TECNAM P2002 JF

detachments, excessive play, unsafe or improper installation as well as for general condition. For control surfaces, visual inspection also involves additional check for freedom of movement and security. Red lubber lines on bolts and nuts shall be intact. TECNAM 2002 01 08 2022 rev 1 7 5. Use protection plug on the Pitot tube and the static ports mounted on left wing 6. Use protection plug on the Pitot tube and the static ports mounted on left wing 7. Left aileron, trim tab and hinges: visual inspection, check free of play, friction; Left tank vent: check for obstructions. 8. Left flap and hinges: visual inspection 9. Left main landing gear: check inflation, tire condition, alignment, fuselage skin condition 10. Horizontal tail and tab: visual inspection, check free of play, friction. 11. Vertical tail, rudder and trim tab: visual inspection, check free of play, friction. 12. Right main landing gear; check inflation, tire condition, alignment, fuselage skin condition. 13. Right flap and hinges: visual inspection. 14. Right aileron, trim tab and hinges: visual inspection, check free of play, friction; Right side tank vent: check for obstructions. 15. Right leading edge and wing skin: visual inspection. 16. Nose wheel strut and tire: check inflation, tire and rubber shock absorber discs condition. 17. Propeller and spinner condition: check for nicks, cracks, dents and Rother defects, propeller should rotate freely. Check fixing and lack of play between blades and hub. 18. Open engine cowling: 1. Check no foreign objects are present. 4. Check radiators. There should be no indication of leakage of fluid and they have to be free of obstructions. 6. Inspect fuel circuit for leakages. 7. Check integrity of silent-block suspensions. 8. Check connection and integrity of air intake system, visually inspect that ram air intake is unobstructed. 9. Check that all parts are secured or safetied. 19. Close engine cowling, check for proper alignment of cam-locks. 20. Visual inspection of the landing and strobe light. 21. Use chocks, stall warning protective covers. TECNAM 2002 01 08 2022 rev 1 8 BEFORE ENGINE STARTING SEAT POSITION AND SAFETY BELTS ADJUST FLIGHT CONTROLS MOVEMENT SMOOTHNESS, FREE OF PLAY AND FRICTION PARKING BRAKE ENGAGE THROTTLE THROTTLE FRICTION AND IDLE CIRCUIT BREAKERS CHECK ALL IN GPU (G500) BREAKER OUT ALTERNATE HORIZON PULL TO CAGE, HOLD MASTER ON, CHECK GENERATOR LIGHT ON AND VOLTAGE (AT LEAST 10.5 V) FUEL PUMP ON CHECK FUEL PRESSURE FUEL PUMP OFF MASTER AVIONIC ON INSTRUMENTS CHECK MASTER AVIONIC OFF FLAPS CYCLE FULLY EXTENDED AND THEN SET T/O PITCH TRIM ON - CYCLE FULLY UP AND DOWN, SET NEUTRAL NAV LIGHTS, ON FUEL QUANTITY CHECK INDICATION CANOPY CLOSED AND LOCKED TECNAM 2002 01 08 2022 rev 1 9 ENGINE STARTING ALTERNATE HORIZON PULL TO CAGE MASTER CHECK ON AVIONC MASTER CHECK OFF THROTTLE IDLE CHOKE AS NEEDED FUEL SELECTOR VALVE SELECT LEFT OR FULLEST TANK FUEL PUMP ON PROPELLER AREA CALL FOR CLEAR AND VISUALLY CHECK MAGNETOS START OIL