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Aviation Artur Trendak T&S J22015S, Руководство по эксплуатации самолета

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AVIATION 

Artur Trendak 

FLIGHT MANUAL 

Restrictions 

Chapter  2 

 

Edition 1 

21 Aug 2014 

Change no.:  

 

Document no.:  TERCEL-AFM-001-EN 

Page  2-7 

 

2.11

 

Crew 

The gyrocopter is a two-seater with an option with single or a double flight control system. 
Minimum crew: 1 pilot. 
 

2.12

 

Sorts of Usage 

This  gyrocopter  can  be  used  for  leisure,  sports,  display  purposes,  for  training,  practice, 

exclusive of air carriage 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 Registration given by Aviation Authority of country of registration.  

 

2.13

 

Fuel 

capacity of the fuel tanks 

120 dm

3

 

admissible quantity of fuel in the tanks 

120 dm

3

 

including 

consumable fuel  118 dm

3

 

 

non-consumable fuel 

2 dm

3

 

 

2.14

 

Wind speed restrictions 

The admissible values of wind speed during flight and landing: 
 
 

direction of wind 

speed 

headwind 

60 km/h 

crosswind 

(90º)

 

30 km/h 

tailwind 

0 km/h 

 

Содержание T&S J22015S

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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