N211RB - WSK PZL MIELEC TS 11 ISKRA

WSK-PZL-MIELEC

TS-11 ISKRA

1H0211

N211RB

Used

Price Slashed! 444 Hours SMOH, FAA Approved Inspection Program General characteristics (courtesy of Wikipedia) Crew: Two - student and instructor Length: 11.15 m (36 ft 7 in) Wingspan: 10.06 m (33 ft 0 in) Height: 3.50 m (11 ft 5½ in) Wing area: 17.5 m² (188 ft²) Empty weight: 2,560 kg (5,644 lb) Loaded weight: 3,734 kg[5] (8,215 lb) Max. takeoff weight: 3,840 kg (8,470 lb) Powerplant: 1 × WSK SO-3 turbojet, 9.81 kN (2,205 lbf) Performance Never exceed speed: 750 km/h (Mach 0.8, 404 knots, 466 mph) Maximum speed: 720 km/h (388 knots, 447 mph) at 5,000 m (16,400 ft) Cruise speed: 600 km/h (324 knots, 373 mph) Stall speed: 140 km/h (92 knots, 106 mph) (power off, flaps down) Range: 1,250 km (673 nmi, 776 mi) Service ceiling: 11,000 m (36,000 ft) Rate of climb: 14.8 m/s (2,913 ft/min) Wing loading: 213 kg/m² (43.6 lb/ft²) Thrust/weight: 0.30

1,235 Hrs TTSNEW

WSK SO-3 turbojet 444 Hrs SMOH

Overall Gray Exterior with Polish Army Markings

Gray and Black Cockpits

Aircraft not flown since April 2007 FAA Approved Inspection Program