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Aviation Artur Trendak T&S J22015S, Flight Manual

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Aviation Artur Trendak T&S J22015S Flight Manual Download Page 46

AVIATION 

Artur Trendak 

FLIGHT MANUAL 

Description of the Gyrocopter and its Equipment 

Chapter  7 

 

Edition 1 

21 Aug 2014 

Change no.:  

 

Document no.:  TERCEL-AFM-001-EN 

Page  7-5 

 

7.5

 

Instrument Panel 

An instrument panel is presented below. Different panel configuration and set of flight and 

navigation  instruments  is  possible.  The  details  concerning  other  variants  are  stated  in  Chapter  9 

“Supplements”.

 

The  presented  below  configuration  of  instruments  consist  of  airspeed  indicator  (Light 

Aircraft  7FMS223),  altimeter  (Light  Aircraft  BG-19),  vertical  speed  indicator  (Light  Aircraft 
BC6), Manifold pressure and RPM indicator (MGL Avionics MAP-2T), universal engine monitor 
and rotor RPM indicator (MGL Avionics E-1), fuel level indicator , trim position indicator. 

 

 
 

Summary of Contents for T&S J22015S

Page 1: ...THE ULTRALIGHT CATEGORY FOR LEISURE SPORTS AND DEMONSTRATION PURPOSES AS WELL AS OTHERS EXCLUDING AIR TRANSPORT USING THIS GYROCOPTER FOR TRAINING AND PRACTICE TO OBTAIN A CERTIFICATE OF QUALIFICATIO...

Page 2: ...f this Aircraft Official Journal 107 section 904 with subsequent amendments It is not allowed to make any entries and supplements in this Flight Manual without the consent of the Civil Aviation Author...

Page 3: ...ing data must be recorded in the table below as well as be approved by the Civil Aviation Authority CAA A new or revised text in changed pages must be marked with a black vertical line on the margin a...

Page 4: ...ON Artur Trendak FLIGHT MANUAL Organizational Information Chapter 0 Page 0 2 Document no TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no Change no Description of change Pages affected Entry date Sig...

Page 5: ...4 1 3 21 08 2014 6 3 21 08 2014 1 4 21 08 2014 6 4 21 08 2014 2 2 1 21 08 2014 7 7 1 21 08 2014 2 2 21 08 2014 7 2 21 08 2014 2 3 21 08 2014 7 3 21 08 2014 2 4 21 08 2014 7 4 21 08 2014 2 5 21 08 2014...

Page 6: ...14 Change no 0 3 Table of Contents Chapter Title 0 Organizational Information 1 General Information 2 Restrictions 3 Emergency Procedures 4 Normal Procedures 5 Performance 6 Weight and Position of the...

Page 7: ...tion Chapter 1 Page 1 1 Document no TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no Chapter 1 General Information 1 page 1 1 Introduction 1 2 1 2 Basis for Airworthiness Acknowledgment 1 2 1 3 Descr...

Page 8: ...r should be entered into aircraft records kept by the Civil Aviation Authority as well as hold current air third party insurance 1 2 Basis for Airworthiness Acknowledgment The legal basis for operatin...

Page 9: ...ous cabin with a width of 136 cm is accessible through a large door on the left and right sides Rich glazing ensures optimum visibility Two ergonomic seats can be set up Each chair is equipped with ad...

Page 10: ...AVIATION Artur Trendak FLIGHT MANUAL General Information Chapter 1 Page 1 4 Document no TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no...

Page 11: ...on 2 2 2 2 Flight Speed 2 2 2 3 Speedometer Markings 2 2 2 4 Driving Unit 2 3 2 5 Rotor Rotational Speed 2 3 2 6 Rotor Tachometer Markings 2 4 2 7 Weights 2 4 2 8 Position of the Centre of Gravity 2 5...

Page 12: ...speed except for tranquil atmosphere and exercising with caution Vmin Minimum speed 60 32 The minimum speed of established horizontal flight CAUTION Speedometer indications fluctuate during steep cli...

Page 13: ...8 bar above 3500RPM 2 5 bar above 3500RPM 7 bar Fuel type Lead free car petrol with the minimum octane number of 91 or above Min fuel pressure 0 15 bar Max fuel pressure 0 4 bar Maximum coolant exit...

