SPECIFICATIONS
Robinson R66 Turbine · Specifications
Overview
This document provides detailed specifications for the Robinson R66 Turbine and its variant, the R66 Turbine Marine. It is intended for pilots, aviation enthusiasts, and maintenance personnel who require comprehensive information about the helicopter's performance, dimensions, and operational capabilities. The R66 Turbine is noted for its reliability, spacious design, and advanced features, including a Rolls-Royce RR300 engine and a two-bladed rotor system. The document outlines critical specifications such as weight limits, fuel capacity, and performance metrics, ensuring users have the necessary data for safe operation and maintenance.
- Engine: Rolls-Royce RR300, 300 shp (derated to 270 shp for takeoff, 224 shp continuous)
- Maximum Gross Weight: 2700 lb (1225 kg)
- Cruise Speed: Up to 125 knots (144 mph)
- Maximum Range: Approximately 350 nm (400 sm)
- Rate of Climb: Over 1000 fpm
- Maximum Operating Altitude: 14,000 ft
- Empty Weight: 1280 lb (581 kg) for R66 Turbine, 1345 lb (610 kg) for Marine variant
Document
Source
Originally published by www.orlandohelitours.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Pages
- 12
- File size
- 985 KB
- Publisher
- www.orlandohelitours.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 350
- Engine (hp)
- 300
- Engine model
- Rolls Royce RR300
- Max speed (kt)
- 125
- Cruise speed (kt)
- 125
- Empty weight (lb)
- 1,280
- Fuel capacity (gal)
- 73.6
- Rate of climb (fpm)
- 1,000
- Service ceiling (ft)
- 14,000
- Max takeoff weight (lb)
- 2,700
Weight & balance
- Useful load (lb)
- 1,420
- Baggage allowance (lb)
- 300
- Basic empty weight (lb)
- 1,280
- Max landing weight (lb)
- 2,700
- Max takeoff weight (lb)
- 2,700
Common. Rarer than 5% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Robinson R66 Turbine.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the ROBINSON R66 Turbine to your watchlist and track it in one place.
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- Airworthiness Bulletin AWB 53-012 Issue 1 - 14 October 2024Other Documents
- Federal Register Index January–September 2024Supplemental Type Certificate
- ROBINSON MAINTENANCE MANUAL MODEL R66Service Bulletins
- Pilot's Operating HandbookWeight And Balance
- R66 PILOT'S OPERATING HANDBOOK AND FAA APPROVED ROTORCRAFT FLIGHT MANUALPilot's Operating Handbook
- R22, R44 & R66 MAINTENANCE & INSPECTION KITS – 20 OCTOBER 2022Parts Catalog
- ROBINSON MODEL R66 SECTION 4 NORMAL PROCEDURESChecklist
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In this document
Engine Specifications
The R66 Turbine is powered by a Rolls-Royce RR300 turbine engine, delivering 300 shaft horsepower (shp), which is derated to 270 shp for takeoff and 224 shp for continuous operation. This engine is designed for reliability and efficiency, operating on Jet A fuel.
Weight and Capacity
The maximum gross weight for both the R66 Turbine and R66 Turbine Marine is 2700 lb (1225 kg). The approximate empty weight for the R66 Turbine is 1280 lb (581 kg), while the Marine variant is slightly heavier at 1345 lb (610 kg). The fuel capacity is 73.6 gallons, equating to 493 lb (224 kg). The combined weight of the pilot, passengers, and baggage with maximum fuel is 927 lb (420 kg) for the R66 Turbine and 862 lb (391 kg) for the Marine version.
Performance Metrics
The R66 Turbine can achieve a cruise speed of up to 125 knots (144 mph) and has a maximum range of approximately 350 nautical miles (400 statute miles). It has a rate of climb exceeding 1000 feet per minute and can operate at a maximum altitude of 14,000 feet.
Dimensions
The R66 Turbine features a rotor radius of 198 inches and overall dimensions that accommodate its spacious design. The helicopter is designed for ease of entry and exit, with a cabin that can comfortably seat five individuals.
