Cessna 206H Stationair — 2000_Cessna_206H_Checklist_v1 NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full Source: Cessna/206H Stationair/2000_Cessna_206H_Checklist_v1.txt Rights: licensed Checklist hash: 71d5b038a1a201406df0c3e84efb4b7d983c1f996413da73518a838261b7f4c6 Verify against the aircraft's own approved documentation before use. ======================================================================== BEFORE ENGINE START ------------------- [ ] Pilot's Operating Handbook [ ] Airplane Weight and Balance ................................. CHECKED [ ] Brakes ................................................. TEST AND SET [ ] Control Wheel Lock [ ] Hobbs Meter [ ] Ignition & Avionics Master ...................................... OFF [ ] Master Switch .................................................... ON [ ] Fuel Quantity Indicator ... CHK QTY & ENSURE LOW FUEL ANNUNCIATORS OFF [ ] Avionics Master Switch ........................................... ON [ ] Avionics Cooling Fan .................................. CHECK AUDIBLY [ ] Avionics Master Switch .......................................... OFF [ ] Flaps [ ] Static Pressure Alternate Source ................................ OFF [ ] Annunciator Panel ................................ TEST/ALL LIGHTS ON [ ] Fuel Selector Valve ............................................ BOTH [ ] Pitot Heat ........................................ ON FOR 30 SECONDS [ ] Pitot Heat ................................ TEST FOR HEAT & POWER OFF [ ] Master Switch ................................................... OFF [ ] Trim Controls [ ] Cockpit Inspect Done [ ] Passenger briefing [ ] Cabin doors ....................................... CLOSED AND LOCKED [ ] Seats/seat belts ................................ ADJUSTED AND LOCKED [ ] Circuit breakers [ ] Avionics circuit breakers [ ] Electrical equipment ............................................ OFF [ ] Avionics master switch .......................................... OFF [ ] Cowl flaps [ ] Fuel selector valve ............................................ BOTH ENGINE START ------------ [ ] Throttle ................................................ OPEN ¼ INCH [ ] Prop [ ] Master switch .................................................... ON [ ] Beacon [ ] Mixture [ ] Prop area [ ] Auxiliary fuel pump switch ....................................... ON [ ] Mixture ... ADVANCE UNTIL THERE IS A RISE IN FUEL FLOW AND MAINTAIN IN THIS POSITION APPROXIMATELY FIVE SECONDS WITH AUX FUEL PUMP ON [ ] Auxiliary fuel pump switch ...................................... OFF [ ] Ignition switch [ ] Mixture ............................................ SMOOTHLY TO RICH ** NOTE: IF 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 [ ] Mixture .......................................... LEANED at 1200 RPM [ ] Flaps ............................................. RETRACT TO NORMAL [ ] Avionics Master / Radios ......................................... ON [ ] EDM 800 .................................... ENTER/VERIFY FUEL VOLUME [ ] KLN94 & MX20 Databases ...................................... CURRENT [ ] KLN94 ........................................... FLIGHT PLAN ENTERED [ ] ATIS/AWOS [ ] Clearance if applicable [ ] Navigation lights ....................................... AS REQUIRED [ ] Taxi light .............................................. AS REQUIRED [ ] Brakes BEFORE TAKEOFF -------------- [ ] Brakes [ ] Seat backs [ ] Passenger Seats .............................. AS FAR FWD AS POSSIBLE [ ] Seats/seat belts ...................................... CHECK SECURED [ ] Cabin doors ....................................... CLOSED AND LOCKED [ ] Flight controls .................................... FREE AND CORRECT [ ] Flight instruments .................................... CHECK AND SET [ ] Directional Gyro [ ] Altimeter [ ] Transponder [ ] GPS & Autopilot [ ] Attitude Indicator AUTOPILOT PREFLIGHT [ ] Power MANUAL ELECTRIC TRIM TEST [ ] Both Halves Down ......................................... VERIFY [ ] Both Halves Up ........................................... VERIFY [ ] MET Up, Hold DISC ........................................ VERIFY [ ] Wheel/Ind Not Moving ................................... VERIFY [ ] Release AP/DISC .......................................... VERIFY [ ] Wheel/Ind Moving ....................................... VERIFY [ ] Baro Setting ............................................... VERIFY [ ] Autopilot ......................................... PRESS AP BUTTON [ ] Flight Controls .................................. VERIFY OVRPWER [ ] A/P Disc ......................................... PRESS & VERIFY [ ] Trim [ ] Fuel quantity [ ] Auxiliary fuel pump ............................................. OFF [ ] Mixture [ ] Cowl flaps [ ] Fuel selector valve .................................... RECHECK BOTH [ ] Throttle ................................................... 1800 RPM [ ] Magnetos [ ] Prop .................................... CYCLE THEN RETURN TO HIGH [ ] Vacuum gauge [ ] Oil pressure [ ] Oil temperature [ ] Ammeter [ ] Annunciator panel .................................. TEST AND CHECK [ ] Throttle ...................................... IDLE/1000 RPM OR LESS [ ] Friction lock [ ] Wing flaps ................................................. 0 to 20° [ ] Cowl Flaps [ ] Electric trim [ ] Elevator/rudder trip [ ] Radios/avionics [ ] NAV/GPS switch [ ] Autopilot [ ] Strobe lights ............................................ AS DESIRED [ ] Taxi/Landing lights ...................................... AS DESIRED [ ] Transponder [ ] Brakes NORMAL TAKEOFF -------------- [ ] Before Taking Runway ........................ XPONDER SET TO ALTITUDE [ ] Tower & Departure Freqs ......................................... SET [ ] Wing flaps ................................................. 0 to 20° [ ] Take Runway [ ] Power ........................................... FULL POWER/2700 RPM [ ] Mixture .................. MAX OR LEANED TO MAX POWER ABOVE 3000 FEET [ ] Elevator control ..................................... ROTATE 56 KIAS [ ] Climb speed [ ] Wing flaps .......................... RETRACT WHEN CLEAR OF OBSTACLES SHORT FIELD TAKEOFF ------------------- [ ] Wing flaps [ ] Brakes [ ] Power ........................................... FULL POWER/2700 RPM [ ] Mixture .................................. MAX OR LEANED TO MAX POWER [ ] Brakes [ ] Elevator control .................. MAINTAIN SLIGHT TAIL LOW ATTITUDE [ ] Climb Speed [ ] Wing flaps .................... RETRACT SLOWLY AFTER REACHING 80 KIAS ENROUTE CLIMB ------------- [ ] Airspeed [ ] Power ................................ 25 INCH OR FULL(LESS)/2500 RPM [ ] Mixture .............................................. LEAN TO 20 GPH [ ] Fuel Selector Valve [ ] Wing flaps ......................................... VERIFY RETRACTED [ ] Cowl flaps MAXIMUM PERFORMANCE CLIMB ------------------------- [ ] Airspeed [ ] Power ........................................ FULL THROTTLE/2700 RPM [ ] Mixture ............ LEAN FOR MAX POWER SEE MINIMUM FUEL FLOW PLACARD [ ] Fuel selector valve [ ] Cowl flaps CRUISE ------ [ ] Landing light ............................................ VERIFY OFF POWER – 75% MAX [ ] Throttle .......................................... 15 to 25 INCHES [ ] Prop ............................................. 2100 to 2500 RPM [ ] Mixture ............................................. LEAN FOR CRUISE [ ] Cowl flaps DESCENT ------- [ ] Power .................................................... AS DESIRED [ ] Mixture ........................................ ENRICHEN AS REQUIRED [ ] Cowl flaps [ ] Altimeter [ ] Fuel selector valve [ ] Flaps .................................................... AS DESIRED [ ] 0° to 10° below 140 KIAS [ ] 10° to 40° below 100 KIAS INSTRUMENT 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 [ ] Flaps .................................................... AS DESIRED [ ] 0° to 10° below 140 KIAS [ ] 10° to 40° below 100 KIAS BEFORE LANDING -------------- [ ] Passenger Seats As Fwd As Practical .......................... VERIFY [ ] Seat backs [ ] Seatbelts [ ] Fuel Selector Valve [ ] Mixture [ ] Prop [ ] Landing light [ ] Autopilot NORMAL LANDING -------------- [ ] Airspeed (flaps up) [ ] Flaps .................................................... AS DESIRED [ ] 0° to 10° below 140 KIAS [ ] 10° to 40° below 100 KIAS [ ] Airspeed (flaps full) [ ] Braking SHORT FIELD LANDING ------------------- [ ] Airspeed (flaps up) [ ] Flaps ..................................... FULL (40°) BELOW 100 KIAS [ ] Airspeed [ ] Power ....................... REDUCE TO IDLE AS OBSTACLES ARE CLEARED [ ] Braking [ ] Flaps BALKED LANDING -------------- [ ] Power ........................................... FULL POWER/2700 RPM [ ] Mixture [ ] Wing flaps [ ] Climb speed [ ] Wing flaps [ ] Cowl flaps AFTER LANDING ------------- [ ] Wing flaps [ ] Cowl flaps [ ] Landing light [ ] Taxi light .............................................. AS REQUIRED [ ] Strobes [ ] Transponder SHUT DOWN --------- [ ] 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 [EMERGENCY] ------------------------------------------ [ ] Throttle [ ] Brakes [ ] Wing flaps [ ] Mixture [ ] Ignition switch [ ] Master switch ENGINE FAILURE – IMMEDIATELY AFTER TAKEOFF [EMERGENCY] ------------------------------------------------------- AIRSPEED [ ] Flaps up [ ] Flaps down [ ] Mixture [ ] Fuel selector valve [ ] Ignition switch [ ] Wing flaps ............................ AS REQUIRED (40° RECOMMENDED) [ ] Master switch [ ] Cabin door [ ] Land ENGINE FAILURE DURING FLIGHT/RESTART [EMERGENCY] ------------------------------------------------- [ ] Airspeed [ ] Fuel selector valve [ ] Auxiliary fuel pump [ ] Engine power ** NOTE: IF RESTART DOES NOT OCCUR [ ] Mixture [ ] Ignition switch .......... CHECK BOTH (START IF PROPELLER IS STOPPED) [ ] Auxiliary fuel pump ... OFF (IF FUEL FLOW DROPS TO ZERO RETURN TO ON) FORCED LANDING W/O ENGINE POWER [EMERGENCY] -------------------------------------------- [ ] Passenger seats [ ] Seatbacks [ ] Seats/Seat Belts AIRSPEED [ ] Flaps up [ ] Flaps down [ ] Transmit 121.5 [ ] Squawk [ ] Mixture [ ] Fuel selector valve [ ] Wing flaps ............................ AS REQUIRED (40° RECOMMENDED) [ ] Master switch [ ] ELT [ ] Door PRECAUTIONARY LANDING W/ENGINE POWER [EMERGENCY] ------------------------------------------------- [ ] 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 [EMERGENCY] --------------------- [ ] Transmit 121.5 [ ] Squawk [ ] Heavy objects [ ] Passenger seats [ ] Seatbacks [ ] Seats/Seat Belts [ ] Wing flaps [ ] POWER .................... ESTABLISH 300 FT/MINUTE DESCENT AT 65 KIAS [ ] If no power [ ] Flaps up [ ] Flaps 10° APPROACH [ ] High winds/Heavy seas ............................... INTO THE WIND [ ] Light winds/Heavy seas ......................... PARALLEL TO SWELLS [ ] Cabin doors [ ] Plan touchdown [ ] Face [ ] ELT [ ] Airplane FIRE DURING GROUND START [EMERGENCY] ------------------------------------- [ ] Ignition switch ........................... START (CONTINUE CRANKING) ** NOTE: ENGINE STARTS [ ] Power [ ] Engine ** NOTE: ENGINE FAILS TO START [ ] Ignition switch ........................... START (CONTINUE CRANKING) [ ] Throttle [ ] Mixture [ ] Fuel selector valve [ ] Auxiliary fuel pump [ ] Master switch [ ] Ignition switch [ ] Airplane [ ] Fire ENGINE FIRE – IN FLIGHT [EMERGENCY] ------------------------------------ [ ] Mixture [ ] Fuel selector valve [ ] Auxiliary fuel pump [ ] Master switch [ ] Cabin air [ ] Cabin heat [ ] Overhead vents [ ] Airspeed ... 105 KIAS (INCREASE WITHIN AIRSPEED LIMITATIONS UNTIL FIRE EXTINGUISHED) [ ] Forced landing ELECTRICAL FIRE IN FLIGHT [EMERGENCY] -------------------------------------- [ ] Master switch [ ] Vents/cabin air/heat [ ] Fire extinguisher [ ] Avionics master switch [ ] All other switches (except ignition) ............................ OFF [ ] Vents/cabin air ......................... OPEN WHEN FIRE EXTINGUISHED [ ] Master switch [ ] Circuit breakers .............. CHECK FOR FAULTY CIRCUIT/DO NOT RESET [ ] Radio switches [ ] Avionics master [ ] Radios/electrical switches CABIN FIRE [EMERGENCY] ----------------------- [ ] Master switch [ ] Vents/cabin air/heat [ ] Fire extinguisher [ ] Vents/cabin air ......................... OPEN WHEN FIRE EXTINGUISHED [ ] Land WING FIRE [EMERGENCY] ---------------------- [ ] Landing light [ ] Taxi light [ ] Navigation lights [ ] Strobe light [ ] Pitot heat [ ] Sideslip [ ] Land [ ] Flaps INADVERTENT ICING ENCOUNTER [EMERGENCY] ---------------------------------------- [ ] Pitot heat [ ] Turn back or change altitude .......................... PULL FULL OUT [ ] Defrost controls [ ] Increase RPM ... IF EXCESSIVE VIBRATION, REDUCE TO 2200 RPM AND THEN RAPIDLY INCREASE TO FULL. CYCLE AS NEEDED. [ ] Watch for induction air filter icing ... 15 INCHES HG IN MP CAN OCCUR ABOVE 8000 FEET [ ] Plan landing [ ] Plan for [ ] Open left window [ ] Flaps ... USE 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 approach ... IF MISSED APPROACH IS MANDATORY, APPLY MAXIMAL POWER AND MAINTAIN 100 KIAS WHILE RETRACTING FLAPS IN 10° INCREMENTS. EXCESSIVE FUEL VAPOR [ABNORMAL] -------------------------------- [ ] Auxiliary fuel pump [ ] Mixture [ ] Fuel selector valve ....... SELECT OPPOSITE TANK IF SYMPTOMS CONTINUE [ ] Auxiliary fuel pump switch ....... OFF AFTER FUEL FLOW HAS STABILIZED AMMETER – EXCESSIVE RATE OF CHARGE [ABNORMAL] ---------------------------------------------- [ ] Alternator [ ] Nonessential electrical equipment [ ] With alternator side of master OFF [ ] Nonessential electrical equipment [ ] Terminate flight LOW VOLTAGE ANNUNCIATOR – AMMETER INDICATES DISCHARGE [ABNORMAL] ----------------------------------------------------------------- [ ] Avionics master [ ] Alternator circuit breaker (ALT FLD) [ ] Master switch [ ] Master switch [ ] Low voltage annunciator ** NOTE: IF LOW VOLTAGE ILLUMINATES [ ] Alternator [ ] Nonessential electrical equipment [ ] Terminate flight EMERGENCY DESCENT [EMERGENCY] ------------------------------ 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 [EMERGENCY] ------------------------------ [ ] Control wheel ......... GRASP FIRMLY AND MAINTAIN CONTROL OF AIRCRAFT [ ] A/P DISC/TRIM INT switch ............................. PRESS AND HOLD [ ] Aircraft [ ] Autopilot breaker STATIC SOURCE BLOCKAGE [EMERGENCY] ----------------------------------- [ ] Static pressure alternate source valve ...................... PULL ON [ ] Heat and air vents .......................................... PULL ON [ ] Vents [ ] Airspeed and altitude ................... REFER TO CALIBRATION CHARTS SPEEDS ------ [ ] Vr — Rotation speed ......................................... 55 KIAS [ ] Vx — Best angle climb .............................. 70 (SL) 75 (10K) [ ] Vy — Best rate climb ............................... 86 (SL) 82 (10K) [ ] Vso — Stall with flaps .......................... 38 (rcog) 44 (fcog) [ ] Vs — Stall without flaps ........................ 50 (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 speed ................................... 182 KIAS [ ] Vno — Maximum structural cruising speed .................... 149 KIAS [ ] Maximum window open [ ] Normal climb out ......................................... 75-85 KIAS [ ] Shortfield/Flaps 20° climb .................................. 74 KIAS [ ] Enroute climb [ ] Normal approach flaps up ................................. 80-90 KIAS [ ] Normal approach flaps 40° ................................ 70-80 KIAS [ ] Short field approach flaps 40° .............................. 67 KIAS [ ] Balked landing flaps 20° .................................... 80 KIAS [ ] Maximum demonstrated crosswind ............................. 20 KNOTS [ ] Engine failure after takeoff flaps up ....................... 80 KIAS [ ] Engine failure after takeoff flaps down ..................... 70 KIAS MAXIMUM GLIDE [ ] 3600 pounds [ ] 3200 pounds [ ] 2800 pounds [ ] Precautionary landing w/engine power ........................ 70 KIAS [ ] Landing without engine power/flaps up ....................... 80 KIAS [ ] Landing without engine power/flaps down ..................... 70 KIAS EMERGENCY DESCENT [ ] Smooth air [ ] Rough air — 3600 pounds [ ] Rough air — 2900 pounds [ ] Rough air — 2200 pounds PERFORMANCE TABLE ----------------- 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 ----------------- [ ] 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