MSFS 2024 · General Aviation

Beechcraft King Air 350i Startup Checklist

Beechcraft King Air 350i Startup Notes

The 350i is a lesson in PT6 discipline. Everything runs through the condition levers: they sit at fuel cutoff for the start, and the moment you lift one to low idle you are committed to fuel and ignition. Engage the starter, wait for N1 to spin up and stabilize, at 12 percent minimum, then bring the condition lever up while watching ITT climb. The second engine is normally a generator-assisted cross start, and the autofeather system gets its own dedicated test at runup.

Hot starts are the big trap. Lifting the condition lever before N1 stabilizes means fuel pooling in a slow-turning engine and an ITT that rockets toward the limit; if it runs away, cut the fuel and keep motoring. Impatience causes the second classic error: cross-starting engine two before the first generator's load has dropped enough to support it. And plenty of sim pilots skip the autofeather test entirely, which on this airplane is a real checklist item, not decoration.

Common mistakes

Raising the condition lever before N1 stabilizes at 12 percent
Cross-starting the second engine before generator load drops
Skipping the autofeather test at runup

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Pilot Tools for This Flight

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General AviationModern

AIRCRAFT BRIEF

The Beechcraft King Air 350 (Model B300) entered service in 1990 as a stretched, winglet-equipped evolution of the King Air 300, cementing Beechcraft's dominance in the executive turboprop market. The 350i variant, introduced in 2008, added a restyled interior with active noise cancellation, making cabin comfort competitive with light jets. Over 440 King Air 350i aircraft had been delivered in its first decade of production, and the type remains among the best-selling business turboprops in history.

RANGE VISUALIZER

Startup Walkthrough

SPECIFICATIONS

manufacturer: Beechcraft (Textron Aviation)
first Flight: 1988 (B300 prototype)
role: Twin-engine turboprop executive transport
crew: 1-2 pilots + up to 9 passengers
engines: 2x Pratt and Whitney Canada PT6A-60A (1,050 shp each)
max Speed: 578 km/h (312 kts)
range: 3,345 km (1,806 nmi)
ceiling: 35,000 ft
weight: 6,804 kg (MTOW)

Sources: Beechcraft Super King Air - Wikipedia, King Air 350 Specs - King Air Nation

FLIGHT2.17.1Checklist

Beechcraft King Air 350iMSFS 2024 · Startup Checklist · 346 steps · 19 phases

DATE PILOT TAIL

PHS 1 - Pre-Flight Planning8 steps

	01	Weather Briefing (METAR / TAF)REVIEWED
	02	NOTAMsREVIEWED
	03	Fuel RequiredCALCULATEDCAUTION: Aviation gasoline is an emergency fuel only: limited to 150 hours between engine overhauls, prohibited if either standby fuel pump is inoperative, and crossfeed is required above FL200.NOTE: Approved commercial fuels: Jet A, Jet A-1, Jet B, Chinese No. 3. Military: JP-4, JP-5, JP-8.
	04	Weight, CG, Performance and V-SpeedsCHECKEDNOTE: Checklist airspeeds are quoted at 15,000 lb (6804 kg).
	05	Takeoff PerformanceCALCULATEDNOTE: V1, VR, V2 and static takeoff power are confirmed again in the Before Takeoff (Runup) checklist.
	06	Route / Flight PlanPREPARED AND LOADED
	07	ATISOBTAINED
	08	Anti-Icing Additive (if used)BLENDED 0.10 TO 0.15% BY VOLUMECAUTION: Improper concentration causes deterioration of the fuel cell sealant.NOTE: Additive conforming to MIL-I-27686 or MIL-I-85470. Check with the fuel supplier whether additive has already been added.

