Specifications for the Robinson R66 Turbine
Robinson R66 Turbine · Specifications
Overview
This document provides detailed specifications for the Robinson R66 Turbine helicopter, highlighting its design features, performance capabilities, and standard equipment. It is intended for pilots, aviation enthusiasts, and potential buyers interested in understanding the operational characteristics and maintenance requirements of the R66. Key aspects include engine specifications, weight limits, performance metrics, and safety features, ensuring users have a comprehensive understanding of the helicopter's capabilities and requirements.
- Engine: Rolls Royce RR300, 300 shp (derated to 270 shp for takeoff)
- Maximum Gross Weight: 2700 lb (1225 kg)
- Cruise Speed: Up to 125 knots (144 mph)
- Maximum Range: Approximately 350 nautical miles (400 statute miles)
- Time Between Overhaul (TBO): 2000 hours or 12 years for airframe.
Document
Source
Originally published by www.rectimo.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Pages
- 6
- File size
- 493 KB
- Publisher
- www.rectimo.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 350
- Engine (hp)
- 270
- 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)
- 927
- Baggage allowance (lb)
- 300
- Basic empty weight (lb)
- 1,280
- 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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- Emergency Checklist R66 – Heli Academy V1.0 2025-09Pilot's Operating Handbook
- Amping Airpower — Electric Vertical Takeoff and Landing for the U.S. Air ForceOther Documents
- 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 turboshaft engine, which delivers 300 shp derated to 270 shp for takeoff and 224 shp continuous. This engine operates on Jet A fuel, providing excellent power and responsiveness.
Weight and Capacity
The maximum gross weight of the R66 is 2700 lb (1225 kg), with an approximate empty weight of 1280 lb (581 kg). The fuel capacity is 73.6 gallons, weighing 493 lb (224 kg). With maximum fuel, the helicopter can carry 927 lb (420 kg) of passengers and baggage.
Performance Metrics
The R66 has a cruise speed of up to 125 knots (144 mph) and a maximum range of approximately 350 nautical miles (400 statute miles). It can achieve a rate of climb of over 1000 feet per minute and has a maximum operating altitude of 14,000 feet.
Safety Features
The R66 meets the latest FAA crashworthiness regulations and includes energy-absorbing seats and a bladder fuel system. The helicopter also features a rotor brake for quick stopping of rotor blades, enhancing safety during shutdown.
Maintenance and Warranty
The R66 requires no scheduled maintenance between 100-hour inspections. The time between overhaul (TBO) is 2000 hours or 12 years for the airframe and 2000 hours or 3000 start cycles for the engine. The helicopter comes with a two-year or 1,000-hour limited warranty.
Safety notes
- Meets latest FAA crashworthiness regulations.
- Energy-absorbing seats and bladder fuel system enhance safety.
- Rotor brake reduces shutdown time and risk of injury.
Full document text
ROBINSON HELICOPTER COMPANY The R66 TURBINE incorporates many of the design features of the R44 including a two-bladed rotor system, T-bar cyclic and an open cabin configuration. Notable differences are the R66’s increased reserve power, improved altitude performance, fifth seat and dedicated baggage compartment. With continued focus on safety, the R66 meets the latest FAA crashworthiness regulations. After five years of research and development, the R66’s design includes a well constructed cabin, energy absorbing seats and a new bladder fuel system. Its open cabin configuration comfortably seats five adults with passenger views that are not obstructed. Increased capacity, lower acquisition and operating costs, make the R66 the ideal turbine helicopter for private, business and utility applications. R66 TURBINE ROLLS ROYCE RR300 TURBOSHAFT ENGINE is a derivative of the RR250 series spe- cifically designed for the R66. The RR300 turbine engine operates on readily avail- able jet A fuel delivering excellent pow- er and responsiveness in a light-weight, compact installation. SIMPLIFIED STARTING PROCEDURE A latching starter and a fuel cutoff con- trol which is separate from the collective twistgrip reduces the chance of over- temping during start-up. ENGINE MONITORING UNIT (EMU) continuously records gas generator/ compressor rpm, turbine rpm, engine torque, and measured gas temperature (MGT). An engine anti-ice system is also standard. OPTIONAL UPGRADES AIR CONDITIONING The air conditioning system features front and rear vents which circulate cool air throughout the cabin. The air conditioning system weighs 42 pounds and has a 17,000 Btu/hr cool- ing capacity. PILOT’S AVIONICS CONSOLE places a GPS unit in an easy-to-see and reach posi- tion, minimizing time spent looking down. The console can accommodate a GPS, GPS/COM, or GPS/NAV/COM. BOSE A20 AVIATION