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AutoGyro MTOsport Flight And Operation Manual

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Flight and Operation Manual
for Gyroplane MTOsport
AutoGyro_FOM_MTOsport
Revision 5.0 – Issue Date 01.04.2011
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  • Page 1 Flight and Operation Manual for Gyroplane MTOsport AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 Pre-pages 1...
  • Page 2 INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 Pre-pages 2...
  • Page 3 Applicability This manual is applicable for MTOsport models from a manufacturing date 15.02.2011 and on. For earlier models please refer to manual version 4.x which will be maintained in current status and revised, if necessary.
  • Page 4 REVISION LOG Rev. Inserted by Date Signature AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 Pre-pages 4...

  • Page 5: Table Of Contents

    List of Effective Pages CONTENTS SECTION 1 - GENERAL....................1-1 Introduction....................1-1 Certification ....................1-1 Performance Data and Operating Procedures ..........1-1 Definition of Terms ..................1-2 Important Note....................1-2 Three-view of the MTOsport ................1-3 Description ....................1-4 Technical Data ....................1-4 Rotor ......................1-4 1.10 Engine......................1-5 1.11 Propeller......................1-6 1.12...
  • Page 6 Flight Manual Table of Contents MTOsport List of Effective Pages 3.14 Failure of Variable Pitch Propeller (if installed) ..........3-7 3.15 Alternative Method of Engine Shut-down............3-8 SECTION 4 - NORMAL PROCEDURES ................4-1 Airspeeds for Safe Operation ................ 4-1 Preparation for Flight..................
  • Page 7 Flight Manual Table of Contents MTOsport List of Effective Pages Pneumatic System..................7-3 Power Plant ....................7-4 Propeller......................7-4 Rotor System....................7-5 Flight Controls ....................7-5 7.10 Electrical System ...................7-7 7.11 Lighting System.....................7-7 7.12 Instrument Panel ...................7-7 7.13 Intercom ...................... 7-12 7.14 Pitot Static ....................7-12 7.15...
  • Page 8 Flight Manual Table of Contents MTOsport List of Effective Pages LIST OF EFFECTIVE PAGES Page(s) Rev. Date Page(s) Rev. Date 1-1 to 1-8 01.04.2011 7-1 to 7-12 01.04.2011 2-1 to 2-10 01.04.2011 8-1 to 8-9 01.04.2011 3-1 to 3-8 01.04.2011 9-1 –...
  • Page 9 Flight Manual SECTION 1 MTOsport GENERAL CONTENTS Introduction....................1-1 Certification ....................1-1 Performance Data and Operating Procedures ..........1-1 Definition of Terms ..................1-2 Important Note....................1-2 Three-view of the MTOsport ................1-3 Description ....................1-4 Technical Data ....................1-4 Rotor ......................1-4 1.10 Engine......................1-5 1.11 Propeller......................1-6 1.12 Unit Conversion.....................1-6 1.13...
  • Page 10 Flight Manual SECTION 1 MTOsport GENERAL INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 1 - ii...

  • Page 11: Section 1 - General

    Certification The MTOsport is designed, tested and certified according to the German design specifications for microlight gyroplanes (“Bauvorschriften für Ultraleichte Tragschrauber”, BUT 2001) including its latest amendment published in “Nachrichten für Luftfahrer” NfL II 13/09 issued 12.02.2009, as well as the British Civil Airworthiness Requirements (BCAR)

  • Page 12: Definition Of Terms

    Flight Manual SECTION 1 MTOsport GENERAL Definition of Terms This manual uses WARNINGs, CAUTIONs and NOTEs in bold capital letters to indicate especially critical and important instructions. Additionally, the colour of the panel (red, yellow, and grey shading) highlights the significance of the instruction. Definitions for each term are given below.

  • Page 13: Three-View Of The Mtosport

    Flight Manual SECTION 1 MTOsport GENERAL Three-view of the MTOsport AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...

  • Page 14: Description

    Flight Manual SECTION 1 MTOsport GENERAL Description General Characteristics  Gyroplane with nose gear wheel chassis  Framework manufactured from inert gas-welded stainless steel tube  Two-seat tandem configuration  Main landing gear with GRP (glass fibre reinforced plastic) spring spar and hydraulic disc brakes ...