PRESSURE RISE WITHIN 10 SEC. (MAX. 7 BAR) GENERATOR ON VOLTMETER 14 V AMMETER GREEN ENGINE INSTRUMENTS CHECK CHOKE OFF PROPELLER RPM 1000-1200 FUEL PUMP OFF FUEL PRESSURE (MIN. 2.2 PSI) GPU (G500) BREAKER IN AVIONIC MASTER ON SET NAV/COMM, BARO, ALT, HDG, CRS, GPS, XDPS, TECNAM 2002 01 08 2022 rev 1 10 TAXI OFF BLOCK TIME NOTE SPACE AROUND THE PLAIN CHECK PARKING BRAKE DISENGAGE BRAKES CHECK DURING TAXI STEERING CHECK FLIGHT INSTRUMENTS CHECK REACTION AND INDICATIONS RUN UP PARKING BRAKE ENGAGE ENGINE INSTRUMENTS CHECK WITHIN LIMITS FUEL PUMP ON, CHECK PRESSURE FUEL VALVE SELECT LEFT OR FULLEST TANK RPM 1640 IGNITION MAGNETOS CHECK L, BOTH, R, BOTH CARB. HEAT TEST RPM 1000 FLAPS SET T/O (15°) PITCH TRIM CHECK NEUTRAL FLIGHT CONTROLS CHECK FREE SEAT BELTS CHECKED FASTENED CANOPY CHECK CLOSED AND LOCKED TECNAM 2002 01 08 2022 rev 1 11 BEFORE TAKE-OFF WIND CHECK DIRECTION AND SPEED APPROACH SECTOR CHECK FREE INSTRUMENTS CHECK SETTINGS AND INDICATIONS TRANSPONDER ALT STROBE LIGHT ON FUEL PUMP CHECK ON CARB. HEAT CHECK OFF FLAPS CHECK T/O LANDING LIGHT ON TAKE-OFF BRIEFING I’LL TAKE-OFF RWY….. SURFACE CONDITION (WET/DRY), WIND…… ROTATION 42, CLIMB SEED VY 66. IN CASE OF EMERGENCY ON THE GROUND ABOARD TAKE-OFF . IN CASE OF ENGINE FAILURE UP TO ALT=500 FT AGL LAND STRAIGHT AHEAD, IN CASE OF ENGINE FAILURE ALT>500 AGL TURN AROUND AND LAND ON RWY WITH TAIL WIND, VG=69 TAKE – OFF BRIEFING COMPLETED TAKE-OFF AND CLIMB PARKING BRAKE DISENGAGE FULL THROTTLE CHECK INSTRUMENTS AND CALL OUT “T/O POWER SET AND CHECK” SPEED CHECK AND CALL OUT “SPEED ALIVE” 42 KTS ROTATION 66 KTS CLIMB ALT>200 FT AGL FLAPS RETRACT, FUEL PUMP OFF, LANDING LIGHT OFF RPM REDUCE AT OR BELOW 2250 TECNAM 2002 01 08 2022 rev 1 12 CRUISE RPM GREEN SECTOR BELOW 2250 ENGINE INSTRUMENTS WITHIN LIMITS CARB. HEAT. AS NEEDED1 PITOT HEAT. AS NEEDED FUEL SELECTOR VALVE AS NEEDED FUEL PUMP ON, CHECK PRESSURE, SWITCH VALVE , CHECK PRESSURE AND WAIT 10-15 s., FUEL PUMP OFF BEFORE LANDING BRIEFING I’LL LAND RWY…. SURFACE CONDITIONS (WET/DRY). WIND…… I’LL LAND WITH …..(FULL / T/O) FLAPS POSITION. T/O FLAPS AFTER BASE APCH SPEED 66 KTS, FULL FLAPS ON FINAL APCH SPEED 55 KTS. ALTIMETERS SET AND CHECKED, LANDING BRIEFING COMPLETED FUEL PUMP ON CARB. HEAT AS REQUIRED1 LANDING LIGHT ON PARKING BRAKE CHECK DISENGAGE BALKED LANDING THROTTLE FULL CARB. HEAT. OFF FLAPS T/O CLIMB AFTER SETTING FLAPS T/O POSITION AND INCREASING SPEED SET CLIMB WITH VX-56 OR VY-66 FUEL PUMP CHECK ON TECNAM 2002 01 08 2022 rev 1 13 AFTER LANDING FLAPS UP FUEL PUMP OFF TRANSPONDER SBY STROBE LIGHT OFF LANDING LIGHT OFF (AT NIGHT USE LANDING LIGHT FOR TAXI) ENGINE SHUT DOWN ON BLOCK TIME NOTE PARKING BRAKE ENGAGE RPM 1000-1200 FOR 1 MINUTE RPM MINIMUM AVIONIC MASTER OFF GPU (G500) BREAKER OUT MAGNETOS OFF NAV LIGHT OFF MASTER AND GENERATOR OFF FUEL SELECTOR VALVE OFF TECNAM 2002 01 08 2022 rev 1 14 Two types of emergency procedures are hereby given: a. „RED”, which must be known by heart and executed in the correct and complete sequence, as soon as possible