CHECK LIST

SINGLE ALTERNATOR FAILURE ................................................... 44 AVIONICS FAILURES ............................................................................................... 45 LOSS OF AIRSPEED / ALTITUDE / VERTICAL SPEED / HEADING .. 45 DISPLAY FAILURE ........................................................................ 45 ATTITUDE FAILURE IN IMC ......................................................... 45 LANDING GEAR ...................................................................................................... 45 LANDING GEAR UNSAFE WARNING ........................................... 45 MANUAL LANDING GEAR EXTENSION ....................................... 46 MISCELLANOUS ..................................................................................................... 46 UNINTENTIONAL SPIN ................................................................ 46 EMERGENCY DESCENT ............................................................... 47 DITCHING ................................................................................... 47 PITOT HEATING SYSTEM FAILURE .............................................. 48 STATIC PORT FAILURE ................................................................ 48 FLAPS SYSTEM MALFUNCTION .................................................. 48 BEFORE START CHECKLIST ..................................................................................... 50 CHECK LIST F-ORCP TABLE OF CONTENT Page 5 of 50 AFTER START UP CHECK-LIST ................................................................................. 50 BEFORE LINE UP CHECK-LIST ................................................................................. 50 AFTER TAKE-OFF CHECKLIST .................................................................................. 50 CRUISE CHECKLIST ................................................................................................. 50 BEFORE DESCENT CHECKLIST ................................................................................ 50 APPROACH CHECKLIST........................................................................................... 50 BEFORE LANDING CHECKLIST ................................................................................ 50 AFTER LANDING CHECKLIST ................................................................................... 50 CHECK LIST F-ORCP TABLE OF CONTENT Page 6 of 50 PAGE LAISSÉE INTENTIONNELLEMENT BLANCHE CHECK LIST F-ORCP PARAMETERS Page 7 of 50 PARAMETERS AIRSPEED LIMIATIONS KIAS Never Exceed Speed VNE 171 Maximum Structural Cruising Speed VNO 138 Designed Manoeuvring Speed VA 122 Maximum Flaps Extended Speed VFE T/O 122 LDG 93 Maximum Gear Extended Speed VLE 122 Maximum Gear Operating Speed VLO 122 Stall Speed – Clean configuration VS1 66 Stall Speed – Landing configuration VS0 53 Maximum demonstrated cross-wind 17 kts NORMAL OPERATIONS SPEED FLAPS KIAS Best Angle Climb Speed VX 0° (UP) 72 Best Rate of Climb Speed VY 0° (UP) 84 OEI SPEED KIAS Air Minimum Control Speed VMCA 62 OEI Best Rate of Climb Speed VYSE 84 FUEL MASS 2 tanks 100 L each Empty Mass 880 kg Total Fuel 200 L MTOW 1230 kg Total Usable Fuel 194.4 L CHECK LIST F-ORCP PARAMETERS Page 8 of 50 FLIGHT PHASE CONFIGURATION ENGINE PITCH IAS GEAR FLAPS MP RPM ROTATION +5 65 DOWN T/O FULL (~29 inHg) MAX (~2350 RPM) INITIAL CLIMB +7 90 UP T/O FULL MAX CLIMB +7 100 UP UP 28 2200 BEST RATE CLIMB +12 84 UP UP FULL MAX BEST ANGLE CLIMB +14 72 UP UP FULL MAX CRUISE 0 135 UP UP 24 2200 DESCENT (VNO) -2 138 UP UP 23 2200 HOLDING +5 100 UP UP 20 2200 APPROACH +4 90 DOWN T/O 22 2200 FINAL APPROACH APP -2 85 DOWN T/O 16 2200 FINALE APPROACH LDG -3 75 DOWN LDN 20 MAX CHECK LIST F-ORCP NORMAL OPERATIONS Page 9 of 50 NORMAL OPERATI ONS WALK AROUND To perform the aircraft walk-around, carry out the checklists according to the pattern shown in the Figure below. If ignition switches are turned ON, a propeller movement can cause the engine starting with consequent hazard for people nearby Visual inspection is defined as follows: check for defects, cracks, delamination, excessive play, unsafe or improper installation as well as for general condition, presence of foreign objects, slippage markers etc. For control surfaces, visual inspection also involves additional check for freedom of movement. Always check the ground in the area of the aircraft for evidence of fuel, oil or operating fluids leakages CHECK LIST F-ORCP NORMAL OPERATIONS Page 10 of 50 1. Pilot door and cabin Check door for integrity. Turn ON the Master Switch and check Stall Warning switch for operation and condition; check lighting of Landing/Taxi/Nav/Str obe lights, then turn OFF the Master Switch. 