  • Page 15: Engine

    Flight Manual SECTION 1 MTOsport GENERAL 1.10 Engine ROTAX 912 ULS  4-cylinder, four-stroke spark-ignition engine with opposed cylinders  Liquid cooled cylinder heads  Air cooled cylinders  Dry sump forced lubrication with separate oil tank  Automatic adjustment by hydraulic valve tappet ...

  • Page 16: Propeller

    Flight Manual SECTION 1 MTOsport GENERAL 1.11 Propeller HTC 3 Blade Airscrew with ground adjustable pitch made of CRP / GRP Model ................ HTC 3 Blade 172 ccw 3B Number of blades ................... 3 Diameter ....................172 cm In-flight pitch adjustment ................none...

  • Page 17: Abbreviations And Terminology

    Flight Manual SECTION 1 MTOsport GENERAL 1.13 Abbreviations and Terminology Anti-collision light Above ground level Calibrated Airspeed – indicated speed corrected for installation errors Counter clock wise Centre of gravity Cylinder Head Temperature Carbon Reinforced Plastic Density Altitude Empty Wt Empty weight of the gyroplane including oil, cooling liquid and unusable fuel...
  • Page 18 Flight Manual SECTION 1 MTOsport GENERAL Speed for best angle of climb Speed for best rate of climb and maximum endurance W&B Weight and balance AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...
  • Page 19 Flight Manual SECTION 2 MTOsport LIMITATIONS CONTENTS General ......................2-1 Environmental Limitations................2-2 Colour Code for Instrument Markings ............2-2 Airspeed Limitations and Instrument Markings..........2-3 Rotor Speed Limitations and Instrument Markings.........2-3 Powerplant Limitations and Instrument Markings ...........2-4 Weight and Balance ..................2-6 2.7.1 Weight Limits ....................2-6 2.7.2...
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  • Page 21: Section 2 - Limitations

    Flight Manual SECTION 2 MTOsport LIMITATIONS SECTION 2 - LIMITATIONS This section contains operating limitations, instrument markings and basic placards which are required for safe operation of the gyroplane, including its engine, and standard equipment or systems. General WARNING The operation of a gyroplane demands professional pilot instruction and dedicated training on gyroplanes.

  • Page 22: Environmental Limitations

    Flight Manual SECTION 2 MTOsport LIMITATIONS NOTE During the certification process all required safe loads have been successfully demonstrated. However, the gyroplane may be exposed to much higher loads especially when operated on rough surfaces, such as an unprepared grass strip.

  • Page 23: Airspeed Limitations And Instrument Markings

    Flight Manual SECTION 2 MTOsport LIMITATIONS Airspeed Limitations and Instrument Markings Air Speed Marking Never Exceed Speed 185 km/h Red radial Yellow arc 120 – 185 km/h Design speed for max. gust intensity 30 - 120 km/h Green arc Yellow arc 0 –...

  • Page 24: Powerplant Limitations And Instrument Markings

    Flight Manual SECTION 2 MTOsport LIMITATIONS Powerplant Limitations and Instrument Markings Engine Speed Marking Maximum engine speed Red radial 5800 RPM 5 minute take-off power regime Yellow arc 5500 – 5800 RPM Maximum continuous power Green arc 1400 – 5500 RPM Yellow arc 0 –...
  • Page 25 Flight Manual SECTION 2 MTOsport LIMITATIONS Manifold Pressure* ROTAX 912 ULS Marking Maximum manifold pressure Red radial 31 In Hg Yellow arc 27 – 31 In Hg Maximum continuous MAP Green arc 0 - 27 In Hg Manifold Pressure* ROTAX 914 UL...

  • Page 26: Weight And Balance

    Flight Manual SECTION 2 MTOsport LIMITATIONS Weight and Balance 2.7.1 Weight Limits Maximum take-off weight (MTOW): ............450 kg CAUTION The take-off weight is the total weight of the gyroplane including empty weight, optional/additional equipment, occupants, fuel, and luggage at take-off. The maximum value specified above must never be exceeded.

  • Page 27: Flight Crew

    Flight Manual SECTION 2 MTOsport LIMITATIONS Flight Crew Minimum crew is one pilot in the front seat. Harness in aft seat must be fastened and tight. The aft control stick must be removed unless the passenger seat is occupied by a qualified flight instructor.

