74bcf9dc4527aba5004f88c76b23d5a7f7bbb5e4c0f26458543dcf3dbb021076 Contains no airspeeds, power settings, fuel quantities or other limitations — must come from aircraft POH. Equipment variations exist across this model/variant. Verify items against the specific aircraft before use.

Required documents (ARROW) AIRWORTHINESS, REGISTRATION, RADIO LICENSE IF REQUIRED, POH/AFM, WEIGHT-AND-BALANCE ON BOARD Fuel quantity — visually inspect both tanks QUANTITY CONFIRMED; ADEQUATE FOR FLIGHT WITH RESERVES Fuel grade and appearance — sample each tank sump and main strainer CORRECT GRADE PER POH; CLEAR, CORRECT COLOR, NO WATER OR SEDIMENT Fuel caps — both tanks SEATED FLUSH AND LOCKED Engine oil level WITHIN OPERATING RANGE PER POH; DIPSTICK RE-SEATED AND SECURED Engine compartment — hoses, wiring, and baffling visible through oil inspection door NO LEAKS; NOTHING LOOSE OR OBSTRUCTED Induction air inlet and filter CLEAR; FILTER CLEAN; ALTERNATE AIR DOOR OPERATES FREELY The Continental IO-540 is fuel-injected — no carburetor heat. Alternate air draws unfiltered air from inside the cowl when selected. Propeller blades — leading edges, tips, and faces NO NICKS, CRACKS, OR DELAMINATION; BLADES SERVICEABLE Spinner SECURE; NO CRACKS Nose gear — strut extension, tire, steering linkage, and wheel fairing STRUT EXTENDED NORMALLY; TIRE INFLATED AND SERVICEABLE; FAIRING CLEAR OF DEBRIS Pitot tube — cover removed, inlet unobstructed COVER OFF, CLEAR Static ports CLEAR Stall warning vane — lift to confirm circuit activates FUNCTIONING; INLET CLEAR Cabin door — left side HINGES INTACT; LATCHES FUNCTION FROM INSIDE AND OUTSIDE; SEAL UNDAMAGED Cargo door — right aft HINGES INTACT; BOTH UPPER AND LOWER LATCHES SECURE; LOCKING PINS FULLY ENGAGED; SEAL UNDAMAGED The 206H cargo door is a primary differentiator. Both latches must be independently confirmed. A partially latched cargo door can depart in flight. Right main gear — strut, tire, and brake assembly STRUT NORMAL; TIRE INFLATED AND SERVICEABLE; BRAKE DISC AND CALIPER SERVICEABLE Right aileron and flap — hinge attachment and travel HINGES SECURE; FULL FREE MOVEMENT; NO DAMAGE Right wingtip and lights UNDAMAGED; LENS INTACT Horizontal stabilizer, elevator, and trim tab UNDAMAGED; HINGES SECURE; TRIM TAB ATTACHMENT PIN IN PLACE; NO EXCESSIVE PLAY Vertical stabilizer and rudder UNDAMAGED; FULL FREE MOVEMENT ELT — switch position and antenna ARMED; ANTENNA CONNECTED Left main gear — strut, tire, and brake assembly STRUT NORMAL; TIRE INFLATED AND SERVICEABLE; BRAKE DISC AND CALIPER SERVICEABLE Left aileron and flap — hinge attachment and travel HINGES SECURE; FULL FREE MOVEMENT; NO DAMAGE Left wingtip and lights UNDAMAGED; LENS INTACT Antennas — all visible UNDAMAGED AND SECURE Tiedowns, chocks, and control lock ALL REMOVED

Passenger and occupant briefing SEAT BELTS, DOOR OPERATION, NO SMOKING, EMERGENCY PROCEDURES BRIEFED Seats — adjusted and locked; seat belts and shoulder harnesses ADJUSTED, LOCKED, AND FASTENED FOR ALL OCCUPANTS Cargo and baggage — weight and balance COMPUTED WITHIN LIMITS; CARGO SECURED; CARGO DOOR LATCHED Control lock REMOVED; FLIGHT CONTROLS FREE AND CORRECT Circuit breakers ALL IN — NONE TRIPPED Avionics master OFF BEFORE APPLYING BATTERY Master switch (battery) ON Fuel quantity gauges CROSS-CHECKED WITH VISUAL INSPECTION; CONSISTENT Annunciator / warning lights — press to test ALL ILLUMINATE ON TEST; NONE REMAIN AFTER Fuel selector BOTH Elevator trim SET TO TAKEOFF POSITION PER POH Flaps UP / 0° Propeller control FULL FORWARD Parking brake SET

