Magni Gyro M24C PLUS Flight Manual Download

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PAGE

DATE

PAGE REV

24 July 2019

209-00-24C

M24C PLUS FLIGHT MANUAL

2.9 TECHNICAL DATA

Weights:

- Dry weight........................................................................................................................ 307 kg

- Empty weight................................................................................................................... 315 kg

- MTOW ............................................................................................................................. 535 kg

Performance:

See Chapter 3.18.

Fuel supply:

- Fuel....................................................................................................................................Petrol

- Fuel tank capacity...........................................................................................................82 litres

- Usable fuel quantity .....................................................................................................78.5 litres

- Reserve ..........................................................................................................................10 litres

- Unusable fuel quantity .................................................................................................3.5 litres

For more information on acceptable fuel and oil please see Chapter 3.17.

Engine:

- Engine type..........................................................................................................Rotax 915 iS A

- Power............................................................................................................................................ 141 hp

- Maximum engine rpm (5 minutes) ............................................................................... 5800 rpm

- Maximum continuous rpm............................................................................................ 5500 rpm

- Maximum MAP (5 minutes)............................................................................................ 51 inHg

- Cylinders................................................................................................................................... 4

- Fuel Consumption/hour (cruise) ..............................................................................18 - 27 litres

- Fuel Consumption/hour (max power) ...........................................................................47 litres

Summary of Contents for M24C PLUS

Page 1: ...w magnigyro it N Registro Imprese di Varese 02207000023 P IVA e c f 02207000023 Capitale sociale 80 000 interamente versato th TITLE M24C PLUS FLIGHT MANUAL CODE 209 00 24C PRODUCT M24C PLUS Revision...

Page 2: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 2 FLIGHT MANUAL M 24C PLUS...

Page 3: ...July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 3 PILOT OPERATING HANDBOOK FOR THE MAGNI GYRO M24C PLUS Registration marks Constructor serial number Engine serial number Aircraft designed and construc...

Page 4: ...TED OPERATIONS 15 2 3 LAY OUT 15 2 4 CHECKLISTS 15 2 5 DEFINITIONS 16 2 5 1 MANUAL ICONS 16 2 5 2 GYROPLANE FRAME 17 2 6 LIST OF ABBREVIATIONS 18 2 7 UNITS OF MEASURE 20 2 8 GYROPLANE GENERAL DATA 20...

Page 5: ...13 TAKEOFF AND LANDING LIMITATIONS 29 3 14 MAX ROTOR RPM 29 3 15 ELECTRICAL LOAD LIMITATIONS 30 3 16 WIND LIMITATIONS 32 3 17 REFUELLING DATA 34 3 17 1 FUELS 34 3 17 2 BRAKE OILS 35 3 17 3 LUBRICANTS...

Page 6: ...FF 45 4 7 SYSTEM RELATED EMERGENCIES 45 4 7 1 LIGHTS 45 4 8 ENGINE FAILURES 47 4 8 1 IN FLIGHT ENGINE FAILURE 47 4 8 2 EXAMPLE OF TEACHING PROCEDURE FOR ENGINE FAILURE 47 4 8 3 IN FLIGHT GENERATORS FA...

Page 7: ...2 TAXIING 69 5 9 BEFORE TAKE OFF CHECKLIST 71 5 10 ROTOR PRE ROTATION PROCEDURE 72 5 11 TAKE OFF 74 5 11 1 NORMAL TAKE OFF 75 5 11 2 CROSSWIND TAKE OFF 76 5 12 FLIGHT MANEUVERS 77 5 12 1 CLIMB 77 5 1...

Page 8: ...GYROPLANE 89 SECTION 6 OPERATIONAL CHARACTERISTICS 6 1 INTRODUCTION 91 6 2 GENERAL FLIGHT CHARACTERISTICS 91 6 3 FLIGHT CHARACTERISTICS IN LEVEL CONDITIONS 91 6 3 1 LOW SPEED 91 6 3 2 HIGH SPEED AND...

Page 9: ...N 99 8 1 2 COCKPIT LAYOUT 102 8 2 INSTRUMENTS AND CONTROLS 103 8 2 1 FLIGHT INTRUMENT PANEL 103 8 2 2 EMS COMM PANEL 104 8 2 3 SWITCH PANEL 107 8 2 4 THROTTLE LEVER 109 8 2 5 ROTOR BRAKE LEVER 109 8 2...