  • Page 28: Fuel

    Flight Manual SECTION 2 MTOsport LIMITATIONS 2.10 Fuel 2.10.1 Approved Fuel Grades Preferred fuel EN 228 Super or EN228 Super plus (min ROZ 95) Alternate fuel AVGAS 100 LL (ASTM D910) For operational constraints and maintenance aspects when using preferred fuel and alternate fuel, refer to the engine manufacturer’s manual...

  • Page 29: Placards

    Flight Manual SECTION 2 MTOsport LIMITATIONS 2.12 Placards In clear view of the pilot: Only VFR day is approved Aerobatic flight prohibited! Low-G manoeuvres prohibited! Flight in icing conditions prohibited! Max. gusts/wind 72 km/h (40 kts)! In clear view of the pilot: Max.
  • Page 30 Flight Manual SECTION 2 MTOsport LIMITATIONS At storage compartment in nose section: Max. load: 10 kg W&B must be respected! At fuel filler neck: Min. ROZ 95 AVGAS 100LL At each fuel tank: Capacity 34 litres At fuel shut-off valve (if installed):...
  • Page 31 Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES CONTENTS Engine Failure ....................3-1 Air Restart Procedure ..................3-2 Landing into Trees or High Vegetation............3-2 Degradation of Engine Power ................3-2 Evacuating the Aircraft...................3-3 Engine Fire....................3-3 Off-field Landing ....................3-4 Flight Control Malfunction ................3-4 3.8.1 Engine Power Control / Throttle ..............3-4 3.8.2...
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  • Page 33: Section 3 - Emergency Procedures

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES SECTION 3 - EMERGENCY PROCEDURES This chapter contains the check lists and procedures to be executed in emergency situations. Emergencies due to defects of the gyroplane or its engine are extremely seldom if the aircraft is checked thoroughly before each flight and continuously maintained.

  • Page 34: Air Restart Procedure

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES NOTE The best engine-off glide ratio is about 1:3 at 100 km/h. Depending on a possible headwind the glide may be extended by slightly increasing airspeed. It is heavily recommended to train your forced landing capabilities regularly, preferably with a qualified flight instructor.

  • Page 35: Evacuating The Aircraft

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES NOTE The phenomenon of carburettor icing is extremely unlikely with this engine type as it is fitted with a hot water heated jacket around the carburettor inlets. Note that the system can work properly only when the engine is at operating temperature.

  • Page 36: Off-Field Landing

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES Off-field Landing A precautionary landing at a non-prepared site may be performed at pilot’s discretion in order to avoid unexpected weather, in case of severe illness of the pilot or a passenger, or if technical defects are suspected, for example sudden and severe rotor vibrations.

  • Page 37: Warning Lights

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES 3.8.3 Rotor Head Control In case of a rotor head control malfunction, control pitch attitude using careful trim input and power setting. Use rudder for directional control and for shallow turns. In some conditions it may be appropriate to reduce power/speed in order to avoid phugoid effects or a possible negative yaw-roll coupling.

  • Page 38: Parameters Out Of Limits

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES 3.10 Parameters out of Limits PARAMETER EXCURSION CORRECTIVE ACTION Engine Oil Upper limit Reduce power and increase air speed. If condition Temperature yellow arc cannot be corrected, land as soon as practicable. Lower limit Allow engine to warm-up on ground.

  • Page 39: Failure Of Variable Pitch Propeller (If Installed)

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES Alternatively, if landing on asphalt is unavoidable, approach normally, with the intent of a zero-speed touch-down directly into wind. Only if impossible to recover the aircraft from the landing area it should be manoeuvred under its own power, as this could further damage the tire and wheel rim.

  • Page 40: Alternative Method Of Engine Shut-Down

    Flight Manual SECTION 3 MTOsport EMERGENCY PROCEDURES 3.15 Alternative Method of Engine Shut-down If the engine continues running after the magnetos have been switched off use one of the following alternative methods: Hold throttle lever in IDLE position firmly while overstretching the cable ends of the carburettor control cables with the other hand.
  • Page 41 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES CONTENTS Airspeeds for Safe Operation.................4-1 Preparation for Flight ..................4-1 Daily or Pre-flight Checks ................4-1 Before Boarding ....................4-5 Before Starting Engine...................4-5 Starting Engine....................4-6 Taxi and Run-up ....................4-7 Take-off Procedure..................4-7 Take-off Run....................4-9 4.10 Climb......................4-9 4.11 Cruise......................4-9...
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  • Page 43: Section 4 - Normal Procedures

