Cessna 206H Stationair — 2000_Cessna_206H_Checklist

BEFORE ENGINE START before_start

Pilot's Operating Handbook
Airplane Weight and BalanceCHECKED
BrakesTEST AND SET
Control Wheel Lock
Hobbs Meter
Ignition & Avionics MasterOFF
Master SwitchON
Fuel Quantity IndicatorCHK QTY & ENSURE LOW FUEL ANNUNCIATORS OFF
Avionics Master SwitchON
Avionics Cooling FanCHECK AUDIBLY
Avionics Master SwitchOFF
Flaps
Static Pressure Alternate SourceOFF
Annunciator PanelTEST/ALL LIGHTS ON
Fuel Selector ValveBOTH
Pitot HeatON FOR 30 SECONDS
Pitot HeatTEST FOR HEAT & POWER OFF
Master SwitchOFF
Trim Controls
Cockpit Inspect Done
Passenger briefing
Cabin doorsCLOSED AND LOCKED
Seats/seat beltsADJUSTED AND LOCKED
Circuit breakers
Avionics circuit breakers
Electrical equipmentOFF
Avionics master switchOFF
Cowl flaps
Fuel selector valveBOTH

ENGINE START engine_start

ThrottleOPEN ¼ INCH
Prop
Master switchON
Beacon
Mixture
Prop area
Auxiliary fuel pump switchON
MixtureADVANCE UNTIL THERE IS A RISE IN FUEL FLOW AND MAINTAIN IN THIS POSITION APPROXIMATELY FIVE SECONDS WITH AUX FUEL PUMP ON
Auxiliary fuel pump switchOFF
Ignition switch
MixtureSMOOTHLY TO RICH
NOTEIF ENGINE FLOODS, VERIFY AUXILIARY FUEL PUMP OFF, OPEN THROTTLE ½ TO FULL, AND CRANK ENGINE. WHEN ENGINE FIRES, ADVANCE MIXTURE TO FULL RICH & RETARD THROTTLE
Oil Pressure
MixtureLEANED at 1200 RPM
FlapsRETRACT TO NORMAL
Avionics Master / RadiosON
EDM 800ENTER/VERIFY FUEL VOLUME
KLN94 & MX20 DatabasesCURRENT
KLN94FLIGHT PLAN ENTERED
ATIS/AWOS
Clearance if applicable
Navigation lightsAS REQUIRED
Taxi lightAS REQUIRED
Brakes

BEFORE TAKEOFF before_takeoff

Brakes
Seat backs
Passenger SeatsAS FAR FWD AS POSSIBLE
Seats/seat beltsCHECK SECURED
Cabin doorsCLOSED AND LOCKED
Flight controlsFREE AND CORRECT
Flight instrumentsCHECK AND SET
Directional Gyro
Altimeter
Transponder
GPS & Autopilot
Attitude Indicator
Autopilot Preflight
Power
Manual Electric Trim Test
Both Halves DownVERIFY
Both Halves UpVERIFY
MET Up, Hold DISCVERIFY
Wheel/Ind Not MovingVERIFY
Release AP/DISCVERIFY
Wheel/Ind MovingVERIFY
Baro SettingVERIFY
AutopilotPRESS AP BUTTON
Flight ControlsVERIFY OVRPWER
A/P DiscPRESS & VERIFY
Trim
Fuel quantity
Auxiliary fuel pumpOFF
Mixture
Cowl flaps
Fuel selector valveRECHECK BOTH
Throttle1800 RPM
Magnetos
PropCYCLE THEN RETURN TO HIGH
Vacuum gauge
Oil pressure
Oil temperature
Ammeter
Annunciator panelTEST AND CHECK
ThrottleIDLE/1000 RPM OR LESS
Friction lock
Wing flaps0 to 20°
Cowl Flaps
Electric trim
Elevator/rudder trip
Radios/avionics
NAV/GPS switch
Autopilot
Strobe lightsAS DESIRED
Taxi/Landing lightsAS DESIRED
Transponder
Brakes

NORMAL TAKEOFF takeoff

Before Taking RunwayXPONDER SET TO ALTITUDE
Tower & Departure FreqsSET
Wing flaps0 to 20°
Take Runway
PowerFULL POWER/2700 RPM
MixtureMAX OR LEANED TO MAX POWER ABOVE 3000 FEET
Elevator controlROTATE 56 KIAS
Climb speed
Wing flapsRETRACT WHEN CLEAR OF OBSTACLES

