Check-list DA-20 RAS - bun

REGIONAL AIR SERVICES

CHECKLIST DIAMOND DA20KATANA

NOVEMBER 2009

PREFLIGHT INSPECTIONIn-cabin Check

1. Structural Temperature Indicator.............If +38°C2. Airplane Documents...............................On Board3. Flight Control Lock................................Removed4. Flight Controls.............................................Check5. Ignition Key...........................................Pulled out6. Carburetor heat...............................Check free, off7. Cabin heat.............................................Check free8. Choke............................Check Free, self-resetting9. Parking brake........................................Check free10. Throttle.........................................Check free, idle11. Propeller.............................Check free, max.RPM12. Master Switch....................................................On13. Warning Lights....................................Illuminated14. Fuel Quantity..........................................Sufficient15. Engine gauges, Ammeter& Voltmeter.........Check16. Circuit Breakers.....................................Pressed in17. Map Light............................................Operational18. Instrument Lights................................Operational19. Trim............................................................Neutral20. Wing Flaps.......................Extend and retract fully21. Trim & Flap Indicator Lights..............Operational22. Exterior Lights....................................Operational23. Master Switch...................................................Off24. Foreign Object Inspection.............................Done25. ELT......................................................Arm or Off26. Fire Extinguisher..........................................Check27. Baggage...................................................Attached28. Canopy..........................................................Clean

PREFLIGHT INSPECTIONWalk around Inspection

Left Main Landing Gear

1. Landing Gear Strut......................visual inspection2. Wheel Fairing..............................visual inspection3. Tire Pressure (33 psi / 2.3 bar)......................check4. Tire, Wheel, Brake......................visual inspection5. Wheel Chocks............................................remove

Left Wing

1. Entire Wing.................................visual inspection2. Stall Warning..................check (suck on opening)3. Pitot-Static Probe........................clean, holes open4. Tie down....................................................remove5. Taxi and Landing Lights.............visual inspection6. Wing Tip, Posit. & Strobe...........visual inspection7. Aileron Balancing Weight..........visual inspection8. Aileron incl. Inspection Panel.....visual inspection

9. Flap incl. Inspection Panel.......visual inspection

Fuselage

1. Skin..........................................visual inspection2. Tank...................................................vent check3. Tank Drain........................................drain water4. Fuel Quantity...........................visual inspection5. Antennas..................................visual inspection

Empennage

1. Stabil. and Control Surfaces. . .Visual inspection2. Tie down.................................................remove3. Trim Tabs.................................visual inspection

Right Wing

1. Entire Wing..............................visual inspection2. Flap incl. Inspection Panel.......visual inspection3. Aileron incl. Inspection Panel..visual inspection4. Aileron Balancing Weight.......visual inspection5. Wing Tip, Posit. & Strobe.......visual inspection6. Tie Down................................................remove

Right Main Landing Gear

1. Landing Gear Strut...................visual inspection2. Wheel Fairing..........................visual inspection3. Tire Pressure (33 psi / 2.3 bar)..................check4. Tire, Wheel, Brake...................visual inspection5. Wheel Chocks.........................................remove

Nose

1. Oil.....................................................check level2. Coolant..............................................check level3. Cowling....................................visual inspection4. Air Intakes (seven)........................................free5. Propeller...................................visual inspection6. Propeller Blades.................perform Pitch Check7. Spinner.....................................visual inspection8. Nose Gear................................visual inspection9. Wheel Fairing..........................visual inspection10. Tire Pressure (26 psi / 1.8 bar)..................check11. Tire and Wheel.........................visual inspection12. Wheel Chocks.........................................remove

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NOVEMBER 2009

BEFORE STARTING ENGINE

1. PREFLIGHT INSPECTION..........PERFORMED2. PEDALS.....................................ADJUST, LOCK3. PASSENGER BRIEFING.............PERFORMED4. SAFETY BELTS....................................FASTEN5. PARKING BRAKE........................................SET6. CONTROLS.................................................FREE7. FUEL SHUT-OFF VALVE.........................OPEN8. CARBURETOR HEAT..................................OFF9. THROTTLE..................................................IDLE10. PROPELLER......................................MAX.RPM11. FRICTION OF THROTTLE...................ADJUST12. AVIONICS MASTER SWITCH....................OFF13. MASTER SWITCH.........................................ON14. GEN. WARNING LIGHT..........ILLUMINATED15. FUEL PRESS WARNING L......ILLUMINATED16. EXTERIOR LIGHTS......................................A/R17. INSTRUMENT PANEL LIGHTING.............A/R18. CANOPY.........................CLOSE AND SECURE19. CANOPY WARNING LIGHT.......................OFF

