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DynAero Limousine S-LSA
 
Dyn-Limo
 
The Limousine S-LSA has elements of the MCR-4S and the Twin-R, designed to fit the LSA category. The airframe is based on the MCR-4S. The cabin is finished with the interior developed for the Twin engine "Twin-R". It includes the new memory foam seats for comfort. The Limousine S-LSA bascally the MCR-4S certified under the S-LSA category. A two seater factory built in compliance with ASTM standards, with options and the interior designed for the Twin-R. It is a MCR-4S factory built and limited to 2 occupants whereas the 4S comes as a kit.
 
For its launch, the Limousine S-LSA was offered at 127,728 Euros +GST/VAT ex factory until 31 December 2010.
 
Engine: Rotax 912S, 100 hp
Propeller: 2 blade fix pitch
Wing span: 8.72 m / 28 ft 5 in
Length: 6.72 m / 22 ft 5 in
Height: 1.95 m / 6 ft 4 in
Wing area: 8,30 m / 87.7 sq ft
Aspect ratio: 9,20
Empty Weight fully equiped: 280 Kg / 616 lbs
Structural MTOW: 750 Kg / 1650 lbs
Useful load at 600Kg: 320 Kg / 704 lbs
Fuel tanks: 2 x 100L=200L Total / 52 US Gal
Wing loading: 77 kg/m / 18.8 lb/sq ft
Speed at 75% Cruise, FL 0: 128 Kts (240 Km/h)
Speed at 75% Cruise , FL80: 139 Kts (257 Km/h)
Consumption at 75%: 20.7 L/h / 5.5 US Gal
Range standard tanks at 75%: 1342 Nm (2486Km)
Speed at 65% & FL110: 132 Kts (245 Km/h)
Consumption at 65%: 17.9 L/h / 5 US Gal
Range standard tanks at 65%: 1477 Nm (2737Km)
Take Off distance: 200 m / 656 ft
Climb rate, FL 0: 700 ft/min
G loading: +3.8 /-1.5 g
Glide ratio: 16/1
Cabin Width: 1.17 m / 46 in
 
 
 
 
 
 


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