Comparison of Nextant G90XT and Pilatus PC-21

Attribute	Nextant G90XT ×	Pilatus PC-21 ×
General
Manufacturer	Nextant Aerospace	Pilatus Aircraft
Model	Nextant G90XT	Pilatus PC-21
Country	United States	Switzerland
Manufactured from (year)	2013	2002
Type	Twin Turboprops	Military Trainers
Icao	G90XT	-
Performance
Engine	2x GE H75-100	1x Pratt & Whitney PT6A-68B
Power, hp (hp)	845	1,600
Avionics	Garmin G1000	BARCO and Meggitt Avionics , Becker Avionics BXT6500 ADS-B transponder
Max cruise speed (km/h)	519	685
Approach speed (km/h)	189	150
Travel range (km)	2,380	1,333
Fuel economy (km/l)	-	0.553
Service ceiling (m)	9,144	7,620
Rate of climb (m/sec)	10.16	21.59
Take off distance (m)	763	725
Landing distance (m)	763	900
Weights
Max take off weight (kg)	4,762	4,250
Max landing weight (kg)	3,595	4,038
Max payload (kg)	972	1,150
Fuel tank capacity (l)	1,173	549
Baggage volume (m³)	1.36	-
Dimensions
Seats	8	2
Cabin height (m)	1.45	-
Cabin width (m)	1.37	-
Cabin length (m)	3.83	-
Exterior length (m)	10.82	11.22
Tail height (m)	4.34	3.75
Fuselage diameter (m)	1.6	1
Wing span (m)	16.36	9.11
Wing tips	No Winglets	No Winglets