The Robinson R44 is a four-place light helicopter produced by the Robinson Helicopter Company since 1992. Based on the company’s two-place Robinson R22, the R44 features hydraulically-assisted flight controls. The R44 was first flown on March 31, 1990, and received FAA certification in December 1992, with the first delivery in February 1993.
The R44 is a single-engined helicopter with a semi-rigid two-bladed main rotor and a two-bladed tail rotor and a skid landing gear. It has an enclosed cabin with two rows of side-by-side seating for a pilot and three passengers. Tail rotor direction of rotation on the R44 is reversed compared to the R22 for improved yaw control authority. On the R44 the advancing blade is on the bottom.
Designed during the 1980s by Frank Robinson and his staff of engineers, the R44 first flew on March 31, 1990. The R44 Astro was awarded an FAA Type Certificate in December 1992, with the first deliveries taking place in January 1993. In January 2000, Robinson introduced the Raven with hydraulically-assisted controls and adjustable pedals. In July 2002, Robinson introduced the Raven II featuring a more powerful, fuel-injected engine and wider blades, allowing a higher gross weight and improved altitude performance.
|Capacity||Four incl. pilot|
|Height||10 ft, 9 in|
|Length||21 ft, 5 in|
|Displacement||360 cu. in|
|Carbureted Or Fuel Injected||Fuel-injected|
|Rotor Diameter||33 ft|
|Tail Rotor Diameter||4 ft, 10 in.|
|Fuel Capacity (Main)||31.6 gallons|
|Fuel Capacity (Aux)||18.5 gallons|
|Min. Octane Fuel||100|
|Weights and Capacities:|
|Takeoff/Landing Weight||2,500 lbs.|
|Standard Empty Weight||1,450 lbs|
|Standard Payload||900 lbs|
|Max. Speed||130 KCAS|
|Cruise Speed||110 KCAS|
|Alt Restictions||14,000 ft or 9,000 ft AGL.|