65e3feaf68fe65be2ec1b8c138793a6ded6eb24b4856b36b2a825cb52022e0a8 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.

Aircraft documents (ARROW) ON BOARD AND CURRENT Fuel quantity — visually inspect both tanks; verify adequate fuel for flight with legal reserves CONFIRMED, ADEQUATE Fuel grade and appearance — sample from all sump drains CORRECT GRADE PER POH; CLEAR, NO WATER OR SEDIMENT Fuel filler caps — both tanks PROPERLY SEATED AND SECURED AFTER SAMPLING Fuel vent lines UNOBSTRUCTED Engine oil level WITHIN OPERATING RANGE PER POH; DIPSTICK SECURE Engine compartment — fuel lines, oil hoses, wiring NO LEAKS; ALL CONNECTIONS SECURE Induction air inlet CLEAR AND UNOBSTRUCTED IO-360 is fuel-injected — no carburetor heat. Alternate air control bypasses the induction filter. Exhaust stacks — visible portions NO CRACKS OR LOOSE HARDWARE Cowling latches CLOSED AND SECURE Propeller blades — nicks, cracks, erosion SERVICEABLE Spinner and prop hub SECURE; NO CRACKS Nose gear — strut, tire, and steering linkage STRUT EXTENDED NORMALLY; TIRE INFLATED; LINKAGE INTACT; GEAR DOOR CLEAR Pitot tube — cover removed, inlet unobstructed COVER OFF; CLEAR Static ports CLEAR Left main gear — strut, tire, brake, gear door, hydraulic lines STRUT NORMAL; TIRE INFLATED; BRAKE PAD VISIBLE; HYDRAULIC LINES UNDAMAGED; UPLOCK MECHANISM CLEAR Left wing leading edge and fuel vent NO DEFORMATION OR FUEL STAINING; VENT CLEAR Left aileron and flap — travel and attachment HINGES SECURE; FULL FREE MOVEMENT; NO DAMAGE Left wingtip and navigation light UNDAMAGED; LENS INTACT Stall warning vane — left wing leading edge MOVES FREELY; ACTIVATES TONE WHEN LIFTED Horizontal stabilizer, elevator, and trim tab UNDAMAGED; HINGES SECURE; NO EXCESSIVE PLAY Vertical stabilizer and rudder UNDAMAGED; FULL FREE MOVEMENT ELT — armed switch and antenna ARMED; ANTENNA CONNECTED Right main gear — strut, tire, brake, gear door, hydraulic lines STRUT NORMAL; TIRE INFLATED; BRAKE PAD VISIBLE; HYDRAULIC LINES UNDAMAGED; UPLOCK MECHANISM CLEAR Right wing — aileron, flap, wingtip, and navigation light SECURE; FULL FREE MOVEMENT; UNDAMAGED; LENS INTACT All tiedowns, chocks, and control locks REMOVED

POH and weight-and-balance data ON BOARD Seats — adjusted and locked; seatbelts and shoulder harnesses for all occupants ADJUSTED, LOCKED, AND FASTENED Rudder pedals ADJUSTED FOR FULL RUDDER AND BRAKE TRAVEL Control lock REMOVED; AILERON, ELEVATOR, AND RUDDER FREE AND CORRECT Trim — elevator SET TO TAKEOFF POSITION PER POH Avionics master switch OFF — before start to protect avionics from start transient All non-essential electrical switches OFF Circuit breakers ALL IN; CHECK FOR ANY TRIPPED Fuel selector FULLEST TANK — DETENT CONFIRMED ENGAGED Mixture RICH — FULL FORWARD Propeller control FULL FORWARD — HIGH RPM Throttle CRACKED PER POH STARTING GUIDANCE Primer — use as required for engine temperature PUMPED PER POH; LOCKED AFTER USE Gear handle position DOWN — GEAR-DOWN INDICATOR LIGHTS CONFIRMED Parking brake SET

