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Edition 1 21 Aug 2014

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Document no.: TERCEL-AFM-001-EN

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TERCEL

PILOT OPERATING HANDBOOK

Chapter 6

Weights and the position of the centre of gravity

6.1 Introduction

Chapter 6 includes information regarding the gyrocopter’s empty weight, the
usable weight, and the admissible load variants assuring the position of the
centre of gravity of the gyrocopter is in the admissible range.

The way of weighing and specifying the position of the centre of gravity of the
gyrocopter is stated in the Aircraft Maintenance Manual (document no. TERCEL-
SM-001-EN) in Chapter 6.

6.2 Weights

The maximum take-off weight (MTOW) is 560 kg (1235 lb).

The empty weight is 295 kg (649 lb. The actual empty weight for a specific
model is included in the up-to-date weighing report and is set out in subsection
6.4 of this manual.

The usable weight is the difference between the maximum weight and the
empty weight. You can calculate this value on your own (for the empty weight
it is equal to 295 kg (649 lb). The cargo weight which includes the weights of the
crew, luggage and fuel, cannot be greater than the usable weight. Restrictions
concerning load weights:

Chapter 6

Weights and centre of gravity

Minimum crew weight

60 kg

132 lb

Maximum crew weight

170 kg

375 lb

Maximum one person weight

120 kg

264 lb

Maximum fuel weight (xx lt)

93 kg

205 lb

Maximum luggage weight

2 x 10 kg

2 x 22 lb

41

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Содержание TERCEL

Страница 1: ...ITY DATED NO THIS GYROCOPTER CAN BE USED IN THE ULTRALIGHT CATEGORY FOR LEISURE SPORTSAND DEMONSTRATION PURPOSES EXCLUDING AIR TRANSPORT THIS MANUAL IS NOT A SUBSTITUTE FOR PROPER THEORETICAL AND PRACTICAL TRAINING BY A QUALIFIED INSTRUCTOR THE GYROCOPTER MUST BE OPERATED TO COMPLY WITH THE RESTRICTIONS AND INFORMATION CONTAINED HEREIN THIS MANUAL MUST ALWAYS BE AVAILABLE ON BOARD THE GYROCOPTER ...

Страница 2: ... the application of some of the Laws of the Act on Air Law for some sorts of aircraft as well as defining the conditions and requirements concerning the use of this Aircraft Official Journal 107 section 904 with subsequent amendments It is prohibited to make any entries or supplements in this Pilot Operating Handbook without the consent of the Civil Aviation Authority ...

Страница 3: ...ed by the CivilAviation Authority CAA A new or revised text in changed pages must be marked with a black vertical line on the margin and a change number The number of the last change in a given page and its date must be placed in the page footer Every time a change is entered the pages listed in the table below must be mentioned Signature Change no Desciption Pages Date ...

Страница 4: ...Signature Change no Desciption Pages Date Register of Changes ...

Страница 5: ...21 08 2014 3 16 19 21 08 2014 4 20 34 21 08 2014 5 35 40 21 08 2014 6 41 45 21 08 2014 7 46 56 21 08 2014 8 57 60 21 08 2014 9 61 21 08 2014 List of Up to Date Pages List of Up to Date Pages Chapter Page Date Chapter Page Date ...

Страница 6: ...estrictions 2 1 Introduction 5 2 2 Flight Speed 5 2 3 Air Speed Indicator Marking 6 2 4 Driving Unit 7 2 5 Rotor Rotational Speed 8 2 6 Rotor Tachometer Markings 9 2 7 Weights 10 2 8 Position of the Centre of Gravity 12 2 9 Approved Manoeuvers and Limitations 12 2 10 Manoeuver Load Factor 13 2 11 Crew 13 2 12 Sorts of Usage 13 2 13 Fuel 13 2 14 Wind Speed Restrictions 13 2 15 Other Restrictions 14...

