Specifications
Broker
Aircraft Details
- Location: England, United Kingdom
- Aircraft status: SOLD
- ARC expiry: 26/10/2026
- Airframe total hours: 340
- Exterior: Volcano Red Pearl Metallic base, Sand Metallic trim
- Interior: Tan leather
- Avionics: Garmin G500H GDU 1060 TXi, Genesys V52 Autopilot, Artificial Horizon, Garmin GTN750 Xi GPS/Com/Nav, Garmin GTR 205 Com, Flight Stream 510 upgrade, GTX345 Mode S ADS-B In/Out, E.L.T Kannad 406 AF, Garmin Radar Altimeter, Garmin GMA 350HC audio panel
- Additional equipment: Fire extinguisher, air conditioning, cabin camera, step, impact resistant windshield, vertical card compass, digital chronometer, helicopter synthetic vision, 4 Bose A30 headsets, accessory bars/USB ports (forward and aft), aft seat dual USB charger, white strobe light, extra corrosion protection, power receptacle, lithium ion battery (aft)
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.