OY /2 BEFORE TAKE-OFF CHECKLIST - 06/06/2015 CLOSED AND LOCKED FREE MOVEMENT SET IDLE MASTER SWITCH CARBURETTOR PRE-HEATING OFF MAGNETO SWITCHES
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1 BEFORE TAKE- CHECKLIST - 06/06/2015 OY /2 PARACHUTE SYSTEM UNLOCKED DOORS AND LOCKED PITOT TUBE PLUG REMOVED TRIM NEUTRAL FLIGHT CTROLS FREE MOVEMENT FREE MOVEMENT SET IDLE BRAKE SET FOR PARK OPEN FUEL CTENT SUFFICIENT MASTER SWITCH CARBURETTOR PRE-HEATING CHOKE SET AS REQ. PROPELLER CLEAR START ENGINE APROX RPM OIL PRESURE MIN / MAX 0.8 BAR / 7.0 BAR BATTERY CHARGING ELECTRIC INSTRUMENTS ALTIMETER SET QNH / QFE OIL TEMP MIN 50 CELCIUS CHECK MAGNETO DROP < 300 RPM@ 4000 RPM CHECK MAX RPM MAX 5200 RPM ELECTRIC FUEL PUMP COWLING FLAP SET AS REQ. WIND DIRECTI? CHECK WINDSOCK RUNWAY AND APPROACH CLEAR FLAPS FREE MOVEMENT & SET POSITI 2
2 TAKE- PROCEDURE - 17/07/2014 OY /2 FULL FORWARD PULL THE STICK SLIGHTLY BACK NOSE WHEEL LIFT APPROX. 27 kts (50 km/h) ACCELERATE NOSE WHEEL UP (5-10cm) THE GROUND THE AIRCRAFT WILL TAKE- AT 38 kts (70km/h) STICK FORWARD TO 59 kts (110 km/h) IN SHALLOW CLIMB CTINUE CLIMB AT 59 kts (110 km/h) RETRACT FLAPS AT APPROX. 500 ft AND REDUCE RPM ENGINE TEMPS AND PRESSURES WITHIN LIMITS ELECTICAL FUEL PUMP TRIM AIRCRAFT TO 59 kts (110 km/h) CTINUE CLIMB COWLING FLAP SET AS REQ.
3 LIMITATIS AND PERFORMANCE - 17/07/2014 OY-9457 VA (MANEUVERING SPEED) - (YELLOW LINE) VB (TURBULENT AIR) VC (CRUISE SPEED) VC (ECO CRUISE SPEED) VNE (NEVER EXCEED) 80 kts (148 km/h) 97 kts (180 km/h) 92 kts (170 RPM 75 kts (140 km/h) 116 kts (216 km/h) MAX CROSSWIND SPEED 16 kts (8 m/s) STRUCTURE LIMITATIS +4 / -2 VX (BEST ANGLE OF CLIMB) - (YELLOW TRIANGLE) VY BEST RATE OF CLIMB (TO CLEAR OBSTACLE) TAKE DISTANCE TAKE- TO CLEAR 50 ft (15m) LANDING DISTANCE Vs1 (STALL FLAP 1) Vs2 (STALL FLAP 2) Vs0 (STALL FLAP 3) VFE (MAX SPEED FLAP 2) VFE (MAX SPEED FLAP 3) 51 kts (95 km/h) 49 kts (90 km/h) 80 M 215 M 150 M 40 kts (75 km/h) 38 kts (70 km/h) 35 kts (65 km/h) 63 kts (116 km/h) 57 kts (105 km/h) MINIMUM SINK RATE (400 ft/min) 46 kts (85 km/h) FLAP 2 BEST GLIDE ANGLE 51 kts (95 km/h) FLAP 1 ROTAX TAKE- (5 MIN) ROTAX MAX CTINUES POWER ROTAX 75 % ROTAX 65 % ROTAX 55% OIL TEMP MIN / MAX OIL TEMP OPTIMAL OIL PRESSURE MIN / MAX OIL PRESSURE NORMAL CYLINDER HEAD TEMP (CHT) MAX CYLINDER HEAD TEMP (CHT) OPTIMAL FUEL CSUMPIT RPM RPM RPM RPM RPM CELCIUS CELCIUS 0.8 BAR / 7.0 BAR 2-5 BAR 135 CELCIUS 110 CELCIUS RPM
