be35dbd81e67cb37193e18adbfa2161d810cd6f1d7d7b5a3bb423f9def3ffbe0 Contains no airspeeds, power settings, fuel quantities, manifold pressure limits, temperature limits, or other numerical limitations — all must come from the specific aircraft POH. Equipment, avionics, and fuel system configurations vary across 310 R airframes. Verify every item against the specific aircraft and its POH before use.

Aircraft documents (AROW) ON BOARD AND CURRENT Fuel quantity — visually inspect both main and aux tanks; confirm caps seated and locked VERIFIED — QUANTITY ADEQUATE FOR FLIGHT WITH RESERVES Fuel sump drains — all sumps on both wings and gascolator SAMPLED; CLEAR, CORRECT COLOR, NO WATER OR SEDIMENT Fuel selector valves — both engines CONFIRMED ACCESSIBLE; POSITION NOTED Oil level — left engine WITHIN ACCEPTABLE RANGE PER POH; CAP SECURE Left engine cowling and induction inlets LATCHES SECURE; INLETS CLEAR OF OBSTRUCTIONS Left propeller blades and spinner NO NICKS, CRACKS, OR EROSION; SPINNER SECURE Left main landing gear — strut, tire, and gear door STRUT EXTENDED NORMALLY; TIRE SERVICEABLE; DOOR CONDITION ACCEPTABLE Left wing — leading edge, fuel vent, tip, and nav light NO DAMAGE; VENT CLEAR; LIGHT LENS INTACT Left aileron and flap — hinge points, fasteners, and travel SECURE; FULL FREE MOVEMENT; NO DAMAGE Static ports CLEAR AND UNOBSTRUCTED Pitot tube — cover removed, inlet clear COVER OFF; UNOBSTRUCTED Nose gear — strut extension, tire condition, steering linkage, and shimmy damper STRUT EXTENDED NORMALLY; TIRE SERVICEABLE; LINKAGE INTACT Nose baggage compartment CONTENTS SECURE; DOOR LATCHED Oil level — right engine WITHIN ACCEPTABLE RANGE PER POH; CAP SECURE Right engine cowling and induction inlets LATCHES SECURE; INLETS CLEAR Right propeller blades and spinner NO NICKS, CRACKS, OR EROSION; SPINNER SECURE Right main landing gear — strut, tire, and gear door STRUT EXTENDED NORMALLY; TIRE SERVICEABLE; DOOR CONDITION ACCEPTABLE Right wing, aileron, flap, and nav light NO DAMAGE; HINGES SECURE; FULL FREE MOVEMENT; LENS INTACT Empennage — horizontal and vertical stabilizer surfaces NO DAMAGE; HINGE POINTS SECURE Elevator, rudder, and trim tabs FREE OF DAMAGE; TRAVEL FREE; TRIM TABS SECURE All tiedowns, chocks, and control locks REMOVED

Seats and rudder pedals — all occupants ADJUSTED AND LOCKED Seat belts and shoulder harnesses FASTENED AND ADJUSTED Circuit breakers ALL IN — NONE POPPED Master switch ON — BATTERY VOLTAGE ACCEPTABLE Fuel quantity indicators — both sides CHECKED — AGREE WITH VISUAL INSPECTION Fuel selectors — both engines MAIN TANKS SELECTED Avionics master OFF FOR START Throttles — both IDLE Mixture controls — both IDLE CUT-OFF Propeller controls — both FULL FORWARD Cowl flaps — both OPEN Elevator trim SET TO TAKEOFF POSITION Rudder trim NEUTRAL Flaps UP — VERIFIED ON INDICATOR Landing gear lever and position lights HANDLE DOWN; THREE GREEN CONFIRMED

Propeller arc — left engine CLEAR — ANNOUNCE AND VISUALLY CONFIRM Left throttle CRACKED OPEN PER POH COLD/HOT START PROCEDURE Left mixture and fuel pump — prime per POH PRIMED PER POH PROCEDURE Left ignition — START ENGAGE STARTER; RELEASE WHEN ENGINE FIRES Left engine oil pressure — after start RISING WITHIN TIME LIMIT PER POH; IDLE RPM STABLE Left mixture — after start ADVANCE TO RICH AFTER OIL PRESSURE CONFIRMED Left alternator ON — CHARGE INDICATION CONFIRMED Propeller arc — right engine CLEAR — ANNOUNCE AND VISUALLY CONFIRM Right throttle and mixture — prime per POH SET PER POH START PROCEDURE Right ignition — START ENGAGE STARTER; RELEASE WHEN ENGINE FIRES Right engine oil pressure — after start RISING WITHIN TIME LIMIT PER POH; IDLE RPM STABLE Right mixture — after start ADVANCE TO RICH AFTER OIL PRESSURE CONFIRMED Right alternator ON — CHARGE INDICATION CONFIRMED Avionics master ON — AFTER BOTH ENGINES RUNNING