Страница 7: ...tle Lever during Flight 19 Chapter 4 Normal Procedures 4 1 Introduction 20 4 2 Attaching the rotor 20 4 3 Daily Inspection 21 4 4 Pre flight Inspection 26 4 5 Before Starting the Engine 27 4 6 Starting the Engine 27 4 7 Checks after Starting the Engine 28 4 8 Taxiing 29 4 9 Checks before Take off 29 4 10 Prerotation and Take off 29 4 11 Climb Cross Country Flight Descent 31 4 12 Approach and Landi...

Страница 8: ...f Gravity 6 1 Introduction 41 6 2 Weights 41 6 3 Position of the Centre of Gravity 43 6 4 Entering the Weights and Position of the Centre of Gravity of the Empty Gyrocopter 45 Chapter 7 Descrition of the Gyrocopter and Equipment 7 1 Introduction 46 7 2 Airframe 46 7 3 Flight Controls 46 7 4 Central Console 49 7 5 Instrument Panel 50 7 6 Main gear Wheel Brakes 51 7 7 Seats and Safety Belts 52 7 8 L...

Страница 9: ...c and Total Pressure System 56 Chapter 8 Manoeuvring Temporary Operation and Maintenance 8 1 Introduction 57 8 2 Periodic Inspection of the Gyrocopter 57 8 3 Repairs and Modifications 57 8 4 Manoeuvring on the Ground Road Transport 58 8 5 Cleaning and Conservation 58 Chapter 9 Supplements 9 1 Introduction 61 9 2 List of Introduced Supplements 61 Contents ...

Страница 10: ...uniqueness of a gyrocopter It is recommended that you study both this Pilot Operating Handbook and the Aircraft Maintenance Manual The gyrocopter can only be used for flight when it is technically operative and holds a valid authorization to perform flights An authorization to perform flights is entered into the ultralight aircraft book This document identifies the ultralight aircraft and contains...

Страница 11: ...tured and delivered in a set blades and hub by Aviation Artur Trendak The blades are made from drawn aluminium and are anodized and perfectly balanced The TERCEL gyrocopter is powered by a CA 912 ULT engine This is a Rotax 912 UL engine expertly modified by Aviation Artur Trendak with an Iveco turbocharger It is equipped with a three blade composite Kaspar Aero 2 3 LT propeller with the capability...

Страница 12: ... width 1 36 m Overall width 2 35 m Overall height 2 87 m Wheel diameter 0 35 m Weight Data kg lb Maximun Take off weight 560 1 235 Empty weight 295 649 Load capacity 265 583 Power Unit Data Engine type CA 912 ULT Horse Power 122 at 5 800 rpm Reducer ratio 1 2 43 Propeller KASPAR Aero 2 3 LT Propeller diameter 1 72 m Fuel tank capacity 120 litres Chapter 1 General Information without rotor ALWAYS c...

Страница 13: ...Edition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page TERCEL PILOT OPERATING HANDBOOK Chapter 1 General Information 4 ...

Страница 14: ...able below Speed IAS km h IAS kt Notes VNE Never exceed speed 200 108 VNO Maximumstructural 130 70 VD Manoeuvring speed 90 49 VMIN Minimum speed 60 32 Do not exceed this speedt any time Do not exceed this speed except in tranquil weather conditions and exercising caution cross country speed Do not perforn full or violent movements above this speed because under certain conditions full movements of...

Страница 15: ...108 Never exceed speed VNE Green arch Yellow arch Red line Yellow triangle 100 54 Flight best ascent speed VY Marking kt Notes Value or Range km h VNE 200 km h VX 95 km h VY 100 km h Vmin 60 km h VD 90 km h 1 person I A S VD 90 km h 2 person VNE 108 kt VX 51 kt VY 54 kt Vmin 32 kt VD 49 kt 1 person I A S VD 49 kt 2 person 6 Chapter 2 Restrictions CAUTION Speedometer indications fluctuate during st...

