Digital aircraft checklist

Beechcraft

Beechcraft Bonanza G36 Checklist Template

Bring the Beechcraft Bonanza G36 into ACE with a structured, editable template designed for a faster and more deliberate setup.

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Beechcraft

Beechcraft Bonanza G36
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Checklists
85
Total items
1008
File format
ACE

Preview only. This sample is not an operational checklist. Always use the applicable approved aircraft documentation.

01 PreflightPreflight Inspection 130 items
  1. 01 Cabin
  2. 02 Emergency Exits CHECK
  3. 03 Safety Wire INTACT
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02 PreflightBefore Engine Start 36 items
  1. 01 Seats POSITION FOR TAKEOFF
  2. 02 Rudder Pedals ADJUST
  3. 03 Seat Belts & Shoulder Harness FASTEN AND ADJUST
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03 PreflightStarting Engine (Battery) 12 items
  1. 01 CAUTION
  2. 02 Do not engage starter for more than 30 seconds in any 4 minute time period.
  3. 03 Cold Start:
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04 PreflightBefore Taxi 53 items
  1. 01 Throttle 1000 TO 1200 RPM
  2. 02 Oil Temperature and Pressure CHECK
  3. 03 Avionics Master ON
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05 PreflightBefore Takeoff (Runup) 40 items
  1. 01 Parking Brake SET
  2. 02 Seat Belts & Shoulder Harnesses CONFIRM BUCKLED
  3. 03 Engine Instruments CHECK WITHIN LIMITS
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06 PreflightBefore Takeoff (Final Items) 10 items
  1. 01 Pitot Heat AS REQUIRED
  2. 02 Lights AS REQUIRED
  3. 03 Air Conditioning OFF
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07 PreflightTakeoff 14 items
  1. 01 Takeoff Power SET
  2. 02 Throttle FULL FORWARD
  3. 03 Propeller HIGH RPM
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08 PreflightClimb 17 items
  1. 01 Power SET
  2. 02 Throttle FULL FORWARD
  3. 03 Propeller SET
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09 PreflightCruise 9 items
  1. 01 Cowl Flaps CLOSE
  2. 02 Power SET
  3. 03 NOTE
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10 PreflightDescent 11 items
  1. 01 Altimeters SET
  2. 02 PFD and Standby
  3. 03 Cowl Flaps CONFIRMED CLOSED
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11 PreflightBefore Landing 11 items
  1. 01 Seat Belts & Shoulder Harnesses FASTENED
  2. 02 Seat Backs POSITION FOR LANDING
  3. 03 Fuel Selector Valve SELECT FULLER TANK
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12 PreflightNormal Landing 4 items
  1. 01 Flaps DOWN
  2. 02 124 KTS or below
  3. 03 Airspeed ESTABLISH NORMAL APPROACH SPEED
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13 PreflightAfter Landing 5 items
  1. 01 Cowl Flaps OPEN
  2. 02 Flaps UP
  3. 03 Landing, Taxi & Strobe Lights AS REQUIRED
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14 PreflightShutdown and Securing 17 items
  1. 01 Parking Brake SET
  2. 02 Avionics OFF
  3. 03 MFD EXTINGUISHED
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15 LandingBalked Landing 6 items
  1. 01 Throttle & Propeller FULL FORWARD
  2. 02 Airspeed 80 KTS
  3. 03 Until clear of obstacles, then trim for 110 KTS
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16 DoorsForward Cabin Door Open in Flight 9 items
  1. 01 Maintain CONTROL OF AIRPLANE
  2. 02 Door DO NOT ATTEMPT TO CLOSE
  3. 03 Until after landing
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17 Starting EngineFlooded Start 7 items
  1. 01 Mixture CUT OFF
  2. 02 Propeller HIGH RPM
  3. 03 Throttle 1/2 OPEN
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18 Starting EngineHot Start 12 items
  1. 01 Mixture CUT OFF
  2. 02 Propeller HIGH RPM
  3. 03 Aux Fuel Pump HI FOR 30 - 60 SECONDS, THEN OFF
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19 Starting EngineStarting with External Power 24 items
  1. 01 Battery 1 & 2, Alternator 1 & 2 OFF
  2. 02 Avionics Master Switch OFF
  3. 03 Electrical Equipment OFF
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20 EngineRough Running Engine 8 items
  1. 01 Fuel Selector Valve SWITCH TANKS
  2. 02 If engine roughness continues:
  3. 03 Aux Fuel Pump LO
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21 ElectricalStarter Engaged [STARTER ENGD] 4 items
  1. 01 After engine start, if the starter relay remains engaged, the starter will remain energized and the [STARTER ENGD] will be displayed in the Annunciator Window. This will eventually lead to the failure of Bus 1.
