This table presents the core technical parameters of Changzhou Zhonglian Aviation’s F600 experimental helicopter, with two instrument configuration options:
✈️ Model Variants
Model
Instrument Type
F600
Garmin-style digital instrument panel
F600
Japanese mechanical instrument panel
All performance specifications are identical between the two variants; only the cockpit instrumentation differs.
⚙️ Key Technical Specifications
Parameter
Value
Details
Engine Model
FB160HT
4-cylinder, air-cooled, dual ignition system
Max. Airspeed
190 km/h
Maximum flight speed limit
Max. Power
175 HP
Engine output power
Max. Cruising Speed
160 km/h
Optimal speed for efficient flight
Max. Range
360 km
Maximum distance on a full tank
Endurance
2 hours
Continuous flight time with full fuel
Fuel Tank Capacity
72 L
Compatible with 98# gasoline or AVGAS 100LL aviation fuel
Empty Weight
395 kg
Weight of the aircraft without fuel or payload
Max. Takeoff Weight
650 kg
Total allowable weight including fuel, payload, and crew
Payload
265 kg
Maximum weight for crew and cargo
Seats
2
Two-seat light helicopter configuration
Total Length
8.22 m
Overall length of the aircraft
Total Height
2.39 m
Overall height of the aircraft
Main Rotor Diameter
6.95 m
Diameter of the main lifting rotor
💡 Application Scenarios
The F600 is an experimental category helicopter, ideal for:
Private flight enthusiasts and recreational flying