Area around aircraft — announce CLEAR PROP CLEAR Master switch (battery) ON Beacon / anti-collision light ON — before cranking Throttle — set per POH for start condition SET Ignition switch START — crank until engine fires; release immediately Throttle — after start REDUCE TO IDLE RPM PER POH Oil pressure RISING WITHIN 30 SECONDS — if not, shut down immediately Avionics master ON — after engine stabilized at idle Engine instruments ALL IN GREEN; OIL TEMPERATURE RISING NORMALLY Alternator / ammeter CHARGING — positive indication confirmed

ATIS / weather information OBTAINED; ALTIMETER SETTING NOTED Altimeter SET TO CURRENT ALTIMETER SETTING; FIELD ELEVATION CROSS-CHECKED Radios and navigation — departure frequencies LOADED AND SET Transponder CODE SET; MODE SELECTED PER ATC REQUIREMENTS Heading indicator ALIGNED WITH MAGNETIC COMPASS ON KNOWN HEADING Gyroscopic instruments — suction gauge IN GREEN ARC Gear indicator lights THREE GREEN — ALL GEAR DOWN-AND-LOCKED CONFIRMED

Parking brake SET Flight controls — free and correct for wind direction VERIFIED Fuel selector FULLEST TANK — DETENT CONFIRMED Mixture — adjust for field elevation SET PER POH Propeller control FULL FORWARD Engine warm-up — oil temperature IN GREEN ARC BEFORE RUN-UP Throttle — advance to run-up RPM per POH SET Magneto check — LEFT, then RIGHT, return to BOTH DROP ON EACH MAG WITHIN LIMITS PER POH; BOTH DROPS WITHIN DIFFERENTIAL LIMIT Maximum single-magneto drop and maximum differential between magnetos per POH. Return selector to BOTH after check. Propeller cycle — move slowly to low RPM; note drop; advance back to full forward RPM DROP OBSERVED; RPM RETURNED TO FULL HIGH; REPEAT 2–3 TIMES; FINAL POSITION FULL FORWARD Cycling warms governor oil and confirms constant-speed mechanism responds. Do not slam the control forward — cycle smoothly. Throttle — return to idle; confirm smooth idle IDLE SMOOTH; RPM WITHIN LIMITS Suction gauge IN GREEN ARC Engine instruments ALL IN GREEN; NO ANOMALIES Heading indicator — aligned with compass SET Altimeter SET TO CURRENT ALTIMETER SETTING Flaps SET TO TAKEOFF POSITION PER POH Doors and windows LATCHED AND SECURED Transponder ALT MODE Takeoff briefing — abort criteria, initial climb airspeeds, departure route REVIEWED

Runway clear — traffic and obstacles CONFIRMED CLEAR Mixture SET PER POH FOR FIELD ELEVATION Propeller control FULL FORWARD — HIGH RPM Throttle — advance smoothly to full power; check engine instruments FULL POWER; INSTRUMENTS IN GREEN Directional control during roll MAINTAINED WITH RUDDER Rotate — at rotation airspeed per POH SMOOTH BACK PRESSURE APPLIED Gear retraction — after positive rate of climb and no runway remaining for landing GEAR HANDLE UP; CONFIRM GEAR RETRACTS AND LIGHTS EXTINGUISH

Airspeed — establish best-rate or cruise-climb speed ESTABLISHED PER POH Engine instruments — oil pressure, oil temp, CHT WITHIN NORMAL RANGE Power — throttle and RPM ADJUSTED PER POH CLIMB POWER SCHEDULE Mixture LEANED PER POH IF ABOVE DENSITY ALTITUDE THRESHOLD; RICH OTHERWISE Fuel selector APPROPRIATE TANK; MONITOR BALANCE Gear indicator UP — NO GREEN LIGHTS; GEAR-UNSAFE HORN SILENT Flaps RETRACTED PER POH SPEED SCHEDULE AFTER POSITIVE CLIMB ESTABLISHED Heading and altitude ON ASSIGNED DEPARTURE CLEARANCE OR VFR COURSE

