Flight Procedures Tecnam P2002-JF type

9.2. Airplane evacuation ............................................................................................ 28 9.3. Engine failure ..................................................................................................... 29 9.3.1. Engine failure before take-off ....................................................................... 29 9.3.2. Engine failure after take-off .......................................................................... 29 9.3.3. Engine failures in-flight ................................................................................ 30 9.3.4. In-flight engine restart .................................................................................. 31 9.3.5. Engine securing ........................................................................................... 31 9.4. Engine fire / Electrical smoke ............................................................................. 32 9.4.1. Engine fire on ground .................................................................................. 32 9.4.2. Engine fire during take-off ............................................................................ 32 9.4.3. Engine fire in-flight ....................................................................................... 33 9.4.4. Cabin fire / electrical smoke in-flight ............................................................ 33 9.4.5. Cabin fire / electrical smoke on ground ........................................................ 33 9.5. Emergency landing............................................................................................. 34 9.5.1. Forced landing without engine power .......................................................... 34 9.5.2. Power-on forced landing .............................................................................. 34 9.6. Other emergencies ............................................................................................. 35 9.6.1. Recovery from unintentional spin ................................................................. 35 9.6.2. Unintentional flight into icing conditions ....................................................... 35 10. Unit conversation table ........................................................................................... 35 11.1. LHGD (Gödöllő) A/P data ................................................................................. 36 11.3. A/P map ........................................................................................................... 38 11.5. A/P limitations .................................................................................................. 38 Flight Procedures Tecnam P2002-JF type airplane Page: 4 Rev 4, 14 May 2019 1. Foreword This guide has been prepared to provide pilots with information for the flight procedures based on the Aircraft Flight Manual. It is the responsibility of the pilot to study carefully the AFM, a deep knowledge of airplane features and limitations is essential for operating the airplane safely. Subtle differences in this document compared to the AFM are company based procedures that ensures the improvement of flight safety. The content of this document is approved by the Head of Training. 2. Flight preparation 2.1. Aircraft weight and CG definition, performance calculation Based on the calculation method in the AFM define the aircraft take-off weight and CG position according the actual traffic load and ramp fuel. Also define the landing weight and CG position calculating with the estimated fuel consumption. Section 5 PERFORMANCES in the AFM provides all necessary data for an accurate and comprehensive planning of flight activity from take-off to landing. Given information in that section is sufficient to plan the flight with the required precision and safety. 3. Pre-flight check This chapter is an extract from AFM Section 4 NORMAL PROCEDURES. For detailed information about pre-flight inspections refer to that section. 3.1. In the cockpit • Check the A/C documentation • Check safety belts condition • Verify that ignition is in OFF and the start key is not inserted to the starter switch. Flight Procedures Tecnam P2002-JF type airplane Page: 5 Rev 4, 14 May 2019 • Master switch ON, check Voltmeter (10-12V), check Ammeter (red), check the fuel quantities and compare it with the planned fuel amount • Extend the flaps to FULL (in order to check outside) • Master switch OFF • Check ELT • Check necessary cabin accessories (first aid kit, canopy hammer, fire extinguisher) 3.2. Aircraft walk-around: To perform the aircraft walk-around, carry out the checklist according to the station shown below: A. Left fuel filler cap: - Check visually for desired fuel level - Drain the left fuel tank by drainage valve using a cup to collect fuel. Drainage operation must