Magni M-16 Tandem Trainer

Tandem Trainer
Role Two seat autogyro
National origin Italy
Manufacturer Magni Gyro srl, Besnate
Introduction 2000
Number built M-16>120; M-22>44


The Magni M-16 Tandem Trainer is an Italian sport autogyro, seating two in tandem. It and the M-22 Voyager, a touring variant with baggage space and increased endurance, remain in production in 2010 with over 150 sold.

Design and development

Magni Gyro currently (2010) produces five sport autogyro models, all with similar pod and low boom, pusher engine layouts. They differ chiefly in the accommodation: both the M-16 and the newer, closely similar M-22 Voyager have open cockpits and tandem seats.[1]

An 85 kW (114 hp) Rotax 914UL flat four engine is mounted high and uncowled behind the pod, driving a 3-bladed pusher propeller. Below it the slender flat-sided boom carries the fibreglass empennage, which consists of a swept horizontal stabilizer with end-plate fins and a larger, central, fin and rudder. The 2-bladed rotor, mounted on a mast above the pod, is of composite construction. The open cockpits are fitted with dual controls. The M-16 has a tricycle undercarriage with the faired mainwheels on spring cantilever legs. The steerable nosewheel is unfaired.[1]

The newer M-22 is optimised for touring with the inclusion of a pair of long side pods into the lower fuselage. These have their own access doors and together provide 150 L (5.3 cu ft) of baggage space. The M-22 is flown only from the front seat.[1]

Operational history

By mid-2010 there were 114 M-16s and 44 M-22s on European (Russia excluded) civil aviation registers.[2][3] At least 6 have appeared on the registers of South Africa and the US.[4]

Most have been used as sports and recreational aircraft but some have been employed in agricultural spraying and survey work over nature reserves, traffic observation, fire prevention and photographic mapping.[5]

Variants

M-16 Tandem Trainer

Data from Jane's All the World's Aircraft 2010/11[1]

M-16 Tandem Trainer
Initial version. Normally powered by a Rotax 914UL, but a 74 kW (99 hp) Rotax 912 ULS may be fitted. Introduced 2000.
M-16-2006 Tandem Trainer
Improved lubrication, cooling, centre of gravity position and avionics. Introduced 2006.
M-19 Shark
Enclosed cockpit version.[6] Only three prototypes built, no production.[7]
M-22 Voyager
Touring version with baggage space. An increase in fuel capacity to 80 L (17.6 Imp gal or 21.1 US gal) gives it an endurance of 4 hrs. Other specifications are as M-16 apart from an empty weight increase to 280 kg (617 lb).[Notes 1] Introduced June 2005.

Specifications (M-16-2006)

Data from Jane's All the World's Aircraft 2010/11[1]

General characteristics

Performance


Notes

  1. ↑ 1.0 1.1 Jane's All the World's Aircraft give the rotor diameter of the M-22 as 8.53 m; some sources, e.g. Magni UK, give the same figure for the M-16. The corresponding area is 57.1 m2.

References

  1. ↑ 1.0 1.1 1.2 1.3 1.4 Jackson, Paul (2010). Jane's All the World's Aircraft 2010-11. Coulsdon, Surrey: IHS Jane's. pp. 396–7. ISBN 978-0-7106-2916-6.
  2. ↑ Partington, Dave (2010). European registers handbook 2010. Air Britain (Historians) Ltd. p. 286. ISBN 978-0-85130-425-0.
  3. ↑ "Magni M-19 registations". Retrieved 2011-11-19.
  4. ↑ "Magni M16 in SA & US UK". Retrieved 2010-12-10.
  5. ↑ "M-16/22 applications". Retrieved 2010-12-10.
  6. ↑ Jackson, Paul (2010). Jane's All the World's Aircraft 2000-01. Coulsdon, Surrey: Jane's Information Group. pp. 396–7. ISBN 0-7106-2011-X.
  7. ↑ "Magni M-19 Shark". Retrieved 2010-12-10.

External links

Wikimedia Commons has media related to Magni M16.