The EM-11 Orka (orca) is a touring and executive aircraft manufactured in Poland.
| EM-11 Orka | |
|---|---|
| |
| EM-11C Orka (SP-YEP) | |
| Role | Utility aircraft |
| Manufacturer | Margański & Mysłowski |
| Designer | Edward Margański |
| First flight | 8 August 2003 |
| Status | entering production, in service |
History edit
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.
Specifications edit
Data from [citation needed]
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)
References edit
External links edit