  2. 02 Battery 1 OFF
  3. 03 Alternator 1 OFF
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22 ElectricalAlternator 1 Overvoltage [BUS 1 VOLT HI] 10 items
  1. 01 An Alternator 1 overvoltage condition will overcharge Battery 1 and possibly damage equipment on Bus 1.
  2. 02 Bus Volts 1 CHECK
  3. 03 If voltage is less than 30 volts a false warning is indicated.
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23 ElectricalAlternator 2 Overvoltage [BUS 2 VOLT HI] 16 items
  1. 01 An Alternator 2 overvoltage condition will overcharge Battery 2 and possibly damage equipment on Bus 2.
  2. 02 Bus Volts 2 CHECK
  3. 03 If voltage is less than 30 volts a false warning is indicated.
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24 ElectricalAlternator 2 Overload 10 items
  1. 01 If Battery 2 is not fully charged when the [BUSES TIED] extinguishes (RPM >= 2000), ALT 2 may exceed 100% for a short period of time. ALT LOAD 2 is approved up to 120% for 5 minutes at which time the display will turn yellow.
  2. 02 If ALT LOAD 2 display turns yellow:
  3. 03 Alternator 2 OFF
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25 ElectricalBus Tie Relay Closed [BUSES TIED] 3 items
  1. 01 If the [BUSES TIED] is illuminated during flight, Bus 1 and Bus 2 will be linked and any failure on one bus may affect the other bus, potentially damaging instruments and equipment on both buses.
  2. 02 Continue TO DESTINATION
  3. 03 Repair AS SOON AS PRACTICAL
26 ElectricalCircuit Breaker Tripped 6 items
  1. 01 Nonessential Circuit DO NOT RESET IN FLIGHT
  2. 02 Essential Circuit necessary for continued safe flight:
  3. 03 Circuit Breaker PUSH TO RESET
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27 Landing GearLanding Gear Manual Extension 20 items
  1. 01 Airspeed 154 KIAS OR LESS
  2. 02 Lower speeds facilitate a manual extension
  3. 03 LANDING GEAR MOTOR Circuit Breaker PULL
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28 Landing GearLanding Gear Retraction After Practice Manual Extension 5 items
  1. 01 After practice manual extension of the landing gear, the gear can only be retracted electrically, as follows:
  2. 02 Handcrank CONFIRMED STOWED
  3. 03 LANDING GEAR MOTOR Circuit Breaker IN
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29 IcingInduction System Icing 2 items
  1. 01 If induction system icing occurs, the Alternate air door should automatically open. To ensure the door opens:
  2. 02 Alternate Air T-Handle PULL AND RELEASE
30 IcingAlternate Static Air Source 6 items
  1. 01 Whenever any obstruction exists in the Normal Static Air System or the Alternate Static Air System is desired for use:
  2. 02 Alternate Static Air Source (ALTERNATE) ON
  3. 03 For Airspeed Calibration and Altimeter Correction refer to Section 5, Performance, in the POH
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31 IcingElectrothermal Propeller Deice (if installed) 18 items
  1. 01 Normal operation: 14 - 18 amps
  2. 02 Zero amps:
  3. 03 Prop Deice Switch CHECK POSITION
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32 Air ConditioningAir Conditioning System Malfunction 3 items
  1. 01 Air Conditioning System OFF
  2. 02 If air conditioning system circuit breakers trip:
  3. 03 Do not reset until the cause of the malfunction has been determined and corrected.
