Specifications
Broker
PENINSULA HELICOPTERS
+61457625303
Aircraft Details
- Model: Robinson R44 Raven II
- Engine: Lycoming IO-540-U2A
- Maximum Takeoff Weight: 2,500 lbs
- Cruise Speed: 120 knots
- Range: 300 nautical miles
- Seating Capacity: 4 (including pilot)
- Rotor System: Two-blade main rotor, two-blade tail rotor
- Avionics: Equipped with advanced avionics package
- Fuel Capacity: 30 gallons
- Performance: Excellent maneuverability and stability
- Ideal for: Personal use, flight training, and aerial tours
The Robinson R44 Raven II is known for its reliability and efficiency, making it a popular choice among private owners and flight schools. Its spacious cabin and smooth flight characteristics enhance the flying experience.
The text implies co-ownership as it highlights the versatility and appeal of the aircraft for various users.
About this Model
Overview
The Robinson R44 Raven II is a single-engine, four-seat light helicopter commonly used for primary/advanced training, personal transport, utility support, and aerial observation. It emphasizes straightforward systems, a relatively low cockpit workload for its class, and broad parts/service availability in many regions. Typical missions center on short to moderate legs with payload managed around fuel, passengers, and environmental conditions (heat/high altitude).
Mission Fit
The R44 Raven II fits operations that prioritize flexible point-to-point access and time-on-task over long range or high payload. It is well suited to mixed use—training plus personal travel—where dispatch reliability depends on disciplined weight-and-balance planning and realistic hot-and-high performance margins.
Cabin
The cabin is compact but practical for four occupants, typically arranged as two front seats and a rear bench. Large windows support outward visibility for training and observation. Noise and vibration are typical of a piston helicopter, so passenger comfort improves with quality headsets and thoughtful loading. Baggage capability is modest and sensitive to fuel load and density altitude.