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King Air C90GTx

The King Air C90GTx from 2010 derives from the C90GTi. Key enhancements to the new C90GTx include an increase in gross weight and the addition of composite winglets, which improve climb performance and further increase fuel efficiency. The maximum ramp weight and maximum takeoff weight of the C90GTx have been increased by 385 pounds to 10,545 and 10,485 pounds respectively.

Since there were no other significant changes please rely for further info on the former King Air C90GTi-section.

Technische Daten

External Dimensions
Length 35 ft 6 in 10.82 m
Height 14 ft 3 in 4.34 m
Span** 53 ft 8 in 16.36 m
** differs from King Air C90GTi by additional Winglets
Cabin Dimensions
Length 12 ft 7 in 3.84 m
Height 4 ft 9 in 1.45 m
Width 4 ft 6 in 1.37 m
Characteristics
Seating (Crew + Pax) 2 + 6
Max Cruise Speed 270 kt 500 km/h
Service Ceiling 30.000 ft 9.144 m
Max Range (Ferry + 1 Pilot) 1,312 nm 2,430 km
Engines
Manufacturer Pratt & Whitney Canada
Model PT6A-135-A
Output (per Engine) 550 shp 550 PS
Inspection Interval (TBO) 3,600 hrs 3,600 Std
Weights**
Max Ramp 10,545 lb 4,783 kg
Max Takeoff 10,485 lb 4,756 kg
Max Landing 9,700 lb 4,400 kg
Max Zero Fuel 9,378 lb 4,254 kg
Typ. Equip. Basic Operating 7,235 lb 3,282 kg
** differs from King Air C90GTi
Capacity
Max Payload (without Pilot) 2,143 lb 972 kg
Useful Load (with 1 Pilot) 3,310 lb 1,501 kg
Max Fuel Capacity 2,573 lb 1,167 kg
** differs from King Air C90GTi

Specifications and performance are subject to change without notice.