STARTING ENGINE

1. FUEL PUMP....................................................ON2. FUEL PRESSURE WARNING LIGHT........OFF3. THROTTLE - COLD START......................IDLE4. THROTTLE - WARM ENGINE...................2CM5. CHOKE - COLD START..........ON AND HOLD6. CHOKE – WARM ENGINE..........................OFF7. TOE BRAKES............................................HOLD8. PROPELLER AREA................................CLEAR9. IGNITION KEY........................................START10. CHOKE..........................................................OFF11. THROTTLE..............................MAX. 1500 RPM12. OIL PRESSURE.................GREEN RANGE/10”13. GENERATOR WARNING LIGHT...............OFF14. EXTERIOR LIGHTS......................................A/R15. FUEL PUMP..................................................OFF

BEFORE TAXIING

1. AVIONICS MASTER......................................ON2. INSTR.&AVIONICS......................................SET3. ENGINE GAUGES..................................CHECK4. VOLTMETER..........................................CHECK5. WARNING LIGHTS..................PUSH TO TEST6. PARKING BRAKE..............................RELEASE

TAXIING

1. BRAKE.....................................................CHECK2. DIRECTION CONTROL.........................CHECK

3. INSTRUMENTS AND AVIONICS.......CHECK4. COMPASS..............................................CHECK

BEFORE TAKE-OFF (ENGINE RUN UP)

1. TOE BRAKES..........................................HOLD2. SAFETY BELTS.............................FASTENED3. CANOPY...........................CLOSED&LOCKED4. FUEL PRESS. WARNING L.........CHECK OFF5. FUEL SHUT-OFF VALVE........CHECK OPEN6. FUEL QUANTITY.................................CHECK7. ENGINE GAUGES..................GREEN RANGE8. TRIM.................................................NEUTRAL9. CONTROLS...............................................FREE10. THROTTLE........................................4000 RPM11. PROPPELLER LEVER..........CYCLE 3 TIMES12. MAGNETOS..........................................CHECK13. THROTTLE........................................1500 RPM14. CARBURETOR HEAT..................................ON15. THROTTLE................................................IDLE16. CARBURETOR HEAT................................OFF17. CIRCUIT BREAKERS.............CHECK ALL IN18. FUEL PUMP..................................................ON19. WING FLAPS................................................T/O20. PARKING BRAKE.....................RELEASE

BEFORE TAKE OFF

1. FUEL PUMP....................................CHECK ON2. MASTER SWITCH.........................CHECK ON3. IGNITION SWITCH..................CHECK BOTH4. CARBURETOR HEAT..................CHECK OFF5. WING FLAPS.................................CHECK T/O6. PROPELLER......................CHECK MAX.RPM

---------------ENTERING IN RUNWAY---------------7. * FINAL..................................................CLEAR8. * LANDING LIGHT......................................ON9. * TRANSPONDER........................................ON

AFTER TAKE-OFF1. FLAPS.............................................................UP2. LANDING LIGHT.......................................OFF3. PROPELLER......................................2400 RPM4. FUEL PUMP.................................................OFF

CLIMB1. PROPELLER......................................2400 RPM2. THROTTLE...............................................FULL3. ENGINE GAUGES................................CHECK4. AIR SPEED.............................................65 KTS5. TRIM.......................................................ADJUST6. ALTIMETER...............................SET QNH/QNE

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NOVEMBER 2009

CRUISE

1. THROTTLE....................................................A/R2. PROPELLER..............................1900-2400 RPM3. WING FLAPS ..................................................UP4. TRIM...............................................................A/R5. ENGINE GAUGES..................................CHECK6. WING FLAPS ..................................................UP

BEFORE DESCENT

1. BRIEFING..................................................DONE2. CARBURETOR HEAT..................................A/R3. INSTRUMENTS.....................................ADJUST4. ALTIMETER..................................................SET5. AVIONICS..............................................ADJUST6. THROTTLE....................................................A/R7. PROPELLER..............................1900-2400 RPM

