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Filling a void of training needed for the professionally minded pilot. This program is a basic knowledge academics. Curriculum can be tailored from a basic academic to be specific make and model turbine transition, Single or Multiengine as listed under Aircraft Specific.
The Robinson R66 Turbine retains many of the design features of the R44, including a two-bladed rotor system, T-bar cyclic, and an open interior cabin configuration. Notable differences are the R66's increased reserve power, improved altitude performance, fifth seat, and large baggage compartment. Popular upgrades including HID landing lights, leather seats, and a stereo audio control panel are standard in the R66.
R66 TURBINE HELICOPTER
R66 TURBINE TRANSITION COURSE
AIRCRAFT SPECIFIC TRAINING PROGRAMS
AS/SA365N Series and A109 Series; 3 day academics and 5 hours flight training EC120, EC130; 2 day academics and 5 hours flight training.
Bell206, AS350, MD500, Robinson R22, R44 (with SFAR), Enstrom, Hu269/300. Other types available for flight training needs per customer request.
The Turbine Transition Course is taught in the Robinson R66 five seat turbine-powered helicopter. The objective is to gain familiarization in the R66 helicopter for pilots that either have no experience in turbine helicopters or no experience in the Robinson R66.
Hold at least a Private Pilot Rotorcraft-Helicopter certificate
Note: The Trainee is not required to have a current flight review or current SFAR 73 sign-offs.
Hold at least a current third class medical certificate.
GROUND LESSON ELEMENTS:
The subject areas below form the foundation of the ground training program, but the Trainee will also review knowledge areas required to give the Trainee a flight review, pursuant to 14 CFR 61.56.
FLIGHT LESSON ELEMENTS:
Enroute and off-airport operations
The student should display proficiency in the listed maneuvers above and familiarization with the R66 Turbine helicopter during oral and practical examination.
Engine Rolls-Royce RR300 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous
Maximum Gross Weight 2700 lb (1225 kg)
Approximate Empty Weight
(including oil & std avionics) 1280 lb (581 kg)
Fuel Capacity (73.6 gal) 493 lb (224 kg)
Pilot, Passengers and Baggage with Maximum Fuel 927 lb (420 kg)
Cruise Speed up to 125 kts (144 mph)
Maximum Range (no reserve) approx 350 nm (400 sm)
Hover Ceiling IGE at Maximum Gross Weight over 10,000 ft
Hover Ceiling OGE at Maximum Gross Weight over 10,000 ft
Rate of Climb over 1000 fpm
Maximum Operating Altitude 14,000 ft
Electrical System 28 volt
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