SHORT FIELD TAKEOFF takeoff

Wing flaps
Brakes
PowerFULL POWER/2700 RPM
MixtureMAX OR LEANED TO MAX POWER
Brakes
Elevator controlMAINTAIN SLIGHT TAIL LOW ATTITUDE
Climb Speed
Wing flapsRETRACT SLOWLY AFTER REACHING 80 KIAS

ENROUTE CLIMB climb

Airspeed
Power25 INCH OR FULL(LESS)/2500 RPM
MixtureLEAN TO 20 GPH
Fuel Selector Valve
Wing flapsVERIFY RETRACTED
Cowl flaps

MAXIMUM PERFORMANCE CLIMB climb

Airspeed
PowerFULL THROTTLE/2700 RPM
MixtureLEAN FOR MAX POWER SEE MINIMUM FUEL FLOW PLACARD
Fuel selector valve
Cowl flaps

CRUISE cruise

Landing lightVERIFY OFF
Power – 75% MAX
Throttle15 to 25 INCHES
Prop2100 to 2500 RPM
MixtureLEAN FOR CRUISE
Cowl flaps

DESCENT descent

PowerAS DESIRED
MixtureENRICHEN AS REQUIRED
Cowl flaps
Altimeter
Fuel selector valve
FlapsAS DESIRED
0° to 10° below 140 KIAS
10° to 40° below 100 KIAS

INSTRUMENT APPROACH approach

Approach brief
KLN94 CDI switch
Frequency/Approach
IDENT
Marker beacon
HSI to Compass
AT FAF
Time
Turn
Twist
Throttle
Talk
Mixture
Prop
Landing light
FlapsAS DESIRED
0° to 10° below 140 KIAS
10° to 40° below 100 KIAS

BEFORE LANDING before_landing

Passenger Seats As Fwd As PracticalVERIFY
Seat backs
Seatbelts
Fuel Selector Valve
Mixture
Prop
Landing light
Autopilot

NORMAL LANDING landing

Airspeed (flaps up)
FlapsAS DESIRED
0° to 10° below 140 KIAS
10° to 40° below 100 KIAS
Airspeed (flaps full)
Braking

SHORT FIELD LANDING landing

Airspeed (flaps up)
FlapsFULL (40°) BELOW 100 KIAS
Airspeed
PowerREDUCE TO IDLE AS OBSTACLES ARE CLEARED
Braking
Flaps

BALKED LANDING go_around

PowerFULL POWER/2700 RPM
Mixture
Wing flaps
Climb speed
Wing flaps
Cowl flaps

AFTER LANDING after_landing

Wing flaps
Cowl flaps
Landing light
Taxi lightAS REQUIRED
Strobes
Transponder

SHUT DOWN shutdown

Throttle
Electrical equipment
Avionics master
Mixture
Ignition switch
Master
Hobbs time
Control lock
Cowl flaps
Fuel Selector Valve
Nosewheel Chock
Fuel Top Off
Cowl Inlet Cover In Place

ENGINE FAILURE – TAKEOFF ROLL engine_failure_before_rotation

Throttle
Brakes
Wing flaps
Mixture
Ignition switch
Master switch

ENGINE FAILURE – IMMEDIATELY AFTER TAKEOFF engine_failure_after_takeoff

Airspeed
Flaps up
Flaps down
Mixture
Fuel selector valve
Ignition switch
Wing flapsAS REQUIRED (40° RECOMMENDED)
Master switch
Cabin door
Land

ENGINE FAILURE DURING FLIGHT/RESTART engine_failure_in_flight

Airspeed
Fuel selector valve
Auxiliary fuel pump
Engine power
NOTEIF RESTART DOES NOT OCCUR
Mixture
Ignition switchCHECK BOTH (START IF PROPELLER IS STOPPED)
Auxiliary fuel pumpOFF (IF FUEL FLOW DROPS TO ZERO RETURN TO ON)

FORCED LANDING W/O ENGINE POWER forced_landing

Passenger seats
Seatbacks
Seats/Seat Belts
Airspeed
Flaps up
Flaps down
Transmit 121.5
Squawk
Mixture
Fuel selector valve
Wing flapsAS REQUIRED (40° RECOMMENDED)
Master switch
ELT
Door

PRECAUTIONARY LANDING W/ENGINE POWER forced_landing

Passenger seats
Seatbacks
Seats/Seat Belts
Transmit 121.5
Squawk
Airspeed
Wing flaps
Avionics Master
Electrical switches
Wing flaps
Airspeed
Master switch
ELT
Doors
Ignition switch
Mixture
Fuel selector valve