APPROACH

1. SEAT BELTS....................................FASTENED2. FUEL PUMP....................................................ON3. LIGHTS ..........................................................A/R4. MASTER SWITCH...........................CHECK ON5. IGNITION SWITCH....................CHECK BOTH6. CARBURETOR HEAT..................................A/R7. THROTTLE....................................................A/R8. AIRSPEED......................................MAX. 81KTS9. WING FLAPS.................................................T/O10. TRIM...............................................................A/R11. PROPELLER.....................................MAX. RPM12. WING FLAPS......................................LANDING13. AIRSPEED................................................57 KTS

BALKED LANDING

1. PROPELLER....................................MAX. RPM2. THROTTLE...............................................FULL3. CARBURETOR HEAT..............................FULL4. WING FLAPS................................................T/O5. AIRSPEED..............................................57 KTS

AFTER LANDING

1. THROTTLE...................................................A/R2. WING FLAPS.................................................UP3. CARBURETOR HEAT................................OFF4. EXTERIOR LIGHTS....................................A/R5. FUEL PUMP.........................................OFF

ENGINE SHUT-DOWN

1. THROTTLE................................................IDLE2. PARKING BRAKE.......................................SET3. ELT.........................................................CHECK4. AVIONICS MASTER..................................OFF5. ELECTRIC CONSUMERS..........................OFF6. IGNITION SWITCH....................................OFF7. INSTRUMENT PANEL LIGHTING...........OFF8. MASTER SWITCH......................................OFF9. TIE DOWNS AND WHEEL CHOKES........A/R

PERFORMANCE

Vx = 57 KTS T/O FLAP Vapp T/O = max 81KTSVy = 65 KTS T/O FLAP Vapp FULL= 57 KTSVa = 104 KTS

Vmaxglide = 65 KTS Vr = 51-57 KTSVFE = 81 KTS

Max. Crosswind= 15 KT

IGNITION SWITCH:- MAX. RPM DROP:................................. 300 RPM- MAX. RPM DIFFERENCE (L/R): ..........120 RPM

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Cruising Performance

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ENGINE EMERGENCIES

ENGINE FAILURE DURING TAKE-OFF

1. THROTTLE..................................................IDLE2. BRAKES.........................................................A/R

ENGINE FAILURE AFTER TAKE-OFF INSUFFICIENT ENGINE POWER

1. AIRSPEED................................................60 KTS2. THROTTLE.................................................FULL3. CARBURETOT HEAT....................................ON4. CHOKE...........................................................OFF5. FUEL SHUT-OFF VALVE.........................OPEN6. IGNITION SWITCH..................................BOTH7. FUEL PUMP....................................................ON8. PROPELLER.....................................MAX. RPM

-----------SHORTLY BEFORE LANDING-----------

9. FUEL SHUT-OFF VALVE...................CLOSED10. IGNITION SWITCH......................................OFF11. MASTER SWITCH........................................OFF

ENGINE FAILURE DURING FLIGHT ENGINE RUNNING ROUGHLY

1. CARBURETOR HEAT...................................ON2. FUEL PUMP....................................................ON3. IGNITION SWITCH CYCLE L-BOTH-R-BOTH4. NO IMPROVEMENT.....................LAND ASAP

ENGINE FAILURE DURING FLIGHT LOSS OF OIL PRESSURE

1. OIL TEMPERATURE.............................CHECK

IF OIL PRESSURE DROPS BELOW GREEN ARC BUT OIL TEMPERATURE IS NORMAL

2. LAND AT NEAREST AIRFIELD

IF OIL PRESSURE DROPS BELOW GREEN ARC AND OIL TEMPERATURE IS RISING

3. REDUCE POWER TO MINIMUM REQUIRED POWER; LAND ASAP. BE PREPARED FOR ENGINE FAILURE AND EMERGENCY LANDING

ENGINE FAILURE DURING FLIGHTLOSS OF FUEL PRESSURE

1. FUEL PUMP.............................ON, LAND ASAP

IF FUEL PRESSURE WARNING LIGHT DOES NOT EXTINGUISH

2. LAND ASAP. BE PREPARED FOR ENGINE FAILURE AND EMERGENCY LANDING

RESTARTING THE ENGINE WITH PROPELLER WINDMILLIG

1. AIRSPEED..................................................70 KTS2. WING FLAPS...................................................T/O3. PROPELLER.......................................MAX. RPM4. FUEL SHUT-OFF VALVE..........................OPEN5. IGNITION SWITCH....................................BOTH6. FUEL PUMP......................................................ON7. THROTTLE...................................................2 CM

