Digital aircraft checklist

Piper

Piper PA-30 Twin Comanche Checklist Template

Bring the Piper PA-30 Twin Comanche into ACE with a structured, editable template designed for a faster and more deliberate setup.

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Piper

Piper PA-30 Twin Comanche
ACE

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Checklists
34
Total items
551
File format
ACE

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

01 PreflightPreflight Inspection 73 items
  1. 01 Cockpit:
  2. 02 Landing Gear Selector DOWN
  3. 03 Master Switch ON
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02 PreflightStarting Engines 20 items
  1. 01 Master Switch ON
  2. 02 Gear Lights CHECK GREEN
  3. 03 Fuel Quantity CHECK GAUGE READING
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03 PreflightWarm Up and Ground Check 13 items
  1. 01 Engines 1000 - 1400 RPM
  2. 02 For not more than two minutes in warm weather, four minutes cold
  3. 03 Propellers LOW PITCH
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04 PreflightTaxiing and Pre-Takeoff 32 items
  1. 01 Brakes CHECK
  2. 02 Use Differential Power and Nose Wheel Steering Rather Than Brakes When Taxiing
  3. 03 Autopilot OFF
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05 In FlightTakeoff and Climb 16 items
  1. 01 Parking Brake OFF
  2. 02 Mixtures FORWARD
  3. 03 Propellers FORWARD
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06 In FlightCruising 1 items
  1. 01 The normal recommended economy cruising power setting is at 65% power. At 12,000 ft this gives a true airspeed of 186 MPH. This power setting is obtained under standard conditions at 2400 RPM and full throttle. Fuel consumption is approxima...
07 In FlightApproach and Landing 12 items
  1. 01 Prior to extending the landing gear for landing, retard both throttle controls to check that the landing gear warning horn is operating.
  2. 02 Final Approach Speed 100 MPH
  3. 03 Propeller SET AT LEAST 2400 RPM
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08 PostflightAfter Landing 4 items
  1. 01 Flaps RETRACT
  2. 02 Cowl Flaps OPEN
  3. 03 Electric Fuel Pump OFF
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09 PostflightShut Down 11 items
  1. 01 Radio OFF
  2. 02 Electrical Equipment OFF
  3. 03 Heater Fan OFF
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10 Engine FailuresEngine Failure During Takeoff 17 items
  1. 01 If 90 MPH IAS Has Not Been Attained:
  2. 02 Throttles BOTH CLOSED
  3. 03 Braking MAXIMUM
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11 Engine FailuresEngine Power Loss During Climb 10 items
  1. 01 Airspeed ESTABLISH VYSE
  2. 02 105 MPH OR 91 KT
  3. 03 Inoperative Engine IDENTIFY AND VERIFY
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12 Engine FailuresEngine Loss During Flight 11 items
  1. 01 Maintain Lateral and Directional Control. If Airspeed is Below Vmca (90 MPH) Reduce Power on Both Engines and Lower Nose of Aircraft As Required To Maintain Control and Increase Speed To 105 MPH
  2. 02 Inoperative Engine IDENTIFY AND VERIFY
  3. 03 Rudder APPLY
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13 Engine FailuresEngine Securing Procedure (Feathering Procedure) 25 items
  1. 01 Before Securing Inoperative Engine:
  2. 02 Fuel Selector SWITCH
  3. 03 To tank containing fuel
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14 Engine FailuresSingle Engine Operation on Crossfeed 11 items
  1. 01 The Fuel Crossfeed System Should Be Used Only During Emergency Conditions and Only in Level Flight
  2. 02 Inoperative Engine Side FUEL VALVE
  3. 03 On MAIN or AUX
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15 Engine FailuresAir Start (Unfeathering Procedure) 17 items
  1. 01 Magneto Switch ON
  2. 02 Mixture RICH
  3. 03 Fuel Selector ON
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16 Engine FailuresEngine Roughness in Flight 16 items
  1. 01 Affected Engine:
  2. 02 Alternate Air ON
  3. 03 If Roughness Continues After One Minute:
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17 FiresEngine Fire During Start 10 items
  1. 01 Affected Engine:
  2. 02 Starter CONTINUE CRANKING ENGINE
  3. 03 Mixture IDLE CUT-OFF