be carried out with the aircraft parked on a level surface) - Check for water or other contaminants Flight Procedures Tecnam P2002-JF type airplane Page: 6 Rev 4, 14 May 2019 - Close filler cap B. Remove protection plug (if provided) and check the Pitot tube and the static ports mounted on left wing are unobstructed. Do not blow inside vents. C. Left side leading edge and wing skin: - Visual inspection D. Left aileron, trim tab and hinges: - Visual inspection, check free play - Friction - Left tank vent: check for obstructions E. Left flap and hinges: - Visual inspection F. Left main landing gear: - Check inflation, tire condition, alignment, fuselage skin condition G. Horizontal tail and tab: - Visual inspection, check free play, friction H. Vertical tail, rudder and trim tab: - Visual inspection, check free play, friction I. Right main landing gear: - Check inflation, tire condition, alignment, fuselage skin condition L. Right flap and hinges: - Visual inspection - M. Right aileron, trim tab and hinges: - Visual inspection, check free play, friction Flight Procedures Tecnam P2002-JF type airplane Page: 7 Rev 4, 14 May 2019 - Right side tank vent: check for obstructions N. Right leading edge and wing skin: - Visual inspection O. Right fuel filler cap: - Check visually for desired fuel level - Drain the right fuel tank by the drainage valve using a cup to collect fuel. Drainage operation must be carried out with the aircraft parked on a level surface - Check for water or other contaminants - Close filler cap P. Set the fuel selector valve to OFF. Drain circuit using a cup to collect fuel by opening the specific drainage valve (part of the gascolator). Check for water or other contaminants. Q. Nose wheel strut and tire: - Check inflation, tire and rubber shock absorber discs condition R. Propeller and spinner condition: - Check for nicks, cracks, dents and other defects, propeller should rotate freely - Check fixing and lack of play between blades and hub S. Open engine cowling: - Check no foreign objects are present. - Verify coolant level in the overflow bottle: level must be between min. and max. mark. Replenish if required. - Only before the first flight of the day: a. Verify coolant level in the expansion tank, replenish as required up to top (level must be at least 2/3 of the expansion tank). b. Turn the propeller by hand to and from, feeling the free rotation of 15°or 30° before the crankshaft starts to rotate. If the propeller can be turned between the dogs with practically no friction at all, further investigation is necessary. Turn propeller by hand in Flight Procedures Tecnam P2002-JF type airplane Page: 8 Rev 4, 14 May 2019 direction of engine rotation several times and observe engine for odd noises or excessive resistance and normal compression. c. Carburetors: check the throttle cable condition and installation. d. Exhaust: inspect for damages, leakage and general condition - Check radiators. There should be no indication of leakage of fluid and they have to be free of obstructions. - Check oil level and replenish as required. Prior to oil check, having magnetos switched off turn the propeller by hand in direction of engine rotation several times to pump oil from the engine into the oil tank, or let the engine idle for 1 minute. This process is finished when air is returning back to the oil tank and can be noticed by a murmur from the open oil tank. Prior to long flights oil should be added so that the oil level reaches the “max” mark. - Inspect fuel circuit for leakages - Check integrity of silent-block suspensions - Check connection and integrity of air intake system, visually inspect that ram air intake is unobstructed - Check that all parts are secured or safetied T. Close engine cowling, check for proper alignment of cam-locks U. Visual inspection of the Landing and Strobe Light V. Remove tow bar and chocks, stow on board pitot, static ports and stall warning protective covers 4. Traffic circuit description This chapter is an extract from AFM Section 4 NORMAL PROCEDURES containing information about the flight procedures for each phase of a normal traffic circuit. For detailed information refer to that section. As a visual aid a simple traffic circuit illustration can be found on page 18. Flight Procedures Tecnam P2002-JF type airplane Page: 9 Rev 4, 14 May 2019 The RPM values in this document are propeller RPM values. RPM indicator in the cockpit panel is measuring the propeller RPM not the engine RPM. Engine RPM value divided by 2,4286 is equal to prop RPM. 3.3. 