The Blue Yonder Twin Engine EZ Flyer is a Canadian designed and built, pusher configuration twin-engined, tandem two-seat, open cockpit aircraft provided as a completed aircraft or in kit form by Blue Yonder Aviation.[1][2]
| Twin Engine EZ Flyer | |
|---|---|
| |
| The prototype Twin Engine EZ Flyer C-ITEZ | |
| Role | Kit plane |
| National origin | Canada |
| Manufacturer | Blue Yonder Aviation |
| Designer | Wayne Winters |
| First flight | 1999 |
| Introduction | 1999 |
| Primary user | Private owners |
| Number built | 1 |
| Developed from | EZ Flyer |
The aircraft can be constructed in Canada as a basic ultra-light, or amateur-built aircraft.[1]
Development
editThe Twin Engine EZ Flyer was designed by Wayne Winters of Indus, Alberta and based on the earlier EZ Flyer. Taking inspiration from the twin-engined Ultraflight Lazair and the Leza-Lockwood Air Cam the aircraft was especially designed for the air-to-ground photography role and also for use over hostile terrain where twin engine safety was desirable.[1]
Winters altered the original EZ Flyer design by creating a new centre wing section to mount two powerplants instead of one, increasing the wingspan to 35.5 feet (10.8 m) and the wing area to 235 sq ft (21.8 m2). The fuselage was also stretched 2.0 ft (1 m) to 23 ft (7 m) total, to give a more unimpeded view from the front seat. The aircraft retained the Junker's ailerons of the original Merlin wing along with the Clark "Y" airfoil and construction featuring a leading edge "D" cell and foam ribs. Like the original EZ Flyer, the twin engine version has an open lattice, "N" girder fuselage constructed from 4130 steel tube along with an enlarged vertical tail to improve handling in engine-out situations. The prototype has two seats in tandem and is powered by two Rotax 503 two stroke engines of 50 hp (37 kW).[1][3]
The prototype of the new design flew in 1999. In the basic ultralight version gross weight is limited to the category maximum of 1,200 lb (544 kg). The amateur-built version has a gross weight of 1,400 lb (635 kg).[1]
The Twin Engine EZ Flyer can be equipped with a variety of powerplants, all mounted side-by-side in pusher configuration:[4]
- Rotax 503 50 hp (37 kW)
- Rotax 582 64 hp (48 kW)
- Rotax 912 80 hp (60 kW)
- Rotax 912S 100 hp (75 kW)
Operational history
editDespite being widely demonstrated and reviewed, the prototype remains the sole registered example.[5]
Operators
edit- Blue Yonder Aviation - flight school
Specifications (Twin Engine EZ Flyer)
editData from Blue Yonder website[2]
General characteristics
- Crew: one
- Capacity: one
- Length: 23 ft 0 in (7.0 m)
- Wingspan: 35 ft 6 in (10.8 m)
- Height: 7 ft 0 in (2.1 m)
- Wing area: 235 sq ft (21.9 m2)
- Airfoil: Clark Y[3]
- Empty weight: 789 lb (358 kg)
- Gross weight: 1,400 lb (635 kg)
- Powerplant: 2 × Rotax 503 fixed pitch, 50 hp (37 kW) each
Performance
- Maximum speed: 100 mph (162 km/h, 87 kn)
- Cruise speed: 70 mph (113 km/h, 61 kn)
- Stall speed: 35 mph (57 km/h, 30 kn)
- Range: 352 mi (567 km, 306 nmi)
- Service ceiling: 15,000 ft (4,575 m)
- Power/mass: 14.00 lb/hp (0.12 kW/kg)
Avionics
- none
See also
edit
Aircraft of comparable role, configuration, and era
References
edit- ^ a b c d e Hunt, Adam: Twice the fun! Flying the Twin Engine EZ Flyer, COPA Flight publication, page C-1, September 2005
- ^ a b Winters, Wayne (n.d.). "Twin Engine EZ Flyer". Archived from the original on 24 March 2009. Retrieved 1 March 2009.
{{cite web}}: CS1 maint: year (link) - ^ a b Lednicer, David (October 2007). "The Incomplete Guide to Airfoil Usage". Archived from the original on 15 May 2008. Retrieved 28 February 2009.
- ^ Winters, Wayne (n.d.). "Twin Engine EZ Flyer Price List". Archived from the original on 24 January 2009. Retrieved 1 March 2009.
{{cite web}}: CS1 maint: year (link) - ^ Transport Canada. "Canadian Civil Aircraft Register". Archived from the original on 27 February 2014. Retrieved 10 April 2014.
External links
edit