PHS 2 - Preflight Inspection - Cabin and Cockpit24 steps

	01	Monogram Electric Toilet Knife Valve (if installed)OPEN
	02	BaggageSECURE
	03	Aft Exit SignON-TESTNOTE: Check sign illumination, then OFF-RESET.
	04	Forward Exit SignON-TESTNOTE: Check sign illumination, then OFF-RESET.
	05	Emergency ExitsSECURE AND UNLOCKED
	06	Control LocksREMOVE
	07	Parking BrakeSET
	08	Landing Gear ControlDOWN
	09	ELT (cockpit installations)ARM
	10	Condition LeversFUEL CUTOFF
	11	Elevator TrimSET TO 2 UNITS NOSE UP
	12	Rudder and Aileron TrimSET TO 0 UNITS
	13	Battery BusNORM
	14	Voltmeter - BAT Position23 VOLTS MINIMUMNOTE: All other positions 0 volts.
	15	BatteryON
	16	Landing Gear LightsL, R AND NOSE ILLUMINATED
	17	Fuel QuantityCHECK MAIN AND AUXILIARY
	18	Voltmeter - TPL FED22 VOLTS MINIMUMNOTE: R GEN and L GEN 0 volts, CTR 23 volts minimum, EXT PWR 0 volts.
	19	Gen TiesMAN CLOSE
	20	Voltmeter - R GEN and L GEN23 VOLTS MINIMUM
	21	Flaps (if desired)CHECKNOTE: Move to and verify they stop at TAKEOFF AND APPROACH, then at DOWN.
	22	Airstair Door CircuitryCHECK
	23	BatteryOFF
	24	Oxygen System Preflight InspectionCOMPLETE

PHS 3 - Preflight Inspection - Left Wing and Nacelle32 steps

	01	Cabin Door Seal, Step Extension Cable, Light Wire, Damper and HandrailsCHECK
	02	Left Side WindowsCHECK
	03	Flaps (condition, asymmetry protection, flap tracks)CHECK
	04	Aileron and TabCHECK
	05	Static Wicks (aileron and winglet)CHECK
	06	Siphon Break VentCLEAR
	07	LightsCHECK
	08	Main Fuel Tank CapSECURE
	09	Stall Warning VaneCHECK
	10	Tie-DownREMOVE
	11	Flush Outboard Fuel DrainDRAIN
	12	Outboard Deice Boot and Stall StripCHECK
	13	Leading-Edge Fuel Tank and Gravity-Line DrainsDRAIN
	14	Inverter Cooling LouversCLEAR
	15	Flush Fuel Vent and Heated Fuel VentCLEAR
	16	Landing Gear (doors, tires, strut, wheel well)CHECK
	17	Engine Oil VentCLEAR
	18	Brake Line and Brake Deice Plumbing (if installed)CHECK
	19	Torque Knee Assembly and Safety SwitchCHECK
	20	BrakesCHECK
	21	Fire Extinguisher PressureCHECKNOTE: Pressure varies with temperature, for example 340 to 420 psi at 40 degF (4 degC) and 455 to 550 psi at 80 degF (27 degC).
	22	ChocksREMOVE
	23	Fuel Strainer and Fuel Filter DrainsDRAIN
	24	Ice Vane and Oil Radiator ExhaustCLEAR
	25	Engine OilCHECK QUANTITY, CAP SECURE
	26	Engine Cowling, Doors and PanelsSECURE
	27	Exhaust Stack and FairingCHECK FOR CRACKS
	28	PropellerCHECK AND ROTATE
	29	Engine and Oil Radiator Air IntakesCHECK
	30	Auxiliary Fuel Tank CapSECURE
	31	Inboard Deice BootCHECK
	32	Auxiliary Fuel Tank DrainDRAIN

PHS 4 - Preflight Inspection - Nose13 steps

	01	OAT Probe / Relief Tube VentCHECK
	02	Brake Reservoir VentCLEAR
	03	Left Avionics Access PanelSECURE
	04	Air Conditioner Condenser Exhaust DuctCLEAR
	05	Windshield and WipersCHECK
	06	Radome ConditionCHECK
	07	Pitot MastsCLEAR
	08	Landing and Taxi LightsCHECK
	09	Nose Gear (shimmy damper, stop block, torque knee, strut, tire)CHECK
	10	ChocksREMOVE
	11	Nose Gear Doors and Wheel WellCHECK
	12	Air Conditioner Condenser Intake DuctCLEAR
	13	Right Avionics Access PanelSECURE

