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General| Manufacturer | Magni Gyro |
|---|---|
| Category | Gyroplane |
| Seats | 2 |
| Engine | Rotax 914 UL |
| Power | 115 hp |
| Maximum takeoff weight | 450 kg |
| Cruise speed | 140 km/h |
| Maximum speed | 160 km/h |
| Service Ceiling | 4, 000 m (13, 123 ft) |
Manual's purpose and target audience for safe and efficient operation.
Defines the approved maneuvers and operations for the gyroplane.
Outlines the manual's structure into six distinct sections.
Describes the manual's content of indexed procedures and definitions.
Explains the use of specific symbols for highlighting important notions.
Details the performance specifications of the gyroplane.
Provides a glossary of aeronautical terms used in the manual.
Description of the M-16 Tandem Trainer, its structure, and configuration.
Provides detailed overall dimensions and key measurements of the gyroplane.
Specifies the dry, empty, and maximum takeoff weights of the aircraft.
Overview of the gyroplane's main components and general layout.
Details the ROTAX 914 engine, its cooling, and performance characteristics.
Explains the dry-crankcase lubrication system of the ROTAX 914 engine.
Describes the intake system, including carburetors and turbocharger.
Details the fuel system, including tank capacity and pump configuration.
Explains the air-water type cooling system for the engine.
Information on the three-bladed Arplast ECO GL3 ground adjustable pitch propeller.
Identifies and describes the main engine controls: ignition, throttle, and choke.
Details the engine instruments, including the FLYDAT monitoring system.
Overview of the gyroplane's electrical system and its components.
Description of essential flight instruments: ASI, Altimeter, VSI.
Details the navigation instruments, specifically the magnetic compass.
Covers control instruments like rotor revolution counter and fuel level.
Explains the flight controls for rotor and direction, including pedals and stick.
Details the hydraulic braking system and its components.
Describes the cockpit layout and seating arrangement for pilot and passenger.
Information on the 4-point safety belts for pilot and passenger.
Details the external lighting system, including landing and anti-collision lights.
Notes on internal lighting and warning lights on the instrument panel.
Provides refueling data, including approved fuels and brake oils.
Specifies the operational limits that must be observed during gyroplane use.
Details reference data required for effective flight planning.
Provides necessary information for takeoff and landing data.
Outlines the limits for weights and balancing of the gyroplane.
References a separate publication for a concise pilot checklist.
Guidance on performing daily preflight checks for safe operation.
Details procedures for engine startup, operation, and limits.
Procedures for taxiing the gyroplane to the holding point.
Comprehensive pre-takeoff checks to ensure airworthiness.
Procedure for engaging the rotor pre-rotation system.
Step-by-step guide for performing a standard takeoff.
Procedure for safe landing, including crosswind considerations.
Instructions for performing unusual maneuvers like slow flight and vertical descent.
General principles and importance of emergency procedures.
Classification of emergency procedures into critical and non-critical.
Procedures for handling emergencies that occur on the ground.
Decision-making process for emergencies occurring during takeoff.
Actions to take in case of fire while the aircraft is on the ground.
Procedures for handling fire incidents that occur during flight.
Recommended actions in case of engine failure.
Guidance on restarting the engine while in flight.
Procedures for safely abandoning the aircraft in an emergency.
Introduction to operational limits for gyroplane usage.
Specifies the minimum crew requirement for any flying activity.
Details the power limitations of the ROTAX 914 engine.
Procedure to follow in case of engine runaway.
Defines the never-exceed and normal operating speed limits.
Limitations on flight maneuvers, including load factors and aerobatics.
Specifies load factor limitations for different flight configurations.
Refers to the height-velocity envelope chart.
Outlines limitations regarding the center of gravity (C of G).
Specifies the maximum allowed weight during takeoff and landing.
Defines the flight conditions, restricted to VMC.
Prohibits applying loads or luggage outside the fuselage.
States maximum crosswind components for takeoff and landing.
Defines the maximum rotor RPM limit.
Specifies the maximum allowed altitude.
General overview of the gyroplane's flight characteristics.
Describes the flight controls operating on three axes.
Details flight characteristics observed in level flight conditions.
Introduction to procedures for flying in adverse conditions.
Guidance for flying during turbulence or storms.
Procedures and warnings related to snow, ice, and rain conditions.
Procedures for operating the gyroplane in low and high temperature conditions.
Details the center of gravity data for the gyroplane.
Provides key performance data such as speeds, distances, and climb rates.
Presents the height-velocity envelope chart for safe operation.
Outlines limitations for various flight maneuvers.
Contains detailed engine performance charts and parameters.
Explains the function and usage of the voltmeter.
