R66 Military Trainer — Military Training and Operational Superiority.
Military Training–Focused Design
The R66 Military Trainer offers a balanced flight profile and high control sensitivity, optimized specifically for military pilot training.
Powerful and Durable Engine Performance
Thanks to its Rolls-Royce engine, the R66 Military Trainer delivers reliable and stable performance during intensive training missions.
Advanced Avionics and Training Capability
Modern avionics systems provide realistic training scenarios in line with military standards, along with precise navigation capabilities.

R66 Military Trainer — Highlights

Compliance with Military Training Standards
The R66 Military Trainer is designed in accordance with military pilot training requirements. Its robust airframe and operational realism enable it to withstand intensive training cycles over long periods.
Powerful Engine and Balanced Flight
Its high-performance engine delivers stable and predictable flight characteristics across varying weather conditions. This ensures safe maneuvering and repeatable training scenarios essential for military instruction.
Realistic Cockpit and Training Ergonomics
The cockpit of the R66 Military Trainer accurately reflects real operational helicopter experience. This allows pilot trainees to achieve the highest level of readiness before transitioning to real mission conditions.
Durability and Extended Training Cycle
Its structure, developed for long-duration training operations, optimizes maintenance intervals and increases operational continuity. This provides a significant cost advantage for military training centers.

Specifications R66 Military Trainer

Engine
Rolls-Royce RR300 turboshaft engine
Horsepower
300 shp (takeoff), approx. 275 shp continuous
Internal Payload
Approx. 430 kg
Fuel Capacity (180 gal)
180 U.S. gallons (approx. 681 liters)
Pilot, Passengers, and Baggage with Maximum Fuel
1 pilot + 1 passenger + limited baggage
Crew
1 pilot
Passengers
1–4 occupants (typically 1 student in military training configuration)
Maximum Range (no reserve)
Approx. 660 km
Endurance with Standard Fuel
Approx. 3.5–4 hours
Hover Ceiling IGE at Maximum Gross Weight
Approx. 2,100 m
Hover Ceiling OGE at Maximum Gross Weight
Approx. 1,200 m
Maximum Operating Altitude
Approx. 4,300 m
Cabin Volume Total
Approx. 2.3 m³
Crew Area
Side-by-side dual controls, NVG compatible
Main Cabin
Modular cabin for training and light mission roles
Cargo Area
Rear cabin area, optional external cargo hook

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