Robinson R44

Robinson R44

RiikUSA
RolliKerge abi- ja trenažöörkopter
Esimene lend31. märts 1990
Ehitatud6400+

2007 Robinson R44 on neljakohaline kerge helikopter, mida toodab Robinson Helicopter Company alates 1992. aastast. Ettevõtte kaheistmelisel Robinson R22-l põhineval R44-l on hüdrauliliselt abistatavad lennujuhtimisseadmed. See lendas esmakordselt 31. märtsil 1990 ja sai FAA sertifikaadi 1992. aasta detsembris, esimene tarne toimus 1993. aasta veebruaris.

Allikas: Robinson R44 Vikipeedias

Robinson R44 Raven II
FotograafidTeadmata
LokaliseerimineTeadmata
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General Characteristics (Raven II Variant)

The Robinson R44 is a popular four-seat, single-engine piston helicopter, widely recognized for its reliability, efficiency, and relatively low operating costs. It is derived from the smaller, two-seat R22 and is extensively used globally for flight training, corporate transport, tourism, and law enforcement.

Property Typical Value (R44 Raven II)
Rolli Light Utility / Trainer / Personal Transport
Tootja Robinson Helicopter Company
First Flight March 31, 1990
Meeskonna 1 pilot
Capacity (Passengers) 3 passengers
Main Rotor Diameter 10.1 m (33 ft 0 in)
Max Takeoff Weight 1,134 kg (2,500 lb)

Design and Powerplant

  • Engine: One Lycoming IO-540-AE1A5 six-cylinder, fuel-injected piston engine (Raven II). The Raven I uses a carbureted O-540.
  • Horsepower: Derated to 245 hp for takeoff and 205 hp continuous (Raven II).
  • Rotor System: Semi-rigid two-bladed main rotor and a two-bladed tail rotor.
  • Controls: Features hydraulically boosted controls to reduce pilot effort and enhance maneuverability.
  • Safety Feature: Equipped with a crashworthy fuel system that includes bladder fuel tanks to mitigate the risk of post-accident fire.
  • Variants: Includes the Raven I (carbureted engine), Raven II (fuel-injected engine), Clipper (with floats for water landings), and Cadet (two-seat trainer/utility).

Performance and Capabilities

  • Maximum Airspeed (Vne): Up to 241 km/h (130 knots, 150 mph).
  • Cruise Speed: Up to 202 km/h (109 knots, 126 mph).
  • Service Ceiling: 4,267 m (14,000 ft).
  • Maximum Range (No Reserve): Approximately 560 km (300 nautical miles).
  • Rate of Climb: Over 1,000 ft/min (5.1 m/s).
  • Useful Load: Approximately 451 kg (995 lb) (varies by variant and fuel load).
  • Fuel Type: Operates on Aviation Gasoline (AVGAS 100LL).

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