Propeller arc and surrounding area CLEAR — ANNOUNCE CLEAR PROP Beacon / anti-collision light ON Continental IO-540 is fuel-injected. Cold start: mixture rich, use boost pump briefly to build fuel pressure, then follow POH priming procedure before engaging starter. Hot start: use POH hot-start technique — typically involves unloading the fuel lines with mixture at cutoff before cranking. Fuel-injected start technique — cold or hot FOLLOW POH PROCEDURE FOR CONDITIONS Starter — engage RELEASE KEY PROMPTLY WHEN ENGINE FIRES Mixture — after engine fires ADVANCE SMOOTHLY TO RICH Oil pressure RISING WITHIN 30 SECONDS; IN GREEN ARC Throttle — set idle STABILIZE AT NORMAL IDLE RPM Alternator output CHARGING — AMMETER OR LOADMETER SHOWING POSITIVE OUTPUT Avionics master ON — AFTER ENGINE STABILIZED

ATIS / weather OBTAINED; ALTIMETER SETTING NOTED Altimeter SET TO CURRENT SETTING; FIELD ELEVATION CONFIRMED Heading indicator UNCAGED AND ALIGNED WITH MAGNETIC COMPASS Attitude indicator ERECT AND STABLE Engine instruments — oil pressure, oil temperature, fuel flow ALL IN GREEN ARC; NORMAL FOR POWER SETTING Transponder SQUAWK CODE SET; MODE ALT Navigation and communication radios DEPARTURE FREQUENCIES SET Taxi clearance or advisory call OBTAINED OR MADE Lights — taxi and nav lights ON AS REQUIRED Parking brake — release to begin taxi; check brakes immediately BOTH BRAKES OPERATIVE

Parking brake SET Flight controls — full deflection check FULL AND FREE; MOVEMENT CORRECT TO INPUT Elevator trim SET TO TAKEOFF POSITION Fuel selector BOTH Fuel quantity — confirm adequate ADEQUATE FOR FLIGHT WITH RESERVES Mixture RICH, OR LEANED FOR HIGH-ELEVATION DEPARTURE PER POH Propeller control FULL FORWARD Throttle — advance to run-up power SET TO RUN-UP RPM PER POH Magneto check — LEFT mag NOTE RPM DROP; WITHIN LIMITS PER POH Magneto check — RIGHT mag NOTE RPM DROP; WITHIN LIMITS PER POH; DROP BETWEEN MAGS WITHIN TOLERANCE Magneto check — return to BOTH RPM RESTORES Propeller governor cycle — reduce RPM PULL PROP CONTROL AFT; OBSERVE EXPECTED RPM DROP PER POH Oil must be at operating temperature before cycling the prop. Cycle at least once to confirm governor response. Advance back to full forward after confirming drop. Propeller governor cycle — advance to full forward RPM RETURNS TO RUN-UP VALUE; PROP CONTROL FULL FORWARD Engine instruments at run-up power OIL PRESSURE AND TEMPERATURE IN GREEN; FUEL FLOW WITHIN NORMAL RANGE Throttle — reduce to idle ENGINE IDLES SMOOTHLY WITHOUT STUMBLING Alternate air CONFIRMED CLOSED / NORMAL POSITION Fuel pump (boost pump) ON FOR TAKEOFF PER POH Flaps SET PER POH FOR DEPARTURE TYPE AND CONDITIONS Doors — cabin and cargo CLOSED AND LATCHED; CARGO DOOR LOCKING PINS CONFIRMED ENGAGED Seat belts and shoulder harnesses — all occupants FASTENED AND SNUG Transponder ALT Runway environment and traffic CLEAR; TAKEOFF CLEARANCE OR RIGHT-OF-WAY CONFIRMED Departure briefing — abort point and emergency intentions REVIEWED

Landing light and strobes ON Throttle — advance smoothly to full power FULL POWER; MANIFOLD PRESSURE AND RPM AT EXPECTED VALUES PER POH Engine instruments — verify on roll OIL PRESSURE, FUEL FLOW, AND RPM NORMAL; ABORT IF ANY INDICATION OUT OF LIMITS Directional control during roll CENTERLINE MAINTAINED WITH RUDDER; TORQUE AND P-FACTOR CORRECTED Rotate — at Vr per POH SMOOTH BACK PRESSURE TO LIFT OFF Positive rate of climb CONFIRMED ON VSI Flaps — retract if extended INCREMENTALLY AFTER OBSTACLES CLEARED AND AIRSPEED SAFE PER POH

