71d5b038a1a201406df0c3e84efb4b7d983c1f996413da73518a838261b7f4c6 Section "ENGINE FAILURE – IMMEDIATELY AFTER TAKEOFF" item count differs between passes (10 vs 11); verify nothing was dropped. Section "FORCED LANDING W/O ENGINE POWER" item count differs between passes (14 vs 13); verify nothing was dropped.

Pilot's Operating Handbook Airplane Weight and Balance CHECKED Brakes TEST AND SET Control Wheel Lock Hobbs Meter Ignition & Avionics Master OFF Master Switch ON Fuel Quantity Indicator CHK QTY & ENSURE LOW FUEL ANNUNCIATORS OFF Avionics Master Switch ON Avionics Cooling Fan CHECK AUDIBLY Avionics Master Switch OFF Flaps Static Pressure Alternate Source OFF Annunciator Panel TEST/ALL LIGHTS ON Fuel Selector Valve BOTH Pitot Heat ON FOR 30 SECONDS Pitot Heat TEST FOR HEAT & POWER OFF Master Switch OFF Trim Controls Cockpit Inspect Done Passenger briefing Cabin doors CLOSED AND LOCKED Seats/seat belts ADJUSTED AND LOCKED Circuit breakers Avionics circuit breakers Electrical equipment OFF Avionics master switch OFF Cowl flaps Fuel selector valve BOTH

Throttle OPEN ¼ INCH Prop Master switch ON Beacon Mixture Prop area Auxiliary fuel pump switch ON Mixture ADVANCE UNTIL THERE IS A RISE IN FUEL FLOW AND MAINTAIN IN THIS POSITION APPROXIMATELY FIVE SECONDS WITH AUX FUEL PUMP ON Auxiliary fuel pump switch OFF Ignition switch Mixture SMOOTHLY TO RICH IF ENGINE FLOODS, VERIFY AUXILIARY FUEL PUMP OFF, OPEN THROTTLE ½ TO FULL, AND CRANK ENGINE. WHEN ENGINE FIRES, ADVANCE MIXTURE TO FULL RICH & RETARD THROTTLE Oil Pressure Mixture LEANED at 1200 RPM Flaps RETRACT TO NORMAL Avionics Master / Radios ON EDM 800 ENTER/VERIFY FUEL VOLUME KLN94 & MX20 Databases CURRENT KLN94 FLIGHT PLAN ENTERED ATIS/AWOS Clearance if applicable Navigation lights AS REQUIRED Taxi light AS REQUIRED Brakes

Brakes Seat backs Passenger Seats AS FAR FWD AS POSSIBLE Seats/seat belts CHECK SECURED Cabin doors CLOSED AND LOCKED Flight controls FREE AND CORRECT Flight instruments CHECK AND SET Directional Gyro Altimeter Transponder GPS & Autopilot Attitude Indicator Autopilot Preflight Power Manual Electric Trim Test Both Halves Down VERIFY Both Halves Up VERIFY MET Up, Hold DISC VERIFY Wheel/Ind Not Moving VERIFY Release AP/DISC VERIFY Wheel/Ind Moving VERIFY Baro Setting VERIFY Autopilot PRESS AP BUTTON Flight Controls VERIFY OVRPWER A/P Disc PRESS & VERIFY Trim Fuel quantity Auxiliary fuel pump OFF Mixture Cowl flaps Fuel selector valve RECHECK BOTH Throttle 1800 RPM Magnetos Prop CYCLE THEN RETURN TO HIGH Vacuum gauge Oil pressure Oil temperature Ammeter Annunciator panel TEST AND CHECK Throttle IDLE/1000 RPM OR LESS Friction lock Wing flaps 0 to 20° Cowl Flaps Electric trim Elevator/rudder trip Radios/avionics NAV/GPS switch Autopilot Strobe lights AS DESIRED Taxi/Landing lights AS DESIRED Transponder Brakes

Before Taking Runway XPONDER SET TO ALTITUDE Tower & Departure Freqs SET Wing flaps 0 to 20° Take Runway Power FULL POWER/2700 RPM Mixture MAX OR LEANED TO MAX POWER ABOVE 3000 FEET Elevator control ROTATE 56 KIAS Climb speed Wing flaps RETRACT WHEN CLEAR OF OBSTACLES

