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Details revisions and updates to the manual.
Defines the purpose and scope of the flight manual.
Explains key terms and symbols used throughout the manual.
Provides a list of common abbreviations used in the document.
Lists key technical specifications of the gyroplane.
Specifies safe operating ranges for engine parameters like temperature and pressure.
Defines critical airspeed limitations (Vne, Vno) for safe flight.
Outlines limits for pilot and cargo to maintain safe center of gravity.
Specifies the maximum permissible rotor revolutions per minute.
Step-by-step procedures for handling an in-flight engine fire.
Procedures for emergencies occurring on the ground.
Comprehensive guidance on dealing with various engine failure scenarios.
Detailed checklist for daily pre-flight inspections to ensure airworthiness.
Specific checks to be performed inside the cockpit and on controls.
Walk-around inspection procedures for the aircraft exterior.
Final checklist to be completed before initiating takeoff.
Steps for preparing the rotor system before takeoff.
Procedures for normal and crosswind takeoff.
Comprehensive guide to landing procedures, including normal and crosswind.
Describes handling and stability at various airspeeds.
Safety procedures and precautions for flying in adverse weather.
Guidelines for operating in precipitation and icing conditions.
Procedures for operating in extreme temperature conditions.
Detailed information on weight and balance, including loading configurations.
Identifies and describes the main external parts of the gyroplane.
Illustrates and labels all components within the cockpit.
Details the various instruments and control systems in the cockpit.
Explains the function of each switch and circuit breaker on the panel.
Describes the operation and functions of the main flight control stick.
Explains the system that warns about door latching status.
Emphasizes the importance of correct maintenance and inspections.
General| Engine | Rotax 914 UL Turbo |
|---|---|
| Empty Weight | 290 kg (639 lb) |
| Cruise Speed | 140 km/h (87 mph, 76 knots) |
| Rate of Climb | 5 m/s (984 ft/min) |
| Fuel Capacity | 72 litres (19 US gallons) |
| Range | 600 km (373 miles, 324 nm) |
| Seating Capacity | 2 |
| Service Ceiling | 4, 000 m |
| Horsepower | 115 hp (86 kW) |
| MTOW | 450 kg (992 lb) |
| Maximum Takeoff Weight | 450 kg (992 lb) |
