Home | Introduction | Galery | Commuter | Jet | Powerplant Location | Fiber Technology | Float-Wing | Technology | Data | Contact | History | Brochure | Imprint
 

P-2000 TWIN  AMPHIBIAN  COMMUTER (20 seats)

 

passenger version

freight version

Soloy, DualPac turboprop engine

P-2000 TWIN  AMPHIBIAN  COMMUTER
SPECIFICATIONS  &  PERFORMANCES
Engine:     Soloy Dual Pac + Pratt & Whitney PT6
Power:      2 x 665 SHP  =  1330 SHP
Propeller:  5-bladed Scimitar reversible 104” Ø  1700 RPM  de-iced
Max seating FAR 23 20
Length 44.10 ft            13.45 m
Wingspan 62.30 ft            19.00 m
Height including propeller 16.40 ft              5.00 m
Empty weight 5,077 lb              2,300 kg
Useful load 7,285 lb              3,300 kg
Max ramp weight 12,538 lb            5,680 kg
Max take off weight 12,362 lb            5,600 kg
Max landing weight 12,141 lb            5,500 kg
Land-takeoff  S.L. 50 ft Obs. ISA 1,640 ft               600 m
Landing S.L. 50 ft Obs. + prop-reversing 1,476 ft               550 m
Water-takeoff  S.L. 50 ft Obs. ISA 1,968 ft               700 m
Watering S.L. 50 ft Obs. + prop-reversing 1,640 ft               600 m
S.L. rate of climb 1,835 fpm        10 m/s
Max cruise speed 27,000 ft          210 kt         390 km/h
Vno normal operating speed         25,000 ft          205 kt         380 km/h
Vne never exceed speed 210 kt       390 km/h
Vsi stalling speed flaps down            61 kt         113 km/h
Service ceiling 27,000 ft        8,230 m
Service ceiling, one engine off 14,000 ft        4,270 m

Max fuel capacity wetwing

  400 gal   =  1,848 l  =  1,755 kg
Fuel flow  387 lb/hr     175.50 kg
Max endurance 10 h
Max range 2,000 nm     3,700 km
G limits normal category + 4.0 / -1.6
CG control cord 25% to 39.5%
©  EQUATOR AIRCRAFT