Page 14: ...326 kg 718lb Minimum crew weight 60 kg 132 lb Maximum crew weight 220 kg 485 lb Maximum one person weight 110 kg 243 lb Maximum fuel weight 93 kg 205 lb the actual proper weight for a particular mode...

Page 15: ...ough the value of the angle whose apex is located on the transverse axle for rotor head suspension on the mast one arm is parallel to the vertical axis of the coordinate system related to the fuselage...

Page 16: ...o TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no Load Factor below 1g during flight cause the rotor rotational speed to fall and if maintained it can lead to disaster DIAGRAM HEIGHT SPEED 2 10 Mano...

Page 17: ...rriage and other reasons Flights can be performed in the Visual Meteorological Conditions VMC covered by Visual Flight Rules VFR Specific usage of gyrocopter is described in Certificate of Registratio...

Page 18: ...ency Procedures 3 page 3 1 Introduction 3 2 3 2 Engine Failure 3 2 3 2 1 During Take off 3 2 3 2 2 During Flight 3 2 3 3 Staring the Engine in Flight 3 2 3 4 Smoke or Fire 3 3 3 4 1 During Taxiing 3 3...

Page 19: ...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 emergency procedures periodically to remain p...

Page 20: ...approaching the ground observe the restrictions following from the height speed diagram page 2 7 In case of a vertical descent commence accelerating the gyrocopter at a height of 80 100 m above the g...

Page 21: ...RCEL AFM 001 EN Edition 1 21 Aug 2014 Change no 3 8 Jamming of the Throttle Lever during Flight x Attempt to move the lever in order to release it x Choose an appropriate spot for landing x Deactivate...

Page 22: ...4 2 4 3 Daily Inspection 4 3 4 4 Pre flight Inspection 4 6 4 5 Before Starting the Engine 4 7 4 6 Starting the Engine 4 7 4 7 Check after Starting the Engine 4 8 4 8 Taxiing 4 8 4 9 Check before Take...

Page 23: ...vibrations in flight The better the alignment of the rotor the greater the comfort of flight the smaller the vibrations and the longer the life of the machine and its subassemblies When the string doe...

Page 24: ...he outside surfaces tail beam pipes and their mounting in the fuselage the rotor mast and its mounting in the fuselage available inside structure of the fuselage for damage corrosion cracks and ensure...

Page 25: ...ar x Check the spark plugs and their caps are securely fixed x Check the condition of the water and oil coolers their fixing and make sure there are no leaks x Check the full and free movement of the...

Page 26: ...hould stop the movement when pulling down the V belts on the left side The clutch cable should have several millimetres of clearance no tension Cabin x Check the doors opening and closing to ensure hi...

Page 27: ...s should be cleared before flight Moreover it is essential to x Check Weight and Balance for flight to make sure it is in limits x Specify the fuel level replenish if necessary x Adjust the chairs che...

Page 28: ...ations if not helps contact AAT certified gyrocopter mechanic 4 5 Starting the Engine CAUTION Only qualified personnel can start the engine x Block the control stick with strap in the extreme front po...

Page 29: ...eto 4 7 Taxiing x For safety reasons it is recommended to stop the rotor during taxiing x During taxi do not exceed a fast walking speed 15 km h x Make sure the pedals operate correctly Left pedal tur...

Page 30: ...ed x Release the wheel brake x Pull the control stick backwards and gradually accelerate x At a speed of 40 km h 22 kt gently lift the front wheel observing attitude of gyrocopter Prerotation lever is...

Page 31: ...Climb Cross Country Flight Descent x Controlling climb and descent is performed by moving the throttle lever coordinated with the movement of the control stick An optimal climb speed is 105 km h x Cli...

Page 32: ...ight line until you stop do not turn during the landing run x Check the rotor until it stops completely x Use the rotor brake below the speed of 150 rpm until it stops CAUTION In case of strong sidewa...

Page 33: ...the rotor head disc rests on the brake x Remove the safety cotter pin and unscrew the nut from the pin for rotor hub suspension in the hub teeter bolt x With the help of another person holding down th...

Page 34: ...o TERCEL AFM 001 EN Page 5 1 Chapter 5 Performance 5 page 5 1 Introduction 5 2 5 2 Characteristic Speeds 5 2 5 3 Take off 5 2 5 4 Climb 5 2 5 5 Diagram of Recalculating Take off distance and Rate of C...