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES This section contains check list items, instructions and procedures for the operation of the gyroplane. However, these procedures do not replace the pilot’s appreciation of the individual situation.
  • Page 44 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES The following checks must be carried out before each flight. However, if the gyroplane is operated by a single pilot or within an organization where the checks are performed by or under the supervision of qualified personnel, check list items marked with a preceding ‘ʘ’...
  • Page 45 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Station 3 (nose) General appearance ..................OK Windshield condition and cleanliness............Check Pitot cover (if installed)................ Removed Rotor lash bag ..................Removed Storage compartment in nose section (if installed) ....Closed and locked ʘ...
  • Page 46 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Station 7 (engine, RH side) ʘ Main frame rear side / welded joints......No cracks, no deformation Oil cooler and hoses RH........Clean, no leaks, fittings tight Water cooler and hoses RH........Clean, no leaks, fittings tight Exhaust system RH ................No cracks...

  • Page 47: Before Boarding

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Station 11 (main gear spring spar, LH) LH Main wheel running surface..............Check Air pressure and slip mark ............. Visual check ʘ Brake and wheel attachment ..............Check Wheel pant and attachment ..............Check ʘ...

  • Page 48: Starting Engine

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Starting Engine Parking brake ....................Set Cold engine: Throttle ......................Idle Choke..................Fully engaged Warm engine: Throttle .................Idle or slightly cracked Choke................... disengaged Master switch ....................ON All engine variants: Note GEN indicator light ON...

  • Page 49: Taxi And Run-Up

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Taxi and Run-up During taxi do not exceed 15 km/h which is approximately jogging speed and steer with careful pedal input. Use wheel brake carefully, if needed, but not before throttle lever has been completely pulled to idle.
  • Page 50 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES WARNING Prior to releasing the wheel brake make sure that the control stick is fully aft. A take-off run with flat rotor system may have fatal consequences. WARNING With the rotor speed below green arc relative speed must be built-up carefully to allow rotor speed to increase first.

  • Page 51: Take-Off Run

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES Take-off Run  Check min. 5400 RPM for take-off. Otherwise, abort take-off  Minimize lateral drift by applying appropriate lateral control stick input into cross wind direction  Maintain directional control i.e. runway alignment with sensitive pedal input ...

  • Page 52: Descent

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES 4.12 Descent  Reduce power setting and lower nose  Adjust trim VPP: With a variable pitch propeller installed, refer to the respective flight manual supplement in CHAPTER 9 for correct power setting and handling procedure.

  • Page 53: Go-Around

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES 4.15 Go-around  Apply take-off power. Counteract yaw tendency and align gyroplane with rudder input.  In horizontal flight, allow gyroplane to gain speed  Climb with safe or best rate of climb speed and adjust trim...

  • Page 54: Engine Shut-Down

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES 4.17 Engine Shut-down Throttle ......................Idle Parking brake ....................Set Turbo charger cool-down (ROTAX 914 engine) ......min. 30 seconds Second fuel pump (if installed)..............OFF Avionics/Radio/Intercom/Lights (except ACL / Strobe) ........ OFF Both MAG switches ..................OFF ACL / Strobe (if installed)................

  • Page 55: Training Engine In-Flight Shut-Down And Air Restart

    Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES 4.21 Training Engine In-flight Shut-down and Air Restart The engine should not be stopped in flight deliberately except as part of forced landing training under the supervision of a qualified flight instructor. If possible, allow the engine to cool down at 3000 rpm for about 30 sec before turning it off.
  • Page 56 Flight Manual SECTION 4 MTOsport NORMAL PROCEDURES INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 4-14...
  • Page 57 Flight Manual SECTION 5 MTOsport PERFORMANCE CONTENTS Demonstrated Operating Temperature ............5-1 Airspeed Calibration ..................5-1 Height-Velocity Diagram ................5-2 Speeds ......................5-3 Rate of Climb....................5-3 Take-off and Landing Data ................5-3 Glide Ratio ....................5-3 Additional Performance Data .................5-4 5.8.1 Fuel flow ....................5-4 5.8.2 Service Ceiling..................5-4 Sound Exposure Level / Noise Characteristics ..........5-4...
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  • Page 59: Section 5 - Performance

    Flight Manual SECTION 5 MTOsport PERFORMANCE SECTION 5 - PERFORMANCE The following data were determined by flight testing and demonstrated with average piloting skills, with engine and aircraft in good condition, as well as clean main rotor and propeller. The parameters apply to standard conditions (15°C at sea level and standard pressure) and a gross mass of 450 kg.