Airspeed — establish climb speed BEST RATE OR CRUISE-CLIMB SPEED PER POH Power — set climb power PER POH Mixture — lean as altitude increases ENRICH BELOW DENSITY ALTITUDE REQUIRING LEANING; LEAN PER POH ABOVE Fuel pump (boost pump) OFF ABOVE PATTERN ALTITUDE UNLESS POH REQUIRES OTHERWISE Engine instruments — CHT, oil temperature, oil pressure ALL WITHIN GREEN ARC Fuel quantity — cross-check gauges ADEQUATE REMAINING; CONSISTENT WITH EXPECTED BURN Heading indicator CROSS-CHECKED WITH COMPASS; ADJUSTED IF DRIFTED

Power — set cruise RPM and manifold pressure PER POH FOR ALTITUDE AND DESIRED PERFORMANCE Mixture — lean using EGT PER POH CRUISE LEANING TECHNIQUE; FUEL FLOW WITHIN CRUISE RANGE Trim — adjust for hands-off level flight TRIMMED Engine instruments — monitor throughout cruise OIL PRESSURE, OIL TEMPERATURE, CHT ALL IN GREEN ARC Fuel quantity — cross-check both tanks against time en route ADEQUATE WITH RESERVES; BURN RATE CONSISTENT WITH POH Fuel selector BOTH Altimeter — update setting CURRENT SETTING; ALTITUDE VERIFIED Navigation — position and route plan ON TRACK; ALTERNATES ADEQUATE

ATIS / destination weather OBTAINED; ALTIMETER SETTING NOTED Altimeter — set destination current setting SET; ALTITUDE VERIFIED Power — reduce gradually AVOID PROLONGED IDLE AT HIGH ALTITUDE TO LIMIT SHOCK COOLING RISK Mixture — enrich as altitude decreases PER POH Fuel selector BOTH Engine instruments WITHIN LIMITS DURING POWER REDUCTION Approach briefing — procedure, runway, frequencies REVIEWED; RADIOS SET Heading indicator CROSS-CHECKED WITH COMPASS; CORRECTED IF NEEDED

Fuel selector BOTH Fuel pump (boost pump) ON Mixture RICH Propeller control FULL FORWARD Flaps — extend to desired setting for approach type and conditions SET PER POH Approach airspeed ESTABLISHED PER POH FOR FLAP SETTING AND WEIGHT Doors — cabin and cargo CLOSED AND LATCHED; CARGO DOOR LOCKING PINS CONFIRMED ENGAGED Seat belts and shoulder harnesses — all occupants FASTENED AND SNUG Landing light ON Runway — in sight, clear of traffic, length adequate CONFIRMED

Final approach — stabilized by 500 ft AGL AIRSPEED AND SINK RATE STABLE PER POH Flaps — full or selected setting for conditions SET PER POH Runway alignment and crosswind correction ON CENTERLINE; WIND CORRECTION APPLIED Threshold crossing and flare — reduce power smoothly FLARE TO NORMAL LANDING ATTITUDE; POWER TO IDLE Touchdown — main wheels first in normal attitude DIRECTIONAL CONTROL MAINTAINED WITH RUDDER Braking — apply smoothly as needed AVOID WHEEL LOCKUP; ADEQUATE FOR AVAILABLE RUNWAY Clear the active runway before stopping TAXI CLEAR; FLAPS UP

Throttle FULL POWER — ADVANCE SMOOTHLY WITHOUT HESITATION Mixture RICH — CONFIRM ALREADY SET Propeller FULL FORWARD — CONFIRM ALREADY SET Pitch — establish climb attitude; apply right rudder for torque ARREST SINK RATE; CLIMBING Flaps — retract to go-around setting immediately INITIAL RETRACT POSITION PER POH Positive rate of climb confirmed VSI AND ALTIMETER INDICATE CLIMB Flaps — retract fully after obstacles cleared and airspeed safe per POH UP Climb airspeed — Vx or Vy as required PER POH Radio — advise ATC or announce on CTAF CALL MADE

Fuel pump (boost pump) — after clearing runway OFF Transponder STANDBY Flaps UP Landing light — after vacating runway OFF Avionics master — before mixture cutoff OFF Engine — cool at idle before shutdown IDLE FOR COOLING PERIOD; OBSERVE CHT DECREASING Mixture — shut down engine PULL TO IDLE CUTOFF; ALLOW ENGINE TO CEASE FIRING COMPLETELY Throttle — after engine stops CLOSED Magnetos / ignition OFF Master switch (battery) OFF Beacon / anti-collision light OFF Parking brake SET Control lock INSTALLED Cargo door — confirm latches and locking pins fully engaged SECURED Fuel caps — both tanks SECURE Tiedowns — all three points SECURED Pitot cover and cowl plugs INSTALLED IF PARKED EXTENDED PERIOD Post-flight discrepancies NOTED IN AIRCRAFT MAINTENANCE LOG