2. Left main landing gear Check fuselage skin status, tire status (cuts, bruises, cracks and excessive wear), slippage markers integrity, gear structure and shock absorber, hoses, gear door attachments and gear micro-switches. There should be no sign of hydraulic fluid leakage. 3. Wheel chock Remove if employed 4. Propeller and spinner The propeller blades and spinner should be free of cracks, nicks, dents and other defects and should rotate freely. Check fixing and lack of play between blades and hub. CHECK LIST F-ORCP NORMAL OPERATIONS Page 11 of 50 5. Left engine nacelle a) Perform following inspections: b) Check the surface conditions. c) Nacelle inlets and exhausts openings must be free of obstructions. If inlet and outlet plugs are installed, they should be removed. d) Check radiators. There should be no indication of leakage of fluid and they have to be free of obstructions. e) Only before the first flight of a day: (1) Verify coolant level in the expansion tank, replenish as required up to top (level must be at least 2/3 of the expansion tank). (2) Verify coolant level in the overflow bottle through the slot under the nacelle: level must be between min. and max. mark. CHECK LIST F-ORCP NORMAL OPERATIONS Page 12 of 50 Replenish if required removing the upper cowling; after that, install upper cowling checking for interferences with radiators (3) Turn the propeller by hand to and fro, 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 direction of engine rotation several times and observe engine for odd noises or excessive resistance and normal CHECK LIST F-ORCP NORMAL OPERATIONS Page 13 of 50 compression. f) Check oil level and replenish as required. Prior to oil check, switch off both ignitions circuits and turn the propeller by hand in direction of engine rotation several times to pump oil from the engine into the oil tank. 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. g) Drain off Gascolator for water and sediment (drain until no water comes off). Then make sure drain valve is closed. h) Check drainage hoses clamps i) Verify all parts are fixed or locked. j) Verify all inspection doors are closed. 6. Air induction system Check engine air inlet for integrity and CHECK LIST F-ORCP NORMAL OPERATIONS Page 14 of 50 correct fixing. The air intake filter must be free of obstructions. 7. Left fuel tank Check that the refuelling port cap is properly secured, then perform the fuel tank sump drainage operating the related valve which, after operation, must be checked closed. Fuel must checked for water and sediment. Verify the tank vent outlet is clear. 8. Landing and taxi lights Visual inspection 9. Left wing leading edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip. 10. Left wing top and bottom panels Visual inspection 11. Left winglet, nav and strobe lights; static discharge wick Check for integrity and fixing 12. Left aileron and balance mass Visual inspection, remove tie-down CHECK LIST F-ORCP NORMAL OPERATIONS Page 15 of 50 devices and control locks if employed. 13. Left flap and hinges Visual inspection 14. Left static port Remove protective cap – Visual inspection 15. Antennas Check for integrity 16. Gear pump, external power and battery compartment Check emergency landing gear extension system pressure (low pressure limit: 20 bar), external power and battery compartments closure. 17. Horizontal and vertical empennage and tabs. Static discharge wicks. Check the actuating mechanism of control surfaces and the connection with related tabs. Check wicks for integrity. Remove tie-down device if employed. 18. Stabilator leading edge Check for integrity 19. Fuselage top and bottom skin Visual inspection 20. Right static port Remove protective cap – Visual inspection 21. Right flap and hinges Visual inspection CHECK LIST F-ORCP NORMAL OPERATIONS Page 16 of 50 22. Right aileron and balance mass Visual inspection, remove tie-down devices and control locks if employed 23. Right winglet, nav and strobe lights: static discharge wicks Check for integrity and fixing and lighting 24. Right wing top and bottom panels Visual inspection 25. Right wing leading edge Visual inspection. Check cabin ventilation inlet and carburettor heating inlet for condition and free of obstruction. Check stall strip. 26. Right fuel tank Check that the refuelling port cap is properly secured, then perform the fuel tank sump drainage operating the related valve which, after operation, must be checked closed. Fuel must checked for water and sediment. Verify the tank vent outlet is clear. 27. Propeller and spinner The propeller blades and spinner should be free of cracks, nicks, dents and other CHECK LIST F-ORCP NORMAL OPERATIONS Page 17 of 50 defects and should rotate freely. Check fixing and lack of play between blades and hub. 28. Right engine nacelle Apply check procedure reported in the walk- around station 5 and 6. 