  • Page 60: Height-Velocity Diagram

    Flight Manual SECTION 5 MTOsport PERFORMANCE Height-Velocity Diagram The H/V diagram indicates combinations of height and speed (avoid area left side of the red graph) where a safe landing may not be possible in case of an engine failure. Therefore, take-offs and landings should be conducted according to the recommended flight profile, provided as blue dashed line.

  • Page 61: Speeds

    Flight Manual SECTION 5 MTOsport PERFORMANCE Speeds The following speeds are relevant for flight performance. For additional speed limitations refer to SECTION 2 LIMITATIONS of this manual. Minimum horizontal speed, TOP (only ROTAX 914) .......30 km/h IAS Minimum horizontal speed, TOP .............35 km/h IAS Minimum horizontal speed, MCP.............40 km/h IAS...

  • Page 62: Additional Performance Data

    Flight Manual SECTION 5 MTOsport PERFORMANCE Additional Performance Data 5.8.1 Fuel Flow The following fuel flow figures are provided as estimates and do not constitute certified performance. Exact fuel flow will vary with environmental conditions, cleanliness of propeller and rotor, piloting technique (minimum side slip), and power setting. For additional procedures about proper power setting consult SECTION 9 for supplemental data concerning the variable pitch propeller, if installed.
  • Page 63 Flight Manual SECTION 6 MTOsport WEIGHT AND BALANCE CONTENTS General ......................6-1 Weight and Balance Record ................6-1 Compliance with Weight and Balance............6-1 AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 6 - i...
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  • Page 65: Section 6 - Weight And Balance

    Compliance with Weight and Balance The MTOsport gyroplane is designed in such way that compliance with weight and balance is provided, if  the gyroplane is loaded within the individual weight limitations for each station as provided in SECTION 2 of this manual, and ...
  • Page 66 Flight Manual SECTION 6 MTOsport WEIGHT AND BALANCE INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...
  • Page 67 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION CONTENTS Introduction....................7-1 Airframe and Undercarriage................7-1 Doors, Windows and Exits................7-1 Fuel System ....................7-1 Pneumatic System..................7-3 Power Plant ....................7-4 Propeller......................7-4 Rotor System....................7-5 Flight Controls ....................7-5 7.10 Electrical System ...................7-7 7.11 Lighting System.....................7-7 7.12 Instrument Panel ...................7-7 7.13...
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  • Page 69: Section 7 - System Description

    Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION SECTION 7 - SYSTEM DESCRIPTION Introduction This section contains the description of the gyroplane and its standard systems and equipment. Optional equipment is described in Chapter 9 of this manual. Airframe and Undercarriage The load carrying structure of the gyroplane consists of an inert-gas welded stainless steel square tube framework and includes mast, forward extension, and aft extension.
  • Page 70 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION As an option, a fuel quantity indication in the cockpit, as well as low fuel sensors may be installed. The LOW FUEL warning light is triggered as soon as 5 litres or less of useable fuel remain in the tanks.

  • Page 71: Pneumatic System

    Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Pneumatic System Aircraft trim, rotor brake and activation of the pre-rotator is controlled by a pneumatic system, consisting of an electrically driven air compressor with dry cartridge, a pressure gauge in the cockpit, solenoid valves, air lines, pneumatic actuators, and the respective cockpit controls.

  • Page 72: Power Plant

    Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Power Plant Engine There are two engine variants available, being the ROTAX 912 ULS normally aspirated reciprocating engine and the ROTAX 914 UL turbo charged version. Both engine types are 4 cylinder, horizontally opposed, 4 stroke engines featuring ...

  • Page 73: Rotor System

    Lateral trim input is not active on MTOsport models. Because of a safety circuit, activation of the pre- rotator is only possible with the pneumatic mode selector in FLIGHT position and the control stick fully forward.
  • Page 74 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Rudder and front wheel control The Rudder is connected to the foot pedals with steel cables which are routed horizontally along the main frame. Both pairs of pedals are interconnected by a linkage. The nose wheel steering is directly linked to pedal/rudder control input by control rods.