Engine instruments — both engines OIL PRESSURE AND TEMP IN GREEN; NO ABNORMAL INDICATIONS Alternators / ammeter — both BOTH CHARGING NORMALLY Fuel pumps OFF UNLESS REQUIRED BY POH DURING WARM-UP Radios and transponder SET — ATIS RECEIVED; FREQUENCIES LOADED Clearance / taxi instructions RECEIVED AND READ BACK Heading indicator SET TO MAGNETIC COMPASS Altimeter SET TO CURRENT ALTIMETER SETTING Brakes TESTED DURING INITIAL TAXI MOVEMENT Engine warm-up — both engines ALLOW BOTH ENGINES TO REACH MINIMUM OPERATING TEMPERATURES PER POH BEFORE RUN-UP

Aircraft position — angled into wind if practical PARKING BRAKE SET Flight controls FREE, CORRECT, AND FULL RANGE OF MOTION Engine temperatures — both OIL TEMP AND CHT IN GREEN ARC BEFORE POWER CHECK Left engine — advance to run-up power per POH POWER SET Left magneto check — LEFT / BOTH / RIGHT RPM DROP WITHIN LIMITS PER POH; NO EXCESSIVE ROUGHNESS Left propeller cycle — advance full forward, reduce to note RPM drop, advance back; repeat per POH GOVERNOR RESPONDING; RPM DROP AND RECOVERY NORMAL Left engine instruments at run-up power ALL IN GREEN; MANIFOLD PRESSURE, OIL PRESSURE, OIL TEMP NORMAL Left throttle — reduce to idle SMOOTH IDLE CONFIRMED Right engine — advance to run-up power per POH POWER SET Right magneto check — LEFT / BOTH / RIGHT RPM DROP WITHIN LIMITS PER POH; NO EXCESSIVE ROUGHNESS Right propeller cycle — advance full forward, reduce to note RPM drop, advance back; repeat per POH GOVERNOR RESPONDING; RPM DROP AND RECOVERY NORMAL Right engine instruments at run-up power ALL IN GREEN Right throttle — reduce to idle SMOOTH IDLE CONFIRMED Fuel selectors — both engines MAIN TANKS Fuel pumps — both ON FOR TAKEOFF PER POH Mixtures — both RICH OR ADJUSTED FOR FIELD ELEVATION PER POH Propellers — both FULL FORWARD Trim — elevator and rudder ELEVATOR SET FOR TAKEOFF; RUDDER NEUTRAL Flaps SET PER POH FOR TAKEOFF CONDITION Landing gear DOWN — THREE GREEN CONFIRMED Doors and windows CLOSED AND LATCHED Transponder ALT MODE — CODE SET Abort plan — brief crew or self BRIEFED: BELOW ROTATION SPEED ABORT ON RUNWAY; ABOVE ROTATION MAINTAIN CONTROL AND CLIMB PER POH

Final runway check — runway clear, wind direction noted CLEARED FOR TAKEOFF Throttles — both simultaneously to takeoff power SYMMETRIC ADVANCEMENT; MANIFOLD PRESSURE PER POH Engine instruments — both during takeoff roll ALL IN GREEN; ABORT IF ABNORMAL Directional control on roll CENTERLINE MAINTAINED WITH RUDDER; NOSE WHEEL STEERING UNTIL RUDDER EFFECTIVE Rotation — at Vr per POH ROTATE SMOOTHLY; POSITIVE CLIMB RATE ESTABLISHED Landing gear — after positive rate, no runway remaining RETRACT Airspeed — accelerate to Vx or Vy per POH CLIMB SPEED ESTABLISHED Fuel pumps — after clearing obstacles OFF PER POH OR MAINTAIN ON TO CRUISE ALTITUDE AS DIRECTED

Airspeed VY OR CRUISE CLIMB SPEED PER POH Power — both engines MANIFOLD PRESSURE AND RPM AT CLIMB SETTING PER POH Mixtures — both ADJUSTED FOR ALTITUDE PER POH Cowl flaps — both OPEN AS REQUIRED TO MAINTAIN CHT WITHIN LIMITS Engine instruments — both OIL PRESSURE, OIL TEMP, CHT, EGT ALL WITHIN LIMITS Fuel selectors BOTH ON MAIN Altimeter SET TO LOCAL OR STANDARD AS REQUIRED ABOVE TRANSITION ALTITUDE Heading indicator CHECKED AGAINST COMPASS; RESET IF NEEDED

