Soloy Pathfinder 21

Airplanes

Length

14.3 m

Flat Wing Span

15.88 m

Height

5.02 m

Flat Wing Area

25.9571 m²

Max Seating

Cruise Speed

337.9622 km/h

Max Ceiling

8350 m

Number of Engines

Number Built

Maximum Take-Off Weight

5.6291 t (paragliders: kg)

Maximum Range

865.6 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Soloy Pathfinder 21	5.6291	865.6

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Handley Page Jetstream	Turbomeca Astazou	14.37	15.85	16	Compare
Beechcraft C-12 Huron		13.1064	16.4592	13	Compare
Embraer EMB 110 Bandeirante	Pratt & Whitney Canada PT6	15.1	15.33	18	Compare
Piaggio P.180 Avanti	Pratt & Whitney Canada PT6	14.417	14.0208		Compare
Scaled Composites ATTT	Pratt & Whitney Canada PT6	13.4112	16.1544		Compare
Beechcraft Premier I	Williams FJ44	14.02	13.56		Compare

All data (23 fields)

Name: Soloy Pathfinder 21
Manufacturer: Soloy Aviation Solutions
Description: The Soloy Pathfinder 21 was a twin-engined, single-propeller, turboprop aircraft.
ICAO Code: C08T
Designer: Soloy Aviation Solutions
Type: Utility aircraft
Length (m): 14.3
Height (m): 5.02
Cockpit Crew: 1
Max Seating: 19
Cruise Speed (km/h): 337.9622
Min Speed (km/h): 122.3101
Max Ceiling (m): 8350
Rate of Climb (m/s): 7.6
Capacity Description: 15-19 passengers
Number Built: 1
Powerplant Description: 2 × Pratt & Whitney Canada PT6D-114A in a Soloy Dual Pac Combined output twin turboprop, 496 kW (664 hp) each
Status: Scrapped
Wikipedia Article (URL): en.wikipedia.org/wiki/Soloy_Pathfinder_21
Flat Wing Span (m): 15.88
Flat Wing Area (m²): 25.9571
Wake Category: L
Number of Engines: 2