Page 10: ...PAGE DATE PAGE REV 24 July 2019 A 209 00 24C M24C PLUS FLIGHT MANUAL 10 SECTION 1 AMENDMENTS RECORD...

Page 11: ...ted in the Pilot Operating Handbook that the superseded pages are removed and that the receipt form enclosed with the amendment list is signed and returned to Magni Gyro UK Ltd No part of this manual...

Page 12: ...019 30 B 24 07 2019 31 B 24 07 2019 32 B 24 07 2019 33 B 24 07 2019 34 B 24 07 2019 35 B 24 07 2019 36 B 24 07 2019 37 B 24 07 2019 PAGE ISSUE DATE 38 B 24 07 2019 39 B 24 07 2019 40 B 24 07 2019 41 B...

Page 13: ...87 B 24 07 2019 88 B 24 07 2019 89 B 24 07 2019 90 B 24 07 2019 91 B 24 07 2019 92 B 24 07 2019 93 B 24 07 2019 94 B 24 07 2019 95 B 24 07 2019 96 B 24 07 2019 97 B 24 07 2019 98 B 24 07 2019 99 B 24...

Page 14: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 14 SECTION 2 GENERAL...

Page 15: ...UALIFIED INSTRUCTOR Finally the manual provides the pilot with the recommended procedures to deal with circumstances such as emergencies adverse meteorological conditions etc 2 2 PERMITTED OPERATIONS...

Page 16: ...d in this manual are as below WARNING DANGER Operation technical and other procedures which if not followed carefully may expose the operator to the risk of serious accident or death WARNING Operation...

Page 17: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 17 2 5 2 GYROPLANE FRAME...

Page 18: ...as Temperature EMS Engine Monitoring System ft Feet g Gravitational acceleration G Gravitational constant GA Glide Angle GPS Global Positioning System h Hour hp Horse power hPa Hecto Pascal inHg Inche...

Page 19: ...RG Rough Ground ROC Rate Of Climb rpm Revolutions per minute Vo Slow flight speed Va Design maneuver speed Vapp Approach speed VMC Visual Meteorological Conditions Vmc Minimum control speed Vmin Mini...

Page 20: ...The aft fuselage The tailplane The forward section of the fuselage contains the pilot compartment and fuel tank The two seats are side by side in a staggered configuration to maximise comfort The gyro...

Page 21: ...acity 82 litres Usable fuel quantity 78 5 litres Reserve 10 litres Unusable fuel quantity 3 5 litres For more information on acceptable fuel and oil please see Chapter 3 17 Engine Engine type Rotax 91...

Page 22: ...tem Cooling system type air liquid Coolant radiator 3 litres Oil radiator 4 litres Electrical Installation Operating voltage 12 V Tyres Nose wheel 4 00 4 Inflating pressure 2 2 2 5 bar Main wheels 4 0...

Page 23: ...S FLIGHT MANUAL 23 2 10 GYROPLANE DIMENSIONS The overall dimensions are indicated below Rotor diameter 8574 mm 28 20 Total length 4400 mm Width 1608 mm Height without rotor 2700 mm Maximum height with...

Page 24: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 24 SECTION 3 OPERATING LIMITS...

Page 25: ...ecorded in the aircraft logbooks Before flying again make sure that all the necessary checks have been completed 3 2 MINIMUM CREW All flights require a crew of at least one pilot NOTE Smoking in the a...

Page 26: ...ndard propeller pitch is set in the factory The pitch angle of the propeller may not be altered as the performance of the gyroplane may be severely reduced WARNING It is possible to exceed maximum rpm...

Page 27: ...r is equal to 3 g A higher load factor will permanently deform the gyroplane structure When the gyroplane flies in a lightly loaded configuration with less than 400 kg weight the maximum permissible a...

Page 28: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 28 Figure 3 1 Height vs velocity diagram...

Page 29: ...prohibited Left seat is the main pilot seat Max pilot weight is subject to MTOW limitations see section 3 10 3 10 LOAD LIMITATIONS Maximum take off weight 535 kg Maximum landing weight 535 kg 3 11 BAG...

Page 30: ...generator 1 produces 14V 16A and it supplies the engine management system The generator 2 produces 14V 30A and it supplies the remaining gyroplane utilities In case of failure of one generator this w...