Page 35: ...the best ascent speed VY 105 57 Approach speed VAPP 90 49 Manoeuvre speed two people VD 90 49 Manoeuvre speed one person VD1 90 49 Minimum speed Vmin 60 32 NOTE The actual speed distinctly differs fr...

Page 36: ...C pressure matching an altitude of 2000 m Connect with a line the points matching the above values on appropriate scales At the point where this line intersects with the middle scale read the results...

Page 37: ...Always make sure that the runway is in required condition 5 6 Landing Approach speed VAPP 90 km h 49 kt Landing from above the obstacle 15 m 50 ft 45 55 m 150 180 ft Standard landing run 0 10 m 0 33...

Page 38: ...on 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page 6 1 Chapter 6 Weights and the Position of the Centre of Gravity 2 page 6 1 Introduction 6 2 6 2 Weights 6 2 6 3 Position of the Centre of...

Page 39: ...nimum crew weight 60 kg 132 lb Maximum crew weight 220 kg 485 lb Maximum one person weight 110 kg 243 lb Maximum fuel weight 78 dm3 93 kg 205 lb The current take off weight is equal to the sum of the...

Page 40: ...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...

Page 41: ...centre of gravity of the empty gyrocopter ensures maintenance in the above range of the positions of the centre of gravity 6 4 Entering the Weight and Position of the Centre of Gravity of the Empty Gy...

Page 42: ...rocopter and its Equipment 7 page 7 1 Introduction 7 2 7 2 Airframe 7 2 7 3 Flight Controls 7 2 7 4 Central Console 7 3 7 5 Instrument Board 7 4 7 6 Main gear Wheel Brakes 7 7 7 7 Seats and Safety Bel...

Page 43: ...foil section are made from drawn aluminium and are entirely anodized and perfectly balanced 7 3 Flight controls Controlling flight is performed by using the control stick and pedals Each of crew membe...

Page 44: ...ol Stick In order to release trimmers pilot has to push the Trim Button and hold it longer than one second This changes position of actuators towards 0 position This will reduce all forces generated b...

Page 45: ...its Equipment Chapter 7 Page 7 4 Document no TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no 7 4 Central Console Board Instrument Switch Fuel Pump Switch Navigation Light Switch Headlight Switch Mas...

Page 46: ...f flight and navigation instruments is possible The details concerning other variants are stated in Chapter 9 Supplements The presented below configuration of instruments consist of airspeed indicator...

Page 47: ...akes Position Recommended during Parking Active Brakes Position Recommended during Prerotation To lock the brake lever in position pull it to demanded position and press the red button marked no 1 In...

Page 48: ...ntirely glazed on the left and right sides The doors open in the forward direction In the closed position they are blocked with a lock accessible both from the outside and inside In the door windows a...

Page 49: ...and information on oil replacement replenishment are included in the Aircraft Maintenance Manual The oil temperature optimal range for engine work is 90 C 110 C If the oil temperature is not correct i...

Page 50: ...instruments and additional appliances connected to installation On the side of the instrument board there is a 12V socket a typical car socket for a lighter giving the possibility of connecting additi...

Page 51: ...Aug 2014 Change no Document no TERCEL AFM 001 EN Page 8 1 Chapter 8 Manoeuvring Temporary Operation and Maintenance 8 page 8 1 Introduction 8 2 8 2 Periodic Inspection of the Gyrocopter 8 2 8 3 Repai...

Page 52: ...tions and manuals The owner user is responsible for the operation of the gyrocopter who must guarantee that all the operation will be performed by authorized personnel 8 3 Repairs and Modifications An...

Page 53: ...gh grade waxes or an abrasive compound of the automotive type Soft fabrics or suede must be used for polishing The glazing is to be rinsed with clean water or a water solution with an addition of mild...

Page 54: ...VIATION Artur Trendak FLIGHT MANUAL Manoeuvring Temporary Operation and Maintenance Chapter 8 Page 8 4 Document no TERCEL AFM 001 EN Edition 1 21 Aug 2014 Change no The page is left blank deliberately...

Page 55: ...Artur Trendak FLIGHT MANUAL Supplements Chapter 9 Edition 1 21 Aug 2014 Change no Document no TERCEL AFM 001 EN Page 9 1 Chapter 9 Supplements 9 page 9 1 Introduction 9 2 9 2 List of Introduced Supple...

Page 56: ...sential for the safe and efficient operation on the gyrocopter when it is equipped with various additional systems and equipment not applied in the standard variant 9 2 List of Introduced Supplements...

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