Specifications
AI Description
- Model: ROBINSON R44 RAVEN I
- Delivery positions available for 2026
- Engine: Lycoming O-540, six-cylinder
- Seats: 4
- Overall length: 11.7 m
- Overall height: 3.3 m
- Rotor diameter: 10.1 m
- Maximum take-off weight: 1,089 kg
- Cruise speed: 113 knots
- Maximum range: 300 nautical miles
- Hover ceiling IGE: 6,400 ft
- Hover ceiling OGE: 4,000 ft
- Known for high quality and cost-effectiveness
- Performance comparable to turbine helicopters
- Optional equipment: Helisas autopilot
- Available as Clipper I with fixed utility floats for over-water operations
- Renowned for long-life and reliability
About this Model
Overview
The Robinson R44 Raven I is a light, four-seat, single-piston helicopter commonly used for primary/advanced training, local aerial work, and personal flying. It emphasizes straightforward systems, low cockpit workload for basic missions, and broad support infrastructure. Capability is best matched to short-to-medium legs with modest payload, where rapid point-to-point access matters more than high cruise speed or all-weather dispatch.
Mission Fit
The R44 Raven I fits missions where simplicity, availability of instructors/parts, and the ability to operate from small pads or confined areas are priorities. Typical use cases include regional day trips, training syllabi, and low-altitude aerial work. Missions that regularly push density-altitude limits, require significant baggage/gear, or demand IFR capability are better served by turbine or IFR-certified platforms.
Cabin
Cabin access is via four doors with a two-front/two-rear seating layout. The experience is functional and utilitarian, with limited baggage volume and a cabin environment that reflects light-helicopter realities (notably noise and vibration). Front-seat visibility is strong for training and observation; rear-seat comfort is suitable for shorter legs with adults depending on body size and installed seating.