Страница 16: ...aximum Continuous Power 100 hp 5500 max 39 0 in Hg 75 Take off Power 90 75 hp max 37 0 in Hg Idle 1450 CA 912 ULT Rotax 912 UL engine modified by AVIATION ARTUR TRENDAK by adding the Iveco Turbo Compressor Engine model Power Oil type Manifold Pressure RPM 10W40 minimum normal maximum 2 5 bar above 3 500 rpm 7 bar 0 8 bar above 3 500 rpm Oil pressure 90 110º C Oil temperature 140º C 50º C 7 ...

Страница 17: ...anufacturer KASPAR AERO Propeller model Ka 2 3 LT Propeller diameter 1 72 m Propeller blade angle Lead free car petrol with the minimum octane number of 95 or above 98 recommended 12º in measurement section in accordance with propeller manual Rotor rotational speed rpm normal at maximum weight MTOW 360 390 normal at minimum weight 330 kg 330 340 during autorotation 310 340 minimum for level flight...

Страница 18: ...e buffeting of the rotor blades and disaster 180 150 2 6 Rotor Tachometer Markings Red line 150 Red triangle 180 During take off min rotor rpm for full throttle Yellow arch 180 330 390 500 Warning range Green arch 330 390 Normal range Marking After landing ma rotor rpm for using the rotor brake Notes Value or range rpm 9 Rotor rotational speed rpm minimum until the full opening of the throttle dur...

Страница 19: ...weight 2 x10 kg 2 x 22 lb Weight without rotor The actual proper weight for a particular model is written in the current weighing report and in subsection 6 4 of this manual The current take off weight is equal to the sum of the empty gyrocopter weight and the weights of the crew luggage and fuel Under no circumstances exceed the approved maximum take off weight MTOW equal to 560 kg 1235 lb The pr...

Страница 20: ... ballast on the passenger seat fastened with seat belts to ensure the appropriate balancing of the machine Ballast in the form of a sack of sand or a can of water is recommended The ballast must be protected against movement The ballast weight is set out below Pilot left seat weight kg Ballast right seat kg Ballast right seat lb 50 60 kg 12 kg 26 lb 60 80 kg 10 kg 22 lb 80 100 kg 8 kg 18 lb Pilot ...

Страница 21: ...gravity of the gyrocopter See subsection 6 3 The admissible range of the position of the centre of gravity of the gyrocopter in flight 1 5º 8 5º 2 9 Approved Manoeuvers The TERCEL gyrocopter has been classified in the ultralight aircraft category The approved manoeuvers include stalls lazy eights vertical zooms steep turns in which the roll angle does not exceed 60º WARNING All aerobatic manoeuvre...

Страница 22: ... Sorts of Usage This gyrocopter can be used for leisure sports display purposes and training practice and other reasons but not including air carriage Flights can only be performed in Visual Meteorological Conditions VMC under by Visual Flight Rules VFR The specific use of the gyrocopter is described in the Certificate of Registration given by the Aviation Authority of country of registration 2 13...

Страница 23: ...ING HANDBOOK 2 15 Other Restrictions It is forbidden to perform Aerobatics Turns in which the roll angle exceeeds 60º Flights in icing conditions Flights when the wind speed exceeds 60 km h Flights in severe turbulance areas Flights above densely populated areas Chapter 2 Restrictions 14 ...

Страница 24: ...ition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page TERCEL PILOT OPERATING HANDBOOK DIAGRAM HEIGHT SPEED 2 12 Chapter 2 Restrictions 15 2 16 High Speed Diagram 0 10 8 21 6 32 4 43 2 54 kts h ...

Страница 25: ...ises Most basic emergency procedures such as power off landings are a part of normal pilot training However these emergency situations are also discussed here This information is not intended to replace such training but only to provide a source of reference and review and to provide information on procedures which are not the same for all gyrocopters It is suggested that the pilot review standard...

