AIRCRAFT AND GYROPLANE PROJECTS

ATTK-AVIA IN PARTNERSHIP WITH STATE UNIVERSITY OF AEROSPACE TECHNOLOGIES
PRESENTS NEW DESIGN OF 4-SEAT TWIN ENGINE AIRCRAFT
CHIEF DESIGNER VADIM Y. DEMIN

M-407

four-seat high wing airplane

 

M-409
four-seat low wing airplane

Multi-purpose four-seat twin engine aircraft have been designed according to AP-23 Aviation Rule requirements,
comply with European CS-23 and American FAR-23

Aircraft applications:
- air carriage;
- initial training and professional selection of pilots;
- air patrol;
- aerial photographing, instrument monitoring;
- air tourism and trips.

General views and dimensions

407 views and dimensions       409 dimensions

Advantages and features:
- maximum cruise and minimum landing speeds;
- retractable landing gear, improved aerodynamic, sufficient maneuverability;
- up-to-date control system with side-sticks;
- glass cockpit with multifunctional displays;
- long range modification is available as option;
- short takeoff and landing distance;
- ability of landing on unprepared runways;
- hydroplane modification with floats is available for 407 model as option;
- wider cabin and better pitch in class;
- luggage compartment behind 2nd row;
- full passengers and airframe rescue system;
- new corrosion resistant aluminum alloy, fiberglass and composites are applied;
- low DOC, long life-cycle;
- Gulf specification is available.

Key data and Performance

Model

407 409
Wing span [m] 11.4 11.7
Wing area [sq.m] 14.3 14.3
Wing aspect ratio 9.1 9.1
Wing profile GA(W)-1 GA(W)-1
Fuselage height [m] 1.48 1.40
Fuselage width [m] 1.28 1.28
Fuselage length [m] 7.45 8.32
Landing gear base [m] 2.12 2.60
Wheel track [m] 1.90 3.20
Wheel size [mm] d445 x w160 d445 x w160
Engines Rotax 912S, 2 x 100 hp Rotax 912S, 2 x 100 hp

Max takeoff weight [kg]

1250 1190

Max payload [kg]

325 325

Passenger capacity [pax]

3 3

Crew

1 1

Maximum / Cruise speed [km/h]

290 / 270 310 / 280

Maximum rate-of-climb [m/s]

6 6

Maximum cruise altitude [m]

3000 3000

Range with maximum payload [km]

1500 1500

Take-off / Landing run [m]

150 / 180 140 / 180

Hydroplane modification ability

yes no
 

Both 407 and 409 projects will be accomplished within investment agreement.