Safety Features
The R66 Turbine is equipped with energy-absorbing seats and a bladder fuel tank, meeting the latest FAA crashworthiness regulations. The helicopter also includes a rotor brake for quick rotor stoppage, enhancing safety during shutdown.
Full document text
The 5-place R66 Turbine is Robinson’s largest and most pow- erful helicopter. Like the R22 and R44, the R66 is built to be excep- tionally reliable, economical and easy to maintain while performing as well or better than its more expensive competitors. The R66 includes many of Robin- son’s signature design features including a two-bladed rotor system, T-bar cyclic and open cabin configuration. What distin- guishes the R66 are its fifth seat, spacious baggage compartment and the Rolls-Royce RR300 turboshaft engine. Designed specifically for the R66, the RR300 is powerful, lightweight, and highly reliable. An Engine Mon- itoring Unit (EMU) continuously records gas generator/compressor RPM, power turbine RPM, engine torque and measured gas tem- perature (MGT). The RR300 oper- ates on readily available Jet A fuel and provides increased reserve power, additional payload, and improved altitude performance. With continued focus on safety, the R66 meets the latest FAA crash- worthiness regulations including energy absorbing seats and a bladder fuel tank. R66 TURBINE w Two-bladed rotor system elimi- nates the need for lag hinges, dampers, and hydraulic struts. w Proven aluminum and stainless steel construction of main rotor blades minimizes environmen- tal wear and tear. w Hydraulic power controls eliminate stick shake and feedback forces. w Center positioned T-bar cyclic enables a comfortable grip position and allows trouble-free entry and exit of the cabin. w Left side flight controls are removable. w Transmit, intercom, and memory channel radio controls are inte- grated into cyclic grip. w Voice-activated intercom elimi- nates the need to use intercom switches during doors-on flights. Intercom switches are included for doors-off flights. w Leather seats w Rotor brake allows the pilot to stop the rotors quickly, reduc- ing shutdown time and risk of injury to passengers and ground personnel. w 18 cu ft, 300 lb capacity baggage compartment w LED anti-collision and navigation lights w Dual HID landing lights w External power receptacle FEATURES w 8-hole instrument panel w Garmin GMA 350H audio panel w Garmin GTR 225B COM radio with 8.33 kHz channel spacing w Garmin GTX 327 Mode C transponder STANDARD AVIONICS Shown with optional artificial horizon, directional gyro, turn coordinator, and fire extinguisher w A variety of Garmin avionics including easy to reach and see touchscreen navigators w Garmin and Aspen Primary Flight and Multifunction Display systems provide instrumentation, moving map navigation, and additional situational awareness including traffic, weather, and terrain. Genesys HeliSAS autopilot developed specifically for light helicopters OPTIONAL AVIONICS Shown with optional G500H PFD/MFD, GTN 750 GPS/COM/NAV, autopilot, radar altimeter, and fire extinguisher INTERIOR UPGRADES w Ceiling-mounted air conditioning features front and rear vents that circulate cool air throughout the cabin. The system weighs 43 pounds and has a 17,000 BTU/hr cooling capacity. w Bose A20 aviation headsets with active noise reduction and Bluetooth interface w Rear center console provides secure storage for travel essentials. The center seat can be re-installed when needed. Shown with optional air conditioning, Bose A20 aviation headset, and rear center console R66 TURBINE MARINE Outfitted with pop-out floats, the R66 Turbine Marine offers an additional level of safety for over-water travel. Designed for emergencies, the six-chamber floats inflate within 2-3 seconds of activation. A lever on the pilot’s collective releases pressurized helium from a tank located under the aircraft’s right rear seat. The activation lever uses a mechanical pull