PC-9 Length: 10.14 m (33 ft 3 in) Wingspan: 10.125 m (33 ft 3 in) Height: 3.26 m (10 ft 8 in) Wing area: 16.29 m2 (175.3 sq ft) Empty weight: 1,725 kg (3,803 lb) Max takeoff weight: 3,200 kg (7,055 lb) Powerplant: 1 × Pratt & Whitney Canada PT6A-62 turboprop, 857 kW (1,149 hp) flat-rated at 708 kW (950 shp)
Performance:
Maximum speed: 593 km/h (368 mph; 320 kn) Stall speed: 143 km/h (89 mph; 77 kn) EAS flaps and gear up, 128 km/h (80 mph; 69 kn) flaps and gear down Range: 1,537 km (955 mi; 830 nmi) Service ceiling: 11,580 m (37,992 ft) Rate of climb: 20.8 m/s (4,090 ft/min) g limits: + 7.0 g to −3.5 g | PC-21 Length: 11.233 m (36 ft 11 in) Wingspan: 9.108 m (29 ft 11 in) Height: 3.749 m (12 ft 4 in) Wing area: 15.221 m² (163.848 ft²) Empty weight: 2,270 kg (5,005 lb) Max. takeoff weight: 3,100 kg (aerobatic) / 4,250 kg (utility) (6,834 lb (aerobatic) / 9,370 lb (utility)) Powerplant: 1 × Pratt & Whitney Canada PT6A-68B Turboprop engine, 1,200 kW (1,600 shp)
Performance:
Maximum speed: 685 km/h (370 knots, 428 mph) Stall speed: 170 km/h (92 knots, 106.25 mph) gear and flaps up (20 km/h less with flaps and gear down) Range: 1,333 km (720 nm, 828 miles) Service ceiling: 11,580 m (38,000 ft) Rate of climb: 1,219 m/min (4,000 ft/min) g limits: + 8.0 g to – 4.0 (aerobatic) / + 5.0 g to – 2.5 g (utility) |