Soloy Pathfinder 21
From Wikipedia, the free encyclopedia
| Soloy Pathfinder 21 | |
|---|---|
| Type | Twin Turboprop |
| Manufacturer | Cessna/Soloy |
| Status | In Service |
| Primary user | Private Owners |
| Number built | Unknown |
| Unit cost | $1.5 million to $1.9 million USD |
| Variants | Cessna 208 |
The Pathfinder 21 is a twin engined, single propeller turboprop aircraft manufactured by the Soloy Corporation, and based off of the successful Cessna 208 airframe. The aircraft is essentially a stock Cessna 208 airframe that has been stretched by 72 inches, with structural reinforcement, and is powered by twin Pratt & Whitney Canada PT6A-114 engines in a DualPack configuration. Image:Cessna.208b.n208nj.arp.jpg
Contents |
[edit] History
[edit] Specifications
General characteristics<h3>
- Crew: 1-2 (Aircraft is certified for single pilot operation)
- Capacity: 15-19
- Length: 46ft 8in (14.3m)
- Wingspan: 52ft 1in (15.88m)
- Height: 16ft 6in (5.02m)
- Wing area: 279.4ft² (85.16m²)
- Empty weight: 7,300lb (3318.2kg)
- Loaded weight: 12,000lb (5454.5kg)
- Max takeoff weight: 12,410lb (5640.9kg)
- Powerplant: 1× Pratt & Whitney Canada Soloy DualPack PT6A-114 Hartzell Five Bladed Reversible, 1329hp (991.05kW)
<h3>Performance<h3>
- Cruise speed: 210mph (337.9km/h)
- Stall speed: 76mph (122.6km/h)
- Range: 539mi (865.6km)
- Service ceiling: 25,000ft (8,350m)
- Rate of climb: 1,500ft/min (7.6m/s)
<ref>PathSpecs. Soloy Corporation. Retrieved on 2006-07-19.</ref>
[edit] References
<references/>
[edit] Related Content
[edit] Related Development
[edit] External links
- Cessna 208 - Technical Data concerning The Cessna 208
- Soloy.com The Soloy Corporation online, products, brochures, etc.
- Caravan Pilots - Cessna Caravan website; Pilot related

