Need help?Do you have a question about the AutoGyro MTOsport and is the answer not in the manual?
General| Model | MTOsport |
|---|---|
| Seats | 2 |
| Manufacturer | AutoGyro |
| Category | Autogyro |
| Engine | Rotax 912 |
| Engine Power | 100 hp |
| Rotor Diameter | 8.4 m |
| Maximum Takeoff Weight | 450 kg |
| Cruise Speed | 160 km/h |
| Maximum Speed | 185 km/h |
Lists key physical and performance specifications of the aircraft.
Describes the ROTAX 912 ULS and ROTAX 914 UL engines used in the gyroplane.
Covers essential operating principles, pilot qualifications, and aircraft use restrictions.
Details maximum and cautionary airspeed ranges and associated instrument markings.
Outlines rotor speed limits and corresponding instrument markings for safe operation.
Specifies limits for engine speed, oil, temperature, and pressure.
Defines weight limits, CG limits, and loading considerations for the gyroplane.
Defines approved flight operations, prohibiting aerobatics and icing conditions.
Details approved fuel grades, tank capacities, and unusable fuel quantity.
Provides procedures for engine failure during takeoff, climb, and cruise.
Details the steps to attempt an engine restart in flight.
Details procedures for handling engine fires on the ground and in flight.
Describes procedures for performing a precautionary landing at a non-prepared site.
Covers responses to failures in primary and secondary flight controls.
Details procedures for variable pitch propeller malfunctions.
Lists recommended airspeeds for various flight phases.
Provides a comprehensive checklist for pre-flight inspections.
Details the procedure for starting the aircraft engine.
Describes the step-by-step process for a normal takeoff.
Details the steps involved in approaching the landing site.
Provides a step-by-step guide for landing the aircraft.
Describes techniques for taking off from short runways.
Explains how to recover from slow speed flight conditions.
Illustrates safe and unsafe flight conditions for engine failure scenarios.
Details take-off and landing distances under specific conditions.
Emphasizes operating within weight and balance limits for safety.
Outlines conditions for maintaining compliance with weight and balance requirements.
Details the available ROTAX engine variants and their systems.
Details how the control stick, trim, and rudder systems operate the aircraft.
Details the different instrument panel layouts and their components.
Outlines legal responsibilities and intervals for aircraft maintenance.
Provides instructions for checking the engine oil level.
Provides detailed steps for rotor system removal and reassembly.
Describes the optional IVO variable pitch propeller system.
To Next Page