DITCHING ditching

Transmit 121.5
Squawk
Heavy objects
Passenger seats
Seatbacks
Seats/Seat Belts
Wing flaps
POWERESTABLISH 300 FT/MINUTE DESCENT AT 65 KIAS
If no power
Flaps up
Flaps 10°
Approach
High winds/Heavy seasINTO THE WIND
Light winds/Heavy seasPARALLEL TO SWELLS
Cabin doors
Plan touchdown
Face
ELT
Airplane

FIRE DURING GROUND START engine_fire_ground

Ignition switchSTART (CONTINUE CRANKING)
NOTEENGINE STARTS
Power
Engine
NOTEENGINE FAILS TO START
Ignition switchSTART (CONTINUE CRANKING)
Throttle
Mixture
Fuel selector valve
Auxiliary fuel pump
Master switch
Ignition switch
Airplane
Fire

ENGINE FIRE – IN FLIGHT engine_fire_in_flight

Mixture
Fuel selector valve
Auxiliary fuel pump
Master switch
Cabin air
Cabin heat
Overhead vents
Airspeed105 KIAS (INCREASE WITHIN AIRSPEED LIMITATIONS UNTIL FIRE EXTINGUISHED)
Forced landing

ELECTRICAL FIRE IN FLIGHT electrical_fire

Master switch
Vents/cabin air/heat
Fire extinguisher
Avionics master switch
All other switches (except ignition)OFF
Vents/cabin airOPEN WHEN FIRE EXTINGUISHED
Master switch
Circuit breakersCHECK FOR FAULTY CIRCUIT/DO NOT RESET
Radio switches
Avionics master
Radios/electrical switches

CABIN FIRE cabin_fire

Master switch
Vents/cabin air/heat
Fire extinguisher
Vents/cabin airOPEN WHEN FIRE EXTINGUISHED
Land

WING FIRE engine_fire_in_flight

Landing light
Taxi light
Navigation lights
Strobe light
Pitot heat
Sideslip
Land
Flaps

INADVERTENT ICING ENCOUNTER icing

Pitot heat
Turn back or change altitudePULL FULL OUT
Defrost controls
Increase RPMIF EXCESSIVE VIBRATION, REDUCE TO 2200 RPM AND THEN RAPIDLY INCREASE TO FULL. CYCLE AS NEEDED.
Watch for induction air filter icing15 INCHES HG IN MP CAN OCCUR ABOVE 8000 FEET
Plan landing
Plan for
Open left window
FlapsUSE 10-20° FLAPS FOR ICE ACCUMULATIONS OF 1 INCH OR LESS. FOR GREATER ICE ACCUMULATION, LAND WITH FLAPS RETRACTED TO ENSURE ADEQUATE ELEVATOR EFFECTIVENESS.
Approach
20° flaps
0-10° flaps
Avoid missed approachIF MISSED APPROACH IS MANDATORY, APPLY MAXIMAL POWER AND MAINTAIN 100 KIAS WHILE RETRACTING FLAPS IN 10° INCREMENTS.

EXCESSIVE FUEL VAPOR fuel_system_malfunction

Auxiliary fuel pump
Mixture
Fuel selector valveSELECT OPPOSITE TANK IF SYMPTOMS CONTINUE
Auxiliary fuel pump switchOFF AFTER FUEL FLOW HAS STABILIZED

AMMETER – EXCESSIVE RATE OF CHARGE alternator_failure

Alternator
Nonessential electrical equipment
With alternator side of master OFF
Nonessential electrical equipment
Terminate flight

LOW VOLTAGE ANNUNCIATOR – AMMETER INDICATES DISCHARGE electrical_failure

Avionics master
Alternator circuit breaker (ALT FLD)
Master switch
Master switch
Low voltage annunciator
NOTEIF LOW VOLTAGE ILLUMINATES
Alternator
Nonessential electrical equipment
Terminate flight

EMERGENCY DESCENT emergency_descent

SMOOTH AIR
Seats and seat belts
Throttle
Propeller
Mixture
Wing flaps
Airspeed
ROUGH AIR
Seats and seat belts
Throttle
Propeller
Mixture
Wing flaps
Weights and airspeed
3600
2950
2300

AUTOPILOT FAILURE autopilot_malfunction

Control wheelGRASP FIRMLY AND MAINTAIN CONTROL OF AIRCRAFT
A/P DISC/TRIM INT switchPRESS AND HOLD
Aircraft
Autopilot breaker