Wing flaps Brakes Power FULL POWER/2700 RPM Mixture MAX OR LEANED TO MAX POWER Brakes Elevator control MAINTAIN SLIGHT TAIL LOW ATTITUDE Climb Speed Wing flaps RETRACT SLOWLY AFTER REACHING 80 KIAS

Airspeed Power 25 INCH OR FULL(LESS)/2500 RPM Mixture LEAN TO 20 GPH Fuel Selector Valve Wing flaps VERIFY RETRACTED Cowl flaps

Airspeed Power FULL THROTTLE/2700 RPM Mixture LEAN FOR MAX POWER SEE MINIMUM FUEL FLOW PLACARD Fuel selector valve Cowl flaps

Landing light VERIFY OFF Power – 75% MAX Throttle 15 to 25 INCHES Prop 2100 to 2500 RPM Mixture LEAN FOR CRUISE Cowl flaps

Power AS DESIRED Mixture ENRICHEN AS REQUIRED Cowl flaps Altimeter Fuel selector valve Flaps AS DESIRED 0° to 10° below 140 KIAS 10° to 40° below 100 KIAS

Approach brief KLN94 CDI switch Frequency/Approach IDENT Marker beacon HSI to Compass AT FAF Time Turn Twist Throttle Talk Mixture Prop Landing light Flaps AS DESIRED 0° to 10° below 140 KIAS 10° to 40° below 100 KIAS

Passenger Seats As Fwd As Practical VERIFY Seat backs Seatbelts Fuel Selector Valve Mixture Prop Landing light Autopilot

Airspeed (flaps up) Flaps AS DESIRED 0° to 10° below 140 KIAS 10° to 40° below 100 KIAS Airspeed (flaps full) Braking

Airspeed (flaps up) Flaps FULL (40°) BELOW 100 KIAS Airspeed Power REDUCE TO IDLE AS OBSTACLES ARE CLEARED Braking Flaps

Power FULL POWER/2700 RPM Mixture Wing flaps Climb speed Wing flaps Cowl flaps

Wing flaps Cowl flaps Landing light Taxi light AS REQUIRED Strobes Transponder

Throttle Electrical equipment Avionics master Mixture Ignition switch Master Hobbs time Control lock Cowl flaps Fuel Selector Valve Nosewheel Chock Fuel Top Off Cowl Inlet Cover In Place

Throttle Brakes Wing flaps Mixture Ignition switch Master switch

Airspeed Flaps up Flaps down Mixture Fuel selector valve Ignition switch Wing flaps AS REQUIRED (40° RECOMMENDED) Master switch Cabin door Land

Airspeed Fuel selector valve Auxiliary fuel pump Engine power IF RESTART DOES NOT OCCUR Mixture Ignition switch CHECK BOTH (START IF PROPELLER IS STOPPED) Auxiliary fuel pump OFF (IF FUEL FLOW DROPS TO ZERO RETURN TO ON)

Passenger seats Seatbacks Seats/Seat Belts Airspeed Flaps up Flaps down Transmit 121.5 Squawk Mixture Fuel selector valve Wing flaps AS REQUIRED (40° RECOMMENDED) Master switch ELT Door

Passenger seats Seatbacks Seats/Seat Belts Transmit 121.5 Squawk Airspeed Wing flaps Avionics Master Electrical switches Wing flaps Airspeed Master switch ELT Doors Ignition switch Mixture Fuel selector valve

Transmit 121.5 Squawk Heavy objects Passenger seats Seatbacks Seats/Seat Belts Wing flaps POWER ESTABLISH 300 FT/MINUTE DESCENT AT 65 KIAS If no power Flaps up Flaps 10° Approach High winds/Heavy seas INTO THE WIND Light winds/Heavy seas PARALLEL TO SWELLS Cabin doors Plan touchdown Face ELT Airplane

Ignition switch START (CONTINUE CRANKING) ENGINE STARTS Power Engine ENGINE FAILS TO START Ignition switch START (CONTINUE CRANKING) Throttle Mixture Fuel selector valve Auxiliary fuel pump Master switch Ignition switch Airplane Fire

Mixture Fuel selector valve Auxiliary fuel pump Master switch Cabin air Cabin heat Overhead vents Airspeed 105 KIAS (INCREASE WITHIN AIRSPEED LIMITATIONS UNTIL FIRE EXTINGUISHED) Forced landing