Page 31: ...enerator 1 16 A Engine management system FUEL PUMPS 2 16 CONT 16 ECU 1 FUSE BOX 2 Generator 2 30 A Aircraft electrical item LANDING LIGHT 1 2 92 INT 2 92 TRIM 1 2 0 INT 2 0 DOOR WARNING 1 0 02 CONT 0...

Page 32: ...Determine Crosswind component Headwind component Solution Crosswind component 16 kt Headwind component 19 kt 1 Wind direction relative to take off heading is 270 230 40 2 Enter chart at reported wind...

Page 33: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 33 Figure 3 2 Wind component chart...

Page 34: ...ts in the oil system AVGAS should only be used in case of problems with vapour lock or when other types of gasoline are unavailable MOGAS should not be used if the fuel temperature exceeds 20 C or at...

Page 35: ...his could result in a slipping clutch during normal operation Heavy duty 4 stroke motorcycle oils meet all the requirements These oils are normally not mineral oils but semi or fully synthetic oils Oi...

Page 36: ...overlap there is no need to change oil viscosity during short term fluctuations of ambient temperatures 3 17 4 COOLANT Standard coolant has a better thermal heat transfer capability than waterless coo...

Page 37: ...35 kn Distances Take off 320 ft Take off to 50 ft 950 ft Landing from 0 to 100 ft Landing from 50 ft 430 ft Climb and glide ROC at MAUW max power ISA conditions 980 ft min Glide rate at MAUW 1250 ft...

Page 38: ...ained using the Rotax engine performance calculator In 3 19 1 and 3 19 2 the curve is relative to 100 throttle percentage In 3 19 3 and 3 19 4 the curves are relative to different throttle percentages...

Page 39: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 39 3 19 2 ENGINE TORQUE 3 19 3 FUEL CONSUMPTION 100 99 4 98 8 97 4 94 1 84 5 72 56 5 Conversion l h kg h x 1 39...

Page 40: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 40 3 19 4 MANIFOLD PRESSURE 100 99 4 98 8 84 5 56 5 94 1 72 97 4 Conversion inHg bar x 29 53...

Page 41: ...M24C PLUS FLIGHT MANUAL 41 3 20 PLACARDS AND MARKINGS The manufacturer s identification placard is located inside the cockpit on the lower right side of the central console Next to rotor brake lever N...

Page 42: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 42 SECTION 4 EMERGENCY PROCEDURES...

Page 43: ...tical emergencies are defined as emergency situations which require a rapid and immediate response that must be instinctive without reference to any checklist and must be learned by the pilot through...

Page 44: ...n a constant blinking manner Proceed as follows 1 FUEL PUMPS OFF 2 LINE A OFF 3 LINE B OFF 4 THROTTLE LEVER OPEN 5 MASTER OFF 6 ABANDON THE GYROPLANE 7 CALL EMERGENCY SERVICES 4 5 3 ABANDONING THE AIR...

Page 45: ...off or abort it His decision might be influenced by the nature of the malfunction by the speed by the point of takeoff when the malfunction was recognized by the pilot training to land safely or conti...

Page 46: ...quired check the CT 4 YELLOW Fix Low fuel level Fuel level is low Land in 10 minutes to avoid the shut down of the engine because of lack of fuel 5 RED Fix WARNING The lever of the brake rotor is in O...

Page 47: ...k fuel gauge to confirm sufficient fuel 4 Attempt engine re start If engine fails to re start 1 Switch fuel pumps Line A and Line B to OFF 2 Flick Master switch to OFF 3 Check harnesses are tight 4 Co...

Page 48: ...uly 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 48 Locate landing area Wind evaluation Master and fuel pumps OFF verbal indication of execution Land within pre set constraints Figure 4 2 Teaching proced...

Page 49: ...he two cases the pilot has to proceed as follows A Fixed red LED 1 Line A 1 Trim the gyroplane at safe altitude and speed if flying 2 Line A switch OFF 3 Line A switch ON If after 5 seconds the LED is...

Page 50: ...engine management sensor the failure is indicated by the flashing of the WARNING LED Line A and or Line B The pilot has to proceed as follows A Red LED 1 Line A flashing 1 Trim the gyroplane at safe...

Page 51: ...rted If the door warning system activates during the take off and it is safe to land ahead the take off should be aborted If there is any doubt that there is sufficient clear distance to abort a landi...

Page 52: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 52 SECTION 5 FLIGHT PROCEDURES...