33 AutopilotFailure of Autopilot Preflight Test - Red [PFT FAIL] 3 items
  1. 01 AP SERVOS Circuit Breaker PULL
  2. 02 [PFT FAIL] Extinguishes
  3. 03 Do not reset circuit breaker unless the airplane is on the ground.
34 AutopilotAutopilot Out of Trim 18 items
  1. 01 Yellow Indications:
  2. 02 [RUD <-]. [RUD ->], [AIL <-], [AIL ->], [UP ELE] or [DOWN ELE]
  3. 03 CAUTION
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35 AutopilotLoss of Flight Director/Autopilot Mode 6 items
  1. 01 Yellow Flashing Mode Annunciator
  2. 02 Loss of Selected Vertical Mode (FLC, VS, ALT or GS) or Loss of Selected Lateral Mode (HDG, VOR, GPS, BC, LOC or VAPP):
  3. 03 Autopilot Mode Control SELECT ANOTHER VERTICAL OR LATERAL MODE
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36 AvionicsLoss of Navigation Information 9 items
  1. 01 [VOR], [VAPP], [GPS], [LOC], [BC] or [GS]
  2. 02 CDI Softkey SELECT ANOTHER NAV SOURCE
  3. 03 HDG Bug SELECT INTERCEPT ANGLE
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37 AvionicsAvionics Master Switch Failure 4 items
  1. 01 If the Avionics Master Switch fails to operate in the ON position:
  2. 02 Avionics Master Circuit Breaker PULL
  3. 03 Left panel
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38 AvionicsTransponder Failure [XPDR FAIL] 4 items
  1. 01 Transponder CONFIRM STATUS WITH ATC
  2. 02 If Transponder is inoperative:
  3. 03 Traffic Advisory System STBY
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39 AvionicsEngine and/or Fuel Display Failure 8 items
  1. 01 If all engine instruments are inoperative:
  2. 02 ENG/AFR SENSOR Circuit Breaker CHECK IN
  3. 03 If partial failure has occurred:
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40 AvionicsFailure of Cooling Fans [PFD FAN FAIL], [MFD FAN FAIL] or [AVIONICS FAN] Advisory Message 2 items
  1. 01 Flight CONTINUE TO DESTINATION
  2. 02 Repair AS SOON AS PRACTICAL
41 AvionicsLoss of, or Invalid GPS Signal 1 items
  1. 01 Navigation USE NAV 1 & NAV 2 RECEIVERS
42 AvionicsPosition Error [POSN ERROR] 1 items
  1. 01 Navigation USE NAV 1 & NAV 2 RECEIVERS
43 AvionicsLoss of RAIM 11 items
  1. 01 During enroute, oceanic, terminal or initial approach phase of flight:
  2. 02 GPS CONTINUE TO USE
  3. 03 NAV 1 or NAV 2 VERIFY POSITION
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44 AvionicsAltimeter Disagreement 4 items
  1. 01 NOTE
  2. 02 If a significant difference is noted between the altitude displayed on the PFD and the standby altimeter, the GPS ALT displayed on the MFD may be used as a third source to help resolve the discrepancy.
