9a5b0ffeca6dc7c4ddd581eed6e5f543d6ae8c48b0ee4eafd5b958bb2fac76d9 Contains no airspeeds, power settings, fuel quantities or other limitations — must come from aircraft POH. Equipment variations exist across SR22 G5 aircraft. Verify all items against the specific aircraft POH and avionics configuration before use.

Aircraft documents — Airworthiness, Registration, Radio station license, Operating limitations (POH/AFM), Weight-and-balance data ON BOARD AND CURRENT Fuel quantity — visually verify both wing tanks; confirm quantity matches planned fuel load VERIFIED; ADEQUATE FOR FLIGHT WITH REQUIRED RESERVES Fuel grade and sample appearance AVGAS 100LL CONFIRMED; SAMPLE CLEAR AND BRIGHT, NO WATER OR DEBRIS Fuel caps — both wing tanks SECURED AND LOCKED Fuel sump drains — both wing sumps and fuel selector/gascolator sump SAMPLED CLEAR; NO WATER OR CONTAMINATION Engine oil level — check dipstick WITHIN OPERATING BAND PER POH; OIL CAP SECURE Engine compartment — hoses, clamps, wiring, and induction components NO LEAKS, CHAFING, OR LOOSE HARDWARE Induction air filter and alternate air door FILTER CLEAN; ALTERNATE AIR DOOR CLOSES FREELY Exhaust system — exhaust stacks, muffler, and heat exchanger visible surfaces NO CRACKS, HOLES, OR LOOSE FASTENERS Cowling and cowl fasteners CLOSED; ALL FASTENERS SECURED Propeller blades — leading edges, trailing edges, and tips for nicks, cracks, or erosion BLADES SERVICEABLE; NO DEFORMATION Spinner and prop hub — security and cracking SECURE; NO VISIBLE CRACKS Nose gear — strut extension, tire condition and inflation, shimmy damper, and fork STRUT EXTENDED NORMALLY; TIRE SERVICEABLE Pitot tube — cover removed, inlet unobstructed COVER REMOVED; INLET CLEAR Angle-of-attack (AoA) probe PORTS CLEAR AND UNDAMAGED Static ports — both sides of fuselage CLEAR AND UNDAMAGED Left wing leading edge and composite skin NO DELAMINATION, CRACKS, OR FUEL STAINING Left aileron — hinge condition, surface travel, and gap seal HINGES SECURE; FULL FREE MOVEMENT; NO BINDING Left flap — hinge attachment and surface condition ATTACHED SECURELY; SURFACE UNDAMAGED Left wingtip, navigation light, and strobe UNDAMAGED; LENS INTACT Left main gear — composite fairing, tire condition and inflation, brake disk and pads FAIRING SECURE; TIRE SERVICEABLE; BRAKE ADEQUATE CAPS parachute handle area — left side of canopy overhead HANDLE GUARD IN PLACE; NO DAMAGE TO HOUSING OR INITIATOR AREA Confirm the CAPS pull handle guard (safety pin removed only for flight) and canopy attachment are visually intact. Do not actuate. Tail — horizontal stabilizer, elevator, and trim tab condition UNDAMAGED; HINGES SECURE; NO EXCESSIVE PLAY Vertical stabilizer and rudder UNDAMAGED; FULL FREE MOVEMENT ELT — switch armed; antenna connection secure ARMED; ANTENNA CONNECTED Right main gear — fairing, tire, and brake SERVICEABLE Right wing — leading edge, aileron, flap, and wingtip NO DAMAGE; CONTROLS FREE Tiedowns, chocks, and control lock ALL REMOVED

Passenger briefing — seat adjustment, belts, exits, no smoking, CAPS handle location COMPLETED Brief passengers on the CAPS handle overhead and that it is only to be pulled at pilot command. Brief on door operation in emergency. Seats — adjusted forward/aft for sidestick reach; seat back upright ADJUSTED AND LOCKED Seat belts and shoulder harnesses — all occupants FASTENED AND SNUG CAPS handle guard (safety pin) REMOVED FOR FLIGHT; STOWED On some configurations a safety pin is used on the ground; confirm per aircraft-specific procedure. Avionics master switch OFF (before applying battery power) Battery master switch ON Fuel quantity indicators on PFD/MFD VERIFY AGAINST VISUAL INSPECTION Annunciator panel / CAS messages — test lamp and confirm clear ALL ILLUMINATE ON TEST; NONE REMAIN Fuel selector valve BOTH Mixture control RICH (or adjusted per POH for field elevation) Propeller control FULL FORWARD Throttle CLOSED, THEN CRACKED SLIGHTLY OPEN PER POH START PROCEDURE Elevator trim SET TO TAKEOFF POSITION Parking brake SET

