754659d9dbe88dd62ff72c07e9d20f780861b46a6629f4e64b7402862cad3d9a Contains no airspeeds, power settings, fuel quantities, or other numerical limitations — all must come from the specific aircraft POH. Equipment variations exist across Baron 58 airframes. Verify every item against the specific aircraft and its POH before use.

Aircraft documents (ARROW) ON BOARD AND CURRENT Weight and balance — computed for planned load WITHIN LIMITS PER POH Fuel quantity — visually inspect both tanks each wing; compare with fuel gauges VERIFIED; ADEQUATE FOR FLIGHT PLUS REQUIRED RESERVES Fuel grade and appearance — sample all sump drains including nacelle sumps on both engines CORRECT GRADE PER POH; CLEAR, NO WATER OR SEDIMENT Fuel caps — all filler ports SEATED AND LOCKED SECURELY Left engine oil level — dipstick pulled, checked, cap secured WITHIN OPERATING RANGE PER POH; CAP SECURED Left engine compartment — fuel injection lines, oil lines, induction ducting, and wiring NO LEAKS, CHAFING, OR LOOSE CONNECTIONS Left engine induction air inlet and air filter UNOBSTRUCTED; FILTER SERVICEABLE Left engine exhaust stacks and heat muffs NO CRACKS, LOOSE CLAMPS, OR HEAVY CARBON DEPOSITS Left engine cowling — all fasteners CLOSED AND LATCHED Left propeller — both blades; leading edges, tips, and faces for nicks, cracks, or erosion SERVICEABLE Left propeller spinner and back plate SECURE; NO CRACKS OR LOOSE SCREWS Left main gear — strut extension, torque links, tire condition and inflation, brake assembly, and gear doors STRUT NORMAL; TIRE SERVICEABLE; BRAKES ADEQUATE; DOORS UNDAMAGED Left wing leading edge and upper/lower skin NO DEFORMATION, FUEL STAINING, OR IMPACT DAMAGE Left fuel filler cap and wing vent CAP LOCKED; VENT CLEAR Left aileron — hinges, control rod, balance weight, and travel SECURE; FULL AND FREE MOVEMENT Left flap — hinge pins, actuator linkage, and condition SECURE; NO DAMAGE OR PLAY Left wingtip — nav light and strobe lens UNDAMAGED; LENS INTACT Nose gear — strut extension, torque links, shimmy damper, and nose tire STRUT INFLATED NORMALLY; TIRE SERVICEABLE; HARDWARE SECURE Nose gear doors and retraction linkage visible through wheel well NO DAMAGE; LINKAGE INTACT Pitot tube — cover removed, inlet clear of obstructions and insects COVER REMOVED; UNOBSTRUCTED Static ports — fuselage ports on both sides CLEAR AND UNOBSTRUCTED Fuselage — skin condition, antennas, ELT, cabin entry door latched, pilot door seals NO DAMAGE; ANTENNAS SECURE; DOORS LATCHED The Baron 58 has a separate aft cabin entry door on the right side — inspect its latch and seal as well as the forward pilot door. Horizontal stabilizer, elevator, and trim tab — both sides UNDAMAGED; HINGES SECURE; NO EXCESSIVE PLAY Vertical stabilizer and rudder — hinges and travel UNDAMAGED; FREE MOVEMENT Tail lighting — nav and beacon LENS INTACT AND SECURE ELT — armed switch position and antenna connection ARMED; ANTENNA CONNECTED Right main gear — strut, tire, brakes, and gear doors STRUT NORMAL; TIRE SERVICEABLE; BRAKES ADEQUATE; DOORS UNDAMAGED Right flap and right aileron — condition and full travel SECURE; FULL AND FREE MOVEMENT; NO DAMAGE Right wing leading edge, fuel cap, and vent NO DAMAGE; CAP LOCKED; VENT CLEAR Right wingtip — nav light and strobe lens UNDAMAGED; LENS INTACT Right engine oil level — dipstick pulled, checked, cap secured WITHIN OPERATING RANGE PER POH; CAP SECURED Right engine compartment — fuel injection lines, oil lines, induction ducting, and wiring NO LEAKS, CHAFING, OR LOOSE CONNECTIONS Right engine induction air inlet and air filter UNOBSTRUCTED; FILTER SERVICEABLE Right engine exhaust stacks and heat muffs NO CRACKS, LOOSE CLAMPS, OR HEAVY CARBON DEPOSITS Right engine cowling — all fasteners CLOSED AND LATCHED Right propeller — both blades; leading edges, tips, and faces SERVICEABLE Right propeller spinner and back plate SECURE; NO CRACKS OR LOOSE SCREWS Tiedowns, chocks, and any external gust locks ALL REMOVED

