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General| Manufacturer | AutoGyro GmbH |
|---|---|
| Model | Cavalon |
| Type | Gyroplane |
| Seats | 2 |
| Engine Type | Rotax 912 series |
| Maximum Speed | 185 km/h (115 mph) |
| Cruise Speed | 160 km/h |
| Range | 800 km |
| Fuel Capacity | 100 liters |
| Rotor Diameter | 8.4 m |
| Height | 2.7 m |
Overview of the manual's purpose and scope for safe and efficient operation.
General operating limitations and warnings for gyroplane use.
Specifies maximum wind, crosswind, tailwind, altitude, and temperature limits.
Defines VNE and other critical airspeed indicators and markings.
Specifies rotor speed limits, caution ranges, and pre-rotation speed.
Details engine speed, oil temp, oil pressure, and manifold pressure limits.
Defines weight limits for seats, compartments, and overall aircraft.
Defines approved operation types (e.g., VFR) and prohibited maneuvers.
Provides procedures for engine failure during takeoff and flight.
Details steps for attempting an engine air restart.
Addresses procedures for smoke or fire detection and response.
Guidance for making a precautionary landing at a non-prepared site.
Procedures for handling malfunctions in flight control systems.
Explains the meaning and action for various warning and caution lights.
Lists recommended airspeeds for climb, endurance, range, and approach.
Detailed checklist for pre-flight inspections of the gyroplane.
Step-by-step procedure for starting the engine.
Procedures for taxiing, engine run-up, and magneto checks.
Detailed steps for a safe and effective take-off.
Guidance on managing the take-off run and lift-off.
Steps for preparing and executing the approach to landing.
Detailed procedure for a safe landing.
Procedure for safely shutting down the engine.
Illustrates safe operating zones for height and speed combinations.
Lists key speeds for various flight regimes and limitations.
Presents data for take-off and landing distances, including obstacle clearance.
Importance of operating within weight and balance limits for safety.
Conditions for maintaining compliance with weight and balance limits.
Describes controls for trim, rotor brake, and pre-rotator activation.
Details the rotor head control, trim, rudder, and pedal systems.
Overview of the 12V DC electrical system, battery, and warning lights.
Outlines owner/pilot responsibilities for aircraft maintenance.
Procedure for refueling the aircraft and checking fuel levels.
Detailed procedures for rotor system removal and installation.
Explanation of the engine fire indication system and its status.
Guidance on avoiding low-G conditions and their consequences.
Advice on performing side slips safely and avoiding excessive use.
Safety precautions regarding the spinning propeller and rotor.
Critical warning about the hazard of flying into power lines.
Emphasizes the danger of flying in reduced or zero visibility.