Страница 26: ...on 3 6 3 3 Starting the Engine in Flight Adopt the gliding attitude Make sure all the switches are in the appropriate position the master switch and the magnetos are ON To start the engine set the throttle lever to the idle position Activate the starter After starting the engine boost the throttle gradually 3 4 Smoke or Fire 3 4 1 During Taxiing Reset the throttle lever to the idle position Close ...

Страница 27: ... a vertical descent commence accelerating the gyrocopter at a height of 250 350 ft above the ground to be able to land safely The highest glide ratio equals 3 1 at a speed of 100 km h 54 kt Then the gyrocopter will head for the area seen in the front bottom window 3 6 Emergency Landing Maintain 100 km h 54 kt to achieve best glide ratio Chose landing spot Land attempting to avoid both possible obs...

Страница 28: ...e the magnetos and the master switch Interrupt the take off Attempt to maintain the direction by means of the pedals and the brake 3 8 Jamming of the Throttle Lever during Flight Attempt to move the lever in order to release it Choose an appropriate spot for landing Deactivate the magnetos when you are within reach of the selected touchdown spot Perform an emergency landing ...

Страница 29: ...string passing through the centre of the hub and along the grooves on the blade tips The rotor must be placed on two supports with a soft surface to avoid damage so that the strained string is about 1 cm above the central opening in the hub When the string does not overlap the hub axle two people are needed for help hold down the blade tips Then push the hub into the right direction After alignmen...

Страница 30: ... the end of the pin Check the rotor head movement range CAUTION When installing the rotor you must only stand on the areas on the fusalage designated for this purpose 4 3 Daily Inspection Most technical faults can be detected during a careful check before flight The safety of operation depends on regular and detailed inspections and servicing An inspection should according to the plan below be con...

Страница 31: ...he fuselage and the available inside structure of the fuselage for damage corrosion and cracks and ensure all components are protected and secured Check the drainage and ventilation holes are not clogged Check the radio antennas are not damaged and are secured Tail Check the fixing of the vertical stabilizers to the tail beams and the horizontal stabilizer to the vertical stabilizers Check the con...

Страница 32: ...rol systems Check the pedals In order to check the free movement of the rudder raise the front wheel by pressing down on the horizontal stabilizer where is joined to the vertical stabilizer Check the condition of rudder pedals ensuring they are securely attached and there are no cracks in the welds and no jamming of the controls Check the control stick moves freely in the full movement range betwe...

Страница 33: ... the engine control system for proper control and connection in the right direction Check that all the wiring around the engine runs freely and is properly attached and connected Make sure both covers of the inspection panels are secure and locked Propeller Check that the propeller blades are securel attached to the hub and the hub to the engine and that the nuts and bolts are secured with safety ...

Страница 34: ...he security of bolts and nuts securing the rotor blades to the hub Check visually blades for scratches nicks signs of cracks or other damage The blades must be clean Check that the rotor swings freely against the head and in the full range between the stops Prerotation mechanism Check the V belts for damage or delamination Check the pre rotation sheave for damage or cracks Check the rotor drive tr...

Страница 35: ...rs and placards are legible 4 4 Pre flight Inspection Before every flight the pilot must perform an overall visual check of the whole gyrocopter Athorough check of the gyrocopter any faults or mechanical issues should be rectified before flight Particularly it is essential to Check that the weight and balance for the flight is within the recommended limits Check the fuel level and replenish if nec...

Страница 36: ...hear the first bubbling from the oil tank Perform 10 more rotations to fully remove the air from the circulating oil From the cockpit check the propeller area is clear and the magnetos off Activate the starter for a maximum of 10 seconds checking that the value of oil pressure is reading a minimum 1 bar If the pressure is too low repeat the previous operations 4 6 Starting the Engine CAUTION Only ...

