Advanced Aviation Explorer
| Explorer | |
|---|---|
| Role | Ultralight homebuilt aircraft |
| Manufacturer | Advanced Aviation |
| First flight | 1990s |
| Developed from | Maxair Drifter Sport Flight Talon |
The Advanced Aviation Explorer is a two-seat ultralight marketed for home building. It is a high-wing taildragger aircraft of pusher configuration with tandem seating.[1]
Design and development
The aircraft is a development of the Talon XP which in turn traces its linage to the Maxair Drifter. The Explorer has been produced by a number of companies and under a variety of names.[1]
The main advance over the Drifter is the Explorer's use of main wing struts and jury struts in place of cable bracing. Like all aircraft in this family they feature excellent visibility, especially from the front seat when the optional fibreglass cockpit pod is removed. As a result the design is often employed as a camera platform. It can be flown on floats and has been used for banner towing.[1]
Construction is of bolted aluminium tube, with the flying surfaces covered in pre-sewn Dacron envelopes. The kit takes about 150 hours to assemble.[1]
The standard engine is the Rotax 582 of 400 hp (298 kW), with the four-stroke 80 hp (60 kW) Rotax 912 optional.[1]
Variants
- Explorer
- Initial version, derived from the Talon XP, but with struts in place of the cable-braced wing. Produced by Advanced Aviation, no longer in production.[1]
- Zephyr
- Similar to the Explorer, but produced by Arnet Pereyra, no longer in production.[1]
- Toucan
- New name for the aircraft when manufacturer Arnet Pereyra changed the company name to Aero Adventure. In production.[1][2]
Specifications (Toucan)
Data from Cliche[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 22 ft 6 in (6.86 m)
- Wingspan: 29 ft 8 in (9.04 m)
- Height: 7 ft 0 in (2.13 m)
- Wing area: 156 sq ft (14.5 m2)
- Empty weight: 480 lb (218 kg)
- Gross weight: 1,050 lb (476 kg)
- Fuel capacity: 12 US gallons (45 litres)
Performance
- Maximum speed: 90 mph (140 km/h, 78 kn)
- Cruise speed: 73 mph (117 km/h, 63 kn)
- Stall speed: 33 mph (53 km/h, 29 kn)
- Range: 200 mi (320 km, 170 nmi)
- Service ceiling: 14,000 ft (4,300 m)
- Rate of climb: 1,100 ft/min (5.6 m/s)
See also
Related development
References
External link
 | This article on an aircraft of the 1990s is a stub. You can help Wikipedia by expanding it. |