3b9b9744bb450559343584c47a52975e7e9834facb2ae60e86c86837cc2189e4

Seat belts Brakes Landing Gear Switch Check DOWN Auxiliary Fuel Pumps OFF Emergency Power Switch OFF Battery Switch ON Alternator Switches ON Voltage Regulator Switch Main Landing Gear Lights Trim Controls Flight Controls Alternate Air Control Check in Altimeter and Clock Set Avionics Master OFF Throttle Open 1 inch Propeller High RPM Mixture Full Rich Fuel Selectors LR MAIN Rotating Beacon ON

Magneto Switches ON Start Engine Auxiliary Fuel Pumps LOW Avionics Master ON

Parking Brake SET Cabin Door CLOSED and LOCKED Throttle setting 1700 RPM Alternators – Check Magnetos -- Check Propellers Check to 1200 RPM Vacuum Pressure Check (4.75 to 5.25”) Oil Temperature Check green arc Throttle setting 700 - 1000 RPM Trim Controls Checked and set Wing Flaps 0° Flight Controls Engine instruments -- Check Parking brake Released Lights as Required ATIS -- Check Transponder -- Set

Auxiliary Fuel Pumps ON (high) Power Full throttle and 2625 RPM Mixture FULL RICH (lean for maximum power above 3000 feet) Maintain Level Attitude Elevator Control Raise nose wheel at 90 MPH Break ground at 105 MPH Brakes Apply momentarily Landing gear retract Climb Speed 124 MPH Auxiliary fuel pumps OFF

Auxiliary Fuel Pumps ON (high) Wing Flaps 15° Power Full throttle and 2625 RPM Mixture FULL RICH (lean for maximum power above 3000 feet) Maintain Level Attitude Elevator Control Raise nose wheel at 84 MPH Break ground at 93 MPH Hold speed until all obstacles are cleared Brakes Apply momentarily Landing gear retract Flaps Retract (after obstacles are cleared) Auxiliary Fuel Pumps OFF

NORMAL CLIMB Airspeed 130-150 MPH Power 24 INCHES Hg or FULL THROTTLE and 2450 RPM Mixture Adjust to climb fuel flow Auxiliary Fuel Pumps ON (above 12,000' altitude to minimize vapor formation) MAXIMUM PERFORMANCE CLIMB Airspeed 124 MPH at sea level, 122 MPH at 10,000' Power FULL THROTTLE and 2625 RPM Mixture Adjust for altitude and power Auxiliary Fuel Pumps ON (above 12,000' altitude to minimize vapor formation)

Cruise Power 15-24 inches Hg and 1200 - 2450 RPM Mixtures Lean as required Fuel Selectors aux after 60 min Trim Tabs adjust

Power As required Mixture ADJUST for smooth operation and gradual enrichment as altitude is lost

Fuel Selectors MAIN Mixtures Full Rich Propellers High RPM Wing Flaps Landing Gear Extended below 160 MPH Auxiliary Fuel Pumps ON Approach 105 MPH

Touchdown Main wheels first Landing roll Lower nose wheel gently Braking As required

Increase engine speed to 2625 RPM and apply full throttle Reduce flap setting to 15° Trim airplane for climb Retract flaps as all obstacles are cleared, and a safe altitude and airspeed are obtained. Do not retract landing gear if another landing approach is to be conducted.

Auxiliary Fuel Pumps LOW Wing Flaps RETRACT Transponder stdby

Auxiliary Fuel Pumps OFF Throttles IDLE Propellers High RPM (full forward) Mixtures IDLE CUT OFF Magneto Switches OFF, after engine stops Avionics Switch OFF All switches OFF Brakes SET Control Lock Install Cabin Door Secure

ENGINE-OUT AFTER TAKEOFF - ABOVE 105 MPH (Without sufficient runway ahead) Mixture Full rich Propellers Full forward Throttles Full forward Landing gear UP Determine inoperative engine (dead foot dead engine) Inoperative engine FEATHER Establish bank 5° toward good engine Climb out to clear any obstacles 105 MPH Accelerate to 120 MPH after obstacle is cleared Wing Flaps UP (if extended) Trim tabs Adjust 5° back toward good engine Secure inoperative engine as follows: A. Mixture IDLE CUT OFF B. Fuel Selector OFF C. Auxiliary Fuel Pump OFF D. Magneto Switches OFF E. Alternator Switch OFF As soon as practical LAND ENGINE-OUT DURING FLIGHT Determine inoperative Power Increase as required Fuel Flow - Check, if deficient, position auxiliary fuel pump switch to ON Fuel Quantity - Check Oil Pressure and Oil Temperature - Check, shut down inoperative engine if oil pressure is low. Check Magneto Switches - Check Secure inoperative engine as follows: A. Throttle CLOSED B. Mixture IDLE CUT-OFF C. Propeller FEATHER D. Fuel Selector OFF E. Auxiliary Fuel Pump OFF F. Magneto Switch OFF G. Alternator Switch OFF Operative Engine - Adjust A. Power Increase as required B. Mixture Adjust for power C. Fuel Selector Main tank D. Auxiliary Fuel Pump ON Trim Tabs ADJUST 5° bank towards good engine Electrical load DECREASE As soon as practical LAND ENGINE RESTARTS IN FLIGHT (After Feathering) Fuel Selector Valve Main Tank Throttle Advance Propeller HIGH RPM Mixture FULL RICH Magneto Switches ON Primer Switch ENGAGE Starter Button PRESS Power Increase slowly NOTE: If start is unsuccessful, turn magneto switches OFF, retard mixture to IDLE CUT-OFF, open throttle fully, and engage starter for several revolutions. Then repeat air start procedure. SINGLE ENGINE APPROACH AND LANDING Approach at 110 MPH with excess altitude Delay extension of landing gear until within gliding distance of field Avoid use of flaps until landing is assured Decrease speed below 105 MPH only if landing is a certainty GO-AROUND (SINGLE ENGINE) If absolutely necessary, and speed is above 105 MPH, increase engine speed to 2625 RPM and apply full throttle Retract landing gear UP Reduce flap setting to 0° (if extended) Climb at 120 MPH (108 MPH with obstacles directly ahead) Trim airplane for single-engine