29. Passenger door and cabin Check door for integrity. Check safety belts for integrity and baggage for correct positioning and fastening. Check ditching emergency exit safety lock. Check passengers ventilation ports for proper setting. 30. Right main landing gear Apply check procedure reported in the walk- around Station 2 31. Wheel chock Remove if employed 32. Bottom fuselage antennas Check for integrity 33. Right cabin ram-air inlet Visual inspection 34. Right Pitot tube Remove protective cap and check for any obstruction 35. Nose landing gear Check tire status CHECK LIST F-ORCP NORMAL OPERATIONS Page 18 of 50 (cuts, bruises, cracks and excessive wear),slippage markers integrity, gear structure and retraction mechanism, shock absorber and gear doors attachments. There should be no sign of hydraulic fluid leakage. 36. Radome Check for integrity 37. Radome access door Visual inspection 38. Left Pitot tube Remove protective cap and check for any obstruction CHECK LIST F-ORCP NORMAL OPERATIONS Page 19 of 50 COCKPIT PREPARATION ACTIONS AIRCRAFT DOCUMENTS ................ CHECK, ON BOARD SEAT ................................................................. ADUST SEAT BELT ....................................................... FASTEN DOORS ...................................... CLOSED AND LOCKED ENGINE STARTING BATTERY VOLTMETER.........CHECK 12 TO 14 VOLT PARKING BRAKE .....................................................SET ALTERNATE STATIC PORT .................... CHECK CLOSED ALL EXTERNAL LIGHTS SWITCHES .......................... OFF FLAPS LEVER ........................................................... UP PROPELLER .................................................. MAX RPM CARBURATOR HEAT (2) ........................................ OFF POWER LEVER ...................................................... IDLE ENGINE LEVERS FRICTION ............................... ADJUST AVIONIC/CROSSBUS/FIELD SWITCHES .................. OFF GEAR LEVER ..................................................... DOWN EMERGENCY BACK BATTERY SWITCH ........... SECURED ELT ........................................................... CHECK ARM CABIN HEAT .......................................................... OFF RH FUEL SELECTOR............................................ RIGHT LH FUEL SELECTOR ............................................... LEFT IGNITION SWITCHES.............................................. OFF BREAKERS ......................................................... ALL IN CHECK LIST F-ORCP NORMAL OPERATIONS Page 20 of 50 BEFORE START ACTIONS MASTER SWITCH .................................................... ON DEPARTURE BRIEFING ............................. PERFORMED STROBE .................................................................. ON FUEL QUANTITY ................................................ CHECK FUEL PUMP .......................................... ON, THEN OFF ➔ Check normal fuel pressure gauge operation, and return to zero FIRE DETECTOR SYSTEM .................................... CHECK CHECK LIST F-ORCP NORMAL OPERATIONS Page 21 of 50 BEFORE START CHECKLIST 1. DEPARTURE BRIEFING ......................... PERFORMED 2. PARKING BRAKE ................................................ SET 3. MASTER SWITCH ................................................ ON 4. STROBE .............................................................. ON 5. POWER LEVER .................................................. IDLE 6. DOORS ....................................... CLOSED & LOCKED RIGHT ENGINE START UP RH CHOKE ............................................ AS NECESSARY RH FUEL PUMP ....................................................... ON RH IGNITION SWITCHES (2 ..................................... ON RH OUTSIDE SAFETY .......................................... CHECK RIGHT ENGINE START PUSHBUTTON .............. ENGAGE ➔ Do not engage starter for more than 10 seconds RH CHOKE ............................................................. OFF RIGHT ENGINE OIL PRESSURE.............. CHECK, > 2 BAR RH THROTTLE LEVER ................................... 1200 RPM ➔ When power is low, RPM are controlled through manifold pressure lever RH FIELD................................................................. ON RH AVIONICS .......................................................... ON RH CROSS BUS........................................................ ON RH AMMETER......................................CHECK CHARGE CHECK LIST F-ORCP NORMAL OPERATIONS Page 22 of 50 LEFT ENGINE START UP LH CHOKE ............................................. AS NECESSARY LH FUEL PUMP ....................................................... ON LH IGNITION SWITCHES (2) .................................... ON LH OUTSIDE SAFETY .......................................... CHECK LEFT ENGINE START PUSHBUTTON ................ ENGAGE ➔ Do not engage starter for more than 10 seconds LH CHOKE .............................................................. OFF LEFT ENGINE OIL PRESSURE ................ CHECK, > 2 BAR LH THROTTLE LEVER .................................... 1200 RPM ➔ When power is low, RPM are controlled through manifold pressure lever LH FIELD ................................................................. ON LH AVIONICS .......................................................... ON LH CROSS BUS ........................................................ ON LH AMMETER ................................................. CHECK CHARGE ➔ Charge should be shared evenly between the two alternators CHECK LIST F-ORCP NORMAL OPERATIONS Page 23 of 50 AFTER START UP ACTIONS XPDR ................................................................... STBY FMS - RADIO/RADIONAV/PROCEDURE ...................SET ATIS/DEPARTURE PARAMETERS ..................OBTAINED NAV LIGHTS............................................................ ON FUEL PUMPS ......................................................... OFF ALTIMETERS ...........................................................SET ELECTRICAL TRIM ............ CHECK RANGE AND DISCONNECTION AUTO PILOT ..................................... CHECK THEN OFF FLIGHT CONTROLS .............................................. FREE FLAPS ................................................. CHECK THEN UP AFTER START UP CHECK-LIST 1. ENGINE OIL PRESSURE...................................CHECK 2. AVIONICS / FIELD / CROSS BUS ........................... ON 3. FMS (RADIO/RADIONAV/PROCEDURE)...............SET 4. ALTIMETERS .......................................................SET 5. FLIGHT CONTROLS ........................................... FREE 6. FLAPS ..................................................................UP 7. FUEL PUMPS...................................................... OFF CHECK LIST F-ORCP NORMAL OPERATIONS Page 24 of 50 TAXIING ACTIONS BLOCK TIME ............................................... REPORTED TAXI LIGHT ............................................................. ON PARKING BRAKE ............................................. RELEASE BRAKES.............................................................. CHECK ➔ Test right seat braking action if occupied INSTRUMENTS & AHRS........ CHECKED DURING TURNS ENGINE RUN-UP PARKING BRAKE .....................................................SET TAXI LIGHT ............................................................ OFF OIL TEMPERATURE ............................................ CHECK FUEL PUMPS .......................................................... ON RPM ............................................................ 1650 RPM ➔ Perform engine run-up on both engines at the same time PROPELLER .........................................FEATHER CHECK ➔ Go swiftly from max RPM to feather position then go back to max RPM, one handle at a time, do not drop more than 400 RPM. ➔ Repeat 3 times for each engine. IGNITION SWITCHES .......................................... CHECK CHECK LIST F-ORCP NORMAL OPERATIONS Page 25 of 50 ➔ Perform check one ignition switch at a time. Check loss of RPM < 130 RPM and maximum in between < 50 RPM CARBURATORS HEAT......................................... CHECK ➔ Check loss of RPM of about 100 RPM and returning to normal AMMETER ......................................................... CHECK POWER LEVERS .................................................... IDLE ➔ Check idle position > 750 RPM RPM ............................................................ 1200 RPM BEFORE LINE UP ACTIONS LANDING LIGHT ...................................................... ON TRIMS..................................................... SET NEUTRAL HEADING AND ALTITUDE BUG.............. AS NECESSARY FLAPS .................................................................... T/O TAKE OFF BRIEFING ................................. PERFORMED CHECK LIST F-ORCP NORMAL OPERATIONS Page 26 of 50 BEFORE LINE UP CHECKLIST 1. ENGINE RUN UP .............................. PERFORMED 2. TAKE OFF BRIEFING ......................... PERFORMED 3. FLAPS ............................................................ T/O 4. FUEL PUMPS................................................... ON 4. RIGHT ENGINE FUEL SELECTOR . RIGHT POSITION 5. LEFT ENGINE FUEL SELECTOR ....... LEFT POSITION 6. PROPELLERS ........................................ MAX RPM 7. TRIMS ................................................... NEUTRAL 8. XPDR ............................................................. ALT LINE-UP ACTIONS QFU AND HEADING ........................................... CHECK PITOT HEAT .......................................... AS NECESSARY CAS ALARM ........................................... CHECK GREEN CHECK LIST F-ORCP NORMAL OPERATIONS Page 27 of 50 TAKE-OFF TAKE OFF TIME ....................................... ANNOUNCED MAP 20 Hg THEN BRAKE RELEASED POWER.................................................................FULL ➔ Check ~ 29 Hg, 2350 RPM ENGINE PARAMETERS ....................................... CHECK SPEED .............................................. ALIVE AND CHECK ANNUNCIATOR PANEL ...................................... CHECK ROTATION SPEED ................................................ 65 kt ➔ Wait for positive climb then LANDING GEAR ....................................................... UP AFTER TAKE-OFF ACTIONS ➔ Wait upon reaching ASD (min. 400 ft AGL) then FLAPS ...................................................................... UP FUEL PUMPS ......................................................... OFF LIGHTS (TAXI & LANDING) .................................... OFF ELECTRICAL FAN………………………………………………….OFF CLIMB POWER ........................................................SET ➔ Manifold pressure : 28 Hg, RPM : 2200 RPM CHECK LIST F-ORCP NORMAL OPERATIONS Page 28 of 50 AFTER TAKE-OFF CHECKLIST 1. LANDING GEAR..................................... UP, LOCKED 2. FLAPS ..................................................................UP 3. CLIMB POWER (MAP & RPM) .............................SET 4. LIGHTS (TAXI & LANDING) ................................ OFF 5. ELECTRICAL FAN………………………………………………OFF 6. FUEL PUMPS...................................................... OFF CLIMB ACTIONS ALTIMETERS ...................................... SET, COMPARED ENGINE POWER .............................................. ADJUST CRUISE ACTIONS CRUISE POWER ......................................................SET ➔ See cruise performance table for correct manifold pressure and RPM settings ENGINE PARAMETERS ....................................... CHECK CHECK LIST F-ORCP NORMAL OPERATIONS Page 29 of 50 CRUISE CHECKLIST 1. CRUISE POWER...................................................SET 2. ENGINE PARAMETERS ...................................CHECK BEFORE DESCENT ACTIONS LANDING PARAMETERS...............................OBTAINED FMS (RADIO/RADIONAV/PROCEDURE) ..................SET ARRIVAL BRIEFING .................................. PERFORMED BEFORE DESCENT CHECKLIST 1. FMS (RADIO/RADIONAV/PROCEDURE) ................... SET 2. ARRIVAL BRIEFING............................... PERFORMED APPROACH ACTIONS ALTIMETERS ...................................... SET, COMPARED APPROACH CHECKLIST 1. ALTIMETERS .................................. SET, COMPARED 2.TAXI LIGHT .......................................................... ON CHECK LIST F-ORCP NORMAL OPERATIONS Page 30 of 50 BEFORE LANDING ACTIONS FLAPS ............................................................ TO/APPR FUEL PUMP ............................................................ ON LANDING GEAR ................................................ DOWN LANDING LIGHTS .................................................... ON FLAPS .................................................................... LDG PROPELLERS ................................................ MAX RPM AUTO PILOT........................................................... OFF BEFORE LANDING CHECKLIST 1. LANDING GEAR ......................... DOWN, THREE GREENS 2. FLAPS ................................................. AS REQUIRED 3. PROPELLERS ............................................ MAX RPM 4. FUEL PUMPS....................................................... ON 5. LANDING LIGHTS ................................................ ON 6. AUTO PILOT ....................................................... OFF AFTER LANDING ACTIONS FLAPS ...................................................................... UP LANDING LIGHTS ................................................... OFF FUEL PUMPS ......................................................... OFF XPDR ................................................................... STBY TAXI LIGHT ............................................................. ON CHECK LIST F-ORCP NORMAL OPERATIONS Page 31 of 50 AFTER LANDING CHECKLIST 1. FLAPS ..................................................................UP 2. LANDING LIGHTS ............................................... OFF 3. FUEL PUMPS...................................................... OFF 4. XPDR ............................................................... STBY APRON CHECKLIST 1. PARKING BRAKE ................................................SET 2. TAXI & NAV LIGHT ............................................ OFF 3. AP .................................................................... OFF 4.ELECTRICAL ...................................................... OFF 5.FLIGHT TIME & ENGINE HOURS................ CHECKED 6. AVIONICS (RH AND LH) .................................... OFF 7. CROSS BUS (RH AND LH) .................................. OFF 8. FIELD (RH AND LH) .......................................... OFF 9. THROTTLE LEVERS ........................................... IDLE ➔ Allow one minute for engine cooldown if necessary 10. IGNITION SWITCHES (RIGHT THEN LEFT) ........ OFF ➔ Turn off one at a time 11. STROBE .......................................................... OFF 12. MASTER SWITCH ............................................ OFF CHECK LIST F-ORCP NORMAL OPERATIONS Page 32 of 50 CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 33 of 50 EMERGEN CY P ROCEDU RES EMERGENCY AIRSPEEDS OEI SPEED KIAS Air Minimum Control Speed VMCA 62 OEI Best Rate of Climb Speed VYSE 84 ENGINE FAILURES ENGINE FIRE / FAILURE BEFORE V1 POWER LEVER ..................................................................... IDLE BRAKES .......................................................................... APPLIED ➔ Maintain runway axis FUEL SELECTORS ................................................................... OFF IGNITION SWITCHES ............................................................. OFF BATTERY ............................................................................... OFF ➔ Evacuate aircraft as necessary CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 34 of 50 ENGINE FIRE / FAILURE AFTER V1 AP ........................................................................................ DISC POWER ................................................................................FULL LANDING GEAR ....................................................................... UP FLAPS ...................................................................................... UP ➔ Identify dead engine (dead foot, dead engine). It is designed engine X. (X being either RIGHT or LEFT) X ENGINE POWER ................................................................ IDLE ➔ Check nothing happens X ENGINE PROPELLER ................................................... FEATHER ➔ Check feather ➔ Reach and climb to 84 kt (blue line) OPERATING ENGINE POWER ......................................ADJUSTED TRIMS ....................................................................................SET X ENGINE FIELD .................................................................... OFF X ENGINE FUEL SELECTOR .................................................... OFF X ENGINE IGNITION SWITCHES ............................................ OFF X ENGINE FUEL PUMP .......................................................... OFF OPERATING ENGINE FUEL SELECTOR ....... CROSSFEED AS NECESSARY LAND AS SOON AS POSSIBLE USE « ONE ENGINE INOPERATIVE APPROACH » CHECKLIST PAGE 41 CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 35 of 50 ENGINE FIRE / FAILURE IN FLIGHT AP ........................................................................................ DISC POWER ................................................................................FULL LANDING GEAR ....................................................................... UP FLAPS ...................................................................................... UP ➔ Identify dead engine (dead foot, dead engine). It is designed engine X. (X being either RIGHT or LEFT) X ENGINE POWER ................................................................ IDLE ➔ Check nothing happens X ENGINE PROPELLER ................................................... FEATHER ➔ Check feather ➔ Reach and climb to 84 kt (blue line) OPERATING ENGINE POWER ......................................ADJUSTED TRIMS ....................................................................................SET X ENGINE FIELD .................................................................... OFF X ENGINE FUEL SELECTOR .................................................... OFF X ENGINE IGNITION SWITCHES ............................................ OFF X ENGINE FUEL PUMP .......................................................... OFF OPERATING ENGINE FUEL SELECTOR ....... CROSSFEED AS NECESSARY LAND AS SOON AS POSSIBLE USE « ONE ENGINE INOPERATIVE APPROACH » CHECKLIST PAGE 41 CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 36 of 50 PROPELLER OVERSPEEDING X ENGINE POWER LEVER ............................................... REDUCE X ENGINE PROPELLER ............................ REDUCE AS PRACTICAL IF UNSUCCESSFUL APPLY “ENGINE SECURING” PAGE 37 ENGINE FIRE / FAILURE ON FINAL AP ....................................................................................... DISC POWER ...................................................................... ADJUSTED FLAPS ................................................................................... APP ➔ Identify dead engine (dead foot, dead engine). It is designed engine X. (X being either RIGHT or LEFT) X ENGINE POWER ................................................................IDLE ➔ Check nothing happens X ENGINE PROPELLER .................................................. FEATHER ➔ Check feather PROCEED FOR SAFE LANDING IF STABLIZED, OR PERFORM ONE ENGINE INOPERATIVE GOING AROUND PROCEDURE CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 37 of 50 ENGINE SECURING OPERATING ENGINE POWER ...................................... ADJUSTED LANDING GEAR ....................................................................... UP FLAPS ...................................................................................... UP X ENGINE POWER LEVER ......................................................IDLE X ENGINE IGNITION SWITCHES ............................................ OFF X ENGINE PROPELLER ................................................... FEATHER ➔ Check feather X ENGINE FUEL PUMP .......................................................... OFF X ENGINE FIELD .................................................................... OFF X ENGINE FUEL SELECTOR .................................................... OFF OPERATING ENGINE FUEL SELECTOR ........CROSSFEED AS NECESSARY CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 38 of 50 INFLIGHT ENGINE RESTART CARBURATOR HEAT .............................................. AS REQUIRED X ENGINE ELECTRICAL FUEL PUMP .......................................ON FUEL SELECTORS ............................................................... CHECK X ENGINE FIELD ................................................................... OFF X ENGINE IGNITION SWITCHES ..............................................ON X ENGINE POWER LEVER ......................................................IDLE X ENGINE PROPELLER ........................................ FULL FORWARD X ENGINE STARTER ..................................................... ENGAGED ➔ Stay idle while engine is warming up X ENGINE FIELD ......................................................................ON If engine restart is unsuccessful : EMERGENCY BATTERY SWITCH .............................................ON ➔ Repeat engine restart procedure IF ENGINE RESTART IS STILL UNSUCCESSFUL APPLY ENGINE SECURING PROCEDURE AND USE ONE ENGINE INOPERATIVE APPROACH CHECKLIST PAGE 41 CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 39 of 50 LOW FUEL PRESSURE FUEL QUANTITY INDICATOR ............................................. CHECK If a fuel leakage can be excluded: FUEL PUMP .............................................................................ON FUEL SELECTOR................................. CONSIDER CROSSFEEDING If a fuel leakage is suspected: APPLY “ENGINE SECURING” PROCEDURE PAGE 37 ON AFFECTED ENGINE, AND DO NOT CROSSFEED LOW OIL PRESSURE POWER (AFFECTED ENGINE) ...............................................IDLE OIL TEMPERATURE ........................................................... CHECK IF OIL TEMPERATURE IS RISING APPLY « ENGINE SECURING» PROCEDURE PAGE 37 EXCESSIVE OIL TEMPERATURE POWER (AFFECTED ENGINE) ...............................................IDLE OIL PRESSURE ................................................................... CHECK IF OIL PRESSURE IS UNDER ACCEPTABLE APPLY « ENGINE SECURING» PROCEDURE PAGE 37 CHECK LIST F-ORCP EMERGENCY PROCEDURES Page 40 of 50 EXCESSIVE CHT POWER (AFFECTED ENGINE) .........................................REDUCE AIRSPEED ............................................. INCREASE AS PRACTICAL OIL TEMPERATURE ........................................................... CHECK IF CHT IS STILL RISING APPLY « ENGINE SECURING» PROCEDURE PAGE 37 COOLANT LIQUID LOW LEVEL CHT (AFFECTED ENGINE) ................................................. CHECK If CHT is above 135 °C: POWER (AFFECTED ENGINE) .........................................REDUCE AIRSPEED ............................................. INCREASE AS PRACTICAL OIL TEMPERATURE ........................................................... CHECK IF CHT IS STILL RISING APPLY « ENGINE SECURING» PROCEDURE PAGE 37