------IF NOT START WITHIN 10”: COLD START------

8. THROTTLE....................................................IDLE9. CHOKE............................................ON(PULLED)10. IGNITION SWITCH..................................START

RESTARTING THE ENGINE WITH PROPELLER AT FULL STOP

1. ELECTRICALLY POWERED EQ..................OFF2. MASTER SWITCH...........................................ON3. PROPELLER.......................................MAX. RPM4. FUEL SHUT-OFF VALVE..........................OPEN5. FUEL PUMP......................................................ON6. THROTTLE...................................................2 CM7. CHOKE............................................................OFF8. IGNITION SWITCH..................................START

------AFTER SUCCESSFUL RE-START------

9. OIL PRESSURE...........................................CHEK10. CHOKE............................................................OFF11. ELECTRICALLY POWERED EQ...........ON A/R12. OIL TEMPERATURE...............................CHECK

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NOVEMBER 2009

EMERGENCY LANDING

EMERGENCY LANDING APPROACH WITH ENGINE OFF

1. AIRSPEED (FLAPS UP)..........................65 KTS2. FUEL SHUT-OFF VALVE...................CLOSED3. IGNITION SWITCH......................................OFF4. SAFETY BELTS.................................SECURED5. RADIO........................MAYDAY PROCEDURE6. MASTER SWITCH........................................OFF

PRECAUTIONARY LANDING WITH ENGINE POWER AVAILABLE

1. FIELD TO LAND...............................CHOOSED2. SAFETY BELTS.................................SECURED3. INITIATE DESCENT......................................OK4. THROTTLE....................................................A/R5. TRIM...............................................................A/R6. WING FLAPS.................................................A/R7. OVERFLY LANDING AEREA..................+500 8. RADIO......................TRANSMIT INTENTIONS9. FINAL APPROACH. . .NORMAL PROCEDURE10. TOUCH DOWN....................MINIMUM SPEED11. BRAKE...........................................................A/R12. FUEL SHUT-OFF VALVE..................CLOSED 13. IGNITION SWITCH......................................OFF14. MASTER SWITCH........................................OFF

FIRE

ENGINE FIRE DURING ENGINE-START-UP ON THE GROUND

1. FUEL SHUT-OFF VALVE...................CLOSED2. THROTTLE.................................................FULL3. MASTER SWITCH........................................OFF4. IGNITION SWITCH......................................OFF5. EVACUATE AIRPLANE IMMEDIATELY

ENGINE FIRE DURING FLIGHT

1. FUEL SHUT-OFF VALVE...................CLOSED2. AIRSPEED................................................70 KTS3. FLAPS.............................................................T/O4. THROTTLE.................................................FULL5. FUEL PUMP..................................................OFF6. CABIN HEAT........................................CLOSED7. PERFORM EMERGENCY LANDING WITH ENGINE OFF

ELECTRICAL FIRE INCLUDING SMOKE DURING FLIGHT

1. MASTER SWITCH........................................OFF2. CABIN AIR.................................................OPEN3. USE THE FIRE EXTINGUISHER ONLY IF SMOKE DEVELOPMENT CONTINUES.

IN CASE THE FIRE IS EXTINGHISHED AND ELECTRIC POWER IS REQUIRED FOR

CONTINUATION OF THE FLIGHT

4. AVIONICS MASTER SWITCH....................OFF5. ELECTRICALLY POWERED EQUP...........OFF6. MASTER SWITCH.........................................ON7. AVIONICS MASTER SWITCH.....................ON8. RADIO.............................................................ON9. LAND AS SOON AS POSSIBLE

ELECTRICAL FIRE INCLUDING SMOKE ON THE GROUND

1. MASTER SWITCH........................................OFF

IF ENGINE RUNNING:

2. THROTTLE..................................................IDLE3. FUEL SHUT-OFF VALVE...................CLOSED4. IGNITION SWITCH......................................OFF5. CANOPY.....................................................OPEN6. FIRE EXTINGUISHER................ DEPLOY A/R

CABIN FIRE DURING GLIGHT

1. MASTER SWITCH........................................OFF2. CABIN AIR.................................................OPEN3. CABIN HEAT........................................CLOSED4. FIRE EXTINGUISHER.................DEPLOY A/R5. LAND AS SOON AS POSSIBLE