PHS 5 - Preflight Inspection - Right Wing and Nacelle31 steps

	01	Ejector ExhaustCLEAR
	02	Auxiliary Fuel Tank DrainDRAIN
	03	Battery Box DrainCLEAR
	04	Lower PanelsSECURE
	05	Heat Exchanger Air Intake and ExhaustCLEAR
	06	Inboard Deice BootCHECK
	07	Battery Access PanelSECURE
	08	Auxiliary Fuel Tank CapSECURE
	09	Engine OilCHECK QUANTITY, CAP SECURE
	10	Engine Cowling, Doors and PanelsSECURE
	11	Collector DrainCLEAR
	12	Exhaust Stack and FairingCHECK FOR CRACKS
	13	PropellerCHECK AND ROTATE
	14	Engine and Oil Radiator Air IntakesCHECK
	15	Generator Air IntakeCLEAR
	16	Ice LightCHECK
	17	Fuel Filter and Fuel Strainer DrainsDRAIN
	18	Landing Gear (doors, tires, strut, wheel well)CHECK
	19	Fire Extinguisher PressureCHECK
	20	BrakesCHECK
	21	ChocksREMOVE
	22	Heated Fuel Vent and Flush Fuel VentCLEAR
	23	Gravity-Line and Leading-Edge Fuel Tank DrainsDRAIN
	24	External Power DoorSECURE
	25	Outboard Deice Boot and Stall StripCHECK
	26	Tie-DownREMOVE
	27	Flush Outboard Fuel DrainDRAIN
	28	Main Fuel Tank CapSECURE
	29	Static Wicks (winglet and aileron)CHECK
	30	AileronCHECK
	31	FlapsCHECK

PHS 6 - Preflight Inspection - Fuselage and Tail20 steps

	01	Lower Antennas and BeaconCHECK
	02	Oxygen Service Access DoorSECURE
	03	Static Ports (right)CLEAR
	04	ELT (aft fuselage installations)AUTO
	05	ELT AntennaCHECK
	06	Aft Compartment Bottom Access DoorSECURE
	07	Tie-DownREMOVE
	08	Ventral Fin Drain HolesCLEAR
	09	Cabin Air ExhaustCLEAR
	10	Ventral Fin and Static WickCHECK
	11	VOR Antennas (right and left)CHECK
	12	Rudder, Rudder Tab, Stinger and Static WicksCHECK
	13	Horizontal Stabilizer, Boots and Static WicksCHECK
	14	Elevator, Tab and Static WicksCHECK
	15	Tabs In Neutral PositionVERIFY
	16	Position Light and Tail FloodlightsCHECK
	17	Access Panels (left)SECURE
	18	Static Ports (left)CLEAR
	19	Oxygen Overpressure Discharge and Aft Compartment Drain TubesCLEAR
	20	Relief TubeCLEAR

PHS 7 - Before Engine Starting39 steps

	01	Weight, CG, Performance and V-SpeedsCHECKED
	02	Airstair DoorLOCKEDWARNING: Only a crew member or properly trained ground personnel should close and lock the airstair door and cargo door.
	03	Cargo Door (B300C)LOCKED
	04	Load and BaggageCONFIRM SECURED
	05	Passenger BriefingCOMPLETE
	06	Seats and TablesPOSITIONEDNOTE: All seat backs upright, headrests fully extended, lateral-tracking seats outboard, tables stowed.
	07	Pilot Seats and Rudder PedalsADJUSTED
	08	Seat Belts and Shoulder HarnessesFASTENED
	09	Parking BrakeCONFIRM SET
	10	Control LocksCONFIRM REMOVED
	11	Oxygen System Preflight InspectionCONFIRM COMPLETE
	12	Fuel PanelCHECKNOTE: Standby pumps OFF, crossfeed OFF, aux transfer switches AUTO, circuit breakers IN.
	13	Pilot's GyroSLAVED (OUT)
	14	Standby Horizon (if installed)TEST
	15	Battery BusCONFIRM NORM
	16	Engine Anti-IceON AND MAIN
	17	Landing Gear Relay Circuit BreakerIN
	18	Landing Gear ControlDOWN
	19	Power LeversIDLE
	20	Prop LeversFULL FORWARD
	21	Condition LeversFUEL CUTOFF
	22	Oxygen ControlsPASSENGER MANUAL DROP-OUT PUSHED OFF / SYSTEM READY ON
	23	EFIS Power (if installed)OFF
	24	Landing Gear Alternate Extension HandleSTOWED
	25	Copilot's SubpanelCHECKNOTE: Window defog OFF, vent blower AUTO, cabin temp mode OFF, environmental bleed air LOW, bleed air valves ENVIR OFF, aft blower OFF, electric heat OFF.
	26	Copilot's GyroSLAVED (OUT)
	27	Right Panel Circuit BreakersIN
	28	Pilot's Static Air SourceNORMAL
	29	BatteryON
	30	AnnunciatorsTEST
	31	Fuel Quantity (main and auxiliary)CHECK
	32	Landing Gear Control LightsTEST
	33	Hydraulic Fluid SensorTESTNOTE: HYD FLUID LO annunciator illuminated.
	34	BeaconON
	35	Cabin Altitude WarningTESTNOTE: CABIN ALT HI and CABIN ALTITUDE illuminated, note aural warning.
	36	Cabin Differential WarningTESTNOTE: CABIN DIFF HI illuminated.
	37	Overspeed WarningTESTNOTE: Note aural warning.
	38	Stall and Landing Gear WarningTESTNOTE: Note aural warning.
	39	Fire Detector and ExtinguisherTESTNOTE: Left and right ENG FIRE illuminated; left and right EXTINGUISHER PUSH and DISCHARGED illuminated.

