MCR 4S

by DynAero
3.4
7
MCR 4S - Photo #1

The objective was to develop, what most thought impossible at that time:

A four seat airplane with STOL performance, equipped with a light 100 HP engine

The 4-S maiden flight was in June 2000.

The MCR 4-S is the only airplane in the aviation world to provide pilots with such an amazing Performance/Economy ratio. Its concept makes it to be the perfect travel aircraft, able to fly comfortably with four people onboard, cruising at more than 250 km/h, and burning only 20 L/h with a 100 hp engine. Those performances can only be reached because of the MCR 4-S very light empty weight . The aircraft can carry up to 150% of its own empty weight!

The research of a very elaborated aerodynamic design, with wing-tips optimized in wind-tunnel, and high efficiency double slotted flaps, provide the MCR 4-S with amazing STOL performances Designed around a roomy cockpit ; 1,20m width at the rear seats, build to allow four people up to 1,95m tall to be easily seated in the airplane.

The aircraft is equipped with a very strong oil-pneumatic undercarriage, allowing landings on any type of runways.

The MCR-4S can be equipped with a choice of different power plants, but may also be fitted with other options such as :

* Ballistic Recovery System parachute(actually in development)

* Extended range fuel tanks

* Toe operated Hydraulic brakes

The MCR-4S is available in kit form in respect with the CNSK regulation (specific kit airworthiness certificate) or in the experimental category ,depending on the registration country.

Text and photo from www.dynaero.com

Specifications

Empty weight:
661 lbs (300 kg)
MTOW:
1653 lbs (750 kg)
Stall speed:
45 kts (52 mph) (83 kph)
Cruise speed:
131 kts (151 mph) (243 kph)
VNE:
146 kts (168 mph) (270 kph)
Climb:
750 ft/min (3.8 m/s)
Take-off distance:
1476 ft (450 m)
Landing distance:
1804 ft (550 m)
Engine:
Rotax 912, 912 S or 914, Jabiru

Watch 1 Video about the MCR 4S

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