PZL
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| Condition: | Used | Model Year: | 1994 |
| Country/Region of Manufacture: | Poland | Make: | PZL |
Raleigh, North Carolina, United States
Vehicle description
Follow this link to watch a video of this plane: COPY & PASTE > > > https:/ youtu.be/woPPaEqGdYY
Dial: for more information (USA Number)Aircraft information:Registration: N21525Year of construction: 1994Total time (TTAF): 1401 TTCountry: North Carolina (United States)City/Aerodrome: Kinston1401.3 hrs Airframe, 231.8 hrs Engine;Speed Ring Cowl, Vortex Generators; DC3 prop conversion; hidraulic fire gate; HS 23E50-505 propeller; AD 81-13-06R2 in Aug 2015, next due Aug 2020, Bendix King KX155.
General characteristics Crew: 1 / 2 (M18BS) Capacity: 2,500 l (660 US gal; 550 imp gal) liquid or 2,200 kg (4,900 lb) dry chemical in fibreglass hopper forward of the cockpit (smaller hopper in M18BS) Length: 9.47 m (31 ft 1 in) Wingspan: 17.7 m (58 ft 1 in) Height: 3.7 m (12 ft 2 in) to tailfin on ground Wing area: 40 m 2 (430 sq ft) Aspect ratio: 7.8 Airfoil : root: NACA 4416 ; tip: NACA 4412 outer wing panels Empty weight: 2,710 kg (5,975 lb) Max takeoff weight: 4,200 kg (9,259 lb) Fuel capacity: 510 kg (1,120 lb) max fuel weight Powerplant: 1 × PZL Kalisz ASz-621R 9-cylinder air-cooled radial piston engine, 731 kW (980 hp) Propellers: 4-bladed PZL Warszawa AW-2-30, 3.3 m (10 ft 10 in) diameter constant speed aluminium alloy propeller Performance Maximum speed: 200 km/h (124 mph; 108 kn) with agricultural equipment Stall speed: 108 km/h (67 mph; 58 kn) flaps down Never exceed speed : 280 km/h (174 mph; 151 kn) Range: 970 km (603 mi; 524 nmi) Ferry range: 2,000 km (1,243 mi; 1,080 nmi) with hopper fuel tank Service ceiling: 6,500 m (21,300 ft) g limits: +3.4 / -1.4 Rate of climb: 6.5 m/s (1,280 ft/min) Wing loading: 105 kg/m 2 (22 lb/sq ft) Power/mass : 5.75 kg/kW (11.92 lb/hp)
Dial: for more information (USA Number)Aircraft information:Registration: N21525Year of construction: 1994Total time (TTAF): 1401 TTCountry: North Carolina (United States)City/Aerodrome: Kinston1401.3 hrs Airframe, 231.8 hrs Engine;Speed Ring Cowl, Vortex Generators; DC3 prop conversion; hidraulic fire gate; HS 23E50-505 propeller; AD 81-13-06R2 in Aug 2015, next due Aug 2020, Bendix King KX155.
General characteristics Crew: 1 / 2 (M18BS) Capacity: 2,500 l (660 US gal; 550 imp gal) liquid or 2,200 kg (4,900 lb) dry chemical in fibreglass hopper forward of the cockpit (smaller hopper in M18BS) Length: 9.47 m (31 ft 1 in) Wingspan: 17.7 m (58 ft 1 in) Height: 3.7 m (12 ft 2 in) to tailfin on ground Wing area: 40 m 2 (430 sq ft) Aspect ratio: 7.8 Airfoil : root: NACA 4416 ; tip: NACA 4412 outer wing panels Empty weight: 2,710 kg (5,975 lb) Max takeoff weight: 4,200 kg (9,259 lb) Fuel capacity: 510 kg (1,120 lb) max fuel weight Powerplant: 1 × PZL Kalisz ASz-621R 9-cylinder air-cooled radial piston engine, 731 kW (980 hp) Propellers: 4-bladed PZL Warszawa AW-2-30, 3.3 m (10 ft 10 in) diameter constant speed aluminium alloy propeller Performance Maximum speed: 200 km/h (124 mph; 108 kn) with agricultural equipment Stall speed: 108 km/h (67 mph; 58 kn) flaps down Never exceed speed : 280 km/h (174 mph; 151 kn) Range: 970 km (603 mi; 524 nmi) Ferry range: 2,000 km (1,243 mi; 1,080 nmi) with hopper fuel tank Service ceiling: 6,500 m (21,300 ft) g limits: +3.4 / -1.4 Rate of climb: 6.5 m/s (1,280 ft/min) Wing loading: 105 kg/m 2 (22 lb/sq ft) Power/mass : 5.75 kg/kW (11.92 lb/hp)