as the failure is detected and recognized. b. „YELLOW”, which should be well theoretically know and mastered, but that are not time critical and can be executed entering and following step by step the AFM appropriate checklist. Land as soon as possible: land without delay at the nearest suitable area at which a safe approach and landing is assured. Land as soon as practical: land at the nearest approved landing area where suitable repairs can be made. GENERATOR LIGHT ILLUMINATES (ALT) GENERATOR OFF MASTER OFF GENERATOR ON MASTER ON IF THE PROBLEM PERSISTS GENERATOR OFF NON-VITAL ELECTRIC EQUIPMENT OFF RADIO COMM REDUCE TO MIN. BATTERY IS CAPABLE TO SUPPLY POWER FOR ABOUT 20 MIN. ELECTRICAL FUEL PUMP FAILURE FUEL PUMP OFF FUEL PUMP ON FUEL PRESSURE CHECK IF FUEL PRESSURE DOESN’T BUILD UP LAND AS SOON AS POSSIBLE MONITORING FUEL PRESSURE TECNAM 2002 01 08 2022 rev 1 15 TRIM SYSTEM FAILURE (LOCKED CONTROL) BREAKERS CHECK TRIM SWITCH LH/RH CHECK FOR CORRECT POSITION SPEED ADJUST TO CONTROL AIRCRAFT WITHOUT EXCESSIVE STICK FORCE LAND AIRCRAFT AS SOON AS POSSIBLE RUNAWAY TRIM SWITCH OFF SPEED ADJUST TO CONTROL AIRCRAFT WITHOUT EXCESSIVE STICK FORCE LAND AIRCRAFT AS SOON AS POSSIBLE AIRPLANE EVACUATION PARKING BRAKE ENGAGE SEAT BELTS UNSTRAP COMPLETELY HEADPHONES REMOVE CANOPY OPEN IF CANOPY IS LOCKED OR DOESN’T SLIDE BREAK IT USING THE HAMMER ESCAPE ENGINE SECURING THROTTLE IDLE MAGNETOS OFF FUEL SELECTOR OFF FUEL PUMP OFF GENERATOR OFF TECNAM 2002 01 08 2022 rev 1 16 ENGINE FAILURE DURING TAKE-OFF RUN THROTTLE IDLE RUDDER KEEP HEADING CONTROL BRAKES APPLY AS NEEDED WHEN SAFELY STOPPED MAGNETOS OFF FUEL SELECTOR VALVE OFF FUEL PUMP OFF GENERATOR & MASTER OFF ENGINE FAILURE AFTER TAKE-OFF ALT<200’ AGL SPEED DEPENDING ON FLAPS POSITION V=(69, 66, 55) > 51 FLAPS AS NEEDED AT, OR RIGHT BEFORE TOUCH DOWN MAGNETOS OFF FUEL SELECTOR VALVE OFF FUEL PUMP OFF GENERATOR & MASTER OFF LOW FUEL PRESSURE FUEL PUMP ON FUEL SELECTOR VALVE CHANGE THE FUEL FEEDING TANK FUEL QUANTITY INDICATORS CHECK LAND AS SOON AS POSSIBLE MONITORING FUEL PRESSURE IF ENGINE STOPS FORCED LANDING PROCEDURE TECNAM 2002 01 08 2022 rev 1 17 OIL PRESSURE LIMITS EXCEEDANCE THROTTLE REDUCE POWER AS PRACTICAL OIL PRESS AND OIL TEMP CHECK WITHIN LIMITS LAND AS SOON AS PRACTICAL OIL PRESSURE UNDER THE LOWER LIMIT (0.8 BAR) THROTTLE REDUCE POWER AS PRACTICAL LAND AS SOON AS PRACTICAL IF OIL PRESSURE CONTINUES TO DECREASE LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING PROCEDURE HIGH OIL TEMPERATURE THROTTLE REDUCE POWER AS PRACTICAL AIRSPEED INCREASE LAND AS SOON AS PRACTICAL IF ENGINE ROUGHNESS, VIBRATIONS, ERRATIC BEHAVIOR, OR HIGH CHT /CT IS DETECTED LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING PROCEDURE CHT/CT LIMIT EXCEEDANCE THROTTLE REDUCE POWER AS PRACTICAL LAND AS SOON AS PRACTICAL IF ENGINE ROUGHNESS OR HIGH CHT /CT IS DETECTED LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING PROCEDURE TECNAM 2002 01 08 2022 rev 1 18 IN-FLIGHT ENGINE RESTART SPEED > 69 ALTITUDE < 4000’ CARB. HEAT. AS