4.1 Cockpit preparation before engine starting - Seat position and safety belts adjustment - Fasten seatbelts Close and lock canopy(3 point) or fix it in open position(1point) - Prohibited to start the engine with unfixed canopy! - Check fuel valve open - Parking brake: apply brakes with left hand then engage with right hand. 4.2. Engine start up - Master switch,Generator switch ON - Electric fuel pump: ON - Choke: as needed (ON for cold start, OFF for hot start) - Fuel pressure check Strobe on Propeller area: call for CLEAR from outside verbally and by holding left hand thumb up - PROP CLEAR?!!! - Engine throttle: idle (left hand) - Push Key to starter(right hand) - Magnetos: BOTH - Magnetos: START At the first starting sound increase thrust a little bit Flight Procedures Tecnam P2002-JF type airplane Page: 10 Rev 4, 14 May 2019 After start: - Check oil pressure rise within 10 sec. (maximum cold value 7 bar) - Set throttle to 1000-1100RPM, (at cold engine 1300RPM to warm up) , set throttle friction setting if needed - Choke: OFF - Fuel pump OFF - Radios and avionics: Turn ON 4.2. Cockpit check before taxi Consequently Check each switches and instruments from left to right, and from top to bottom, on the instrument panel and in the cockpit. - Check suction (with short RPM increase) - Elevator Trim: cycle fully up and down, from both left and right controls, - Check for trim disconnect switch operation. - Flap: set up to zero. - Check Generator lamp, generator operation, Ammeter check “green”, Voltmeter: check more than 14V - Check ELT Armed - Check flight instruments - Set QNH or aifield elevation - Engine instruments: Check in normal range, - Fuel Quantity and assimetry - Change Fuel valve to higher value side - Check cabin heating, Master and Gen switches on, Fuel pump OFF, Ignition BOTH, Choke OFF, Carb heat OFF, Flaps up, strobe ON - Check circuit brakers on - Activate GPS and Radios, Check local frequency on - Transponder: STBY (set code 7000) 4.3. Taxi out RT: -Gödöllő Traffic, Good Day!. HA-VOG request radio check! Flight Procedures Tecnam P2002-JF type airplane Page: 11 Rev 4, 14 May 2019 -H-OG after start up taxiing from the CAVOK hangar to the holding point of RWY 31/13 Left hand on the throttle, right hand on the brake. - Check left hand side, right hand side, straight ahaed clear. - Set idle power - Release parking brake(with right hand) and increase power - Brakes – Check - Steering – Check Taxi slowly! Use minimal power in straight lines, apply more power for initiating taxi and for the turns only. Do not fight the throttle with the brakes, decrease it to slow down instead. 4.4. Engine run-up check - Stop at Holding Point and set Parking brake on, with two hands. - Engine warm, parameters in green. Verify that pressures and temperatures are in the operative range. Engine run-up test: - Ignition magnetos check: - Set RPM 1700 - Ignition switch LEFT, BOTH, RIGHT, BOTH - The drops shall not be higher than 130 RPM / side and the difference between the two side shall be less than 50 RPM. The engine shall run smooth with either circuit. - Carburetor heating check: - RPM 1700, pull Carb. heat knob fully out, it shall drop 50-100 RPM. Push it back, all parameters should restore to the previous value. - Full power on ground – Check appr. 2100 RPM, - Idle power – Check appr. 600 - 800 RPM - Check oil pressure in green band at both power Flight Procedures Tecnam P2002-JF type airplane Page: 12 Rev 4, 14 May 2019 When Pre-flight check, Cockpit check and Engine check completed the A/C is fit for flight. If you have found any abnormality during these, taxi back and call Maintenance! 4.5. Before T/O at the holding point - Verify fuel quantity – sufficient for the task according to fuel requirements - Fuel selector valve – Fullest tank - Cabin canopy – Close and Check closed and locked on 3 points - Pitch trim – Check neutral - Align directional giro with the magnetic compass - Fuel pump – ON - Flaps 15 - Transponder to ALT mode - Flight controls - Check free and logical movements and flaps position - Check for any possible arriving traffic on final - Check the runway for any departing traffic, crossing vehicle or people RT: H-OG at the holding point of rwy 13/ 31 lining up and taking-off. At this pont or earlier report: -task: traffic circuit; airspace work or cross- country flight, -POB, and -PIC name. When the RWY and Final clear - Landing light – ON - Release the parking brake with right hand - Line up the plane 4.7. Take-off Push forward the brake lever and move your right hand to control stick. Increase full power, keep the aircraft on runway centerline using the wheel steering and the rudder. Simultanously pull the control stick slightly to ease up the nose gear. Rotate the A/C smoothly at 50 KIAS. Start accelerating in a shallow climb and maintain 60 KIAS. Flight Procedures Tecnam P2002-JF type airplane Page: 13 Rev 4, 14 May 2019 4.8. Climbing - Maintain 60 KIAS with pitch attitude - At 200 ft AAL (in case of LHGD 900 ft QNH) - Change hand Flaps Up Landing light – OFF -Change hand Fuel pump – OFF Reduce the power to 2050 RPM 4.9. Turning to crosswind leg At reaching 500 ft AAL turn to the crosswind leg.