POH — aboard and accessible to crew ON BOARD Seats — position adjusted, seat-back locked; seat belts and shoulder harnesses for all occupants ADJUSTED, LOCKED, AND FASTENED Control lock REMOVED Flight controls — full travel check for freedom of movement FREE AND CORRECT Avionics master switch OFF (prior to applying battery power) Master switch (battery) ON Fuel quantity gauges — both engines CHECK; CONSISTENT WITH VISUAL INSPECTION Annunciator panel — press-to-test ALL LAMPS ILLUMINATE ON TEST; NONE REMAIN LIT Landing gear position indicators THREE GREEN; DOWN-AND-LOCKED CONFIRMED Gear warning horn — throttles retarded, confirm audible warning HORN SOUNDS Left fuel selector LEFT TANK (or fullest tank per POH; NOT OFF) Right fuel selector RIGHT TANK (or fullest tank per POH; NOT OFF) Elevator trim SET FOR TAKEOFF PER POH Rudder trim SET NEUTRAL OR PER POH Aileron trim SET NEUTRAL OR PER POH Flaps UP — confirmed on position indicator Propeller controls — both FULL FORWARD (high RPM) Mixture controls — both RICH (or as required for field elevation per POH) Throttles — both CLOSED; THEN CRACKED SLIGHTLY OPEN Parking brake SET

Area around aircraft — clear of persons and obstructions on both sides CLEAR The IO-550 engines are fuel-injected. Use the hot-start and cold-start procedures from the POH — priming with the boost pump followed by a specific throttle position differs between hot and cold conditions. Left fuel selector LEFT TANK — CONFIRMED ON Left mixture RICH (or as required per POH) Left boost pump — energise briefly to prime per POH cold-start procedure ON MOMENTARILY; FUEL FLOW INDICATED; THEN OFF Left throttle CRACKED OPEN PER POH START SETTING Left ignition switch START — engage starter Left oil pressure — confirm pressure rise after start RISING; WITHIN LIMITS PER POH Left throttle — after engine fires REDUCE TO IDLE PER POH Right fuel selector RIGHT TANK — CONFIRMED ON Right mixture RICH (or as required per POH) Right boost pump — energise briefly to prime per POH cold-start procedure ON MOMENTARILY; FUEL FLOW INDICATED; THEN OFF Right throttle CRACKED OPEN PER POH START SETTING Right ignition switch START — engage starter Right oil pressure — confirm pressure rise after start RISING; WITHIN LIMITS PER POH Right throttle — after engine fires REDUCE TO IDLE PER POH Avionics master switch ON Alternators — both; confirm charging indication BOTH CHARGING; LOADMETERS INDICATING NORMALLY

Oil pressures and oil temperatures — both engines WITHIN NORMAL RANGE PER POH Engine instruments — vacuum, fuel flow, CHT, both engines ALL INDICATING NORMALLY Annunciator panel — confirm no warning lights remain CLEAR Flight instruments — altimeter, heading indicator, attitude indicator, VSI ALTIMETER SET; GYROS ERECTING; INSTRUMENTS ALIVE Heading indicator — aligned with magnetic compass ALIGNED Navigation and communication radios — all sets FREQUENCIES SET; VOLUMES ADJUSTED Transponder CODE SET; IN STANDBY Taxi and position lights as required ON Parking brake RELEASE WHEN READY TO TAXI

