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 3 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) |
2,062 lb |
935 kg |
| Useful Load (with 1 Pilot) |
3,310 lb |
1,500 kg |
| Max Fuel Capacity |
2,573 lb |
1,167 kg |
| ** differs from King Air C90GTi |
Specifications and performance are subject to change without notice.