(In case of LHGD 1200 ft QNH) ( In case or LHGD RWY 31 left hand circuit: 1300ft QNH or above due to hill !) The speed in the turn shall be 65 KIAS so lower the nose to reach and maintain 65 KIAS, during the turn hold the pitch accordingly until the nose points to the new direction. When the turn is completed raise the nose again for the 60 KIAS equivalent attitude. This turn normally less than 90° because of the wind correction. 4.10. Turning to downwind leg This turn shall be initiated when the landing threshold mark can be seen looking 30° behind the lateral axis. Take care of the wind correction on the downwind leg if there is crosswind so that the A/C track is parallel to the RWY centerline. 4.11. Transition to level flight Level off to 1000 ft AAL(LHGD 1700ft QNH) with lowering the nose to maintain the circuit altitude. Let the A/C to accelerate through 75 KIAS and then set 1800-1900 RPM and trim the plane for level flight. Flight Procedures Tecnam P2002-JF type airplane Page: 14 Rev 4, 14 May 2019 4.12. Downwind leg Fly the aircraft parallel to the RWY centerline, correct for crosswind as necessary. At the beginning of downwind check location and track, check engine parameters and fuel assimetry. Change fuel tank if assimetry observed. When passed abeam of threshold, before the base turn, switch on the electric fuel pump, pull the carburetor heat and adjust power 50-100 more to compensate the effect of the carb heat. Report intention to turn base on the radio. RT: H-OG turning LH/ RH base for RWY 31/13, -for touch and go/full stop landing 4.13. Turning to base leg The place for the base turn is when the threshold mark is 35° behind the lateral axis. This turn is a level turn and normally more than 90° due to the wind correction on the base leg. After turning reduce the power to 1300 RPM and extend the flaps to 15, landing light ON, then lower the nose for the descend and maintain 70 KIAS with the pitch. 4.14. Final turn The place for starting the final turn is when the landing threshold is 10° in front of the lateral axis and turn into the runway centerline. Arrange the turn to roll out by 500 ft AAL latest.(LHGD 1200 ft QNH) Increase the power slightly if necessary in order to reduce the descent rate. Maintain 70 KIAS during the turn and on the final. 4.15. Configuration the A/C for landing Normal landing flaps is 40 (FULL). The landing flap shall be extended to 40 earlier or later as the wind strength requires it. Reduce and check speed in the white arc (at or below 67 KIAS) before extending flaps to FULL. -Speed checked -Flaps 40 Flight Procedures Tecnam P2002-JF type airplane Page: 15 Rev 4, 14 May 2019 As the flap extended to 40 lower the nose and increase power to maintain 60 KIAS. Adjust the power and control the pitch in order to point the nose to the aiming point approximately 30 m in front of the threshold mark. With increasing power raise the nose and when reducing the power lower the nose so that the speed remains 60 KIAS. At the short final -Carb heat OFF Landing Reaching 20-5 meters height reduce the power to idle and break the angle of the approach. Start the flare at appr. 1 meter height from the ground. Finish the flare always below half meter height of the main wheels maintaining runway direction and wing levels. Land the A/C to the main wheels with nose gear in the air. On Runways with hard pavement(asphalt,concrete): - Use Flap 15(T/O) for landing - Avoid high flare or overflare the A/C or „stall” landing! -Roll the main wheels on the pavement in „half flared” attitude. In case of crosswind align the A/C axis with the rudder to fly parallel with the RWY and bank into the wind so that the plane will not move sideways from the landing axis. Land on the lower wheel in crosswind then let the other wheel down. Control the roll out with rudder and neutral the aileron as the speed drops. Use flaps 15 (T/O) for landing if - windspeed 15 kts or more - crosswind component 10 kts or more Flight Procedures Tecnam P2002-JF type airplane Page: 16 Rev 4, 14 May 2019 - the wind is so gusty or turbulency on the final that unable to maintain the approach speed between 60-67 KIAS) - on hard pavement(asphalt,concrete) -non normal situation (trim, flight control troubles etc.) The approach speed with Flaps 15 (T/O) is 65 KIAS. Use Flaps 0 for landing in case of malfunctioning of the flaps only. The approach speed with Flaps 0 (UP) is 70 KIAS. 4.16. Full stop landing After touch down maintain the RWY direction with the rudder and release the nose gear down immediatly but gently. In case of full stop landing let the A/C decelerate, use light braking only as neccesary. At taxi speed vacate the RWY to the appropriate direction and report. Avoid stopping on the runway or unnessecarily occupying it. RT:, H-OG RWY vacated. 