Page 53: ...in Section 7 5 5 PILOT CHECKLIST A concise pilot checklist is supplied as a separate document 5 6 DAILY PRE FLIGHT CHECKS Perform these checks before the first flight of the day with the gyroplane ri...

Page 54: ...off ground Function and correct adjustment for the pilots height 6 Control rods Condition 7 Pedal assemblies Correctly attached to the floor C CONTROL STICKS 8 Control sticks Full and free movement 9...

Page 55: ...ening system and stays Operational condition 20 Locking system Operational condition 21 Hinges Condition 22 Transparencies and bonding of transparencies to the frame of the door Condition 5 6 2 EXTERN...

Page 56: ...nd tight B UNDERCARRIAGE RIGHT HAND SIDE 6 Undercarriage leaf spring and mounting bolts Condition Bolts installed and tight Free of cracks or impact marks and not damaged C WHEEL AND WHEEL PANT RIGHT...

Page 57: ...ring by usinga screwdriver to release the fasteners NOTE There is a coolant expansion tank Fig 5 2 2 and a coolant overflow bottle Fig 5 2 3 installed in the engine compartment Make sure you correctly...

Page 58: ...Make sure that the oil level is not more than MAX otherwise oil can get into the venting system The difference between the MIN and MAX marks is 0 45 l 4 Check the oil level as indicated on the dipsti...

Page 59: ...ed 13 Spark plugs and their connection coverings Tight Condition Free of corrosion leaks or chafing and not damaged 14 Engine probes connectors and fasteners Tight Condition Free of corrosion leaks or...

Page 60: ...s linkages bearings and fiberlock nuts Tight Condition 22 Rod end bearings Insignificant play in the Uniball Free of corrosion and not damaged 23 Control rods Shape straight Not damaged Free to rotate...

Page 61: ...ble shaft and Bendix pre rotation gear Sufficiently coated with grease 5 6 5 REAR SECTION A RADIATORS 1 Radiator surfaces Free of fluid leaks or chafing and not damaged 2 Clamps and fixing points Tigh...

Page 62: ...movement 15 Tail wheel Condition Free movement 16 Rudder cables Correct tension 17 Wire locking of the turnbuckles Lock wire installed and serviceable 5 6 6 ENGINE COMPARTMENT LEFT HAND SIDE Open the...

Page 63: ...e Condition Free of rubbing marks and not damaged 4 Brake system Condition Components are not damaged No fluid leaks or chafing of brake lines Brake line pipes and cables secured correctly NOTE The ch...

Page 64: ...up Condition Installed correctly E COCKPIT AND FUSELAGE LEFT HAND SIDE 11 External surface of the fuselage Condition Foreign objects Clean 12 Static port left hand side Clean and not blocked F NOSE W...

Page 65: ...locked position Then move the co pilot handle to the locked position The warning light should remain illuminated and the rotor rpm gauge should remain inactive because the co pilot door is open 2 Mov...

Page 66: ...the gyroplane During ground operations the following precautions are recommended in order to avoid any overheating As far as possible keep the gyroplane in to wind Avoid any prolonged waiting Constan...

Page 67: ...13 Starting push start button WARNING If starting results difficult keep the starter push button pressed for several seconds In order not to damage the starting system it is recommended to press the...

Page 68: ...se down either by hand or by using the dedicated control lock Keep an appropriate safety distance from people and objects especially when the rotor is turning WARNING DANGER It is strictly forbidden t...

Page 69: ...he end of the landing roll or when stopping the gyroplane during taxiing operations and only with the engine at minimum rpm 5 8 2 TAXIING CAUTION Do not move the stick rapidly back wards after you rel...

Page 70: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 70 Figure 5 4 Minimum turning radius...

Page 71: ...light switch ON 8 Strobe lights As necessary 9 Breakers ON 10 Minimum temperatures Minimum 50 C OIL and CT 11 Engine instruments Check within limits 12 Doors Correctly closed lock lever lowered and d...

Page 72: ...remain inactive until both doors are securely closed and both handles placed in the over centre LOCKED position CAUTION Keep the control stick fully forward until reaching 130 rpm rotor speed 1 Align...

Page 73: ...until reaching a rotor speed of 220 rpm standard pre rotation WARNING DANGER The minimum rotor pre rotation speed is 150 rpm It is strictly forbidden to proceed with takeoff operations if the rotor r...