PHS 8 - Engine Starting (Battery)24 steps

	01	Gen Ties (for night operation)MAN CLOSE
	02	Propeller AreaCLEAR
	03	Right Ignition and Engine StartONCAUTION: Starter use is limited to 30 seconds ON, 5 minutes OFF, 30 seconds ON, 5 minutes OFF, 30 seconds ON, then 30 minutes OFF.NOTE: R IGNITION ON illuminated, R FUEL PRES LO extinguished.
	04	Right Condition Lever (after 12% N1 minimum)LOW IDLEWARNING: Do not introduce fuel below 12% N1.
	05	Right ITT and N1MONITORWARNING: Maximum starting ITT is 1000 degC, time limited to 5 seconds.
	06	Right Oil PressureCHECKNOTE: Starting oil pressure range 0 to 200 psi; minimum oil temperature -40 degC.
	07	Right Ignition and Engine Start (at 50% N1 or above)OFF
	08	Right Condition LeverHIGH IDLENOTE: High idle limits power operation to a minimum of 70% N1; low idle to a minimum of 62% N1.
	09	Right GeneratorRESET, THEN ONNOTE: R DC GEN, L GEN TIE OPEN and R GEN TIE OPEN extinguished.
	10	BatteryCHARGENOTE: Until the loadmeter reads approximately 50% or less.
	11	Left Ignition and Engine StartONNOTE: L IGNITION ON illuminated, L FUEL PRES LO extinguished.
	12	Left Condition Lever (after 12% N1 minimum)LOW IDLE
	13	Left ITT and N1MONITORWARNING: Maximum starting ITT is 1000 degC, time limited to 5 seconds.
	14	Left Oil PressureCHECK
	15	Left Ignition and Engine Start (at 50% N1 or above)OFF
	16	Right Condition LeverREDUCE TO LOW IDLE
	17	Left and Right Prop RPM1050 MINIMUMNOTE: Minimum idle prop speed limit is 1050 RPM.
	18	L PROP PITCH and R PROP PITCHILLUMINATED
	19	VoltmeterL GEN - 27.5 TO 29.0 VOLTS
	20	Left GeneratorRESET, THEN ONNOTE: L DC GEN extinguished.
	21	Right GeneratorRESET, THEN ONNOTE: L GEN TIE OPEN and R GEN TIE OPEN remain extinguished with the switch in the RESET position.
	22	Hot Start or Hung StartCONDITION LEVER FUEL CUTOFFWARNING: Condition lever FUEL CUTOFF, ignition and engine start to STARTER ONLY, and at ITT below 400 degC set IGNITION AND ENGINE START OFF. Do not attempt another start until the cause has been corrected.
	23	No Light StartCONDITION LEVER FUEL CUTOFFWARNING: If no ITT rise is observed within 10 seconds after moving the condition lever to LOW IDLE: condition lever FUEL CUTOFF, ignition and engine start OFF, allow 5 minutes for fuel to drain and the starter to cool, then perform Engine Clearing.
	24	Engine ClearingSTARTER ONLY FOR MAX 30 SECONDSNOTE: Condition lever FUEL CUTOFF, ignition and engine start STARTER ONLY for a maximum of 30 seconds, then OFF. Allow 5 minutes before another start attempt.