4.17. Touch and go After touch down maintain the RWY direction with the rudder and release the nose gear down immediately but gently. Then change the hand to keep the stick in the left hand and retract the flap to 15° (T/O) position. Check/Set Carb Heat OFF! - Flaps 15 - Carb Heat OFF Minimise to look inside the cockpit to be able to control the A/C running direction. Change the hands back then apply full power smoothly and continue with take off run. If the remaining runway length is not enough for safe T/O, do full stop actions. Flight Procedures Tecnam P2002-JF type airplane Page: 17 Rev 4, 14 May 2019 4.18. Go around In case the landing can’t be completed safely (due to other traffic, car or personnel on the RWY, the A/C is too high or low for the safe landing, the weather is not suitable for the landing, RWY is not visible or the instructor/controller advises so etc…) go around must be flown. Apply full power and maintain RWY track, turn off the carburetor heating. At the same time stop the descent, check speed increasing and pitch up for climb attitude. When the A/C starts to climb (confirm positive rate on VSI) retract the flap slowly to 15° (T/O) maintain 60 KIAS then proceed to fly a normal traffic circuit and report. RT: H- OG Going around! 4.19. Taxi in If the RWY is vacated during taxi retract the landing flap to 0, turn the landing light OFF, set transponder to STBY and turn fuel pump OFF. At higher temperatures allowed to open the canopy and taxi with it. Stop the A/C, open and fix the canopy(1 point), continue taxi. Prohibited to open canopy at moving A/C or taxiing without fixed canopy! RT : If situation clear: -H-OG taxiing to the CAVOK hangar; to the refueling place, holding point…etc. Stop the A/C at parking position, set parking brake with two hands. 4.20. Before engine shut down Turn off the radios,GPS and Transponder. 4.21. Shut down Turn the ignition key to OFF and pull the key out from the ignition slot. Then turn the Generator and Masterswitch and finally the Strobe to OFF. Put the key to the gyro instrument knob and open canopy. Flight Procedures Tecnam P2002-JF type airplane Page: 18 Rev 4, 14 May 2019 4.22. Tecnam P2002-JF traffic circuit illustration (not to scale) Flight Procedures Tecnam P2002-JF type airplane Page: 19 Rev 4, 14 May 2019 Flight Procedures Tecnam P2002-JF type airplane Page: 20 Rev 4, 14 May 2019 4.3 Emergency manouevers at LHGD 4.3.1 Rejected(aborted) take off If the engine is operating abnormally during take off roll or the take off is not safe due to any reason REJECT the TAKE OFF! Set the thrust lever to idle and hold! Land the A/C as soon as possible with pulled (!) nose (to avoid landing to the nose wheel). When on the ground release the nose immediatly down, release the control stick and pull brake lever with the right hand. Left hand is pulling the throttle. Avoid obstacles with intensiv rudder input if nessecary. -THRUST LEVER IDLE -LAND THE A/C -NOSE DOWN -RELEASE STICK, PULL BRAKE Flight Procedures Tecnam P2002-JF type airplane Page: 21 Rev 4, 14 May 2019 4.3.2 In case of engine failure in the traffic circuit: Simultaneously: - PITCH DOWN - TURN TOWARDS SUITABLE LANDING SITE - SPEED 70 After stabilized: - FUEL PUMP ON - CARBURETOR HEAT ON - COMMUNICATE When reaching the landing site: - FLAPS AS REQUIRED - Note that the gliding properties differ from an actual stopped propeller - When landing anywhere else than on airfield - use full flaps 40 (FULL) - Usually 1000ft AAL is a known altitude from which one can turn back to the airfield - It is common to stall the plane on a steep turn back to the field with inadecuate pitch down - Unofficially 45° bank angle is the maximum during an engine failure emergency. 45° increases the stalling speed by 20% Flight Procedures Tecnam P2002-JF type airplane Page: 22 Rev 4, 14 May 2019 4.3.3 Emergency landing possibilities from traffic circuits No.1 emergency landing place is the airfield! - Blue marks the traffic circuit. - Red marks the designated emergency landing areas where to turn when unable to complete the turn to reach the airfield. - Yellow marks the direction of the first turn on each phase of the flight. - Orange marks the abeam threshold area, where the pilot can choose according to the wind and circumstanses affecting - whether to land tailwind or headwind direction of the runway in use. - The emergency landing fields have several problems and their conditions may change! Details and actual informations by verbal briefing. Flight Procedures Tecnam P2002-JF type airplane Page: 23 Rev 4, 14 May 2019 5. Flight phase transition procedures 5.1. Transition from climb to level flight: Climb: - Speed: 60 KIAS - Power: 2050 RPM Lower the nose to level attitude position, let the plane to accelerate to 75 KIAS and than set the power to 1800 RPM. Reduce the right rudder input during this maneuver to keep the ball centered. 