Страница 37: ...all Clear Propeller Press the starter button for a maximum of 10 seconds After starting the engine all the necessary devices can be activated Deactivate the choke Initionally warm up the engine at about 2000 rpm gradually increasing to 2500 rpm until the oil temperature in the engine reaches 50 C 4 7 Checks after Starting the Engine If any of the parameters are outside the normal range turn off th...

Страница 38: ...edal turn right Check the brakes Avoid using brakes during turns it leads to an unnecessary overload on the front wheel and the pedals 4 9 Checks before Take off Make sure Quantity of fuel is sufficient A visual inspection of fuel in tank is recommended Doors are closed Seats are set up appropriately and the seat belts fastened Choke disengaged Trimmer is loose The gyrocopter is facing against the...

Страница 39: ...tion to fully engaged Set the throttle lever so that the rotor revolutions reach 150 rpm and then pull the control stick back 10 cm 4 and hold on until the rotor revolutions reach 180 200 rpm Set pre rotation to fully disengaged make sure that the prerotation mechanism is deactivated Release the wheel brake Pull the control stick backwards and gradually accelerate At a speed of 40 km h 22 kt gentl...

Страница 40: ...he gyrocopter and the engine parameters CAUTION Since the pilot sits to the side of the gyrocopter s axis remember not move the control stick diagonally if you want to make a move straight forward It is recommended to practise this reflex reaction on the ground with an instructor 4 11 Climb Cross Country Flight Descent Controlling the climb and descent is performed by moving the throttle lever coo...

Страница 41: ...ate approach speed about 95 km h 51 kt Avoid sudden sideways movements Make sure the front wheel is straight At an appropriate level initiate round out so as to align just above the ground and touch down gently Remember landing does not finish when all the wheels touch the ground Perform the landing run along a straight line until you stop Do not turn during the landing run Check the rotor until i...

Страница 42: ...ions occur during flight it is important to inform competent personnel 4 15 Detaching the Rotor The rotor must be detached from the gyrocopter for transportation and in case of longer hangar storage NOTE When detaching the rotor you must only stand on those areas on the fuselage assigned for this purpose Make sure the wheel brakes are activated position 1 Immobilize the control stick by fully tigh...

Страница 43: ...ts withdraw the M8x65 bolts 10 pieces and remove the blades from the sockets in the hub Piece together and assemble back the hub sockets M8 65 bolts washers and nuts Place the pin teeter bolt in the hub with washers screw on a nut and pass through the cotter pin safety pin The removed blades for storage or transportation must be appropriately fastened and protected against damage 34 ...

Страница 44: ...and landing and also data about noise Unless stated otherwise the values refer to a take off weight equal to 560 kg and standard atmospheric conditions 5 2 Characteristic Speeds IAS km h kt Never Exceed Speed VNE 200 108 Maximun structural cross country speed VNO 130 70 Normal structural cross country speed VC 120 65 Best rate of climb VY 100 54 Approach speed VAPP 90 49 Manoeuver speed two people...

Страница 45: ... ft obstacle after accelerating to VY 100 km h 54 kt is about 115 m 350 ft 5 4 Climb The maximum rate of climb at ground level with a speed of VY 100 km h 54 kt is about 1 180 ft min 6 m s and with a one person crew it can reach 1 380 ft min 7 m s The practical ceiling is 10 000 ft Above Sea Level 3 000 m 5 5 Diagram for calculating Take off distance and Rate of Climb depending on Air Temperature ...

Страница 46: ...FM 001 EN Page TERCEL PILOT OPERATING HANDBOOK Example Conditions at the take off airfield temperature 15 ºC pressure matching an altitude of 2 000 m Connect with a line the points matching the above values on appropriate scales Chapter 5 Performance 37 ...

Страница 47: ... atmospheric conditions CAUTION Some runway conditions such as high grass sand mud and snow etc can make take off impossible Always make sure that the runway is in suitable condition 5 6 Landing Approach speed VAPP 90 km h 49 kt Landing above the obstacle 50 ft 15 m 150 180 ft 45 55 m Standard landing run 0 33 ft 0 10 m 5 7 Range and Flight Endurance Average fuel consumption at a cross country spe...

