PC-21
生产厂家:皮拉图斯飞机有限公司
简介：市场参考价：1702万人民币
Utilising the 1600 shp PT6A-68B engine from Pratt & Whitney Canada , the PC-21 pushes the speed and climb rate of the turboprop into an area that, until now, was exclusively jet territory. The engine is coupled to a five-blade Scimitar graphite propeller made by Hartzell.
A digital power management system and automatic yaw compensation make the PC-21 easy to fly at low speed and in the circuit, while providing the performance required for advanced training.
The PC-21 is capable of sustained low-level speeds in excess of 323 knots (598 km/h); hydraulically-assisted ailerons and roll spoilers produce fighter-like rates of roll in excess of 200° per second.
Utilising the 1600 shp PT6A-68B engine from Pratt & Whitney Canada , the PC-21 pushes the speed and climb rate of the turboprop into an area that, until now, was exclusively jet territory. The engine is coupled to a five-blade Scimitar graphite propeller made by Hartzell.
A digital power management system and automatic yaw compensation make the PC-21 easy to fly at low speed and in the circuit, while providing the performance required for advanced training.
The PC-21 is capable of sustained low-level speeds in excess of 323 knots (598 km/h); hydraulically-assisted ailerons and roll spoilers produce fighter-like rates of roll in excess of 200° per second.
性能数据：座位8个
Performance
The PC-21 performs as follows under international standard atmospheric (ISA) conditions:
Take-off distance over 50 ft (15 m) obstacle at sea level 2,379 ft 725 m
Landing distance over 50 ft (15 m) obstacle at sea level 2,953 ft 900 m
Max. rate of climb, sea level 4,250 ft/min 21.59 m/sec
Max. operating speed (Vmo) 370 KEAS 685 km/h
Max. horizontal speed (Vh) at sea level 323 KTAS 598 km/h
Max. horizontal speed (Vh) at 10,000 ft 337 KTAS 624 km/h
Stall speed
- flaps and gear up (Vs) 92 KCAS 170 km/h
- flaps and gear down (VSO) 81 KCAS 150 km/h
G loads aerobatic category utility category
- Max. positive 8.0 g - 4.0 g
- Max. negative 5.0 g -2.5 g
Max. range 720 nm 1,333 km
Weights
Basic empty weight (typical, dep. on configuration) 5,026 lb 2,280 kg
Max. take-off weight, acrobatic category 6,834 lb 3,100 kg
Dimensions & Geometry
Fuselage length 36 ft 11 in 11.233 m
Wing span 29 ft 11 in 9.108 m
Performance
The PC-21 performs as follows under international standard atmospheric (ISA) conditions:
Take-off distance over 50 ft (15 m) obstacle at sea level 2,379 ft 725 m
Landing distance over 50 ft (15 m) obstacle at sea level 2,953 ft 900 m
Max. rate of climb, sea level 4,250 ft/min 21.59 m/sec
Max. operating speed (Vmo) 370 KEAS 685 km/h
Max. horizontal speed (Vh) at sea level 323 KTAS 598 km/h
Max. horizontal speed (Vh) at 10,000 ft 337 KTAS 624 km/h
Stall speed
- flaps and gear up (Vs) 92 KCAS 170 km/h
- flaps and gear down (VSO) 81 KCAS 150 km/h
G loads aerobatic category utility category
- Max. positive 8.0 g - 4.0 g
- Max. negative 5.0 g -2.5 g
Max. range 720 nm 1,333 km
Weights
Basic empty weight (typical, dep. on configuration) 5,026 lb 2,280 kg
Max. take-off weight, acrobatic category 6,834 lb 3,100 kg
Dimensions & Geometry
Fuselage length 36 ft 11 in 11.233 m
Wing span 29 ft 11 in 9.108 m
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