STATIC SOURCE BLOCKAGE pitot_static_failure

Static pressure alternate source valvePULL ON
Heat and air ventsPULL ON
Vents
Airspeed and altitudeREFER TO CALIBRATION CHARTS

SPEEDS limitations

Vr — Rotation speed55 KIAS
Vx — Best angle climb70 (SL) 75 (10K)
Vy — Best rate climb86 (SL) 82 (10K)
Vso — Stall with flaps38 (rcog) 44 (fcog)
Vs — Stall without flaps50 (rcog) 54 (fcog)
Va — Maneuvering speed
3600 pounds
2900 pounds
2200 pounds
Vfe — 0 to 10°140 KIAS
Vfe — 20 to 40°100 KIAS
Vne — Never exceed speed182 KIAS
Vno — Maximum structural cruising speed149 KIAS
Maximum window open
Normal climb out75-85 KIAS
Shortfield/Flaps 20° climb74 KIAS
Enroute climb
Normal approach flaps up80-90 KIAS
Normal approach flaps 40°70-80 KIAS
Short field approach flaps 40°67 KIAS
Balked landing flaps 20°80 KIAS
Maximum demonstrated crosswind20 KNOTS
Engine failure after takeoff flaps up80 KIAS
Engine failure after takeoff flaps down70 KIAS
Maximum glide
3600 pounds
3200 pounds
2800 pounds
Precautionary landing w/engine power70 KIAS
Landing without engine power/flaps up80 KIAS
Landing without engine power/flaps down70 KIAS
Emergency descent
Smooth air
Rough air — 3600 pounds
Rough air — 2900 pounds
Rough air — 2200 pounds

PERFORMANCE TABLE reference

STAGE — MP — RPM — PITCH — KIAS — VSI
Climb
Cruise
Cruise Descent
Appr Climb
Approach
Appr Descnt
Downwind -10 Degr Flps
Downwind -20 Degr Flps
Base
Final

EDM 800 REFERENCE reference

Voltage
Outside Air Difference between hottest and coldest EGT
RPM/MAP
Fuel Remaining
Fuel required to next GPS WPT or destination
Fuel Reserve at next GPS WPT or destination
Nautical Miles per Gallon
Time to Empty
Fuel flow rate
Total Fuel Used
EGT, CHT
Oil Temperature
Shock cooling

Cessna 206H Stationair — 2000_Cessna_206H_Checklist_v1

Ratings & reviews

BEFORE ENGINE START before_start

ENGINE START engine_start

BEFORE TAKEOFF before_takeoff

NORMAL TAKEOFF takeoff

SHORT FIELD TAKEOFF takeoff

ENROUTE CLIMB climb

MAXIMUM PERFORMANCE CLIMB climb

CRUISE cruise

DESCENT descent

INSTRUMENT APPROACH approach

BEFORE LANDING before_landing

NORMAL LANDING landing

SHORT FIELD LANDING landing

BALKED LANDING go_around

AFTER LANDING after_landing

SHUT DOWN shutdown

ENGINE FAILURE – TAKEOFF ROLL engine_failure_before_rotation

ENGINE FAILURE – IMMEDIATELY AFTER TAKEOFF engine_failure_after_takeoff

ENGINE FAILURE DURING FLIGHT/RESTART engine_failure_in_flight

FORCED LANDING W/O ENGINE POWER forced_landing

PRECAUTIONARY LANDING W/ENGINE POWER forced_landing

DITCHING ditching

FIRE DURING GROUND START engine_fire_ground

ENGINE FIRE – IN FLIGHT engine_fire_in_flight

ELECTRICAL FIRE IN FLIGHT electrical_fire

CABIN FIRE cabin_fire

WING FIRE engine_fire_in_flight

INADVERTENT ICING ENCOUNTER icing

EXCESSIVE FUEL VAPOR fuel_system_malfunction

AMMETER – EXCESSIVE RATE OF CHARGE alternator_failure

LOW VOLTAGE ANNUNCIATOR – AMMETER INDICATES DISCHARGE electrical_failure

EMERGENCY DESCENT emergency_descent

AUTOPILOT FAILURE autopilot_malfunction

STATIC SOURCE BLOCKAGE pitot_static_failure

SPEEDS limitations

PERFORMANCE TABLE reference

EDM 800 REFERENCE reference

Download this checklist

Send yourself a preflight proof