PHS 9 - Before Taxi18 steps

	01	Electrical SystemCHECK
	02	InvertersCHECK AND ON
	03	Avionics MasterON
	04	Master Panel and Cockpit LightsAS REQUIRED
	05	Mic SwitchesNORMAL
	06	Cabin LightsAS REQUIRED
	07	FurnishingsAS REQUIRED
	08	Cabin SignNO SMK/FSB OR FSB
	09	Standby Horizon (if installed)ON
	10	Prop SyncON
	11	Exterior LightsAS REQUIRED
	12	EFIS Power (if installed)ON
	13	Environmental System ControlsSET
	14	AltimetersSET
	15	Standby Horizon (if installed)UNCAGE
	16	FlapsUP
	17	Flight ControlsCHECK FOR FULL FREEDOM OF MOVEMENT AND PROPER DIRECTION OF TRAVEL
	18	BrakesRELEASE AND CHECK

PHS 10 - Before Takeoff (Runup)18 steps

	01	Avionics and RadarCHECK
	02	PressurizationCHECK AS REQUIRED AND SET
	03	AutopilotCHECK
	04	Yaw DampCHECK
	05	Electric Pitch TrimCHECK
	06	Trim TabsSET
	07	Engine Controls Friction LocksSET
	08	FlapsCHECK AND SET
	09	Overspeed Governors and Rudder BoostCHECK
	10	Low Pitch Stops and Primary GovernorsCHECK
	11	AutofeatherCHECK
	12	AutofeatherARMNOTE: AUTOFTHER OFF extinguished.
	13	Manual Propeller FeatheringCHECK
	14	Instrument Vacuum and Deice PressureCHECK
	15	Engine Anti-IceCHECK
	16	Ice Protection Equipment (if required)CHECK
	17	Fuel Quantity, Flight and Engine InstrumentsCHECK
	18	V1, VR, V2 and Static Takeoff PowerCONFIRM

PHS 11 - Before Takeoff (Final Items)20 steps

	01	Engine Auto IgnitionARM (IF REQUIRED)NOTE: L IGNITION ON and R IGNITION ON illuminated if armed.
	02	Engine Anti-IceAS REQUIRED
	03	Exterior LightsAS REQUIRED
	04	Windshield Anti-IceNORMAL/HI (IF REQUIRED)
	05	Prop DeiceAUTO (IF REQUIRED)
	06	Left and Right Fuel Vent HeatON
	07	Stall Warning HeatON
	08	Left and Right Pitot HeatON
	09	TransponderALT
	10	Prop LeversCONFIRM FULL FORWARD
	11	TrimCONFIRM SET
	12	FlapsCONFIRM SET
	13	Environmental Bleed AirLOW ABOVE 10 DEGC / NORMAL AT OR BELOW 10 DEGC
	14	Bleed Air ValvesAS REQUIRED
	15	Electric HeatOFFNOTE: ELEC HEAT ON extinguished.
	16	Aft BlowerAS REQUIRED
	17	Interior LightsAS REQUIRED
	18	Generator LoadCHECKCAUTION: Ground generator load limit is 75% between 62% and 70% N1, and 100% between 70% and 100% N1.NOTE: When OAT is greater than 10 degC: with A/C ON loadmeters must be 30% or less; with A/C OFF 50% or less.
	19	Battery AmmeterCHECKNOTE: Charge current 10 amps or less if required. Applies to airplanes FL-215 thru FL-382 except FL-381, FM-10 and FM-11.
	20	AnnunciatorsOFF OR CONSIDERED

