Beechcraft King Air
Specifications

King Air
C90GTi
B100
Crew
1–2
1–2
Passengers
7 max
13 max
Length
35 ft 6 in / 10.82 m
39 ft 11 in / 12.17 m
Span
50 ft 3 in / 15.32 m
45 ft 11 in / 14.0 m
Height
14 ft 3 in / 4.34 m
15 ft 5 in / 4.7 m
Area
294 ft² / 27 m²
279.7 ft² / 26.0 m²
Empty Weight
6,950 lb / 3,150 kg
7,092 lb / 3,212 kg
MTOW
10,100 lb / 4,580 kg
11,800 lb / 5,352 kg
Powerplant
2xPT6A-135A
2xTPE-331-6-251B or -252
Power
550/ 410 kW
715 shp / 533 kW
Propellers
Hartzell HC-E4N-3N
4-bladed
Cruise TAS
226 kn / 416 km/h
-
Max TAS
270 kn / 500 km/h
265 kn / 491 km/h
Stall IAS (flaps down)
78 kn / 145 km/h
-
Range
1,321 nmi / 2,446 km
1,325 nmi / 2,455 km
Fuel consumption
-
2.08 lb/nmi (0.51 g/m)
Ceiling
30,000ft / 9,144 m
24,850 ft / 7,574 m
Climb rate
2,000 ft/min / 10.2 m/s
2,140 ft/min / 10.87 m/s
Wing loading
34.3 lb/ft² / 170 kg/m²
42.2 lb/ft² / 205.84 kg/m²
Power/weight
0.099 hp/lb / 179 W/kg
0.121 hp/lb / 199.17 W/kg

Question: What engine was the C90GT fitted with and how much power did it make?
Answer: The C90GT was fitted with PT6A-135As and 550 shp (410 kW).