| 1 | A | B | C |
| --- | --- | --- | --- |
| 2 | Beechcraft King Air - Specifications |  |  |
| 3 | King Air | C90GTi | B100 |
| 4 | Crew | 1–2 | 1–2 |
| 5 | Passengers | 7 max | 13 max |
| 6 | Length | 35 ft 6 in / 10.82 m | 39 ft 11 in / 12.17 m |
| 7 | Span | 50 ft 3 in / 15.32 m | 45 ft 11 in / 14.0 m |
| 8 | Height | 14 ft 3 in / 4.34 m | 15 ft 5 in / 4.7 m |
| 9 | Area | 294 ft² / 27 m² | 279.7 ft² / 26.0 m² |
| 10 | Empty Weight | 6,950 lb / 3,150 kg | 7,092 lb / 3,212 kg |
| 11 | MTOW | 10,100 lb / 4,580 kg | 11,800 lb / 5,352 kg |
| 12 | Powerplant | 2xPT6A-135A | 2xTPE-331-6-251B or -252 |
| 13 | Power | 550/ 410 kW | 715 shp / 533 kW |
| 14 | Propellers | Hartzell HC-E4N-3N | 4-bladed |
| 15 | Cruise TAS | 226 kn / 416 km/h | - |
| 16 | Max TAS | 270 kn / 500 km/h | 265 kn / 491 km/h |
| 17 | Stall IAS (flaps down) | 78 kn / 145 km/h | - |
| 18 | Range | 1,321 nmi / 2,446 km | 1,325 nmi / 2,455 km |
| 19 | Fuel consumption | - | 2.08 lb/nmi (0.51 g/m) |
| 20 | Ceiling | 30,000ft / 9,144 m | 24,850 ft / 7,574 m |
| 21 | Climb rate | 2,000 ft/min / 10.2 m/s | 2,140 ft/min / 10.87 m/s |
| 22 | Wing loading | 34.3 lb/ft² / 170 kg/m² | 42.2 lb/ft² / 205.84 kg/m² |
| 23 | 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).