Power setting — both engines MANIFOLD PRESSURE AND RPM AT CRUISE SETTING PER POH Mixtures — both LEANED PER POH FOR ALTITUDE AND POWER SETTING Cowl flaps — both CLOSED OR AS REQUIRED FOR TEMPERATURE MANAGEMENT Engine instruments — both ALL WITHIN GREEN ARCS; BOTH ENGINES RUNNING SYMMETRICALLY Fuel selectors — verify or switch per schedule CONFIRMED ON MAIN; SWITCH TO AUX PER POH BURN SCHEDULE IF EQUIPPED Fuel quantity — both sides MONITOR; SUFFICIENT FOR DESTINATION PLUS RESERVES Electrical — ammeter and voltmeter NORMAL; NO EXCESSIVE LOAD Navigation and communication EN ROUTE FREQUENCIES SET; POSITION VERIFIED

Power — reduce gradually; avoid abrupt throttle reduction on turbocharged engines POWER REDUCED SMOOTHLY PER POH Mixtures — both ENRICH GRADUALLY AS ALTITUDE DECREASES PER POH Cowl flaps ADJUST TO MAINTAIN CHT WITHIN LIMITS DURING DESCENT ATIS / AWOS — destination airport RECEIVED — ALTIMETER SETTING, RUNWAY, AND WIND NOTED Altimeter SET TO DESTINATION ALTIMETER SETTING Fuel selectors — both MAIN TANKS Fuel pumps — both ON FOR APPROACH AND LANDING PER POH Engine instruments — both NORMAL; NO ANOMALIES

Fuel selectors — both engines MAIN TANKS Fuel pumps — both ON Mixtures — both RICH Propellers — both FULL FORWARD Landing gear — GEAR DOWN HANDLE DOWN; THREE GREEN LIGHTS CONFIRMED; NO RED LIGHT Flaps SET PER POH FOR APPROACH TYPE Approach speed ESTABLISHED ON APPROACH SPEED PER POH Engine instruments — both NORMAL; ENGINES AT PROPER TEMPERATURE FOR POTENTIAL GO-AROUND

Landing gear — down and locked THREE GREEN LIGHTS; HANDLE IN DOWN POSITION; NO RED LIGHT Perform gear check at a consistent point every pattern. Confirm verbally and visually before every landing. If the gear warning horn sounds on approach with power reduced, the gear is NOT down. Do not land. Recycle gear or go around and troubleshoot.

Final approach speed ON SPEED PER POH FOR WEIGHT AND FLAP SETTING Landing gear — last check on short final THREE GREEN CONFIRMED Threshold crossing — reduce power; initiate flare FLARE TO TOUCHDOWN ATTITUDE Touchdown — main gear first on normal landing DIRECTIONAL CONTROL MAINTAINED Throttles after touchdown IDLE Braking APPLIED AS REQUIRED; AVOID LOCKING WHEELS Flaps — after clearing runway RETRACT PER POH

Throttles — both FULL FORWARD — ADVANCE SMOOTHLY AND SIMULTANEOUSLY Propellers — both FULL FORWARD Mixtures — both RICH Pitch — establish positive climb attitude CLIMB ATTITUDE SET Flaps — retract incrementally per POH NOT ALL AT ONCE AT LOW SPEED Landing gear — after positive rate of climb RETRACT Airspeed — accelerate to Vy per POH CLIMB SPEED ESTABLISHED Cowl flaps OPEN AS REQUIRED FOR ENGINE COOLING ATC — notify of go-around NOTIFIED; INSTRUCTIONS RECEIVED

Flaps RETRACT FULLY Fuel pumps — both OFF AFTER CLEARING ACTIVE RUNWAY Cowl flaps — both OPEN TO ALLOW ENGINE COOLING DURING TAXI Transponder STANDBY OR AS INSTRUCTED BY ATC Landing lights OFF

Parking brake SET Avionics master OFF — BEFORE ENGINE SHUTDOWN TO PROTECT AVIONICS FROM VOLTAGE SPIKE Engine cool-down at idle — both ALLOW TURBOCHARGED ENGINES TO COOL FOR TIME SPECIFIED IN POH BEFORE SHUTDOWN Do not shut down hot turbocharged engines. Premature shutdown can damage turbocharger bearings. Left mixture IDLE CUT-OFF — ALLOW ENGINE TO STOP Left ignition OFF AFTER ENGINE STOPS Left alternator OFF Right mixture IDLE CUT-OFF — ALLOW ENGINE TO STOP Right ignition OFF AFTER ENGINE STOPS Right alternator OFF Master switch OFF Fuel selectors — both OFF OR MAIN PER OPERATOR PREFERENCE AND POH Control locks INSTALLED Pitot cover INSTALLED Tiedowns and chocks SECURED Squawks and discrepancies NOTED IN AIRCRAFT LOGBOOK OR SQUAWK SHEET