Power — throttle and propeller RPM SET TO CRUISE POWER PER POH Set manifold pressure and RPM per POH power table for desired percent power and altitude. Mixture — lean to peak EGT then enrich per POH cruise guidance SET PER POH FOR SELECTED POWER SETTING Trim ADJUSTED FOR HANDS-OFF LEVEL FLIGHT Engine instruments — oil pressure, oil temp, CHT, EGT ALL WITHIN NORMAL RANGES; MONITORED CONTINUOUSLY Fuel quantity — switch tanks per POH interval guidance MONITORED; TANKS BALANCED Gear indicator — confirm UP NO GREEN LIGHTS ILLUMINATED Altimeter and heading indicator — cross-check compass SET AND TRACKING Traffic and airspace — see-and-avoid; altitude and clearance MAINTAINED

ATIS / destination weather OBTAINED; RUNWAY AND APPROACH IN USE NOTED Altimeter — update to destination setting SET TO CURRENT ALTIMETER SETTING Fuel selector — switch to fullest or appropriate tank for approach SELECTED; DETENT ENGAGED Mixture — gradually enrichen as altitude decreases; rich by pattern altitude ENRICHENING WITH DESCENT Power — reduce gradually to avoid shock cooling REDUCED IN INCREMENTS PER POH Heading indicator — cross-check and re-align with compass if needed ALIGNED Radios — approach and tower frequencies; ATC contact established SET AND ACTIVE

Fuel selector — fullest tank; detent confirmed engaged FULLEST TANK SELECTED Mixture RICH — FULL FORWARD FOR GO-AROUND CAPABILITY Propeller control FULL FORWARD — HIGH RPM FOR GO-AROUND AVAILABILITY Gear — place handle DOWN; confirm three green lights; gear-unsafe horn silent THREE GREEN — NOSE, LEFT MAIN, RIGHT MAIN ALL DOWN-AND-LOCKED Verbalize THREE GREEN to confirm positive indication. The gear-unsafe horn should be silent with throttle at approach power setting. Flaps — extend to approach setting SET PER POH Airspeed — stabilize at approach speed ESTABLISHED PER POH Seatbelts — all occupants SECURED

Gear — final verification before crossing threshold THREE GREEN CONFIRMED Approach — stable on glidepath, centerline, and airspeed STABILIZED Flaps — landing setting as required SET PER POH Flare — initiate at appropriate height; reduce power smoothly to idle SMOOTH FLARE; POWER TO IDLE Touchdown — main wheels first; nose lowered gently after speed decays DIRECTIONAL CONTROL MAINTAINED WITH RUDDER Braking — smooth and progressive; avoid wheel lockup APPLIED AS NEEDED; AERODYNAMIC BRAKING USED DURING ROLLOUT

Throttle FULL POWER — advance smoothly and promptly Pitch — establish positive climb attitude; arrest descent POSITIVE CLIMB ATTITUDE ESTABLISHED Flaps — retract to first notch or takeoff setting; full retraction in stages at safe airspeed per POH RETRACTING IN STAGES Airspeed — accelerate to climb speed before further flap retraction CLIMBING AIRSPEED ESTABLISHED Gear — UP after positive rate of climb established and no landing option remains GEAR HANDLE UP; LIGHTS EXTINGUISHING Trim ADJUSTED TO REDUCE CONTROL FORCES DURING CLIMB ATC — advise of go-around; comply with missed approach or traffic pattern instructions ADVISED

Flaps — retract after clear of active runway RETRACTED Transponder STBY OR GROUND MODE Taxi speed — brakes tested gently; maintain awareness of gear-unsafe horn sensitivity CONTROLLED

Parking brake SET Mixture — idle cutoff to shut down engine IDLE CUTOFF — ENGINE STOPPED Ignition switch OFF — after engine stops Avionics master OFF All electrical switches OFF Master switch OFF Fuel selector LEFT OR RIGHT PER OPERATOR PRACTICE; AVOID LEAVING ON BOTH UNATTENDED Flight controls — gust lock or control lock INSTALLED PER OPERATOR PRACTICE Pitot cover and tiedowns COVER INSTALLED; AIRCRAFT TIED DOWN AND CHOCKED IF OUTSIDE