HEADSETS with active noise reduction and Bluetooth communications interface. AVIONICS COM radio and transponder are stan- dard. A variety of Bendix/King and Gar- min avionics upgrades are available. Shaded area indicates silhouette of optional 9-hole instrument panel R66 COCKPIT Shown with 7-hole instrument panel and optional Pilot’s Avionics Console Open cabin design comfortably seats five adults. HYDRAULIC POWER CONTROLS eliminate stick shake and control forces enabling precise hovering and a smoother ride. ROTOR BRAKE enables the pilot to stop the rotor blades more quickly reducing shutdown time and risk of injury to by- standers. CENTER-POSITIONED CYCLIC Robinson’s center-positioned teetering T-Bar cyclic makes it easy to enter and exit the cockpit. Left-seat flight controls are removable. PISTOL-GRIP CYCLIC incorporates two- position trigger switches for intercom and transmit. Pilot-side grip has but- tons for convenient switching of COM frequencies. R66 TURBINE ROBINSON HELICOPTER COMPANY TRI-HINGE ROTOR DESIGN eliminates lag hinges, dampers, and hydraulic struts. Blades resist corrosion and have thick leading edges to minimize erosion. AIR VENTS in each door and in the nose provide fresh air for pilot and passengers. GROUND HANDLING is made easy with ground handling wheels. A tow cart adaptor is included for use with Robin- son’s optional electric tow cart. FEATURES BAGGAGE COMPARTMENT The spacious 18 cubic-foot, 300 lb capacity compart- ment can accommodate three or four full-size suitcases. Additional storage space is provided under each seat for personal belongings. SERVICE No scheduled maintenance is required between 100 hour inspections. Main and tail rotor drive systems use mainte- nance-free flexible couplings in place of universal joints or gear couplings. Pri- mary controls actuate by bell cranks and push-pull tubes eliminating cables and pulleys. Teflon lined bearings reduce periodic lubrication requirements. TIME-BETWEEN-OVERHAUL (TBO) is 2000 hours or 12 years for the airframe and 2000 hours or 3000 start cycles for the engine, whichever occurs first. All life limited components have approved service lives of at least 2000 hours. WORLDWIDE SERVICE is readily available with factory trained technicians at Rob- inson approved service centers through- out the world. WARRANTY The R66 comes with a two year or 1,000 hour limited aircraft warranty. ROBINSON HELICOPTER COMPANY Engine Type 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) 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 7-Hole Instrument Panel standard Electrical System 28 volt SPECIFICATIONS STANDARD INSTRUMENTS • Airspeed indicator • Altimeter • Digital outside air temperature gage • Hour meter • Magnetic compass • Oil temperature & pressure gages • Quartz clock • Rotor/engine dual tachometer • Vertical speed indicator • N1 Tachometer • Torque Meter • Turbine Gas Temperature Indicator ANNUNCIATOR LIGHT PANEL • Engine fire • Low fuel • Low oil pressure • Low rotor RPM • Main gearbox temperature • Main gearbox chip • Tail rotor gearbox chip • Engine chip • Anti ice • Gen • Fuel filter • Cowl Door • Air filter • EMU STANDARD EQUIPMENT • Leather seats • HID landing lights • Anti-collision light • Belly hard point • Cabin heater and defogger • Door locks • Floor and hand intercom switches • Navigation, panel and map lights • Integrated oil filter w/bypass indicator • Engine air filter w/bypass indicator • 160 Amp starter generator • Engine compressor rinse nozzle • Pilot-side adjustable pedals • Rotor blade tie downs • Tinted windscreen and windows • Tow cart adapter • Windshield cover
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• Robinson travel bag DIMENSIONS © Robinson Helicopter Company. Robinson and R66 are registered trademarks of Robinson Helicopter Company. All other trademarks or registered trademarks are copyright of their respective companies. (rev. A) QUALITY MANUFACTURING 2901 Airport Drive • Torrance, CA • 90505 • USA Phone: 310-539-0508 • Fax: 310-539-5198 www.robinsonheli.com ROBINSON HELICOPTER COMPANY To ensure the highest quality, Robinson manufactures, assembles, inspects and flight tests all of its helicopters at its Tor- rance, California factory. The facility fea- tures state of the art equipment includ- ing computer numerically controlled (CNC) machining centers, electrical dis- charge machines (EDM), and water jet and laser cutting machines. Coordinate measuring machines (CMM) capable of checking dimensional tolerances within 3 microns or 120 millionths of an inch are used to inspect precision machined parts. This level of accuracy is essential to the design and fabrication of inter- changeable parts. To maximize efficiency and productivity, a large percentage of parts are manufac- tured in-house allowing the company to better control costs, eliminate delays and ensure the best possible quality. Flight test CNC machining centers Robinson’s 617,000 square foot facility.