  3. 03 WARNING
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45 AvionicsIllumination of CAUTION Annunciator 7 items
  1. 01 ALERTS Softkey PRESS
  2. 02 Displays message in alerts window
  3. 03 NOTE
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46 AvionicsOil Pressure Low [OIL PRESS LO] 4 items
  1. 01 Oil Pressure CONFIRM < 30 PSI
  2. 02 If confirmed:
  3. 03 Land NEAREST SUITABLE AIRPORT
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47 AvionicsFuel Quantity Low [FUEL QTY LO] 6 items
  1. 01 Fuel Indicators CONFIRM QTY
  2. 02 Fuel Tank CHANGE TO FULLEST TANK
  3. 03 Power REDUCE AS REQUIRED
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48 AvionicsAlternator 1 Load High [ALT 1 LOAD] 8 items
  1. 01 Alternator 1 Load CONFIRM > 100%
  2. 02 Non-Essential Electrical Equipment OFF
  3. 03 If load does not decrease below 100% and annunciation remains displayed:
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49 AvionicsAlternator 2 Load High [ALT 2 LOAD] 15 items
  1. 01 If Battery 2 is not fully charged when the [BUSSES TIED] extinguishes (RPM greater than 2,000), [ALT 2 LOAD] may exceed 100%. The alternator is approved for up to 120% for 5 minutes. The [ALT 2 LOAD] illuminates when this limit is exceede...
  2. 02 Alternator 2 Load CONFIRM > 100%
  3. 03 Non-Essential Electrical Equipment OFF
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50 AvionicsAlternator 1 Low Voltage [BUS 1 VOLT LO] 8 items
  1. 01 Bus 1 Volts CHECK
  2. 02 If voltage is greater than 24 volts, a false warning is indicated:
  3. 03 Alternator 1 CONTINUE TO USE
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51 AvionicsAlternator 2 Low Voltage [BUS 2 VOLT LO] 10 items
  1. 01 Bus 2 Volts CHECK
  2. 02 If voltage is greater than 24 volts, a false warning is indicated:
  3. 03 Alternator 2 CONTINUE TO USE
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52 TakeoffAborted Takeoff 12 items
  1. 01 Throttle CLOSED
  2. 02 Brakes AS REQUIRED
  3. 03 If airplane cannot be stopped on remaining runway:
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53 Engine And PropEngine Failure on Ground 10 items
  1. 01 NOTE
  2. 02 The most probable cause of engine failure are loss of fuel flow, ignition system malfunction or blockage of the induction system.
  3. 03 Engine Failure During Takeoff Ground Roll
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54 Engine And PropEngine Failure in Flight 23 items
  1. 01 WARNING
  2. 02 If engine failure happens immediately after takeoff, landing straight ahead is usually advisable.
  3. 03 Airspeed 85 KIAS
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55 Engine And PropPropeller Overspeed 9 items
  1. 01 Throttle RETARD
  2. 02 Airspeed REDUCE
  3. 03 Until propeller RPM is at or below 2700
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56 Engine And PropFuel Flow High [FUEL FLOW HI] 4 items
  1. 01 Fuel Flow CONFIRM >27.4 GPH
  2. 02 Boost Pump OFF
  3. 03 Unless required
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57 Engine And PropCylinder Head Temperature High [CHT HI] 11 items
  1. 01 CHT CONFIRM >238º C
  2. 02 Cowl Flaps OPEN
  3. 03 Mixture ENRICH AS REQUIRED
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58 Engine And PropOil Temperature High [OIL TEMP HI] 10 items
  1. 01 Oil Temperature CONFIRM >116º C
  2. 02 Cowl Flaps OPEN
  3. 03 Power REDUCE TO LOWEST PRACTICAL
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59 Engine And PropOil Pressure High [OIL PRESS HI] 4 items
  1. 01 Oil Pressure CONFIRM >100 PSI
  2. 02 Power REDUCE AS REQUIRED
  3. 03 Continue AT PILOT'S DISCRETION
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60 Engine And PropOil Pressure Low [OIL PRESS LO] 4 items
  1. 01 Oil Pressure CONFIRM <10 PSI
  2. 02 If confirmed:
  3. 03 Land AT NEAREST SUITABLE AIRPORT
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61 Engine And PropFuel Quantity Low [FUEL QTY LO] 3 items
  1. 01 Fuel Indicators CONFIRM LO QTY AND TANK
  2. 02 Fuel Tank CHANGE TO FULLEST TANK
  3. 03 Land AT NEAREST SUITABLE AIRPORT
62 Engine And PropEmergency Speed Reduction 7 items
  1. 01 Throttle IDLE
  2. 02 Landing Gear DOWN
  3. 03 Airspeed MONITOR
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63 FireEngine Fire in Flight 11 items
  1. 01 Firewall Air Control Knob PULL TO CLOSE
  2. 02 The red FIREWALL AIR control knob on the outboard side of the left lower subpanel should be pulled to close off all heating system outlets so that smoke and fumes will not enter the cabin.
