Specifications .28PC-21.29 Pilatus PC-21



the pilatus pc-21; note stepped tandem cockpit



data pilatus aircraft


general characteristics



crew: 2 (student & instructor)
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 , flaps (20 km/h less flaps , 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)
wing loading: 208 kg/m² (42.7 lb/ft²)
power/mass: 0.39 kw/kg (0.23 hp/lb)
g limits: + 8.0 g – 4.0 (aerobatic) / + 5.0 g – 2.5 g (utility)

armament



hardpoints: provisions provided 4× under-wing , 1× centerline external store stations, capable of mounting 1,150 kg (2,540 lb) of payload of air-to-ground weapons operate in counter-insurgency role.




^ pilatus: pc-21 fact sheet (pdf). pilatus aircraft ltd. retrieved 29 april 2010. 
^ cite error: named reference pil brouch invoked never defined (see page).






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