Specifications
AI Description
- Model: ROBINSON R44 RAVEN II
- Exterior Color: New paint (2023) - Gray base with black
- Interior: New gray leather seats and interior
- Total Time Since Overhaul (TTSOH): 200 hours
- Optional Equipment:
- Hydraulic controls (standard equipment)
- Garmin GNC 430 GPS/NAV/COM
- King KY196A COM
- Garmin GTX330 transponder with remote mode C
- Garmin G106A CDI/GS
- Artificial horizon
- Directional gyro
- Turn coordinator
- Heater/defogger
- Air conditioning
- Digital clock
- Vertical compass
- NATAA 12 audio controller
- 5-point safety harness
- Bose interfaces (4) (no headsets)
- Oil filter
- LED landing lights
- Fire extinguisher
- Bladder tanks
- Tail beacon
- ADS-B
- New tail rotor blades per AD
- New asymmetrical horizontal stabilizer
- 100-hour/annual inspection due December 2025
- Located in Los Angeles, California
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.