  3. 03 Engine SHUTDOWN
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64 FireEngine Fire on Ground 7 items
  1. 01 Mixture CUT OFF
  2. 02 Starter CONTINUE TO CRANK
  3. 03 Fuel Selector Valve OFF
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65 FireElectrical Smoke or Fire 25 items
  1. 01 Battery 1 OFF
  2. 02 Alternator 1 OFF
  3. 03 Firewall Air Control PULL
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66 Approach And LandingEmergency Descent 7 items
  1. 01 Power IDLE
  2. 02 Propeller HIGH RPM
  3. 03 Landing Gear DOWN
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67 Approach And LandingDitching, Off-Airport Landing, or Flying VFR Around Unique Terrain 7 items
  1. 01 Inhibit the the visual and voice alerts of the TAWS system using the following procedure. The terrain page will remain operational on the MFD and the GPWS functions will still be operational.
  2. 02 On the MFD:
  3. 03 Large FMS Knob SELECT MAP GROUP
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68 Approach And LandingMaximum Glide Configuration 15 items
  1. 01 Landing Gear UP
  2. 02 The landing gear will not retract unless the throttle is in a position corresponding to approximately 17 inches of manifold pressure or above.
  3. 03 Flaps UP
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69 Approach And LandingLanding without Power 11 items
  1. 01 Fuel Selector Valve OFF
  2. 02 Mixture CUTOFF
  3. 03 Magnetos OFF
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70 Approach And LandingLanding with Gear Retracted - With Power 12 items
  1. 01 If possible, choose firm sod. Make normal approach using flaps as necessary.
  2. 02 The landing gear will not retract unless the throttle is in a position corresponding to approximately 17 inches of manifold pressure or above.
  3. 04 Throttle CLOSED
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71 ElectricalAlternator 1 & 2 Failure [ALT 1 - 2 INOP] & [BUSES TIED] 16 items
  1. 01 Alt 1 & Alt 2 CHECK
  2. 02 Alternator 1 & 2 Switches VERIFY ON
  3. 03 Alt Load 1 & 2 CHECK
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72 ElectricalAlternator 1 Failure [ALT 1 INOP] 15 items
  1. 01 Alternator 1 CHECK
  2. 02 Alternator 1 Switch VERIFY ON
  3. 03 Alt Load 1 CHECK
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73 ElectricalAlternator 2 Failure [ALT 2 INOP], [BUSES TIED] 18 items
  1. 01 During ground operations, a failure of Alternator 2 can only be detected at RPMs above 2000.
  2. 02 It is normal for the [BUSES TIED] to be displayed when engine RPM < 2000 RPM, such as during ground operations and during landing.
  3. 03 An inoperative Alternator 2 will allow the bus tie relay to close. Battery 2 and BUS 2 will receive power from Bus 1.
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74 ElectricalAlternator 2 Failure & Bus Tie Failure [ALT 2 INOP] 16 items
  1. 01 Illumination of the [ALT 2 INOP] without the illumination of the [BUSES TIED] indicates that the bus tie contactor has failed to close. Thus, Bus 2 will only be powered by Battery 2.