Parking brake SET Flight controls — full travel sweep FREE AND CORRECT Trim tabs — elevator, rudder, and aileron SET FOR TAKEOFF PER POH Left fuel selector LEFT TANK OR PER POH; CONFIRM NOT OFF Right fuel selector RIGHT TANK OR PER POH; CONFIRM NOT OFF Mixtures — both engines RICH (or as required for field elevation per POH) Engine run-up — advance both throttles together to run-up power per POH RPM STABILISED AT RUN-UP SETTING ON BOTH ENGINES Left magneto check — select LEFT, then RIGHT, then BOTH RPM DROP ON EACH MAG WITHIN LIMITS PER POH; SPREAD ACCEPTABLE Right magneto check — select LEFT, then RIGHT, then BOTH RPM DROP ON EACH MAG WITHIN LIMITS PER POH; SPREAD ACCEPTABLE Left propeller cycle — advance to full forward, reduce RPM to observe drop, advance back to full forward RPM DROP NOTED; OIL CIRCULATING; CONTROL RETURNS SMOOTHLY Right propeller cycle — advance to full forward, reduce RPM to observe drop, advance back to full forward RPM DROP NOTED; OIL CIRCULATING; CONTROL RETURNS SMOOTHLY Propeller controls — after cycling, both FULL FORWARD (high RPM) FOR TAKEOFF Engine instruments at run-up power — both engines OIL PRESSURE, OIL TEMP, FUEL FLOW, AND CHT ALL WITHIN LIMITS Annunciator panel NO AMBER OR RED LIGHTS Throttles — reduce to idle after run-up SMOOTH IDLE ON BOTH ENGINES Landing gear handle — confirm DOWN position DOWN; THREE GREEN INDICATORS Flaps — set for takeoff TAKEOFF POSITION PER POH; INDICATOR CONFIRMED Doors — pilot door and cabin entry door LATCHED AND SECURED Seat belts and shoulder harnesses — all occupants FASTENED Boost pumps — both, as required for takeoff per POH ON OR OFF PER POH Takeoff briefing — engine failure procedure, abort point, Vmc and Vyse review COMPLETED

Strobes and landing lights ON Transponder ALT (or ON for non-Mode-C) Throttles — advance smoothly to full takeoff power, both engines together FULL POWER; POWER SYMMETRIC Engine instruments — brief crosscheck during roll MANIFOLD PRESSURE, RPM, AND FUEL FLOW NORMAL BOTH ENGINES Rotation — at rotation speed per POH ROTATE SMOOTHLY Landing gear — after positive rate of climb established GEAR UP; THREE GREEN EXTINGUISHED; GEAR-IN-TRANSIT LIGHT OUT Airspeed — climb at or above Vmc; target Vy or Vx per POH POSITIVE CLIMB CONFIRMED

Airspeed — establish climb speed per POH ON SPEED PER POH Power — set climb power per POH (manifold pressure and RPM) CLIMB POWER SET BOTH ENGINES Mixtures — adjust per POH for altitude and climb power ADJUSTED PER POH Boost pumps — off when clear of traffic area per POH OFF PER POH Flaps — retract on schedule per POH if takeoff flaps used UP; CONFIRMED ON INDICATOR Engine instruments — monitor both engines throughout climb OIL PRESSURE, OIL TEMP, CHT, AND FUEL FLOW WITHIN LIMITS Fuel balance — check both tank gauges; consider switching tanks if imbalance developing WITHIN BALANCE LIMITS PER POH Altimeter — set to current altimeter setting; transition to 29.92 at transition altitude as applicable SET

Power — set cruise power per POH (manifold pressure then RPM) CRUISE POWER SET; BOTH ENGINES MATCHED Mixtures — lean per POH for cruise altitude and power setting LEANED TO PEAK EGT OR PER POH PROCEDURE Fuel selectors — confirm tank selection per POH fuel management schedule CORRECT TANKS SELECTED; NEITHER SELECTOR IN OFF Engine instruments — both engines; oil pressure, oil temp, fuel flow, CHT, EGT ALL WITHIN NORMAL CRUISE LIMITS PER POH Fuel quantities — both tanks; compute remaining endurance and compare with plan FUEL BURN CONSISTENT WITH PLANNED CONSUMPTION Alternators and electrical load — both bus voltages and load indicators BOTH ALTERNATORS CHARGING; LOADS BALANCED Vacuum / suction gauge — confirm pressure within operating range WITHIN LIMITS PER POH Autopilot — engage if desired after aircraft is in trim ENGAGED OR HAND FLYING Outside air temperature — monitor for icing conditions NOTED; NO ICING CONDITIONS INDICATED