PHS 12 - Takeoff9 steps

	01	BrakesHOLDWARNING: Do not cycle boots during takeoff.
	02	Power LeversSET STATIC TAKEOFF POWERWARNING: Takeoff limits: torque 100%, ITT 820 degC, N1 104%, prop 1700 RPM, oil pressure 90 to 135 psi, oil temperature 0 to 110 degC.CAUTION: Torque excursions up to 102% are time limited to 7 minutes; propeller excursions up to 1735 RPM are time limited to 7 minutes.
	03	Autofeather AnnunciatorsILLUMINATED
	04	BrakesRELEASE
	05	VRROTATE TO APPROXIMATELY 10 DEG
	06	Landing Gear (positive climb established)UP
	07	AirspeedMAINTAIN V35 UNTIL CLEAR OF OBSTACLES
	08	Flaps (at 125 knots minimum)UP
	09	Rolling Takeoff VariantPOWER SET WITHIN 10 SECONDS OF BRAKE RELEASENOTE: For a rolling takeoff, release brakes first and set static takeoff power within 10 seconds of brake release, observing ITT limits.

PHS 13 - Climb11 steps

	01	Bleed Air ValvesOPEN
	02	Environmental Bleed AirAS REQUIRED
	03	Yaw DampON
	04	Climb PowerSETWARNING: Cruise climb ITT limit is 785 degC, which is lower than the maximum cruise limit.
	05	Props1600 RPM, OR AS DESIRED
	06	Windshield Anti-IceNORMAL
	07	Engine InstrumentsMONITOR
	08	Cabin SignAS REQUIRED
	09	PressurizationCHECK
	10	LightsAS REQUIRED
	11	Climb Speed ReferenceVX 125 KIAS / VY 140 KIASNOTE: Cruise climb: 170 kt to 10,000 ft, 160 kt to 15,000 ft, 150 kt to 20,000 ft, 140 kt to 25,000 ft, 130 kt to 30,000 ft, 120 kt to 35,000 ft.

PHS 14 - Cruise14 steps

	01	Cruise PowerSET PER CRUISE POWER TABLES OR GRAPHSWARNING: Do not lift the power levers in flight.NOTE: Maximum cruise ITT limit 820 degC; maximum continuous 820 degC. N1 maximum 104%, prop 1700 RPM.
	02	AutofeatherOFF
	03	Aft BlowerAS REQUIRED
	04	Engine InstrumentsMONITOR
	05	Fuel GagesMONITORNOTE: Ensure that fuel is being transferred from the auxiliary tanks.
	06	Engine Ice ProtectionON IN VISIBLE MOISTURE AT +5 DEGC AND BELOWWARNING: If in doubt, actuate the engine anti-ice system. Engine icing can occur even though no surface icing is present.NOTE: Check for proper operation by noting the torque drop. L ENG ANTI-ICE and R ENG ANTI-ICE illuminated.
	07	Engine Auto-IgnitionARM
	08	Prop DeiceAUTONOTE: Relieve propeller imbalance due to ice by increasing RPM briefly and returning to the desired setting.
	09	Surface Deice (ice accumulation 1/2 to 1 inch)SINGLE AND RELEASEWARNING: An accumulation of one inch of ice on the leading edges can cause a 500 FPM loss of climb rate, up to 75 knots TAS cruise speed reduction and up to 15 knots IAS stall speed increase. Maintain a minimum of 140 knots in sustained icing.NOTE: Pneumatic pressure gage should indicate 12.0 to 20.0 psi before boots are activated. WING DEICE illuminates within 6 seconds and TAIL DEICE within 10 seconds in SINGLE mode.
	10	Windshield Anti-IceNORMAL/HICAUTION: Maximum airspeed for effective windshield anti-icing is 226 knots. In the event of windshield icing, reduce airspeed to 226 knots or below.
	11	Left and Right Fuel Vent HeatON
	12	Left and Right Pitot HeatON
	13	Stall Warn HeatON
	14	Wing Ice LightsAS REQUIRED

PHS 15 - Descent9 steps

	01	Pressurization - Cabin AltitudeSET
	02	Pressurization - Rate ControlAS DESIRED
	03	AltimeterSET
	04	Cabin SignAS REQUIRED
	05	Windshield Anti-IceAS REQUIRED
	06	Windshield DefrostAS REQUIRED
	07	Window DefogAS REQUIRED
	08	Fuel BalanceCHECK
	09	Seats and TablesPOSITIONEDNOTE: All seat backs upright, headrests fully extended, lateral-tracking seats outboard, tables stowed.

