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Pilatus PC-12

Pilatus PC-12 Specifications

General characteristics

Crew: one or two pilots
Capacity: 9 passengers standard, 6-8 executive
Payload: 1,500 kg (3,502 lb)
Length: 14.40 m (47 ft 3 in)
Wingspan: 16.23 m (53 ft 3 in)
Height: 4.26 m (14 ft 0 in)
Wing area: 25.81 m² (277.8 ft²)
Empty weight: 2,761 kg (5,867 lb)
Loaded weight: 4,700 kg (10,450 lb)
Max takeoff weight: 4,740 kg (10,450 lb)
Powerplant: 1× Pratt & Whitney Canada PT6A-67B turboprop, 895 kW (1,200 shp)
*Maximum landing: 4,700 kg (10,450 lb)
Maximum payload full fuel: 539 kg (1,189 lb)
Tail wingspan: 5.20 m (17 ft 1 in)
Propeller: Hartzell HC - E4A - 3D/E10477K – 4 blade aluminum
Propeller diameter: 2.67 m (8 ft 9 in)
Propeller RPM: 1,700 rpm constant speed

Performance

Cruise speed: 500 km/h (312.5 mph / 270 KTAS)
Stall speed: 120 km/h (74.8 mph / 65 KCAS)
Service ceiling 9,150 m (30,000 ft)
Rate of climb: 512 m/min at sea level (1,680 ft/min)
Wing loading: 174.3 kg/m² (35.7 lb/ft²)
Power/mass: 3.7 kg/shp (8.2 lb/shp)
Range 0 passenger: 4,149 km (2,593 mi) (2,239 nm)
Range 9 passenger: 2,804 km (1,753 mi) (1,513 nm)
Takeoff distance over 15 m (50 ft) obstacle: 701 m (2,300 ft)
Takeoff distance ground roll: 450 m (1,475 ft)
Landing distance over 15 m (50 ft) obstacle: 558 m (1,830 ft)
Landing distance ground roll: 228 m (945 ft)

Wikipedia: Offers detailed aircraft specifications for the PC-12

Beechcraft KingAir 200

Description: The Beechcraft Super King Air family is part of a line of twin-turboprop aircraft produced by the Beech Aircraft Corporation (now the Beechcraft Division of Hawker Beechcraft). The King Air line comprises a number of model series that fall into two families: the Model 90 series, Model 100 series (these models comprising the King Air family), Model 200 series and Model 300 series. The latter two models were originally marketed as the "Super King Air" family, but the "Super" was dropped in 1996.

Beechcraft KingAir 200 Specifications

General characteristics

Crew: 1-2
Capacity: 13 passengers
Length: 43 ft 9 in (13.34 m)
Wingspan: 54 ft 6 in (16.61 m)
Height: 15 ft 0 in (4.57 m)
Wing area: 303 ft² (28.2 m²)
Empty weight: 7,755 lb (3,520 kg)
Max takeoff weight: 12,500 lb (5,670 kg)
Powerplant: 2× Pratt & Whitney Canada PT6A-42 turboprops, 850 shp (635 kW) each

Performance

Maximum speed: 339 mph (294 knots, 545 km/h) at 25,000 ft (7,600m)
Cruise speed: 333 mph (289 knots ,536 km/h) at 25,000 ft (max cruise)
Stall speed: 86 mph (75 knots, 139 km/h) IAS (flaps down)
Range: 2,075 mi (1,800 nm, 3,338 km) with maximum fuel and 45 minute reserve
Service ceiling 32,800 ft (10,700 m)
Rate of climb: 2,450 ft/min (12.5 m/s)
Wing loading: 41.3 lb/ft² (201.6 kg/m²)
Power/mass: 0.14 hp/lb (220 W/kg)

Wikipedia: Offers detailed aircraft specifications for the Beechcraft KingAir 200.

Cessna CitationJet

Description: The Cessna CitationJet/CJ series (Model 525) are American turbofan-powered light corporate jets built by the Cessna Aircraft Company in Wichita, Kansas. The Citation brand of business jets encompasses six distinct "families" of aircraft. The Model 525 CitationJet was the basis for one of these families, which encompasses the CJ1, CJ1+, CJ2, CJ2+, CJ3, and CJ4 models.

General characteristics

Crew: 1
Capacity: 5 passengers
Payload: 615 lb (279 kg)
Length: 42 ft 7 in (12.98 m)
Wingspan: 46 ft 11 in (14.30 m)
Height: (4.19 m)
Empty weight: 6,765 lb (3,069 kg)
Useful load: 3,835 lb (1,740 kg)
Max takeoff weight: 10,700 lb (4,853 kg)
Powerplant: 2× Williams FJ44-1AP turbofan, 1,965 lb (8.74 kN) each

Performance

Cruise speed: 389 ktas (720 km/h)
Stall speed: 83 kcas (153 km/h)
Range: 1,300 nm (2,408 km)
Service ceiling 41,000 ft (12,497 m)
Rate of climb: 3,290 fpm (1,003 m/min)

Source: http://cj1plus.cessna.com/specifications.chtml