  • Page 75: Electrical System

    Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION 7.10 Electrical System The 12V DC electrical system consists of an engine driven electrical generator, a battery, master switch, indicators, switches, electrical consumers, and cabling. With the ROTAX 914 UL engine an electrical power supply is vital for continued engine operation as this engine variant solely relies on electrically driven fuel pumps.
  • Page 76 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Panel Layout - Standard 1 – Engine RPM 14 – Radio (if installed) 2 – Pneumatic mode selector 15 – Manifold pressure gauge (if inst.) 3 – Rotor RPM 16 – ATC transponder (if installed) 4 –...
  • Page 77 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Panel Layout – Moving Map Landscape 1 – 12V power receptacle (if installed) 14 – Hour meter 2 – Overdrive push button 15 – Radio (if installed) 3 – Altimeter 16 – ATC transponder (if installed) 4 –...
  • Page 78 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Panel Layout – Moving Map Portrait (Garmin 695) 1 – Engine RPM 14 – Radio 2 – Overdrive push button 15 – MAG switches 3 – Rotor RPM 16 – Master/starter switch 4 – Altimeter 17 –...
  • Page 79 Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION Panel Layout – Glass Cockpit (FlyMap LD) 1 – 12V power receptacle (if installed) 12 – Hour meter 2 – Overdrive push button 13 – Radio (if installed) 3 – FlyMap Integrated Display 1 14 –...

  • Page 80: Intercom

    Flight Manual SECTION 7 MTOsport SYSTEM DESCRIPTION 7.13 Intercom The standard intercom system features a socket with bayonet coupling on a loose cable to connect a helmet. The intercom amplifier and VOX control is integrated in the respective radio. See manufacturer’s manual for additional information.
  • Page 81 Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE CONTENTS Maintenance Obligations ................8-1 General ......................8-1 Ground Handling ...................8-2 Cleaning ......................8-2 Refuelling ......................8-2 Checking of Engine Oil Level.................8-2 Checking of Engine Coolant Level ..............8-3 Tire Pressure....................8-3 Lubrication and Greasing................8-3 8.10 Replenishing of Fluids ...................8-4 8.10.1...
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  • Page 83: Section 8 - Handling And Servicing

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE SECTION 8 - HANDLING AND SERVICING This chapter contains guidelines for correct handling and servicing of the gyroplane, as well as manufacturer recommendations helping to keep its performance, reliability and value. Maintenance Obligations...

  • Page 84: Ground Handling

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE Ground Handling Experience shows that aircraft may be exposed to much higher loads when operated on ground, than when in flight. Such loads caused by rumbling on rough terrain, or bouncing the aircraft over the hangar threshold may easily exceed the design load in peak.

  • Page 85: Checking Of Engine Coolant Level

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE To gain access to the oil reservoir hinge the rear seat forward, open and remove oil reservoir cap and remove dipstick. Turn the engine over using the propeller in the correct sense of rotation until you clearly hear the oil gurgle in the tank.

  • Page 86: Replenishing Of Fluids

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE 8.10 Replenishing of Fluids 8.10.1 Engine oil See engine manufacturer’s manual. 8.10.2 Engine coolant See engine manufacturer’s manual. 8.11 Engine Air Filter The air intake filters need to be replaced or cleaned according to the manufacturer‘s recommendation.

  • Page 87: Removal, Disassembly, Assembly And Installation Of The Rotor

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE During winter operations the necessary operating temperature for oil and cooling agent may not be reached. This can be compensated by taping some portion of the coolers. Monitor all engine temperatures closely after having the coolers taped and modify, if necessary.

  • Page 88: Disassembly Of The Rotor System

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE The shim washers and the teeter block in the hub are marked on each side with either one or two engraved dots. Directly after the disassembly the shim washers need to be fixed on their respective side with cable ties.

  • Page 89: Assembly Of The Rotor System

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE Push out all fitting bolts (4) without any force, but use no more than a gentle tapping if necessary. Tilt the rotor blade up and down to support easy removal of the bolt.

  • Page 90: Road Transport

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE 8.15.4 Installation of the Rotor System CAUTION During installation make sure to have each and every part of the rotor system installed in exactly the same way and orientation as it was before.