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18 FiresFire in Flight 18 items
  1. 01 Determine Source of Fire ELECTRICAL OR ENGINE
  2. 02 Electrical Fire (or Smoke in Cabin):
  3. 03 Master Switch OFF
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19 Emergency LandingsPower off Landing (Both Engines Out) 42 items
  1. 01 Suitable Field LOCATE
  2. 02 Preferably with an alternate
  3. 03 Wind Direction DETERMINE
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20 Emergency LandingsSingle Engine Landing 4 items
  1. 01 On Final Approach, When It is Certain The Field Can Be Reached:
  2. 02 Landing Gear EXTEND
  3. 03 Wing Flaps EXTEND 15º
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21 Emergency LandingsSingle Engine Go-Around 13 items
  1. 01 Power FULL POWER
  2. 02 Rudder APPLY
  3. 03 Towards operating engine as required
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22 Electrical Failures (With Dual Generators)Excessive Discharge 19 items
  1. 01 NOTE
  2. 02 Generators produce no charging output when engines are operated below 1200 RPM
  3. 03 An excessive rate of discharge at normal operating RPM indicates a defective generator or voltage regulator
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23 Electrical Failures (With Dual Generators)Battery Overcharge 11 items
  1. 01 A High Rate of Charge is Normal for The First Few Minutes of Flight
  2. 02 An excessive rate of charge after several minutes at normal operating RPM indicates a defective battery or voltage regulator
  3. 03 Ammeter INDICATES EXCESSIVE CHARGE
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24 Electrical Failures (Non-Paralleling Dual Alternators)Battery Overcharge 39 items
  1. 01 NOTE
  2. 02 Depressing and holding the alternator "left" or "right" press-to-test switch will indicate the output of the corresponding alternator. The outputs of the two alternators should be approximately equal
  3. 03 Ammeter INDICATES BATTERY DISCHARGE
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25 Engine EmergenciesHigh Oil Temperature 7 items
  1. 01 Cowl Flaps OPEN
  2. 02 Mixture ENRICH
  3. 03 Power REDUCE IF NECESSARY
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26 Engine EmergenciesHigh Cylinder Head Temperature 7 items
  1. 01 Cowl Flaps OPEN
  2. 02 Mixture ENRICH
  3. 03 Power REDUCE IF NECESSARY
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27 Engine EmergenciesLoss of Oil Pressure 3 items
  1. 01 Aircraft LAND
  2. 02 As soon as possible and investigate cause
  3. 03 Prepare for "Engine Power Loss During Flight" Procedure
28 Engine EmergenciesLoss of Fuel Pressure 7 items
  1. 01 Fuel Selector SWITCH
  2. 02 To a tank containing fuel
  3. 03 Electric Fuel Pump ON
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29 Engine EmergenciesPropeller Overspeed 9 items
  1. 01 Affected Engine:
  2. 02 Propeller Control AFT - DECREASE RPM
  3. 03 Throttle RETARD
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30 Descent And LandingLanding Gear Failure and Manual Extension 28 items
  1. 01 Prior To Executing Emergency Procedure:
  2. 02 Master Switch CHECK ON
  3. 03 Landing Gear Circuit Breakers CHECK AND RESET
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31 Descent And LandingEmergency Descent 17 items
  1. 01 Oxygen System Failure:
  2. 02 Seat Belt and Harness SECURE
  3. 03 Throttles RETARD
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32 Other EmergenciesInduction System Icing 11 items
  1. 01 The first indication of induction system icing is usually a drop in fuel flow, followed by engine roughness
  2. 02 Alternate Air FULL ON
  3. 03 Throttle FULL OPEN
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33 Other EmergenciesGyro Suction Failure 9 items
  1. 01 Suction Below 4.8 in Hg:
  2. 02 RPM INCREASE TO 2700
  3. 03 Altitude DESCEND
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34 Other EmergenciesOpen Door in Flight 8 items
  1. 01 To Close Door in Flight:
  2. 02 Airspeed BELOW 100 MPH (87 KT)
  3. 03 Cabin Vents CLOSE
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Source checklist: Piper PA-30 Twin Comanche Checklist

Showing 100 of 551 items. The remaining procedures stay in the app.

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