Page 74: ...TAKEOFF LEG climb CROSSWIND LEG climbing until reaching the circuit level DOWNWIND LEG AND BASE in level flight FINAL alignment for landing Figure 5 5 Take off phases 1 Engine starting 2 Holding point...

Page 75: ...n acceleration must be gradual Engine rpm must be increased very carefully 2 Alignment use the rudder pedals to keep the alignment on the runway WARNING During the balancing phase the attitude must be...

Page 76: ...nose up or nose down until reaching and stabilizing the desired speed Carefully release the control stick to check if the speed is maintained correctly NOTE Trimming may start during the climb after...

Page 77: ...only if it is possible to respect the limits of that intensity Inexperienced pilots should be consider their own skill level and not attempt to take off in cross wind conditions which exceed their own...

Page 78: ...ct the desired altitude select the reference point 3 Descent decrease power maintain airspeed attitude control maintain reference point NOTE Max efficiency speed Vy 5 12 4 LEVEL FLIGHT 1 Purpose Fligh...

Page 79: ...t turning with the control stick use the pedals to assist the turn reach and maintain the desired bank angle manage attitude and airspeed reach the reference point centralize the pedals reduce power r...

Page 80: ...duce power as necessary start turning with the control stick less than 15 of bank angle reach and maintain the desired bank angle manage attitude and airspeed reduce or increase power 50 ft in advance...

Page 81: ...head wind level flight 400 ft Vy 3 Decrease speed decrease power maintain attitude reach Vo increase power to maintain altitude 4 Recovery change attitude to increase airspeed reduce power upon reach...

Page 82: ...tle and progressive pitch movements in order to avoid excessive nose up pitch attitudes and obtain a more efficient recovery whilst minimising height loss 5 13 3 IN FLIGHT ENGINE RESTART The engine mu...

Page 83: ...in level flight ALIGNMENT on runway centreline commence descent CONTROL attitude until close to ground while maintaining alignment Figure 5 6 Before landing phases 1 Flight altitude 600 1000 ft QFE 2...

Page 84: ...enter the runway downwind at 45 3 Downwind enter according the parameters indicated for the pattern check engine parameters 4 Base leg maintain specified altitude and speed check traffic on final and...

Page 85: ...of descent with a slight reduction of speed 5 Close to the ground start soft and progressive flare to level off in ground effect 6 In ground effect with a nose up attitude continue the flare until the...

Page 86: ...d landing phases 1 Wind sock 2 Pattern crosswind leg 3 Downwind check landing parameters 4 Base check traffic in final 5 Final alignment and descent Vapp IDLE 6 First flare 7 Flare in ground effect 8...

Page 87: ...priate to land diagonally across the runway in order to limit the crosswind component 5 14 4 GO AROUND 1 Throttle increase to full power 2 Pedal use right pedal to maintain aligned with the runway 3 N...

Page 88: ...ght OFF 3 Navigation lights OFF 4 Radio OFF 5 Navigation instruments OFF 6 Fuel pump B OFF 7 Line B OFF 8 Fuel pump A OFF 9 Line A OFF 10 Master OFF 5 14 7 DOORS OPENING Lift the locking lever to unlo...

Page 89: ...recommended that the parking brake is released after the tie down procedure Temperatures below 0 C can freeze the parking brake in the applied position 1 Apply the parking brake parking brake lever t...

Page 90: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 90 SECTION 6 OPERATIONAL CHARACTERISTICS...

Page 91: ...ed In any flight conditions yaw control is effective down to Vmra Yaw control can be maintained down to zero airspeed by maintaining engine rpm at more than 3 000 rpm 6 3 2 HIGH SPEED AND CRUISING SPE...

Page 92: ...icated speed adjust the attitude in order maintain the best gust penetration speed 6 5 SNOW ICE AND RAIN The gyroplane is not fitted with anti icing systems for the control surfaces of both propeller...

Page 93: ...and with nose high and keep the gyroplane flying as long as possible To completely stop the gyroplane gently pull the control stick back when the main wheels touch the runway Taxi slowly Use the brake...

Page 94: ...TE The radiator is equipped with a fan that automatically switches ON when the temperature reaches the value of 110 C It switches OFF automatically 2 When using maximum power for long periods check th...

Page 95: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 95 SECTION 7 MASS AND CG DATA...

