Digital flygplanschecklista

Bristell

Bristell B23-915 Garmin ACE-checklista

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Bristell B23-915 - Rotax 915iS Turbo
ACE

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Utforska Bristell B23-915 - Rotax 915iS Turbo-checklistan

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Checklistor
54
Punkter totalt
514
Filformat
ACE

Endast förhandsvisning. Det här exemplet är ingen operativ checklista. Använd alltid gällande godkänd flygplansdokumentation.

01 PreflightPreflight Inspection 55 punkter
  1. 01 Cockpit
  2. 02 LANE A and LANE B OFF
  3. 03 Avionics and Instruments CHECK CONDITION
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02 PreflightBefore Engine Starting 8 punkter
  1. 01 Allow the Rotax 915iS time to adjust to any new situation. Many actions are followed by a check of a warning light which may take a few seconds.
  2. 02 Luggage and Loose Objects SECURED
  3. 03 Rudder Pedal Position SET
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03 PreflightEngine Starting 35 punkter
  1. 01 Engine starting is limited to ambient temperature below 50°C and oil temperature above -20°C.
  2. 02 Circuit Breakers CHECK
  3. 03 Master Switch ON
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04 PreflightAfter Engine Start 7 punkter
  1. 01 Avionics ON
  2. 02 MFD SELECT ENGINE SCREEN
  3. 03 ALT C ON
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05 PreflightEngine Warmup 3 punkter
  1. 01 Throttle 2500 RPM UNTIL OIL TEMP 50°C
  2. 02 Throttle SET IDLE
  3. 03 Best cooling on the ground is not at idle but at 2500 to 3000 RPM.
06 PreflightBefore Taxiing 2 punkter
  1. 01 Nav Light (At Night) AS REQUIRED
  2. 02 Landing and Taxi Light AS REQUIRED
07 PreflightTaxiing 4 punkter
  1. 01 Keep engine speed below 2500 RPM until oil temperature reaches 50°C. Taxi carefully when wind exceeds 20 knots; hold the stick to properly deflect a crosswind.
  2. 02 Ground Control CHECK NOSE GEAR STEERING
  3. 03 Brakes CHECK FUNCTION
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08 PreflightEngine Run-Up 36 punkter
  1. 01 Perform the run-up heading upwind and not on loose terrain, or the propeller may suck grit and damage the blade leading edges.
  2. 02 Park Brake SET
  3. 03 Oil Temperature MINIMUM 50°C
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09 PreflightBefore Takeoff 14 punkter
  1. 01 Altimeter and Baro SET
  2. 02 Instruments CHECK
  3. 03 Pitch Trim SET TAKEOFF POSITION
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10 In FlightTakeoff 9 punkter
  1. 01 Brakes RELEASE
  2. 02 Propeller Control FULL FORWARD
  3. 03 Throttle FULL POWER
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11 In FlightShort and Soft Field Takeoff 14 punkter
  1. 01 Runway USE ALL AVAILABLE
  2. 02 Flaps 10°
  3. 03 Trim AS REQUIRED
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12 In FlightClimb 8 punkter
  1. 01 Climb Speed BEST RATE 82 KIAS, BEST ANGLE 66 KIAS
  2. 02 Throttle FULL FORWARD
  3. 03 Propeller Control SET ENGINE SPEED
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13 In FlightCruise 5 punkter
  1. 01 Fuel Selector LEFT OR RIGHT
  2. 02 Switch tanks in regular intervals of about 25 min. A low fuel caution indicates about 5 liter usable remaining in that tank, roughly 12 min at moderate power.
  3. 03 Throttle SET AS DESIRED
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14 In FlightDescent 5 punkter
  1. 01 Throttle REDUCE, 15 TO 17 INHG
  2. 02 Propeller Control SET MAX 5000 RPM
  3. 03 Airspeed SET 90 TO 100 KIAS
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15 In FlightBefore Landing 15 punkter
  1. 01 Seat Belts TIGHTEN
  2. 02 Cockpit PREPARE
  3. 03 Autopilot DISENGAGE
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16 In FlightBalked Landing (Go-Around) 7 punkter
  1. 01 Throttle FULL FORWARD
  2. 02 Speed ACCELERATE TO 70 KIAS
  3. 03 Flaps SET 10°
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17 In FlightLanding 4 punkter
  1. 01 Throttle CLOSE
  2. 02 Touchdown ON MAIN WHEELS
  3. 03 Brakes APPLY AS NEEDED
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18 In FlightShort Field Landing 6 punkter
  1. 01 Throttle FULLY CLOSE BEFORE FLARE
  2. 02 Touchdown ON MAIN WHEELS
  3. 03 Flare MINIMUM FLOAT
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19 In FlightSoft Field Landing 7 punkter
  1. 01 Touchdown ON MAIN WHEELS
  2. 02 Flare ADD POWER BEFORE TOUCHDOWN
  3. 03 Expect excessive ground friction. Power keeps the elevator effective to avoid a violent nose gear drop and keep weight off the nose wheel.