  2. 02 Alternator 2 CHECK
  3. 03 Alternator 2 Switch VERIFY ON
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75 ElectricalComplete Electrical Failure 8 items
  1. 01 Airplane Control MAINTAIN USING STBY INSTRUMENTS
  2. 02 Standby Attitude Indicator PRESS STBY PWR BUTTON
  3. 03 Confirm flag is pulled
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76 SpinsSpin Recovery 6 items
  1. 01 Intentional spins are prohibited. If an unintentional spin is encountered, perform the following procedure IMMEDIATELY -- THE LONGER THE DELAY, THE MORE DIFFICULT THE RECOVERY WILL BECOME. Steps 1 through 3 should be done AGGRESSIVELY and...
  2. 02 Control Column FULL FORWARD, AILERONS NEUTRAL
  3. 03 Full Rudder OPPOSITE DIRECTION OF SPIN
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77 AutopilotAutopilot Automatic Disengagement 8 items
  1. 01 Loss of the following items will cause the autopilot to disconnect. The autopilot will remain inoperative and cannot be re-engaged until the inoperative item is restored. AHRS, ADC, PFD, GIA 1 (INTEG AVION 1) and GIA 2 (INTEG AVION 2).
  2. 02 AP DISC Switch PRESS
  3. 03 To cancel tone and flashing [AP]
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78 AutopilotAutopilot Overspeed Recovery [MAXSPD] 10 items
  1. 01 Throttle REDUCE POWER AS REQUIRED
  2. 02 Autopilot DISCONNECT
  3. 03 Manually slow the airplane
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79 AutopilotAutopilot Response to Erroneous AHRS Input 12 items
  1. 01 A failure of the AHRS may cause erroneous autopilot responsiveness and/or electric pitch trim deviations. One or more of the following indications may be present. Red [AFCS], Yellow or Red [AP], Yellow [CHECK ATTITUDE], unexpected Roll or ...
  2. 02 Control Wheel HOLD FIRMLY
  3. 03 Standby Attitude Indicator CROSS CHECK
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80 AutopilotElectric Pitch Trim Failure [PTRM] 12 items
  1. 01 Illumination of the red [PTRM] annunciator on the PFD:
  2. 02 Control Wheel HOLD FIRMLY
  3. 03 Be prepared for out of trim condition
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81 AutopilotUnscheduled Electric Pitch Trim 11 items
  1. 01 Red flashing [PTRM] and possibly Yellow [DOWN ELE] or [UPELE]
  2. 02 Airplane Attitude MAINTAIN USING ELEVATOR CONTROL
  3. 03 Expect residual pitch forces
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82 AvionicsAir Data Computer (ADC) Failure 3 items
  1. 01 Yellow [AIRSPEED FAIL], Yellow [ALTITUDE FAIL], Yellow [VERT SPEED FAIL] and Red X over TAS and OAT displays.
  2. 02 Refer to STANDBY Airspeed and Altimeter CHECK
  3. 03 Land AS SOON AS PRACTICAL
83 AvionicsAttitude and Heading Reference System (AHRS) Failure 6 items
  1. 01 Yellow [ATTITUDE FAIL], Red X over Attitude Display, Removal of Sky/Ground Display, Yellow HDG with red X, Compass Rose Digits Removed, Course Indicator will point straight up and Autopilot and Yaw Damper will disengage.
  2. 02 AP DISC Switch PRESS
  3. 03 If required to cancel autopilot tone & flashing [AP]
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84 AvionicsFailure of Either PFD or MFD 4 items
  1. 01 If the remaining display does not automatically revert to the reversionary mode:
  2. 02 DISPLAY BACKUP button PRESS
  3. 03 NOTE
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85 AvionicsFailure of Both PFD and MFD 4 items
  1. 01 Standby Instruments TRANSITION TO
  2. 02 NOTE
  3. 03 121.5 MHz will automatically be available to the pilot through the pilot's headset.
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Source checklist: Beechcraft Bonanza G36 Checklist

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