NEEDED FUEL PUMP ON FUEL QUANTITY CHECK FUEL SELECTOR VALVE CHANGE THE FUEL FEEDING TANK MAGNETOS BOTH MAGNETOS START THROTTLE SET AS REQUIRED IN CASE OF UNSUCCESSFUL ENGINE RESTART ENGINE SECURE LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING PROCEDURE ENGINE FIRE ON THE GROUND FUEL SELECTOR VALVE OFF FUEL PUMP OFF MAGNETOS OFF THROTTLE FULL POWER CABIN HEAT OFF GENERATOR & MASTER OFF PARKING BRAKE ENGAGED EVACUATION IMMEDIATELY TECNAM 2002 01 08 2022 rev 1 19 ENGINE FIRE DURING TAKEOFF BEFORE ROTATION ABORT TAKE OFF THROTTLE LEVER IDLE RUDDER KEEP HEADING CONTROL BRAKES AS REQUIRED FUEL SELECTOR OFF FUEL PUMP OFF MAGNETOS OFF CABIN HEAT OFF GENERATOR & MASTER OFF PARKING BRAKE ENGAGED EVACUATION IMMEDIATELY ENGINE FIRE IN-FLIGHT CABIN HEATING OFF FUEL SELECTOR VALVE OFF FUEL PUMP OFF THROTTLE FULL FORWARD until the engine stops MAGNETOS OFF CABIN VENTS OPEN LAND AS SOON AS POSSIBLE APPLYING FORCED LANDING PROCEDURE TECNAM 2002 01 08 2022 rev 1 20 CABIN FIRE / ELECTRICAL SMOKE IN CABIN DURING FLIGHT CABIN HEATING OFF CABIN VENTS OPEN CANOPY OPEN, IF NECESSARY FIRE EXTINGUISHER USE TOWARDS FLAME BASE IF SMOKE PERSISTS MASTER OFF GENERATOR OFF LAND AS SOON AS POSSIBLE AND EVACUATE THE AIRCRAFT ELECTRICAL SMOKE/FIRE IN CABIN ON THE GROUND GENERATOR OFF THROTTLE IDLE MAGNETOS OFF FUEL SELECTOR VALVE OFF MASTER OFF EVACUATION IMMEDIATELY TECNAM 2002 01 08 2022 rev 1 21 FORCED LANDING WITHOUT ENGINE POWER FLAP UP AIRSPEED 69 PLACE TO LAND FIND A SUITABLE FUEL SELECTOR VALVE OFF FUEL PUMP OFF MAGNETOS OFF SAFETY BELTS TIGHTEN CANOPY LOCKS CHECK LOCKED FLAPS AS NECESSARY GENERATOR & MASTER OFF POWER-ON FORCED LANDING AIRSPEED 69 FLAPS UP PLACE TO LAND FIND A SUITABLE SAFETY BELTS TIGHTEN CANOPY LOCKS CHECK LOCKED BEFORE TOUCH DOWN FLAPS AS NECESSARY FUEL SELECTOR VALVE OFF FUEL PUMP OFF MAGNETOS OFF GENERATOR & MASTER OFF TECNAM 2002 01 08 2022 rev 1 22 LANDING WITH A FLAT NOSE TIRE PRE-LANDING CHECKLIST COMPLETE FLAPS FULL LAND AND MAINTAIN AIRCRAFT NOSE HIGH ATTITUDE AS LONG AS POSSIBLE ENGINE SECURE EVACUATION PERFORM LANDING WITH A FLAT MAIN TIRE PRE-LANDING CHECKLIST COMPLETE FLAPS FULL LAND THE AEROPLANE ON THE SIDE OF RUNWAY OPPOSITE TO THE DEFECTIVE TIRE TOUCHDOWN WITH THE GOOD TIRE FIRST AND HOLD AIRCRAFT WITH THE FLAT TIRE OFF THE GROUND AS LONG AS POSSIBLE ENGINE SECURE EVACUATION PERFORM RECOVERY FROM UNINTENTIONAL SPIN THROTTLE IDLE RUDDER FULL, IN THE OPPOSITE DIRECTION OF THE SPIN STICK CENTRALIZE AND HOLD NEUTRAL AS THE SPIN STOPS RUDDER SET NEUTRAL AEROPLANE ATTITUDE SMOOTHLY RECOVER THROTTLE READJUST TECNAM 2002 01 08 2022 rev 1 23 UNINTENTIONAL FLIGHT INTO ICING CONDITIONS CARB. HEAT ON PITOT HEAT ON IMMEDIATELY FLY AWAY FROM ICING CONDITIONS CONTROLS SURFACES CONTINUE TO MOVE TO MAINTAIN THEIR MOVABILITY PROPELLER SPEED INCREASE RPM CABIN HEAT ON 1 Carburetor heating use only if necessary when rpm idle. Using carburetor heating when rpm at or above 1800 can lead to fuel boiling and engine failure. SERVICE INFORMATION LETTER N° SIL-2017–02