5.2. Transition from level flight to climb Level flight: - V/S: 0 - Power 1800 RPM Raise the nose to the climb attitude, simultaneously increase the power to 2050 RPM and adjust the speed to 60 KIAS. Apply right hand rudder input when giving power to maintain the ball centered. 5.3. Transition from level flight to descent Level flight: - V/S: 0 - Power 1800 RPM Switch Fuel pump and Carburator heating on. Reduce the power to 1300 RPM. Maintain level flight until the speed reduce to 70 KIAS, then lower the nose to descend attitude while maintain 70 KIAS. Some left rudder may be required to center the ball. 5.4. Transition from descent to level flight Descent: Flight Procedures Tecnam P2002-JF type airplane Page: 24 Rev 4, 14 May 2019 - Speed: 70 KIAS - power: 1300 RPM - Carb heat ON - Fuel pump ON Push the carburettor heating and fuel pump to OFF. Apply power to 1800 RPM and simultaneously raise the nose to the level flight attitude and maintain 0 vertical speed. 6. Remarks 6.1. Fuel selector valve operation in-flight During cross country flight monitor and manually compensate asymetrical fuel consumption by switching fuel selector valve. The maximum allowed difference of fuel amount between the tanks is 12 litres (1/4 marking). Switch ON the electric fuel pump prior to swap the fuel feeding from one thank to another. Monitor the fuel pressure after switching fuel supply and turn the electric fuel pump off if the fuel pressure does not change. Approaching Gödöllő from airspace work or cross country flight, check fuel 1 minute prior joining traffic pattern and change fuel tank if necessary. 7. Normal checklist BEFORE START MASTER .................................................. ON BEACON .................................................. ON FUEL PUMP ............................................ ON FUEL SEL VALVE .......... LESS FUEL TANK BRAKE LEVER ................................... PULL THROTTLE (COLD ENGINE: IDLE) .......15% CHOKE (COLD ENGINE) .................... PULL PROPELLER AREA ............................ FREE IGNITION KEY ................................... START AFTER ENGINE START OIL PRESSURE ............................... CHECK RPM .............................................. 1000-1200 Flight Procedures Tecnam P2002-JF type airplane Page: 25 Rev 4, 14 May 2019 CHOKE ................................................ PUSH GENERATOR .......................................... ON FUEL PUMP ...........................................OFF ELECTRICAL EQUIPMENTS .................. ON ENGINE TEST RUN ENGINE PARAMETERS ............. IN GREEN BRAKE LEVER ................................... PULL CONTROL STICK ................................ PULL RPM ....................................................... 1700 IGNITERS ......... 1, 2, ON 1700 RPM CHECK RPM MAX .............................................. 2100 CARB HEAT ..................................... CHECK ENGINE IDLE ....................... 570 – 660 RPM BEFORE TAKE OFF FUEL PUMP ............................................ ON FUEL SEL VALVE .............. FULLEST TANK FLAPS ..................................................... 15° CONTROLS ......................................... FREE AFTER TAKE OFF (200’ AAL) FUEL PUMP ...........................................OFF FLAPS ....................................................... 0° BEFORE LANDING FUEL PUMP ............................................ ON FUEL SEL VALVE .............. FULLEST TANK FLAPS ..................................... 15° OR FULL CARB HEAT ......................... AS REQUIRED 8. Tecnam P2002-JF aircraft data, limitations Description Values Maximum Take-off / Landing Weight 580 kgs Standard empty weight 337 kgs Max Useful Load 243 kgs Maximum baggage compartment load 20 kgs Center of Gravity limit (Datum: from the propeller support flange without spacer) Forward limit (aft of datum for all weights) Aft limit (aft of datum for all weights) 1,693 m (26,0% MAC) 1,782 m (32,5% MAC) Flight Procedures Tecnam P2002-JF type airplane Page: 26 Rev 4, 14 May 2019 Load limits in flight Flaps - CLOSED Flaps - EXTENDED +3,8 g – -1,9 g + 1,9 g – 0 g Oil capacity Min load Full load Oil temperature Min temperature Normal range Max temperature Oil pressure Min pressure Normal range Max pressure CHT Max CHT 2,0 l 3,0 l 50 °C 90 - 110 °C 130 °C 0,8 bar 2 - 5 bar 7 bar 135 °C Fuel Total load (Two tanks) Usable (Two tanks) RON 95 100,0 l 99,0 l Maximum engine power (HP) 98,5 HP Propellel RPM Max RPM Take-off Max Continous Idle 2350-2450 RPM 2200 RPM 570-660 RPM Description KIAS - Indicated Air Speed Roration Speed (in take-off, VR) (580 kg) 50 kts Normal climb, flaps 15° Short field T.O, flaps 15°, speed until 50 ft AGL 60 kts 56 kts Normal climb speed flaps 0° 60 kts Best Angle of Climb Speed - VX flaps 0° 56 kts Best Rate of Climb Speed - VY flaps 0° 66 kts Best Glide Speed 69 kts Flight Procedures Tecnam P2002-JF type airplane