Master switch Vents/cabin air/heat Fire extinguisher Avionics master switch All other switches (except ignition) OFF Vents/cabin air OPEN WHEN FIRE EXTINGUISHED Master switch Circuit breakers CHECK FOR FAULTY CIRCUIT/DO NOT RESET Radio switches Avionics master Radios/electrical switches

Master switch Vents/cabin air/heat Fire extinguisher Vents/cabin air OPEN WHEN FIRE EXTINGUISHED Land

Landing light Taxi light Navigation lights Strobe light Pitot heat Sideslip Land Flaps

Pitot heat Turn back or change altitude PULL FULL OUT Defrost controls Increase RPM IF EXCESSIVE VIBRATION, REDUCE TO 2200 RPM AND THEN RAPIDLY INCREASE TO FULL. CYCLE AS NEEDED. Watch for induction air filter icing 15 INCHES HG IN MP CAN OCCUR ABOVE 8000 FEET Plan landing Plan for Open left window Flaps USE 10-20° FLAPS FOR ICE ACCUMULATIONS OF 1 INCH OR LESS. FOR GREATER ICE ACCUMULATION, LAND WITH FLAPS RETRACTED TO ENSURE ADEQUATE ELEVATOR EFFECTIVENESS. Approach 20° flaps 0-10° flaps Avoid missed approach IF MISSED APPROACH IS MANDATORY, APPLY MAXIMAL POWER AND MAINTAIN 100 KIAS WHILE RETRACTING FLAPS IN 10° INCREMENTS.

Auxiliary fuel pump Mixture Fuel selector valve SELECT OPPOSITE TANK IF SYMPTOMS CONTINUE Auxiliary fuel pump switch OFF AFTER FUEL FLOW HAS STABILIZED

Alternator Nonessential electrical equipment With alternator side of master OFF Nonessential electrical equipment Terminate flight

Avionics master Alternator circuit breaker (ALT FLD) Master switch Master switch Low voltage annunciator IF LOW VOLTAGE ILLUMINATES Alternator Nonessential electrical equipment Terminate flight

SMOOTH AIR Seats and seat belts Throttle Propeller Mixture Wing flaps Airspeed ROUGH AIR Seats and seat belts Throttle Propeller Mixture Wing flaps Weights and airspeed 3600 2950 2300

Control wheel GRASP FIRMLY AND MAINTAIN CONTROL OF AIRCRAFT A/P DISC/TRIM INT switch PRESS AND HOLD Aircraft Autopilot breaker

Static pressure alternate source valve PULL ON Heat and air vents PULL ON Vents Airspeed and altitude REFER TO CALIBRATION CHARTS

Vr — Rotation speed 55 KIAS Vx — Best angle climb 70 (SL) 75 (10K) Vy — Best rate climb 86 (SL) 82 (10K) Vso — Stall with flaps 38 (rcog) 44 (fcog) Vs — Stall without flaps 50 (rcog) 54 (fcog) Va — Maneuvering speed 3600 pounds 2900 pounds 2200 pounds Vfe — 0 to 10° 140 KIAS Vfe — 20 to 40° 100 KIAS Vne — Never exceed speed 182 KIAS Vno — Maximum structural cruising speed 149 KIAS Maximum window open Normal climb out 75-85 KIAS Shortfield/Flaps 20° climb 74 KIAS Enroute climb Normal approach flaps up 80-90 KIAS Normal approach flaps 40° 70-80 KIAS Short field approach flaps 40° 67 KIAS Balked landing flaps 20° 80 KIAS Maximum demonstrated crosswind 20 KNOTS Engine failure after takeoff flaps up 80 KIAS Engine failure after takeoff flaps down 70 KIAS Maximum glide 3600 pounds 3200 pounds 2800 pounds Precautionary landing w/engine power 70 KIAS Landing without engine power/flaps up 80 KIAS Landing without engine power/flaps down 70 KIAS Emergency descent Smooth air Rough air — 3600 pounds Rough air — 2900 pounds Rough air — 2200 pounds

STAGE — MP — RPM — PITCH — KIAS — VSI Climb Cruise Cruise Descent Appr Climb Approach Appr Descnt Downwind -10 Degr Flps Downwind -20 Degr Flps Base Final

Voltage Outside Air Difference between hottest and coldest EGT RPM/MAP Fuel Remaining Fuel required to next GPS WPT or destination Fuel Reserve at next GPS WPT or destination Nautical Miles per Gallon Time to Empty Fuel flow rate Total Fuel Used EGT, CHT Oil Temperature Shock cooling