93a29bde8fd53ab7c847cb0d3062c4684ee2f4a8073ba5f5aa778da471db1ee5 Contains no airspeeds, power settings, fuel quantities, manifold pressure limits, or other numerical limitations — all must come from the specific aircraft POH. Equipment and avionics vary widely across 210 N airframes. Verify every item against the specific aircraft and its POH before use.

Aircraft documents (ARROW) ON BOARD AND CURRENT Weight and balance COMPUTED AND WITHIN LIMITS Fuel quantity — visually confirm both tanks; compare with gauges VERIFIED, ADEQUATE FOR FLIGHT WITH REQUIRED RESERVES Fuel grade and appearance CORRECT GRADE PER POH; COLOR CONSISTENT, NO CONTAMINATION OR WATER Fuel caps — both tanks SECURELY SEATED AND LOCKED Fuel sump drains — both wing tanks and gascolator SAMPLED; CLEAR, CORRECT COLOR, NO WATER OR SEDIMENT Fuel vent outlets CLEAR AND UNOBSTRUCTED Engine oil level WITHIN OPERATING RANGE PER POH; FILLER CAP SECURE Engine compartment — fuel lines, oil lines, turbocharger, intercooler hoses, and wiring NO LEAKS, CHAFING, OR LOOSE CONNECTIONS Induction air inlet and alternate induction door CLEAR; DOOR CLOSES AND SEALS PROPERLY Turbocharger — oil lines, clamps, and turbine housing SECURE; NO OIL STAINING OR CRACKS Exhaust system — stacks, risers, and turbocharger outlet; check for cracks NO CRACKS, LOOSE HARDWARE, OR SOOTING Cowling fasteners CLOSED AND LATCHED Propeller blades — nicks, cracks, erosion, and leading edges SERVICEABLE Propeller spinner and hub SECURE, NO CRACKS OR LOOSE SCREWS Nose gear strut, torque links, and nose tire STRUT EXTENDED NORMALLY; TIRE INFLATED AND SERVICEABLE Pitot tube — cover removed, inlet clear COVER OFF, UNOBSTRUCTED Static ports — both sides CLEAR Left wing leading edge and upper/lower skin NO DEFORMATION, FUEL STAINING, OR IMPACT DAMAGE Left wing fuel cap and vent CAP LOCKED; VENT CLEAR Left aileron — hinge pins, balance weight, and full travel SECURE; FULL FREE MOVEMENT Left flap — hinge attachment, actuator, and condition SECURE; NO DAMAGE Left wingtip and navigation/strobe light UNDAMAGED; LENS INTACT Left main gear — strut extension, tire, brake assembly, and gear door STRUT NORMAL; TIRE SERVICEABLE; BRAKES ADEQUATE; DOOR UNDAMAGED Left gear retraction linkage and up-lock — visible check NO OBVIOUS DAMAGE OR LOOSE HARDWARE Fuselage — antennas, skin condition, and cabin door seals SECURE; NO DAMAGE Horizontal stabilizer, elevator, and trim tab — both sides UNDAMAGED; HINGES SECURE; NO EXCESSIVE PLAY Vertical stabilizer and rudder UNDAMAGED; FREE MOVEMENT; NO BINDING ELT — armed switch and antenna ARMED; ANTENNA CONNECTED AND SECURE Right main gear — strut, tire, brake, and gear door STRUT NORMAL; TIRE SERVICEABLE; BRAKES ADEQUATE; DOOR UNDAMAGED Right flap and aileron — condition and full travel SECURE; FULL FREE MOVEMENT; NO DAMAGE Right wing leading edge, fuel cap, and vent NO DAMAGE; CAP LOCKED; VENT CLEAR Right wingtip and navigation/strobe light UNDAMAGED; LENS INTACT All tiedowns, chocks, and gust locks REMOVED

POH and weight-and-balance documents ON BOARD Seats — adjusted fore/aft and locked; occupant seat belts and shoulder harnesses ADJUSTED AND FASTENED Control lock REMOVED; CONTROLS CHECKED FOR FULL FREE MOVEMENT Avionics master OFF (before applying battery power) Master switch (battery) ON Fuel quantity gauges CHECK — agree with visual inspection Annunciator / warning lights — press-to-test ALL ILLUMINATE ON TEST; NONE REMAIN ON AFTER TEST Landing gear position lights THREE GREEN; GEAR-DOWN INDICATION Gear warning horn — verify audible with throttle at idle HORN SOUNDS WITH GEAR HANDLE DOWN AND THROTTLE REDUCED Fuel selector FULLEST TANK (or per POH fuel management) Elevator trim SET TO TAKEOFF POSITION Flap position indicator INDICATES UP Propeller control FULL FORWARD (HIGH RPM) Mixture control RICH (or adjusted per POH for field elevation) Throttle CLOSED THEN CRACKED SLIGHTLY OPEN Alternate air control CLOSED (NORMAL) Cowl flaps OPEN Parking brake SET

