Margański & Mysłowski EM-11 Orka

EM-11 Orka
EM-11C Orka (SP-YEP)
General information
Type	Utility aircraft
Manufacturer	Margański & Mysłowski
Designer	Edward Margański
Status	entering production, in service
History
First flight	8 August 2003

The EM-11 Orka (orca) is a touring and executive aircraft manufactured in Poland.

The EM-11 was designed by Edward Margański of Margański & Mysłowski Zakłady Lotnicze (Margański & Mysłowski Aviation Works), who were previously known for their Swift S-1 and MDM-1 Fox sailplanes. Work on this new low cost, light utility aircraft, of unorthodox configuration, with slim glider-like fuselage and two pusher engines, started in 2001 and was constructed of composite materials with a 4-seat cab placed low, for easier boarding. Luggage is stored behind the rear seats. Composite fuselage was a development of sailpane fuselage.^[1] As the designer Edward Margański pointed out, his goal was to create flying limousine "for people, not only for pilots", offering good visibility, comfort and ease of boarding.^[1] He expressed also, that his ambition was always to create beautiful aircraft, an in this field his inspiration was Let L-200 Morava.^[1]

The first prototype EM-11, registered SP-YEN, flew 8 August 2003.^[1] It has a fixed tricycle landing gear and Rotax 912 (100 hp (75 kW)) engines. The second prototype, registered SP-YEP, was to be a pattern for serial production variant EM-11C, flew 20 October 2005 with Lycoming IO-320 engines and retractable landing gear. In April 2011 EM-11C Orka was EASA certified and is currently in production. Prior to certification, two prototypes and three further aircraft had been built.

Several variants are planned including, a patrol aircraft with an FLIR head, an air ambulance, a cargo aircraft, and an amphibious version.

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General characteristics

• Crew: One
• Capacity: Three passengers
• Wingspan: 13.4 m (44 ft 0 in)
• Width: 10.5 m (34 ft 5 in) wings folded
• Height: 2.585 m (8 ft 6 in)
• Wing area: 16.5 m² (178 sq ft)
• Max takeoff weight: 1,820 kg (4,012 lb)
• Powerplant: 2 × Lycoming IO-320 4-cylinder air-cooled horizontally-opposed piston engines, 118 kW (158 hp) each
• Propellers: 3-bladed MTV-12 constant-speed pusher propellers LH and RH rotation

Performance

• Maximum speed: 359 km/h (223 mph, 194 kn)
• Cruise speed: 261 km/h (162 mph, 141 kn)
• Stall speed: 109 km/h (68 mph, 59 kn)
• Range: 1,700 km (1,100 mi, 920 nmi) with 45 minutes reserve
• Rate of climb: 5.1 m/s (1,000 ft/min)

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