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20 PostflightAfter Landing 2 punkter
  1. 01 Engine Speed SET AS REQUIRED FOR TAXIING
  2. 02 Landing Light AS REQUIRED FOR TAXI
21 PostflightShutdown 17 punkter
  1. 01 Propeller Control FINE PITCH (FULLY FORWARD)
  2. 02 Engine Speed IDLE
  3. 03 Engine Instruments CHECK WITHIN LIMITS
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22 PostflightParking and Tie-Down 7 punkter
  1. 01 LANE Switches CHECK OFF
  2. 02 Master Switch CHECK OFF
  3. 03 Parking Brake SET
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23 Engine FailureEngine Failure During Takeoff Run 3 punkter
  1. 01 Throttle IDLE
  2. 02 LANE A and LANE B OFF
  3. 03 Brakes APPLY
24 Engine FailureEngine Failure Enroute or During Takeoff 17 punkter
  1. 01 Speed GLIDE AT 67 KIAS
  2. 02 Below 150 FT AGL LAND IN TAKEOFF DIRECTION
  3. 03 Over 150 FT AGL AREA WITH LITTLE DEVIATION
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25 Engine FailureIn-Flight Engine Restart 9 punkter
  1. 01 AUX Pump ON
  2. 02 Fuel Selector FULLEST TANK
  3. 03 Throttle Lever MIDDLE
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26 Smoke and FireEngine Fire on Ground at Engine Starting 8 punkter
  1. 01 Brakes APPLY
  2. 02 Fuel Selector CLOSE
  3. 03 Heating CLOSE
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27 Smoke and FireFire on Ground With Engine Running 10 punkter
  1. 01 Heating CLOSE
  2. 02 Brakes APPLY
  3. 03 Fuel Selector CLOSE
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28 Smoke and FireEngine Fire During Takeoff 11 punkter
  1. 01 Speed 67 KIAS
  2. 02 Heating CLOSE
  3. 03 If Landing Is Ensured or Fire Gets Critical
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29 Smoke and FireEngine Fire in Flight 9 punkter
  1. 01 Heating CLOSE
  2. 02 Fuel Selector CLOSE
  3. 03 LANE A and LANE B OFF
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30 Smoke and FireFire in the Cockpit 11 punkter
  1. 01 Master Switch OFF
  2. 02 GEN A/B OFF
  3. 03 ALT C OFF
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31 Emergency LandingGlide 3 punkter
  1. 01 Speed 67 KIAS
  2. 02 Flaps RETRACTED
  3. 03 An engine stopped by failure may degrade glide performance beyond the tested windmilling condition.
32 Emergency LandingLanding Without Engine Power 15 punkter
  1. 01 Speed BEST GLIDE 67 KIAS
  2. 02 Propeller TAKEOFF POSITION
  3. 03 Trim ADJUST
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33 Emergency LandingPrecautionary Landing 13 punkter
  1. 01 Speed 67 KIAS (BEST GLIDE)
  2. 02 Propeller TAKEOFF POSITION
  3. 03 Trim ADJUST
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34 Emergency LandingLanding With a Flat Tire 3 punkter
  1. 01 Damaged Wheel KEEP ABOVE GROUND AS LONG AS POSSIBLE
  2. 02 Use aileron or elevator control as applicable.
  3. 03 Direction MAINTAIN WITH RUDDER ON ROLL OUT
35 Emergency LandingLanding With Defective Landing Gear 4 punkter
  1. 01 Main Gear Damaged TOUCH DOWN AT LOWEST SPEED
  2. 02 If possible maintain direction during the landing run.
  3. 03 Nose Wheel Damaged HOLD NOSE OFF AS LONG AS POSSIBLE
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36 Emergency LandingAircraft Turn Over 5 punkter
  1. 01 Airplane LEAVE AS SOON AS POSSIBLE
  2. 02 Mitigates the risk of post-crash fire from leaking fuel.
  3. 03 Emergency Hammer USE IF CANOPY INTACT
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37 Unusual AttitudesLoss of Spatial Orientation 3 punkter
  1. 01 LVL Button on Autopilot (If Installed) PRESS
  2. 02 The autopilot takes over control and puts the airplane in a level attitude.
  3. 03 If Control Not Regained CONSIDER AEPS ACTIVATION
38 Unusual AttitudesRecovery From Unintentional Spin 9 punkter
  1. 01 Intentional spins are prohibited.
  2. 02 Power IDLE
  3. 03 Aileron Control NEUTRALIZE
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39 Rotax 915iS EmergenciesLANE Warning Lamps 6 punkter
  1. 01 LANE A and B lamps OFF is the nominal condition.
  2. 02 Both Lamps ON Steady LOSS OF ENGINE POWER POSSIBLE
  3. 03 The system relies on default values and tries to maintain operation. On ground: maintenance required, flight not permissible. In flight: landing as soon as practical is advised.
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40 Rotax 915iS EmergenciesInternal Generator Failure 13 punkter
  1. 01 If Generator A fails, the ECU automatically switches the EMS supply to Generator B with no performance drop. Both lamps flash: the airframe is then not supplied by an internal generator.