Propeller arc and surrounding area CLEAR — ANNOUNCE 'CLEAR PROP' Beacon / anti-collision light ON Throttle CRACKED OPEN PER POH Mixture RICH (or per POH for hot/cold start) Cold start: prime per POH. Hot start: follow manufacturer hot-start procedure — flooding a TSIO-520 is common. Ignition switch START — RELEASE WHEN ENGINE FIRES Oil pressure RISES WITHIN 30 SECONDS; INDICATION IN GREEN ARC Throttle — adjust SET TO IDLE OR LOW WARM-UP POWER PER POH Avionics master ON Engine instruments — oil temperature, oil pressure, CHT, EGT MONITOR; WARM UP BEFORE INCREASING POWER Alternator output and ammeter CHARGING; AMMETER IN NORMAL RANGE

Radios and avionics — ATIS, clearance, and COM frequencies SET Transponder SET CODE; ALTITUDE MODE VERIFIED Heading indicator ALIGNED WITH MAGNETIC COMPASS Altimeter SET TO LOCAL ALTIMETER SETTING; CHECK FIELD ELEVATION Electrical load — lights, pitot heat, and other equipment CHECKED ON AND OFF; AMMETER RESPONDS NORMALLY Brakes — parking brake release; confirm brake effectiveness BRAKES EFFECTIVE Taxi clearance OBTAINED IF AT TOWERED FIELD

Parking brake SET Flight controls — full travel check FREE AND CORRECT Instruments — airspeed, altimeter, VSI, turn coordinator, attitude indicator, heading indicator CHECKED AND SET Fuel selector FULLEST TANK (per POH) Mixture RICH (or per POH for field elevation) Cowl flaps OPEN Engine run-up — advance throttle to run-up power per POH POWER SET; ENGINE SMOOTH Magneto check — left, right, both DROP WITHIN LIMITS PER POH; BOTH EQUAL OR NEAR EQUAL; NO ROUGHNESS Propeller cycle — advance to full forward, then reduce RPM; note drop; advance back RPM DROP NOTED; PROP RETURNS TO GOVERNED RPM; OIL CIRCULATED Cycle prop at least once; some operators cycle 2–3 times to ensure warm oil reaches the governor and dome. Verify prop responds immediately to movement of the prop control. Manifold pressure — check turbocharger controls at run-up power MP STABLE; NO OVERBOOST; WASTEGATE OPERATING NORMALLY PER POH Engine instruments — oil temperature, oil pressure, CHT, EGT ALL IN GREEN; TEMPERATURES ADEQUATE FOR TAKEOFF Alternate air control CLOSED; CHECK POWER LOSS WHEN OPENED (PER POH) Throttle — reduce to idle; confirm smooth idle SMOOTH IDLE; NO ROUGHNESS Landing gear handle and indicator lights DOWN; THREE GREEN Flaps SET PER POH FOR TAKEOFF CONFIGURATION Elevator trim SET TO TAKEOFF POSITION Doors and windows — latched SECURED Seats and belts — all occupants SECURED AND UPRIGHT Departure briefing — runway, obstacles, emergency landing area if engine fails COMPLETE

Transponder ALTITUDE MODE (ALT) Landing lights ON Throttle — advance smoothly to takeoff power FULL THROTTLE; MANIFOLD PRESSURE WITHIN LIMITS PER POH Engine instruments at full power RPM AND MP WITHIN LIMITS; ALL INSTRUMENTS IN GREEN Rotate at Vr ROTATE PER POH Landing gear — retract after positive rate of climb GEAR UP; THREE GREEN EXTINGUISHES; GEAR DOORS CLOSE Airspeed — establish Vx or Vy PER POH Flaps — retract when obstacle clearance assured and airspeed within flap retraction range RETRACTED

Airspeed — set best rate of climb or cruise climb PER POH Power — reduce to climb power after obstacle clearance MP AND RPM SET PER POH CLIMB TABLE Cowl flaps OPEN; ADJUST AS NEEDED TO KEEP CHT IN NORMAL RANGE Engine instruments — oil temp, oil pressure, CHT, EGT, MP MONITOR; ALL IN GREEN Landing gear indicator CONFIRM UP AND LOCKED; NO WARNING LIGHTS Fuel selector — switch tanks per POH fuel management schedule PER POH Mixture — lean as altitude increases per POH ADJUSTED PER POH FOR ALTITUDE AND POWER SETTING Altimeter and heading indicator RECHECK AND RESET AS NEEDED