  • Page 91: Repairs

    Flight Manual SECTION 8 MTOsport HANDLING / MAINTENANCE 8.17 Repairs IMPORTANT NOTE Repairs may only be executed by persons authorized by the manufacturer, and in strict compliance with maintenance and repair instructions. AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...
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  • Page 93: Section 9 - Supplements

    Flight Manual SECTION 9 MTOsport SUPPLEMENTS SECTION 9 - SUPPLEMENTS LIST OF SUPPLEMENTS 9-1 Variable Pitch Propeller - IVO 9-2 Lights 9-3 GPS/Moving Map Systems AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...
  • Page 94 Flight Manual SECTION 9 MTOsport SUPPLEMENTS INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011...

  • Page 95: Variable Pitch Propeller - Ivo

    Flight Manual SECTION 9-1 MTOsport Variable Pitch Propeller - IVO 9-1 Variable Pitch Propeller - IVO 9-1.1 General A variable pitch propeller (VPP) manufactured by IVO is available as optional equipment to optimize the propeller efficiency, fuel consumption, and noise in all flight regimes and power settings.
  • Page 96 Flight Manual SECTION 9-1 MTOsport Variable Pitch Propeller - IVO 9-1.5 Performance ROTAX 912 ULS Power setting Engine RPM Fuel flow [l/h] Max. TOP 5800 27.5 Max. MCP 5500 27.0 75% MCP 5000 26.0 65% MCP 4800 26.0 55% MCP 4300 24.0...
  • Page 97 Flight Manual SECTION 9-1 MTOsport Variable Pitch Propeller - IVO the propeller blades. Actual blade feathering motion is achieved by twisting the complete blade, without having the need for a pitch change bearing. 9-1.8 Handling and Servicing Refer to the manufacturer’s documentation.
  • Page 98 Flight Manual SECTION 9-1 MTOsport Variable Pitch Propeller - IVO INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 9-1 - 4...

  • Page 99: Lights

    Flight Manual SECTION 9-2 MTOsport Lights 9-2 Lights 9-2.1 General Depending on customer’s configuration the gyroplane can be equipped with optional  Landing lights  Navigation /position lights  Strobe lights 9-2.2 Limitations No change to standard aircraft 9-2.3 Emergency Procedures No change to standard aircraft 9-2.4 Normal Procedures...
  • Page 100 Flight Manual SECTION 9-2 MTOsport Lights INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 9-2 - 2...

  • Page 101: Gps/Moving Map Systems

    Flight Manual SECTION 9-3 MTOsport GPS/Moving Map Systems 9-3 GPS/Moving Map Systems 9-3.1 General Depending on customer’s configuration the gyroplane can be equipped with different GPS/Moving Map Systems as optional equipment. NOTE Any moving map system shall be used for reference only and does not replace proper flight planning and constant oversight and awareness.
  • Page 102 Flight Manual SECTION 9-3 MTOsport GPS/Moving Map Systems INTENTIONALLY LEFT BLANK AutoGyro_FOM_MTOsport Revision 5.0 – Issue Date 01.04.2011 9-3 - 2...

  • Page 103: Section 10 - Appendix

    Appendix SECTION 10 - APPENDIX LIST OF APPENDICES Customer Feedback Form Change of Ownership Form Incident Reporting Form Appendix...
  • Page 104 Appendix INTENTIONALLY LEFT BLANK Appendix...
  • Page 105 Your feedback or error reporting - use extra sheets if needed and include a suggestion for correction or remedial action, if possible Reported by Email Date Below fields are used for AutoGyro internal processing – do not fill in! Investigation completed Action and response Internal reference Customer Feedback...
  • Page 106 Appendix 1 Customer Feedback Form Customer Feedback AutoGyro Form AG-F-CFB-V1.A...
  • Page 107 This form is supplied to enable the new owner to register the change of ownership, so that he/she may receive any service or other information relating to the aircraft. The information is stored in a database and is only used within AutoGyro GmbH for the above purpose.
  • Page 108 Appendix 2 Change of Ownership Form Change of Ownership AutoGyro Form AG-F-CHO- V1.A...
  • Page 109 Depending on the incident information supplied, a corrective action is investigated and, if needed, supplied back to the customer(s). The information is stored in a database and is only used within AutoGyro GmbH for the above purpose. Return this form to: AutoGyro GmbH Dornierstraße 14...
  • Page 110 Appendix 3 Incident Reporting Form Incident Reporting AutoGyro Form AG-F-AIR-V1.A...

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