Propeller arc and ground area ahead — visual check CLEAR — announce CLEAR PROP Beacon / anti-collision light ON The IO-550 is fuel-injected. Cold start and hot start techniques differ. Follow the POH procedure for ambient temperature and soak conditions. Avoid over-priming, which can wash cylinder walls and cause hard starts. Fuel pump — prime per POH start technique FOLLOW POH COLD/HOT START PROCEDURE Ignition switch — to START ENGAGE STARTER; RELEASE WHEN ENGINE FIRES Throttle — adjust after start REDUCE TO IDLE; ENGINE RUNNING SMOOTHLY Oil pressure RISING WITHIN LIMITS PER POH; ABORT IF NOT RISING Electrical system — ammeter and voltmeter POSITIVE CHARGE; VOLTAGE NORMAL Avionics master switch ON Perspective avionics — await initialization; check for CAS messages SYSTEMS INITIALIZED; NO ABNORMAL MESSAGES Engine instruments — oil temp, oil pressure, fuel flow WITHIN NORMAL BANDS PER POH

ATIS or weather advisory OBTAINED; ALTIMETER SETTING NOTED Altimeter — set to current reported setting SET; FIELD ELEVATION CONFIRMED ON PFD PFD attitude indicator — confirm upright and stable ERECT AND STABLE Transponder — mode and code ALT; SQUAWK CODE SET Navigation sources — GPS databases current; flight plan loaded if applicable DATABASE CURRENT; ROUTE VERIFIED Taxi clearance or radio call OBTAINED OR ANNOUNCED Parking brake RELEASE

Parking brake SET Flight controls — full sidestick deflection in pitch and roll; rudder pedals full travel both directions FULL AND FREE; CORRECT SENSE CONFIRMED Elevator trim TAKEOFF POSITION Fuel selector BOTH Fuel quantity CONFIRMED ADEQUATE FOR PLANNED FLIGHT PLUS RESERVES Mixture RICH OR PER POH FOR FIELD ELEVATION Propeller control FULL FORWARD Throttle — advance to run-up power setting per POH STABILIZED AT RUN-UP RPM Left magneto check — select L only NOTE RPM DROP; WITHIN LIMITS PER POH Right magneto check — select R only NOTE RPM DROP; WITHIN LIMITS PER POH Magneto switch — return to BOTH RPM RESTORES Propeller governor cycle — pull prop control aft to reduce RPM OBSERVE RPM DROP PER POH; OIL MUST BE AT OPERATING TEMPERATURE Confirm governor response by pulling the prop control aft to reduce RPM, then advancing back to full forward. Perform at least one full cycle. Do not cycle a cold engine. Propeller governor cycle — advance prop control to full forward RPM RETURNS TO RUN-UP VALUE; PROP CONFIRMED FULL FORWARD Engine instruments at run-up power OIL TEMP AND PRESSURE IN GREEN; ALL GAUGES NORMAL Throttle — reduce to idle; verify smooth idle IDLES WITHOUT ROUGHNESS OR STUMBLE CAS annunciators NO ABNORMAL MESSAGES Flaps SET PER POH FOR DEPARTURE TYPE Doors — both front doors closed and latched; verify green door-closed indication LATCHED; DOOR ANNUNCIATOR OUT Seat belts and shoulder harnesses — all occupants final check FASTENED AND SNUG Runway environment and traffic CLEAR; TAKEOFF CLEARANCE OR RIGHT-OF-WAY CONFIRMED Departure briefing — runway, initial heading, abort plan, CAPS availability BRIEFED

Transponder ALT (if not already set) Landing light and strobes ON Mixture RICH OR PER POH Propeller control FULL FORWARD — CONFIRMED Throttle — advance smoothly to full power FULL POWER; ENGINE INSTRUMENTS CHECKED IN GREEN Directional control during roll — sidestick and rudder pedals MAINTAIN RUNWAY CENTERLINE Rotate at Vr per POH LIFT OFF AT CORRECT AIRSPEED Establish positive rate of climb; confirm on altimeter POSITIVE RATE CONFIRMED Climb at Vx or Vy as required per POH CLIMBING AT APPROPRIATE AIRSPEED Flaps — retract after positive rate and obstacle clearance, per POH schedule RETRACTED

Throttle and power — set climb power per POH SET; INSTRUMENTS CONFIRMED IN NORMAL RANGE Propeller control — set climb RPM if reducing from full forward SET PER POH Mixture — lean as required for altitude during climb per POH ADJUSTED PER POH CLIMB GUIDANCE Fuel flow and engine instruments WITHIN NORMAL OPERATING RANGE Fuel selector BOTH Altimeter — confirm correct setting; update as received SET AND CROSS-CHECKED Landing light — turn off per preference or ATC area AS REQUIRED Radar altimeter / terrain display on MFD REVIEWED FOR TERRAIN AWARENESS