Page 96: ...0 10 0 0 10 7 2 10 Pilot 65 80 55 120 100 80 75 90 120 110 75 Copilot 0 0 55 0 90 65 90 0 0 110 75 Fuel 56 30 42 55 18 55 52 55 5 5 55 XXXXXX 0 0 0 0 0 0 0 0 0 0 0 Total 437 426 468 491 534 516 533 47...

Page 97: ...TE Conversion rate for fuel mass is 1 litre fuel 0 72 kg Max permissible fuel loading is 535 kg aircraft empty weight occupant weights Example fuel mass calculation 535 kg 316 5 kg aircraft empty weig...

Page 98: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 98 SECTION 8 SYSTEM DESCRIPTION...

Page 99: ...ts consistently 8 1 1 MAIN COMPONENTS DESCRIPTION Figure 8 1 External Front view 1 Fuel tank filler 2 Rotor hub bar 3 Rotor head 4 Rotor hub fairing optional 5 Rotor 6 Mast fairing optional 7 Mast upp...

Page 100: ...flexible shaft 5 Control forks assembly 6 Rotor brake 7 Four blade propeller with ground adjustable pitch 8 Pre rotator assembly 9 Vertical fin 10 Trim tab 1 2 4 3 6 5 10 9 11 12 13 14 18 17 20 16 15...

Page 101: ...UAL 101 Figure 8 3 Engine bay 1 Engine 2 Radiator cap 3 Fuse box 4 Oil tank 5 Battery 6 Exhaust system muffler 7 Cooling fan 8 Air filter 9 Oil filter 10 Pre rotation assembly 11 Overflow bottle 12 Cy...

Page 102: ...Switch panel 5 Co pilot pedals 6 Parking brake lever 7 Co pilot control stick 8 Co pilot throttle lever 9 Seats 10 Pilot control stick 10 11 12 11 Seat belt 12 Pre rotation control lever 13 Pilot thro...

Page 103: ...pressure The pitot tube is located at the front of the fuselage The static intake is connected to the two static ports located on the side of the fuselage 2 ALTIMETER The indicator is supplied with a...

Page 104: ...dicates a voltage drop in the lane A 2 Red LINE B lane B voltage drop This warning light indicates a voltage drop in the lane B 3 Yellow FAN cooling fan enabled This light indicates that the cooling f...

Page 105: ...stem If the light is blinking with a regular beat it indicates that one of the sensors in the engine bay has detected temperatures above 120 degrees or the cable of the sensor are in short circuit and...

Page 106: ...ime totalizer 11 Transponder optional For details see instructions manual supplied with the instrument 12 Radio VHF optional For details see instructions manual supplied with the instrument 13 Rotor R...

Page 107: ...circuit breaker 16 F1 circuit breaker Figure 8 8 Switch panel 1 EMS circuit breaker This circuit breaker protects the Kanardia instrument and the rotor tachometer 2 Accessories circuit breaker This ci...

Page 108: ...ery to supply the ECU in case of failure of both generators 10 Master switch Push the lever of the switch upward to ON position to power all electrical utilities 11 Line A switch This switch powers th...

Page 109: ...e power delivered Moving the throttle backward reduces the power delivered Throttle movement goes from 0 to 100 of maximum continuous power NOTE The maximum available power 100 5800 rpm 51 inHg MAP ca...

Page 110: ...ver Torelease the parking brake lift up the top section of the lever and move the lever forward 8 2 7 DIRECTION CONTROLS The control pedals operate the rudder as well as the front wheel thus allowing...

Page 111: ...ight changes the angle of bank of the gyroplane and consequently the direction of flight heading 3 Pre rotation lever This lever allows the activation of the pre rotator It is used during pre takeoff...

Page 112: ...luminated it indicates that at least one of the doors has not been latched and locked correctly Additionally if the system registers an incorrectly closed door then the rotor rpm gauge is rendered ina...

Page 113: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 113 Figure 8 11 Door warning system Figure 8 12 Door locking mechanism Locking pin Door pin Door pin detection switch...

Page 114: ...PAGE DATE PAGE REV 24 July 2019 B 209 00 24C M24C PLUS FLIGHT MANUAL 114 SECTION 9 HANDLING AND SERVICING...

Page 115: ...B 209 00 24C M24C PLUS FLIGHT MANUAL 115 9 1 INSPECTIONS Correct maintenance of the gyroplane is necessary for the safety of flight operations It is strongly recommended that users obey the Maintenan...

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