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NOVEMBER 2009

ICING

UNINTENTIONAL FLIGHT INTO ICING AREA

1. LEAVE ICING AREA CHANGING ALTITUDE OR DIRECTION2. CONTINUE TO MOVE CONTROL SURFACES TO MANTAIN THEIR MOVEABILITY3. CARBURETOR HEAT.....................................ON4. INCREASE RPM TO AVOID ICING OF PROPELLER BLADES (OBSERVE MAXIMUM RPM)5. CABIN HEAT...............................................OPEN

SPIN

RECOVERY FROM UNINTENTIONAL SPIN

1. THROTTLE....................................................IDLE2. RUDDER............FULL OPPOSITE DIRECTION 3. CONTROL STICK...................EASE FORWARD4. RUDDER......................NEUTRAL AFTER STOP5. WING FLAPS....................................................UP6. ELEVATOR........................PULL CAUTIOUSLY

LANDING WITH DEFECTIVE TIRE ON MAIN LANDING GEAR

1. FINAL APPROACH WITH WING FLAPS IN LANDING POSITION2. LAND AIRPLANE ON THE SIDE OF RUNWAY OPPOSITE TO THE SIDE WITH THE DEFECTIVE TIRE TO COMPENSATE FOR CHANGE IN DIRECTION WICH IS TO BE EXPECTED DURING FINAL ROLLING3. LAND WITH WING SLIGHTLY TIPPED IN THE DIRECTION OF THE NON-DEFECTIVE TIRE. TO INCREASE THE MANEUVRABILITY DURING ROLLING, THE NOSE-WHEEL SHOULD BE BROUGHT TO THE GROUND AS SOON AS POSSIBLE AFTER TOUCH-DOWN.4. TO EASE THE LOAD ON THE DEFECTIVE TIRE, THE AILERON SHOULD BE FULLY APPLIED IN THE DIRECTION OF THE NON-DEFECTIVE TIRE.

GLIDING

1. WING FLAPS...................................................T/O2. AIRSPEED..................................................72 KTS

3. GLIDE RATIO 14, WHICH MEANS AT1000 FT/305M ABOVE GROUND, AND WITH NOWIND THE DISTANCE OF GLIDE IS 2.5 NM (4.3 KM)

ELECTRICAL POWER FAILURE

TOTAL ELECTRICAL POWER FAILURE

1. BATTERY CIRCUIT BREAKER..............RESET2. MASTER SWITCH............................CHECK ON3. IF UNSUCCESSFUL........................LAND ASAP

GENERATOR FAILURE

1. MASTER SWITCH....................CYCLE OFF-ON2. GENERATOR CIRCUIT BREAKER........RESET3. GENERATOR CONTROL BREAKER.....RESET4. IF GENERATOR CANNOT BE BROUGHT ON-LINE SWITCH OFF ALL NON-FLIGHT ESSENTIAL ELECTRICAL CONSUMERS. MONITOR AMMETER AND VOLTMETER. LAND AT NEAREST SUITABLE AIRPORT.

THERE ARE 30 MINUTES OF BATTERY LIFE REMAINING AT A DISCHARGE LOAD OF 20 AMPERES.

LOW VOLTAGE INDICATION

LOW VOLTAGE INDICATION WHILE AIRPLANE ON GROUND

1. PROPELLER RPM....................INCREASE RPM2. NON-FLIGHT ESSENTIAL ELECTRICAL CONSUMERS: SWITCH OFF CONSUMERS UNTIL NEEDLE IS IN THE GREEN ARC.3. IF NEEDLE REMAINS IN THE YELLOW ARC AND THE AMMETER IS INDICATING TO THE LEFT OF CENTRE (DISCHARGE): DISCONTINUE ANY PLANNED FLIGHT ACTIVITY

LOW VOLTAGE INDICATIONDURING FLIGHT

1. ALL NON-FLIGHT ESSENTIAL ELECTRICAL CONSUMERS: SWITCH OFF2. IF NEEDLE IS REMAINING IN THE YELLOW ARC AND THE AMMETER IS INDICATING TO THE LEFT OF CENTRE (DISCHARGE): PROCEED AS GENERATOR FAILURE

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NOVEMBER 2009

IF AT ANY TIME THE VOLTMETER NEEDLE INDICATES IN THE RED ARC, YOU SHOULD

LAND AT THE NEAREST SUITABLE AIRFIELD AND SERVICE THE AIRCRAFT

ACCORDINGLY BEFORE CONTINUING THE FLIGHT.