Power — set cruise power MP AND RPM PER POH CRUISE TABLE FOR ALTITUDE AND TEMPERATURE Cowl flaps ADJUST TO MAINTAIN CHT IN NORMAL OPERATING RANGE Mixture LEANED PER POH — EGT PEAK METHOD OR SPECIFIC PROCEDURE Engine instruments — oil temp, oil pressure, CHT, EGT, fuel flow, MP ALL IN GREEN; MONITOR PERIODICALLY Fuel quantity — check gauges periodically; compare with planned fuel burn CONSISTENT WITH PLANNED CONSUMPTION; ADEQUATE RESERVES Fuel selector — switch tanks on schedule per POH SWITCHED PER POH TO BALANCE FUEL LOAD Gear position — confirm UP UP; NO WARNING LIGHTS Altimeter and altimeter setting — update with current ATIS or ATC CURRENT SETTING; ALTITUDE CONFIRMED

Power — reduce gradually; avoid rapid throttle reductions on turbocharged engine POWER REDUCED SMOOTHLY PER POH Mixture — enrichen progressively as altitude decreases ENRICHENED PER POH Cowl flaps ADJUST TO MANAGE CHT DURING POWER REDUCTION Engine instruments — CHT and oil temperature MONITOR; AVOID SHOCK COOLING FROM RAPID POWER REDUCTION Fuel selector FULLEST TANK OR PER POH FOR APPROACH Altimeter setting UPDATED WITH CURRENT LOCAL SETTING FROM ATIS OR ATC Destination weather and runway information OBTAINED; APPROACH BRIEFED

Fuel selector FULLEST TANK Mixture RICH (or per POH for field elevation) Propeller FULL FORWARD (HIGH RPM) — ready for go-around Cowl flaps OPEN Landing gear — extend; check handle DOWN GEAR DOWN Gear position indicator lights THREE GREEN — GEAR DOWN AND LOCKED Gear warning horn — confirm operative if throttle reduced HORN SOUNDS AT LOW POWER WITH GEAR HANDLE DOWN AND GEAR NOT LOCKED (normal test) Flaps SET TO APPROACH POSITION PER POH Airspeed — stabilize at approach speed PER POH Landing light ON Seats and belts — all occupants SECURED AND UPRIGHT

Landing gear handle DOWN Gear position indicator lights THREE GREEN — CONFIRMED DOWN AND LOCKED Gear warning horn — active if throttle below threshold HORN AUDIBLE OR SYSTEM VERIFIED Do not land without confirming THREE GREEN. If any light is absent or red, execute go-around and follow the Gear Unsafe procedure.

Final approach airspeed PER POH Gear — three green confirmed DOWN AND LOCKED Flaps — full or as required for landing type PER POH Touchdown — firm but smooth; no ballooning MAINS FIRST OR FULL-STALL PER TECHNIQUE AND CONDITIONS Brakes — apply smoothly after touchdown; avoid nose-wheel first landing SMOOTH AND PROGRESSIVE Rudder steering — maintain directional control during rollout POSITIVE CONTROL MAINTAINED

Throttle — advance smoothly to go-around power FULL THROTTLE; MP WITHIN LIMITS PER POH Propeller FULL FORWARD Mixture RICH Pitch attitude — establish climb attitude; arrest sink POSITIVE CLIMB ESTABLISHED Flaps — retract incrementally; do not retract all at once from full flaps REDUCE TO APPROACH SETTING THEN RETRACT WHEN POSITIVE CLIMB CONFIRMED Landing gear — retract after positive rate confirmed and landing assured to be impossible GEAR UP Airspeed — accelerate to Vy or climb airspeed PER POH Cowl flaps OPEN ATC — advise of go-around NOTIFIED

Flaps RETRACT — VERIFY UP Landing gear — confirm DOWN; three green THREE GREEN Cowl flaps OPEN — allow engine to cool before shutdown Transponder STANDBY OR AS DIRECTED BY ATC Landing light OFF Trim — reset to takeoff position SET

Parking brake SET Avionics and radios OFF Engine — allow to cool at idle; turbocharger cool-down per POH before shutdown IDLED FOR COOL-DOWN PERIOD; TURBO COOLANT FLOW ADEQUATE Mixture IDLE CUTOFF — pull to stop engine Ignition switch OFF (after prop stops) Master switch OFF Fuel selector OFF (if equipped) or LEFT/RIGHT per owner preference Control lock INSTALLED Pitot cover INSTALLED IF APPLICABLE Gear position — confirm DOWN; chocks placed THREE GREEN; CHOCKED Tiedowns — wings and tail SECURED Oil level and visible leaks — post-flight check OIL LEVEL NOTED; NO NEW LEAKS Hobbs and tach — log flight time RECORDED