cable and does not rely on an electrically actuated system for inflation. Floats may be activated and flown at speeds up to 80 knots. The installation adds approximately 65 pounds to the helicopter’s empty weight. When not in use, floats roll-up and stow in protective covers along the aircraft’s landing skids. The streamlined, low profile design minimizes drag and allows for easy entry and exit of the cabin. MAINTENANCE Pop-out floats require preflight verification of the helium tank pressure, annual leak checks, and emergency deployment tests every three years. The R66 Turbine Marine with floats inflated is approved for periodic training and limited amphibious use at reduced gross weight. limited components have approved service lives of at least 2000 hours. SERVICE WARRANTY The R66 carries a two-year or 1000-hour limited aircraft warranty. Factory-trained technicians are available worldwide at R66 service centers. No scheduled maintenance required between 100-hour inspections. Main and tail rotor drive systems use maintenance- free flexible couplings. Primary controls actuate by push-pull tubes and bell-cranks elimi- nating cables and pulleys. Teflon-lined or sealed bear- ings eliminate grease fittings. The Time-Between-Overhaul (TBO) is 2000 hours or twelve years for the airframe and 2000 hours or 3000 start cycles for the engine. Life- STANDARD EQUIPMENT w Hydraulic power controls w Bladder fuel tank w Integrated oil filter with bypass indicator w Engine air filter with bypass indicator w Main gearbox oil filter w 160 amp starter generator w Engine compressor rinse nozzle w Electronic engine monitoring unit (EMU) w Engine anti-ice system w Cabin heater and defogger w Rotor brake w Floor and hand intercom switches w Avionics master switch w Tinted windows w Leather seats w 3-point shoulder harnesses w Pilot-side adjustable pedals w Door locks w Belly hard point w LED anti-collision and navigation lights w Dual HID landing lights w LED panel and map lights w Tow cart adapter w Ground handling wheels w Rotor blade tie-downs w Windshield cover w Travel bag STANDARD INSTRUMENTS w Airspeed indicator w Altimeter w Rotor/engine dual tachometer w Vertical speed indicator w Magnetic compass w Torque meter w N1 tachometer w MGT gage w Oil temp and pressure gages
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w Fuel gage w Ammeter w Digital OAT gage/voltmeter w Hourmeters w Quartz clock ANNUNCIATOR LIGHT PANEL w Engine fire w Low fuel w Low oil pressure w Low rotor RPM (light & horn) w MR gearbox temp/press w MR gearbox chip w TR gearbox chip w Engine chip w Anti-ice w Generator w Fuel filter w Cowl door w Air filter w EMU SPECIFICATIONS © Robinson Helicopter Company. Robinson and R66 are registered trademarks of Robinson Helicopter Company. All other trademarks are property of their respective companies. 310-539-0508 • WWW.ROBINSONHELI.COM ROBINSON HELICOPTER COMPANY SPECIFICATIONS DIMENSIONS R66 Turbine R66 Turbine Marine Engine Rolls Royce RR300 turbine Rolls Royce RR300 turbine Horsepower 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous Maximum Gross Weight 2700 lb (1225 kg) 2700 lb (1225 kg) Approximate Empty Weight (including oil & std avionics) 1280 lb (581 kg) 1345 lb (610 kg) Fuel Capacity (73.6 gal) 493 lb (224 kg) 493 lb (224 kg) Pilot, Passengers and Baggage (with maximum fuel) 927 lb (420 kg) 862 lb (391 kg) Cruise Speed up to 125 kts (144 mph) up to 120 kts (138 mph) floats stowed Maximum Range (no reserve) approx 350 nm (400 sm) approx 350 nm (400 sm) Hover Ceiling IGE at Maximum Gross Weight over 10,000 ft over 10,000 ft Hover Ceiling OGE at Maximum Gross Weight over 10,000 ft over 10,000 ft Rate of Climb over 1000 fpm over 1000 fpm Maximum Operating Altitude 14,000 ft 14,000 ft Electrical System 28 volt 28 volt 354 IN. 58 IN. ROTOR RADIUS 198 IN. 90 IN. 92 IN. 72 IN. 137 IN. 459 IN. 60 IN. 354 IN. 58 IN. ROTOR RADIUS 198 IN. 90 IN. 92 IN. 72 IN. 137 IN. 459 IN. 60 IN.