  2. 02 Suspected GEN B Failure
  3. 03 A GEN B failure in flight is not detected by the ECU and not annunciated.
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41 Rotax 915iS EmergenciesEngine Not Responding to Throttle 6 punkter
  1. 01 Possible breakage or blockage of the throttle valve actuation. On breakage the valve jumps to wide open position.
  2. 02 Except for in-flight emergency, never attempt starting the engine with a disconnected, broken or blocked throttle valve actuation. This may lead to excessive engine speeds.
  3. 03 Power Control USE PROPELLER CONTROL
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42 Rotax 915iS EmergenciesEmergency Engine Shut-Off 3 punkter
  1. 01 LANE A OFF
  2. 02 LANE B OFF
  3. 03 The ECU must be deactivated before the fuel pumps. Shutting down by fuel pumps alone is only allowed in emergency situations.
43 Rotax 915iS EmergenciesSprag Clutch Fails to Decouple 3 punkter
  1. 01 Audible as a creeping, abnormal engine sound.
  2. 02 Shut down the engine. Risk of fire and of the electric starter overheating.
  3. 03 Engine SHUT DOWN PER EMERGENCY SHUT-OFF
44 Rotax 915iS EmergenciesFuel Pressure Outside Range 8 punkter
  1. 01 Reduce engine power to the minimum necessary and prepare for in-flight shutdown and precautionary landing.
  2. 02 High Fuel Pressure
  3. 03 If AUX Pump ON AUX PUMP OFF
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45 Rotax 915iS EmergenciesLoss of Oil Pressure 5 punkter
  1. 01 Engine Power REDUCE TO MINIMUM NECESSARY
  2. 02 Oil Temperature CHECK
  3. 03 If Temperature High CONTINUE ON LOW POWER
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46 Rotax 915iS EmergenciesHigh Oil Pressure 4 punkter
  1. 01 Engine Power REDUCE TO MINIMUM NECESSARY
  2. 02 Engine RPM (Propeller) REDUCE BELOW 5000
  3. 03 Speed 67 KIAS
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47 System EmergenciesVibration 4 punkter
  1. 01 Engine Speed SET WHERE VIBRATIONS ARE LOWEST
  2. 02 In case of severe vibration of powerplant origin endangering structural integrity, shut the engine down.
  3. 03 Land AS SOON AS PRACTICAL
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48 System EmergenciesAutopilot Malfunction 5 punkter
  1. 01 AP OFF Button (Stick) PRESS
  2. 02 Autopilot Circuit Breaker PULL
  3. 03 Takeoff, initial climb, final approach and landing with autopilot engaged, and any operation with a malfunctioning autopilot, are PROHIBITED.
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49 System EmergenciesBus System Failure 14 punkter
  1. 01 The bus system has two main sections, Pilot/GEN A/B with the avionics sub-bus and BATT/ALT C, connected via the BUS TIE circuit breaker.
  2. 02 Upon Complete Loss of Electric Power
  3. 03 Backup Power ON
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50 System EmergenciesOvervoltage 6 punkter
  1. 01 Overvoltage is more than 15 volts.
  2. 02 Engine RPM REDUCE (PROPELLER AND POWER)
  3. 03 GEN A/B and ALT C CHECK TO IDENTIFY FAULTY SIDE
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51 System EmergenciesInadvertent Icing Encounter 6 punkter
  1. 01 Operation in known icing conditions is PROHIBITED.
  2. 02 Pitot Heat ON
  3. 03 Icing Conditions EXIT, CHANGE ALTITUDE OR TURN BACK
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52 System EmergenciesLoss of Primary Instruments 5 punkter
  1. 01 The independent standby EFIS is the primary flight display. In case of Garmin display malfunction or discrepancy refer to the standby EFIS.
  2. 02 Loss of One GDU460 CONTINUE FLIGHT
  3. 03 Loss of Both GDU460 LAND AS SOON AS PRACTICAL
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53 System EmergenciesRPM Overspeed or Propeller Vibration 4 punkter
  1. 01 Propeller control by the hydraulic governor depends on the oil circuit and a chain of mechanical connections.
  2. 02 Throttle and RPM Control ADJUST FOR SMOOTH RUNNING
  3. 03 If Engine Within Limits LAND AS SOON AS PRACTICAL
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54 Rescue SystemAEPS Activation (If Installed) 19 punkter
  1. 01 Use the airplane emergency parachute system as a last resort for loss of control, loss of structural integrity, loss of spatial orientation or inability to land safely.
  2. 02 The rescue system must be unlocked during flight to allow immediate use in emergency.
  3. 03 Minimum effective altitude is 1000 ft above ground. Avoid activation in strong updrafts; leave the updraft first if possible.
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