PHS 16 - Before Landing9 steps

	01	Approach SpeedsCONFIRMNOTE: VREF at 15,000 lb (6804 kg) is 109 kt; 14,000 lb 105 kt; 13,000 lb 102 kt; 12,000 lb 100 kt; 11,000 and 10,000 lb 100 kt. Approach climb is VREF + 10 knots; balked landing is VREF.
	02	AutofeatherARM
	03	Environmental Bleed AirLOW
	04	Cabin SignNO SMK/FSB OR FSB
	05	FlapsAPPROACHCAUTION: Maximum speed with flaps in approach position is 202 KIAS.
	06	Landing GearDOWN
	07	Exterior and Interior LightsAS REQUIRED
	08	RadarAS REQUIRED
	09	Surface DeiceAS REQUIREDNOTE: Prior to a landing approach, cycle the deicing boots to shed any accumulated ice.

PHS 17 - Normal Landing9 steps

	01	FlapsDOWNCAUTION: Maximum speed permissible with flaps extended beyond approach is 158 KIAS.
	02	AirspeedVREF
	03	Yaw DampOFF
	04	Power LeversIDLE
	05	Prop LeversFULL FORWARD
	06	Power Levers (after touchdown)LIFT AND SELECT GROUND FINE
	07	BrakesAS REQUIRED
	08	Maximum Reverse Thrust Landing VariantCONDITION LEVERS HIGH IDLECAUTION: Max reverse limits: ITT 760 degC, prop 1650 RPM, oil temperature 0 to 99 degC.NOTE: For a maximum reverse thrust landing set condition levers HIGH IDLE before landing, then after touchdown lift the power levers through ground fine and into reverse, brakes as required, and return the condition levers to LOW IDLE.
	09	Balked LandingMAXIMUM ALLOWABLE POWER / MAINTAIN VREFNOTE: Balked landing: power maximum allowable, maintain VREF, flaps APPROACH at VREF + 10 knots, landing gear UP with positive climb, flaps UP at 125 knots minimum.

PHS 18 - After Landing10 steps

	01	Engine Auto-IgnitionOFF
	02	Engine Anti-IceON
	03	LightsAS REQUIRED
	04	Ice ProtectionOFF
	05	TransponderSTANDBY
	06	RadarSTANDBY OR OFF
	07	TrimSET
	08	FlapsUP
	09	Pressurization DifferentialVERIFY 0
	10	Bleed Air ValvesENVIR OFF

PHS 19 - Shutdown and Securing28 steps

	01	Parking BrakeSET
	02	Electric HeatOFF
	03	EFIS Power (if installed)OFF
	04	Standby Horizon (if installed)CAGED AND OFF
	05	Avionics MasterOFF
	06	InvertersOFF
	07	AutofeatherOFF
	08	Exterior LightsOFF
	09	Vent BlowerAUTO
	10	Cabin Temp ModeOFF
	11	Aft BlowerOFF
	12	Aft HeatAS DESIRED
	13	Oxygen ControlsPUSH OFF
	14	BatteryCHARGED
	15	Brake Deice (if installed, last flight of the day)ON, THEN OFFCAUTION: The brake deice system is not to be continuously operated above 15 degC ambient temperature.
	16	ITTSTABILIZED AT MINIMUM OBTAINABLE TEMPERATURE FOR ONE MINUTE
	17	Instrument Emergency LightsON IF DESIRED FOR A NIGHT SHUTDOWN
	18	Condition LeversFUEL CUTOFF
	19	Prop LeversFEATHER
	20	Overhead Panel SwitchesOFF
	21	Battery and Generator Switches (below 15% N1)OFF
	22	Control LocksINSTALL
	23	Instrument Emergency LightsOFF
	24	Tie-Downs and ChocksINSTALL
	25	External CoversINSTALL
	26	Parking BrakeOFF
	27	Baggage Compartment LightsOFF
	28	Cabin Entry LightsOFF