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CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
CURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for saleCURTI AEROSPACE DIVISION ZEFHIR New Piston Helicopters for sale
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CURTI AEROSPACE DIVISION ZEFHIR

Piston Helicopters
Call for price 

Seller Information

MD Helicopters Australia

Contact:Darren Fayle

Mitchell, Australia

General

Manufacturer
CURTI AEROSPACE DIVISION
Model
ZEFHIR
Condition
New
Description
Maximum takeoff weight: 600/650 kgControl system: FADECCapacity: 2 passengersSpeed: 102 knotsRange: 318 nautical milesEngine type: TurbinePerformanceMaximum takeoff weight: 600 kg (1,322 lbs)Cruise speed: 161 km/h (87 kts)Maximum level speed: 185 km/h (100 kts)Never exceed speed VNE (sea level): 189 km/h (102 kts)Hovering ceiling OGE (600 kg): 4,000 m (13,100 ft)Best Endurance: 2h 21min @78 km/h (42 kts) (+10 min reserve) Range 182 km (98nm) in 150 ltr tank configurationMaximum range: 318 km (172 nm) @185 km/h (+10 min reserve) (100 kts), Endurance 1h 43 min in 150 ltr tank configurationMaximum range: 638 km (344 nm) (+10 min reserve) @185 km/h (100 kts) in 287 ltr tank configurationTransmissionPrimary transmission: DirectMain gearbox: Bevel spiral gear with a reduction ratio of 12/49Tail gearbox: Bevel spiral gear with a multiplication ratio of 19/15Features:Seating: 2 crashworthy seats (according to CS-27)Cabin width: 1.34 m (4.4 ft)Maximum luggage capacity: 320 dm³ / (11.3 ft³)Standard fuel capacity: 150 ltr / (40 Usgal)Maximum auxiliary fuel capacity: 137 ltr / (36 Usgal)Approved fuel type: JET A, JET A-1, JET B, according to DERD 2494. TS-1, T2, RT according to GOST 10227Main RotorType: TeeteringNumber of blades: 2Diameter: 7.6 m (24.9 ft)Chord: 195 mm (7.7 in)Speed: 528 rpmTail RotorType: TeeteringNumber of blades: 2Diameter: 1.2 m (3.9 ft)Chord: 120 mm (4.7 in)Speed: 3,062 rpmEngineEngine type: PBS TS100 Turboshaft Engine (gas generator turbine & power turbine)Maximum continuous power: 105 kW (141 shp)Output speed: 2,158 rpmParachuteMinimum deployment altitude: 150 m (450 ft)
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