Throttle — set cruise power percent per POH and performance charts SET PER POH Propeller — set cruise RPM per POH SET Mixture — lean to peak or lean-of-peak EGT per POH technique for altitude and power LEANED PER POH; EGT/TIT MONITORED Fuel flow and engine instruments — cross-check at cruise power FUEL FLOW, OIL TEMP, OIL PRESSURE, AND CHTs WITHIN LIMITS Fuel quantity and fuel balance — monitor both tanks QUANTITY ADEQUATE; TANKS IN BALANCE Altimeter — confirm or update as needed in cruise CURRENT SETTING CONFIRMED Autopilot — engage if desired; check engaged modes on PFD ENGAGED AND TRACKING CORRECTLY Position and flight plan progress — verify on MFD ON ROUTE; FUEL REMAINING CONSISTENT WITH PLAN Weather radar / XM Weather — monitor for en-route hazards REVIEWED

ATIS or destination weather — obtain and note altimeter setting OBTAINED Altimeter — set to destination setting SET; FIELD ELEVATION CROSS-CHECKED Fuel quantity and fuel selector QUANTITY ADEQUATE; SELECTOR ON BOTH Mixture — enrichen as altitude decreases per POH ADJUSTED FOR ALTITUDE AND POWER Power — reduce per POH descent technique; monitor CHT cooling rate POWER REDUCED GRADUALLY; CHTs WITHIN LIMITS Avoid rapid power reductions that shock-cool cylinders. Follow POH recommendations for descent power settings. Approach briefing — runway, approach type, missed approach plan BRIEFED Navigation aids and GPS approach loaded, if applicable APPROACH LOADED AND VERIFIED

Fuel selector BOTH Mixture — enrichen to full rich at pattern altitude unless high elevation RICH OR PER POH FOR FIELD ELEVATION Propeller control — advance to full forward for go-around readiness FULL FORWARD Gear — fixed; no action required; verify no abnormal drag FIXED GEAR CONFIRMED; COMPOSITE FAIRINGS INTACT (CONFIRMED ON WALK-AROUND) Seat belts and shoulder harnesses — all occupants tightened SECURE AND SNUG Landing light ON Flaps — extend to approach setting per POH EXTENDED PER POH Airspeed — establish approach speed per POH for flap setting and weight STABILIZED AT CORRECT APPROACH SPEED

Final approach — confirm stabilized; airspeed per POH STABILIZED; SPEED CORRECT; GLIDEPATH CONFIRMED Runway — confirm clear of traffic; clearance obtained or traffic rights confirmed CLEAR TO LAND Flaps — full or per POH for conditions SELECTED; POSITION CONFIRMED ON PFD Throttle at touchdown — reduce to idle IDLE AT FLARE Landing attitude — main wheels first, then nose gear; sidestick back through rollout SMOOTH TOUCHDOWN; NOSE HELD OFF Braking — apply after nose gear lowered; brake firmly as required CONTROLLED DECELERATION Runway exit — clear at safe taxi speed CLEARED AT FIRST SUITABLE TURNOFF

Throttle — advance promptly to full power FULL POWER Pitch — establish positive climb attitude on sidestick CLIMB ATTITUDE SET Flaps — retract to approach flap setting immediately; full retraction after positive rate and obstacle clearance RETRACTED PER POH SCHEDULE Airspeed — accelerate to and maintain climb speed per POH ESTABLISHED AT CORRECT SPEED Propeller FULL FORWARD Mixture RICH OR PER POH Advise ATC of missed approach; comply with published or ATC missed approach instructions ATC NOTIFIED; PROCEDURE FOLLOWED

Transponder SQUAWK VFR OR PER ATC INSTRUCTION Flaps RETRACT FULLY AFTER CLEARING RUNWAY Landing light OFF (or per preference) Strobes OFF AFTER CLEARING ACTIVE RUNWAY Mixture — adjust for taxi conditions if extended ground operation at high elevation ADJUSTED AS NEEDED Brakes — confirm normal taxi brake pressure NORMAL

Parking brake SET Avionics — turn off all avionics before killing power OFF Throttle — reduce to idle IDLE Mixture — pull to IDLE CUTOFF to shut down engine IDLE CUTOFF; ENGINE STOPS Ignition switch OFF AFTER ENGINE STOPS Master switch — battery off OFF CAPS handle guard (safety pin) REINSTALLED PER AIRCRAFT PROCEDURE Control lock INSTALLED ON SIDESTICK Fuel selector BOTH (or per POH — confirm aircraft-specific preference) Doors and windows CLOSED AND SECURED Tiedowns — attach all three points; nose ring and wing tiedowns SECURED Pitot cover INSTALLED Aircraft logbook entry — flight time, squawks if any COMPLETED