for. Dual-seat share the fun with a companion in comfort and security with exceptional cross-country speed and range. The tandem configuration affords efficient and effective training. The M16 has even demonstrated utility as an agricultural crop sprayer (with Micronair atomizers and 150 lt. tank)
M16DRAW2M16DRAW1M16DRAW3
WEIGHT
 
Empty weight (914) 270 Kg (595 lb.)
Empty weight (912 ULS) 265 Kg (585 lb.)
Maximum take-off gross wt - USA 550 Kg (1212 lb.) (Note: European "ultralight" limitations are 450 Kg)
Useful Load - USA 280 Kg (617 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.
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. Available also with Rotax 912 ULS (100 HP).
Propeller: Arplast 67 inch three-blade carbon fiber with ground adjustable pitch.
Rotor: two-blade, composite materials
Controls: Dual
Trim Electric
STANDARD EQUIPMENT
  • Electric Starter
  • Airpeed Indicator
  • Altimeter
  • Flydat or EIS Instrument Monitor
  • Cockpit partial enclosure
  • Prerotator
  • Rotor Brake
  • Carburetor 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