Fuel selectors — both engines; confirm active tanks have adequate fuel for approach and alternate TANK SELECTION CONFIRMED; FUEL ADEQUATE Mixtures — enrich per POH as altitude decreases ADJUSTED FOR ALTITUDE PER POH Power — reduce gradually; avoid shock-cooling by keeping power changes gentle DESCENT POWER SET PER POH Engine instruments — confirm CHT not falling below limits during descent CHT WITHIN RANGE PER POH Altimeter — set to current destination altimeter setting SET ATIS / destination weather — obtain and brief OBTAINED; RUNWAY AND APPROACH TYPE NOTED Avionics — communications and navigation frequencies set for arrival SET

Fuel selectors — both engines; fullest available tank or per POH CORRECT TANKS CONFIRMED; NOT OFF Mixtures — both engines; rich for landing RICH (or adjusted for field elevation per POH) Propellers — both controls full forward for maximum RPM availability FULL FORWARD Boost pumps — both; on for approach per POH ON PER POH Landing gear — DOWN at or below gear extension speed per POH GEAR DOWN; THREE GREEN; HORN SILENT Flaps — extend to landing position at or below flap extension speed per POH FLAPS SET PER POH; INDICATOR CONFIRMED Seat belts and shoulder harnesses — all occupants FASTENED AND SNUG Landing lights ON

Landing gear handle position DOWN Three green gear-down indicator lights ALL THREE GREEN ILLUMINATED Gear warning horn — confirm silent at approach power; if sounding, verify gear handle is down SILENT (GEAR DOWN AND LOCKED)

Final approach — stabilised on speed per POH ON SPEED AND GLIDEPATH Gear — confirm three green on short final THREE GREEN Flares and touchdown — round out over the runway threshold; land on main gear first SMOOTH TOUCHDOWN Throttles — retard to idle at touchdown CLOSED Brakes — apply smoothly after mains are firmly on the runway APPLIED AS NEEDED Directional control — maintain centreline with rudder; use nosewheel steering once speed permits CONTROLLED

Throttles — advance smoothly to full takeoff power on both engines simultaneously FULL POWER Pitch — establish a climb attitude; airspeed at or above Vmc immediately POSITIVE CLIMB ATTITUDE; AIRSPEED ABOVE VMC Flaps — retract to takeoff position on first increment per POH TAKEOFF FLAP SETTING Landing gear — retract after positive rate of climb established GEAR UP; IN TRANSIT CONFIRMED Flaps — retract fully after obstacle clearance and positive climb confirmed UP Airspeed — accelerate to Vy per POH once clear of obstacles VY PER POH ATC — advise of go-around and intentions NOTIFIED

Flaps RETRACT — UP Boost pumps — both OFF (unless POH specifies otherwise) Transponder STANDBY OR AS APPROPRIATE Landing lights OFF OR TAXI SETTING AS REQUIRED Mixtures — both engines; adjust to rich for taxi as appropriate RICH FOR TAXI (OR PER POH) Brakes — test gently during taxi clear of runway EFFECTIVE

Parking brake SET Avionics master switch OFF Electrical loads — non-essential switches OFF Engine cooling — run both engines at idle for a brief cooling period per POH before shutdown COOL-DOWN PERIOD COMPLETE Left mixture — pull to idle cutoff to stop left engine IDLE CUTOFF; ENGINE STOPS Left ignition switch — off after engine stops OFF Right mixture — pull to idle cutoff to stop right engine IDLE CUTOFF; ENGINE STOPS Right ignition switch — off after engine stops OFF Master switch OFF Fuel selectors — both OFF Control lock INSTALLED Doors — pilot door and cabin entry door SECURED; WINDOWS CLOSED Tiedowns and chocks INSTALLED Pitot tube cover INSTALLED