Страница 48: ...Edition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page TERCEL PILOT OPERATING HANDBOOK Chapter 5 Performance 39 THE PAGE INTENTIONALLY LEFT BLANK ...

Страница 49: ...Edition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page TERCEL PILOT OPERATING HANDBOOK 40 THE PAGE INTENTIONALLY LEFT BLANK ...

Страница 50: ...The maximum take off weight MTOW is 560 kg 1235 lb The empty weight is 295 kg 649 lb The actual empty weight for a specific model is included in the up to date weighing report and is set out in subsection 6 4 of this manual The usable weight is the difference between the maximum weight and the empty weight You can calculate this value on your own for the empty weight it is equal to 295 kg 649 lb T...

Страница 51: ...to place ballast on the unoccupied seat fastened with seat belts to ensure the appropriate balancing of the machine Ballast in the form of a sack of sand or a can of water is recommended The ballast must be protected against movement The ballast weight is set out below Pilot left seat Weight kg 50 60 kg 60 80 kg 80 100 kg Ballast right seat kg 12 kg 10 kg 8 kg Ballast right seat lb 26 lb 22 lb 18 ...

Страница 52: ...on of the centre of gravity of the gyrocopter a sideways view is specified through the value of the angle whose apex is located on the transverse axis for rotor head suspension on the mast one arm is parallel to the vertical axis of the coordinate system related to the fuselage and the other arm passes through the centre of gravity of the gyrocopter LINE DRAWING OF ADMISSIBLE C of G 43 ...

Страница 53: ...entre of gravity of the empty gyrocopter for a specific model is included in the up to date weighing report and is set out in subsection 6 4 of this manual The admissible range of the position of the centre of gravity of the gyrocopter in flight is 4 5º 8 5º NOTE Observing the conditions of the admissible load and the proper position of the centre of gravity of the empty gyrocopterensures maintena...

Страница 54: ...of the centre of Gravity of the Empty Gyrocopter The table below serves to enter periodic weighing checks of the gyrocopter or weighing checks after making changes in the equipment repairs or lacquering Date Gyrocopter empty Position of centre Approved by weight of gravity kg degrees Signature Chapter 6 Weights and centre of gravity 45 ...

Страница 55: ...ing of a stabilizer and rudder The empennage is attached to two pipes made of an aluminium alloy guided from the fuselage A metal mast is affixed to the fuselage structure on which the control head with the lifting rotor is mounted The two blade rotor with metal structure is manufactured and delivered in a set blades a hub by AVIATION ARTUR TRENDAK Company The blades with a 8H12 air foil section a...

Страница 56: ...ght pedal causes rudders to deflect right Deflecting the rudder right pushes the tail left and causes the nose to yaw to the right The gyrocopter is equipped with an electrical trim system This device reduces the effort required to adjust or maintain a desired flight attitude Electrical trimming is implemented by means of electrical actuators installed in the control system By clicking the appropr...

Страница 57: ...r there is a relieving flap which aims at facilitating flight straight ahead without the necessity for the pilot to use the pedals It is installed by the manufacturer after the phase of test flights If needed flap position can be corrected by gently bending it in or out see Aircraft Maintenance Manual Chapter 7 Gyrocopter and its Equipment 48 ...

Страница 58: ...e TERCEL PILOT OPERATING HANDBOOK Navigation Light Switch Chapter 7 Gyrocopter and its Equipment Prerotation Clutch Lever red Throttle Lever black Choke Lever blue Broad Instrument Switch Master Switch red key Headlight Switch Fuel Pump Switch 7 4 Central Console 49 ...

Страница 59: ...OOK Chapter 7 Gyrocopter and its Equipment INSTRUMENT PANEL DIAGRAM 7 5 Instrument Panel A sample instrument panel is shown below Different panel configurations and sets of flight and navigation instruments are possible The details concerning other variants are set out in Chapter 9 Supplements 50 ...