4 LANDING - 17/07/2014 OY-9457 TRIM ELECTRIC FUEL PUMP REDUCE SPEED AND SET FLAP 3 OR WITH FLAP 2 FLAP 2 KEEP SPEED FLAP 3 KEEP SPEED TOUCH DOWN SPEED (STALL) ELECTRIC FUEL PUMP ENGINE COOL DOWN ELECTRIC INSTRUMENTS MAIN POWER SWITCHES PARACHUTE SYSTEM WRITE LOG BOOK CLEAN AIRCRAFT SET FOR LANDING kts ( km/h) kts ( km/h) 58 kts (110 km/h) 48 kts (90 km/h) 38 kts (70 km/h) LY AT INCREASED TEMPS LOCKED
5 EMERGENCY CHECKLIST - 17/07/2014 OY /2 AVIATE - NAVIGATE - COMMUNICATE LOSS OF ENGINE POWER DURING TAKE LOWER NOSE AND TRIM TO GLIDING SPEED 54 kts (100 km/h) FLAP1 DO NOT RETURN TO AIRFIELD IF ALTITUDE IS BELOW 260 ft (80 m) LOOK FOR SUITABLE LANDING FIELD LAND INTO WIND IF POSSIBLE LOSS OF ENGINE POWER DURING FLIGHT / RESTART LOWER NOSE AND TRIM TO GLIDING SPEED 54 kts (100 km/h) FLAP1 / 48kts (90km/h) FLAP2 LOOK FOR SUITABLE LANDING FIELD LAND INTO WIND IF POSSIBLE MASTER SWITCH OPEN FUEL SUFFICIENT ELECTICAL FUEL PUMP 1/4 OPEN START ENGINE AIRSPEED TO WINDMILL THE PROP CAN HELP DECLARE EMERGENCY TRANSPDER SET 7700 CALL RADIO: PAN-PAN OR MAYDAY LOOK FOR SUITABLE LANDING FIELD REDUCE SPEED AND SET FLAP 3 OR WITH FLAP 2 FLAP 2 KEEP SPEED FLAP 3 KEEP SPEED TOUCH DOWN SPEED (STALL) EMERGENCY LANDING LAND INTO WIND IF POSSIBLE kts ( km/h) kts ( km/h) 58 kts (110 km/h) 48 kts (90 km/h) 38 kts (70 km/h)
6 EMERGENCY CHECKLIST - 17/07/2014 OY /2 AVIATE - NAVIGATE - COMMUNICATE CARBURETTOR FIRE ELECTICAL FUEL PUMP FULL (TO BURN THE REMAINING FUEL FAST) CABIN HEAT AND AIR SIDESLIP LAND IMMEDIATELY! LAND AS SO AS PRACTICAL LOSS OF OIL PRESSURE PREPARE FOR IMMINENT ENGINE FAILURE CARBURATTOR ICE / ENGINE RUNNING ROUGH RPM DROP APROX WITH SMALL REDUTI IN POWER IF RPM INCREASE WITHIN 1-2 MINUTES Carburettor icing was likely to have been occuring and the carburettor heat control should be left on for the remainder of the flight. Use of the carburettor heat control at other times is not recommended. TO DEPLOY THE PARACHUTE MINIMUM SAFE ALTITUDE 660 FEET PULL HANDLE FIRMLY ABOUT 25 MM PROTECT FACE AND BODY WITH YOUR ARMS PRESS INTO SEAT BY EXTENDING YOUR LEGS Dulfu havari undersøgelses gruppe: Niels Gregersen Philip Nathansen Nattergalevej 33 Fridtjof Nansensvej Galten 8200 Århus N Tlf Tlf Mobil: Mobil John Carlsen Edvard Braae Østre Parkvej 5A Vedelsvej Ringsted 6760 Ribe Tlf/Fax: Tlf/Fax: Mobil: Mobil: Lars Severinsen Ternevej Aalborg Tlf Mobil: Øvrige: Naviair briefing DMIs flyvemeteorologiske kontor Havarikommissionen / AkutTelefonen (syg uden for din egen læges åbningstid) 1813
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