Page: 27 Rev 4, 14 May 2019 Stalling Speed (Bank angle 0) Most forward center of gravity (26% MAC) Idle power - flaps 0 (VS1) Idle power - flaps T.O. - (VS1) Idle power - flaps FULL - (VSO) 40 kts 35 kts 30 kts Approach Speed Normal approach - flaps T.O Final approach - flaps FULL 66 kts 60 kts Maximum Flaps Extended Speed - VFE Flaps - FULL Flaps - T.O. 67 kts 97 kts Design Maneuvering Speed - VA 96 kts Maximum Structural Cruising Speed - VNO 110 kts Never Exceed Speed - VNE 138 kts Maximum cross-wind 22 kts 9. Tecnam P2002-JF emergency procedures This chapter contains a brief list only about the airplane emergency procedures. It is mandatory to become thoroughly familiar with the emergency procedures before operating this aircraft. For complete information refer AFM Section 3 EMERGENCY PROCEDURES. 9.1. Malfunctions 9.1.1. Electric power system malfunction • Generator switch – OFF • Master switch – OFF • Generator switch – ON • Master switch – ON If the problem persists: • Generator switch – OFF • Non-vital electric equipment – OFF Flight Procedures Tecnam P2002-JF type airplane Page: 28 Rev 4, 14 May 2019 9.1.2. Electrical fuel pump failure • Fuel pump – OFF • Fuel pump – ON • Fuel pressure – CHECK raise If fuel pressure doesn’t build up: • Land ASAP monitoring fuel pressure 9.1.3. Trim system failure 9.1.3.1. Locked control • Circuit breakers – CHECK • Trim switch LH/RH – CHECK for correct position • Airspeed – Adjust to control A/C without exessive stick force • Land ASAP 9.1.3.2. Trim runaway • Trim disconnect switch – OFF • Airspeed – Adjust to control A/C without exessive stick force • Land ASAP 9.2. Airplane evacuation • Fuel selector valve – OFF • Throttle – IDLE • Ignition – OFF • Electric fuel pump – OFF • Master switch – OFF • Seat belts – Unstrap completely • Headphones – Remove • Cabin canopy – OPEN Flight Procedures Tecnam P2002-JF type airplane Page: 29 Rev 4, 14 May 2019 If the canopy doesn’t slide break it using the hammer, escape away from flames / hot engine compartment / spilling fuel tank. 9.3. Engine failure 9.3.1. Engine failure before take-off • Throttle – IDLE • Rudder – Keep heading control • Brakes – Apply as needed When safely stopped: • Ignition key – OFF • Fuel selector valve – OFF • Fuel pump – OFF • Generator – OFF • Master switch – OFF 9.3.2. Engine failure after take-off Immediate landing should be planned straight ahead with only small changes in directions not exceeding 45° to the left and 45° to the right. • Maintain airspeed – 69 KIAS • Flaps – As needed Before touch-down: • Throttle – IDLE • Ignition key – OFF • Fuel selector valve – OFF • Fuel pump – OFF • Generator – OFF • Master switch – OFF • Landing – Ahead avoiding obstacles, if any Flight Procedures Tecnam P2002-JF type airplane Page: 30 Rev 4, 14 May 2019 9.3.3. Engine failures in-flight 9.3.3.1. Low fuel pressure If the fuel pressure indicator falls below 2.2 psi (0.15 bar): • Electric fuel pump – ON • Fuel selector valve – Change the fuel feeding tank • Fuel quantity - Verify If fuel pressure doesn’t build up: • Land ASAP monitoring fuel pressure If engine stops: • Land ASAP applying forced landing procedure 9.3.3.2. Oil pressure limits exceedance If oil pressure exceeds upper limit (7 bar): • Throttle – REDUCE as practical • Oil pressure & temp – CHECK within limits • Land as soon as practical If oil pressure is under the lower limit (0,8 bar): • Throttle - REDUCE minimum practical • Land as soon as practical If oil pressure continues to decrease: • Land ASAP applying forced landing procedure 9.3.3.3. High oil temperature If oil pressure is within limits: • Throttle – REDUCE minimum practical If oil temperature does not decrease: Flight Procedures Tecnam P2002-JF type airplane Page: 31 Rev 4, 14 May 2019 • Airspeed – INCREASE • Land as soon as practical If engine roughness, vibrations, erratic behaviour, or high CHT is detected: • Land ASAP applying forced landing procedure 9.3.3.4. CHT limit exceedance If CHT is above 135°C: • Throttle – REDUCE Minimum practical • Land as soon as practical If CHT continues to rise and engine shows roughness or power loss: • Land ASAP applying forced landing procedure 9.3.4. In-flight engine restart After a mechanical engine seizure, fire or a major propeller damage engine restart is not recommended. It is preferred to restart the engine at an altitude below 4000ft and at the suggested speed of 69 KIAS or more. • Carb heat – ON if required • Fuel pump – ON • Fuel quantity indicator – CHECK • Fuel Selector – Change the fuel feeding tank • Ignition key – BOTH • Ignition key – START • Throttle – SET as required In case of unsuccessful engine restart: • Engine – SECURE • Land ASAP 9.3.5. Engine securing Following procedure is applicable to shut-down the engine in flight: Flight Procedures Tecnam P2002-JF type airplane Page: 32 Rev 4, 14 May 2019 • Throttle – IDLE • Ignition key – OFF • Fuel selector – OFF • Fuel pump – OFF • Generator – OFF 9.4. Engine fire / Electrical smoke 9.4.1. Engine fire on ground • Fuel Selector – OFF • Fuel pump – OFF • Ignition key – OFF • Throttle - FULL power • Cabin Heat – OFF • Generator – OFF • Master Switch – OFF • Aircraft Evacuation – Carry out immediately 9.4.2. Engine fire during take-off Before rotation, abort take-off: • Throttle – IDLE • Rudder – Keep heading control • Brakes – Apply as needed With A/C under control: • Fuel selector valve – OFF • Fuel pump – OFF • Ignition key – OFF • Cabin heat – OFF • Generator – OFF • Master switch – OFF • Aircraft Evacuation – Carry out immediately Flight Procedures Tecnam P2002-JF type airplane Page: 33 Rev 4, 14 May 2019 9.4.3. Engine fire in-flight • Cabin heating – OFF • Fuel selector valve – OFF • Fuel pump – OFF • Throttle – FULL power • Ignition key – OFF • Cabin vents – OPEN • Land ASAP applying forced landing procedure CAUTION! AFTER AN ENGINE FIRE DO NOT TRY TO RE-START THE ENGINE 9.4.4. Cabin fire / electrical smoke in-flight • Cabin heating – OFF • Cabin vents – OPEN • Canopy – OPEN, if necessary • Fire extinguisher (if fire is in the cabin) – TO BE USED If smoke persists: • Generator – OFF • Master switch – OFF • Land ASAP 9.4.5. Cabin fire / electrical smoke on ground • Generator – OFF • Throttle – IDLE • Ignition key – OFF • Fuel selector valve - OFF • Master switch – OFF • Fire extinguisher – TO BE USED • Aircraft Evacuation – Carry out immediately Flight Procedures Tecnam P2002-JF type airplane Page: 34 Rev 4, 14 May 2019 9.5. Emergency landing 9.5.1. Forced landing without engine power • Flaps – Closed • Airspeed – 69 KIAS • Throttle – IDLE • Safety belts – Tighten • Canopy locks – CHECK LOCKED • Gliding ratio (no power) – 12,8 • Landing place – IDENTIFY • Fuel selector valve – OFF • Fuel pump – OFF • Ignition key – OFF When certain to land: • Flaps – As necessary • Generator – OFF • Master switch – OFF • The flare shall be done on top of the vegetation and pull the stick at touch down 9.5.2. Power-on forced landing • Airspeed – 69 KIAS • Flaps – CLOSED • Safety belts – Tighten • Canopy locks – CHECK LOCKED When certain to land, right before touch down: • Flaps – As necessary • Fuel selector valve – OFF • Fuel pump – OFF • Ignition key – OFF • Generator – OFF • Master switch – OFF Flight Procedures Tecnam P2002-JF type airplane Page: 35 Rev 4, 14 May 2019 • The flare shall be done on top of the vegetation and pull the stick at touch down 9.6. Other emergencies 9.6.1. Recovery from unintentional spin • Throttle – IDLE • Rudder – Opposite to the spin rotation – APPLY FULL • Control stick – NEUTRAL As the spin stops: • Rudder – NEUTRAL • Control stick – Gentle proceed to level flight • Throttle – Set for level flight WARNING! INTENTIONAL SPINNING IS PROHIBITED 9.6.2. Unintentional flight into icing conditions • Carburetor heating – ON Immediately fly away from icing conditions (changing altitude and direction of flight, out of clouds, visible moisture, precipitations). • Controls surfaces - Continue to move to maintain their movability • Propeller speed – Increase RPM • Cabin heat – ON WARNING! FLYING INTO KNOWN ICING CONDITIONS IS PROHIBITED 10. Unit conversation table 1 knots = 1 NM/h =1,853 km/h 1 lbs (librae = pounds) = 0,4536 kg 1 qts (US quart) = 0,946 l Flight Procedures Tecnam P2002-JF type airplane Page: 36 Rev 4, 14 May 2019 1 gal (US gallon) = 3,78 l 1 in (inch) = 2,54 cm 1 psi (pounds per square inch) = 6894,76 Pa = 6,89476 kPa = 0,0689476 bar 1 inHg (Hg inch) = 25,4 mmHg = 3386,39 Pa n F° = ((n-32)*5) / 9C° 11.1. LHGD (Gödöllő) A/P data ICAO code: LHGD Name: Gödöllő Location: 2 km / 1NM SSW Gödöllő Position: N473425 E0191957 Elevation: 218 m / 715 ft Frequency: 119,060 MHz Runways 31/13 (Centerline 306/126 degrees Magnetic) Traffic circuit: 31LH/RH; 13RH/LH; 1000 ft AAL Airfield category: Non public aerodrome Operation: SR-SS NVFR: N/A IFR: N/A Flight Procedures Tecnam P2002-JF type airplane Page: 37 Rev 4, 14 May 2019 11.2. VFR map Flight Procedures Tecnam P2002-JF type airplane Page: 38 Rev 4, 14 May 2019 11.3. A/P map 11.5. A/P limitations RWY Size (m) Surface TORA (m) LDA (m) Load Lighting 13 / 31 1300 x 60 grass 1300 x 60 950 x 60 15 / 5 N / A 11.4. Aerial photo Flight Procedures Tecnam P2002-JF type airplane Page: 39 Rev 4, 14 May 2019 Remarks: -Displaced tresholds -TORA, LDA appr. 800 m/2600 ft only - Only day VFR - The A/P can be used after permitted by the operator except for urgency or emergency - Establish contact 4-5 minutes flight time prior reaching the field at Gödöllő INFO (119,060 MHz) - The A/P directory can be checked at: www.lhgd.hu site - Warnings: - Sheeps on the RWY - Budapest TMA over the field: max permitted altitude 2000 ft AMSL - Possible activities: parachuting; winch started paragliding; remote controlled model flying