Страница 60: ...ing the rudder pedals Normal operating range of the tyre pressure is 2 5 4 bar The main landing gear wheels are equipped with hydraulic disc brakes The brakes are activated with the lever on the control stick and act simultaneously on both wheels To lock the brake lever in Position 1 or Position 2 pull it to the required position and press the red button marked no 1 In order to release the brake p...

Страница 61: ...pushing the lever beneath the seat Each seat is equipped with adjustable four point belts 7 8 Luggage Compartment The luggage is located behind the seats and holds 2 x 10 kg 2 x 22lb In addition a maximum of 8 kg 18lb may be placed under the seats All luggage should be secured to avoid movement in flight 7 15 Glazing Doors The glazing is made of Plexiglas with a thickness of 3 mm and comprises a p...

Страница 62: ...in the instruction manual of the CA 912 ULT engine CA 912 ULT engine characteristics 7 10 2 Propeller The KASPAR Aero 2 3 LT three blade left rotational propeller with a diameter of 1 72 m is fitted in the pushing position having the capability to manually change pitch The hub and blades are made of a composite reinforced carbon fibre The angle of the blade setting measures 714 mm from the axis of...

Страница 63: ...only to use oil with the API classification SJ SG or SL Recommended oils are contained in the Rotax engine manual Recommended oil Aeroshell oil sport plus Do not use oils from diesel engines A diagram of the oil system and information on oil replacement and replenishment are included in the Aircraft Maintenance Manual The oil temperature optimal range for engine work is 90 ºC 110 ºC If the oil tem...

Страница 64: ...l of 98 RON 98 is recommended if available For fuels according to ASTM D4814 specifications following AKI Anti Knock Index value has to be observed min AKI 91 NOTE AVGAS should not be used on a regular basis Average fuel consumption at a cross country speed of VC 130 km h 70kt is about 25 lt h 6 6 US Gal h 7 13 Electrical System The diagram of the electrical system of the gyrocopter is shown in Ch...

Страница 65: ...r there is a failure an orange charging indicator light is illuminated on the instrument panel and then the electrical units will be powered by the battery 7 14 Static and Total Pressure System The total pressure feeder in the form of a pitot tube is located in the nose of the gyrocopter s fuselage It is connected with a plastic hose directly to the speedometer Static pressure to the speedometer a...

Страница 66: ... out in the Aircraft Maintenance Manual of the gyrocopter Regardless of these periodic inspections the gyrocopter will also be subject to the inspections required by the appropriate AviationAuthority The owner user is responsible for the operation of the gyrocopter and must ensure that all the necessary operations are performed by authorized personnel 8 3 Repairs and Modifications Any repairs and ...

Страница 67: ...be performed with great caution by using a forked drawbar grappled by the front wheel axle or a rope grappled by the front leg When parking with the rotor installed tie the rotor to the fuselage by means of turnbuckles with pockets fitted on the blade tips or by using two straps 8 5 Cleaning and Conservation The outside surfaces of the fuselage rotor and propeller should be washed with water with ...

Страница 68: ...ATING HANDBOOK Chapter 8 Manoeuving Operaton Maintenance The cockpit interior chairs rugs and upholstery should be cleaned with a vacuum cleaner It is recommended to apply commercially available cleaning agents for car upholstery Clean the engine in accordance with the Engine Manual 59 ...

Страница 69: ...Edition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page TERCEL PILOT OPERATING HANDBOOK 60 ...

Страница 70: ...cient operation of the gyrocopter when it is equipped with various systems and equipment not durin the standard model 9 2 List of Introduced Supplements In the Notes column confirm by hand whether there is additional equipment or systems in the gyrocopter model for which this manual is intended Document no Title of an Attached Supplement Notes Chapter 9 Supplements Chapter 9 Supplements 61 ...

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