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R44 Raven I Brochure

R44 Raven I Brochure

R44 Raven I Brochure

Product catalog summary
Overview: The document provides detailed information about the R44 Raven I and Clipper I helicopters, highlighting their high performance, reliability, and ease of maintenance. These helicopters feature a two-bladed rotor system, T-bar cyclic, and advanced Robinson technology, including streamlined instrument panels and crashworthy bladder fuel tanks.
Design and Performance: The R44's aerodynamic fuselage enhances airspeed and fuel economy. Hydraulic controls offer responsive handling by eliminating feedback forces. Noise reduction is achieved through a low tail-rotor tip speed, a newly designed muffler, and a large cambered tail.
Engine and Safety: Both helicopter models are powered by Lycoming's O-540 carbureted engine, which includes a carburetor heat assist system to automatically adjust carburetor heat, enhancing safety and reducing pilot workload.
Options: Available options include leather seats in various colors, Aspen Primary and Multifunction Flight Displays, Garmin GTN 600/700 Series Touchscreen Navigators, Genesys HeliSAS Autopilot, Garmin ADS-B Compliant Transponders, Garmin GMA 350Hc Audio Panel, and Bose A20 Headsets with Bluetooth.
Specifications:
  • Dimensions: Not specified in the document.
  • Engine: Lycoming O-540, six-cylinder, carbureted.
  • Horsepower: Derated to 225 for takeoff and 205 continuous.
  • Maximum Gross Weight: 2400 lb (1089 kg).
  • Empty Weight: Raven I: 1450 lb (658 kg), Clipper I: 1500 lb (680 kg).
  • Fuel Capacity: Standard Fuel: 29.5 gal (177 lb/80 kg), Auxiliary Fuel: 17.0 gal (102 lb/46 kg).
  • Cruise Speed: Raven I: up to 108 kts (200 km/h), Clipper I: up to 101 kts (187 km/h).
  • Maximum Range: Approximately 300 nm (550 km) without reserve.
  • Hover Ceiling IGE: 6400 ft @ 2400 lb.
  • Hover Ceiling OGE: 4000 ft @ 2300 lb.
  • Rate of Climb: Over 1000 fpm.
  • Maximum Operating Altitude: 14,000 ft.
  • Electrical System: 28 volt.
Standard Avionics and Instruments: The helicopters come with a six-hole instrument panel, GTR 225B COM radio, GTX 327 Mode C transponder, and a comprehensive set of standard instruments including airspeed indicator, altimeter, dual tachometer, manifold pressure gauge, and more.
Standard Equipment: Features include hydraulic power controls, RPM throttle governor, throttle correlator, carburetor heat assist, crashworthy fuel bladder tanks, engine oil filter, cabin heater, carbon monoxide detector, rotor brake, intercom switches, and various lighting and safety equipment.
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Catalog excerpts

R44 Raven I Brochure-1

Four-seat R44 Raven I and Clipper I helicopters are high performing, reliable and easy to maintain. R44s have a two-bladed rotor system, T-bar cyclic and the latest in Robinson technology including streamlined instrument panels and crashworthy bladder fuel tanks. The R44’s aerodynamic fuselage optimizes airspeed and fuel economy. Hydraulic controls eliminate feedback forces and provide responsive handling. A low tail-rotor tip speed, newly designed muffler and large cambered tail reduce flyover noise. Raven I and Clipper I helicopters are powered by Lycoming’s O-540 carbureted engine with carburetor heat assist that automatically adjusts carburetor heat enhancing safety and reducing pilot workload. OPTIONS • Leather Seats in Tan, Charcoal or Gray • Aspen Primary and Multifunction Flight Displays • Garmin GTN 600/700 Series Touchscreen Navigators • Genesys HeliSAS Autopilot • Garmin ADS-B Compliant Transponders • Garmin GMA 350Hc Audio Panel • Bose A20 Headsets with Bluetooth Optional Panel shown with optional Aspen EFD 1000H PFD, turn coordinator, digital clock, GMA 350Hc audio controller, GTX 345 transponder, Garmin GTN 750 in pilot-side-console, left accessory bar Standard Panel shown with optiona

 Open the catalog to page 1
R44 Raven I Brochure-2

STANDARD AVIONICS • Six-hole instrument panel • GTR 225B COM radio • GTX 327 Mode C transponder SPECIFICATIONS Helicopter STANDARD INSTRUMENTS Raven I Clipper I with fixed floats Lycoming O-540, six cylinder, Lycoming O-540, six cylinder, carbureted carbureted Derated to 225 for takeoff and Derated to 225 for takeoff and 205 continuous 205 continuous Maximum Gross Weight Approximate Empty Weight (incl. oil & standard avionics) Pilot, Passengers, and Baggage (with standard fuel) Cruise Speed at Maximum Gross Weight Maximum Range (no reserve) Rate of Climb Maximum Operating Altitude Electrical...

 Open the catalog to page 2

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