FLAP SYSTEM FAILURE

FLAP POSITION INDICATOR FAILURE

1. VISUAL CHECK OF THE FLAP POSITION2. SELECT AIRSPEED WITHIN THE RANGE OF THE WHITE ARC MARKED ON THE AIRSPEED INDICATOR3. CHECK ALL POSITIONS OF THE FLAP TOGGLE SWITCH (FLAP STOPS ARE FAIL-SAFE)4. MODIFY APPROACH AND LANDING AS FOLLOWS:

• ONLY UP AVAILABLE: - RAISE APPROACH SPEED BY 5 KTS- THROTTLE AS REQUIRED- FLAT APPROACH ANGLE

• ONLY T/O AVAILABLE: - NORMAL APPROACH SPEED- THROTTLE AS REQUIRED- FLAT APPROACH ANGLE

• ONLY LDG AVAILABLE: - NORMAL LANDING

STARTER FAILURE

STARTER DOES NOT DISENGAGE AFTER STARTING THE ENGINE

1. THROTTLE....................................................IDLE2. IGNITION SWITCH......................................OFF

DISCONTINUE ANY PLANNED FLIGHT

AVIONICS SYSTEM FAILURE

TOTAL AVIONIC FAILURE

1. CHECK AVIONIC MASTER CIRCUIT BREAKER: IF TRIPPED, RE-ENGAGE AND MONITOR STATUS, IF IT TRIPS AGAIN, LAND AT NEAREST SUITABLE AIRPORT2. CHECK AVIONIC MASTER SWITCH: TOGGLE AVIONIC MASTER SWITCH, IF AVIONIC SYSTEM REMAINS OFF-LINE, PULL AVIONIC MASTER CONTROL CIRCUIT BREAKER AND LAND AT NEAREST SUITABLE AIRPORT

RADIO SYSTEM OPERATIVE, NO RECEPTION

1. MICROPHONE KEY: CHECK FOR STUCK MICROPHONE KEY ON TRANSCEIVER DISPLAY2. HEADPHONES CHECK: DEACTIVATE SQUELCH FOR A FEW MOMENTS, IF SQUELCH NOT HEARD, CHECK HEADSET CONNECTION

RADIO SYSTEM OPERATIVE, TRANSMITTING NOT POSSIBLE

1. SELECTED FREQUENCY: CHECK IF CORRECT2. MICROPHONE CHECK: IF AVAILABLE USE DIFFERENT ONE (HEADSET)

PROBLEM CANNOT BE RESOLVED: SWITCH TRANSPONDER (IF AVAILABLE) TO "COMM

FAILURE" CODE IF REQUIRED BY THE SITUATION AND PERMITTED BY APPLICABLE

NATIONAL REGULATIONS.


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NOVEMBER 2009

TRIM SYSTEM FAILURE

STUCK TRIM

1. CIRCUIT BREAKER CHECK: RESET IF BREAKER IS TRIPPED2. ROCKER SWITCH: DEPRESS IN BOTH DIRECTIONS, WAIT 5 MINUTES, TRY AGAIN3. LAND AT NEAREST SUITABLE AIRPORT

RUNAWAY OF TRIM

1. CONTROL STICK GRIP: STICK AND MAINTAIN CONTROL OF AIRPLANE2. TRIM MOTOR CIRCUIT BREAKER: PULL CIRCUIT BREAKER3. ROCKER SWITCH: CHECK IF DEPRESSED

INSTRUMENT PANEL LIGHTING FAILURE

TOTAL PANEL LIGHTING FAILURE

1. ROCKER SWITCH, MAP LIGHT...................ON2. I-PANEL LIGHTING.................CYCLE OFF/ON3. DIMMING CONTROL..... FULLY CLOCKWISE4. I-LIGHTING CIRCUIT BREAKER.......... RESET5. IF NOT SUCCESSFUL........ USE FLASHLIGHT

EXPECT ELECTRICAL POWER FAILURE

TACHOMETER FAILURE

OPERATION AT T/O (5MINUTE) POWER

1. AIRSPEED DO NOT EXCEED 110 KIAS

OPERATION AT MCT

1. PROPELLER SPEED CONTROL LEVER: ENSURE LEVER IS AT LEAST ½ INCH (10MM) (MEASURED AT SLOT) AFT OF FULL FORWARD POSITION. ENGINE WILL NOW BE OPERATING AT, OR BELOW, MAXIMUM CONTINUOUS POWER.

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