Digital flygplanschecklista

Bristell

Bristell B23-912iS Garmin ACE-checklista

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Bristell B23-912iS - Rotax 912iS
ACE

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Utforska Bristell B23-912iS - Rotax 912iS-checklistan

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Checklistor
56
Punkter totalt
555
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 9 punkter
  1. 01 Allow the Rotax 912iS 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 46 punkter
  1. 01 Engine starting is limited to ambient temperature below 50°C and oil temperature above -20°C.
  2. 02 Backup Battery Check
  3. 03 Backup Battery Switch ON, WAIT FOR PFD NORMAL MODE
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04 PreflightAfter Engine Start 7 punkter
  1. 01 Avionics Switch ON
  2. 02 MFD SELECT ENGINE SCREEN
  3. 03 ALT C ON
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05 PreflightEngine Warmup 5 punkter
  1. 01 Power Lever APPROX 2000 RPM FOR APPROX 2 MIN
  2. 02 Power Lever 2500 RPM UNTIL OIL TEMP 50°C
  3. 03 Engine Instruments CHECK TEMPERATURES AND PRESSURE
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06 PreflightBefore Taxiing 4 punkter
  1. 01 Nav Light (At Night) AS REQUIRED
  2. 02 Landing and Taxi Light AS REQUIRED
  3. 03 PFD, EFIS, MFD CHECK ADAHRS STABILIZED
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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 42 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 After a full-load ground test allow a short cooling run at idle speed to prevent vapor formation in the cylinder head.
  3. 03 Park Brake SET, FEET READY ON BRAKE PEDALS
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09 PreflightBefore Takeoff 15 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 Park Brake PUSH KNOB FORWARD TO RELEASE
  2. 02 Wheel Brakes RELEASE
  3. 03 Power Lever MAX (FULL FORWARD)
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11 In FlightShort and Soft Field Takeoff 12 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 74 KIAS, BEST ANGLE 62 KIAS
  2. 02 Power Lever MAX (FULL FORWARD)
  3. 03 Maximum 5800 RPM for 5 minutes, then reduce to maximum continuous 5500 RPM. Consider early reduction to reduce noise and engine stress.
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13 In FlightCruise 4 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 20 min at moderate power.
  3. 03 Power Lever SET AS DESIRED, MAX 5500 RPM
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14 In FlightDescent 5 punkter
  1. 01 Power Lever SET AS REQUIRED
  2. 02 Airspeed SET 90 TO 100 KIAS
  3. 03 Trim AS NEEDED
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15 In FlightBefore Landing 14 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 Power Lever MAX (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 Power Lever 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 Power Lever FULLY AFT 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 Power Lever IDLE
  2. 02 Engine Instruments CHECK WITHIN LIMITS
  3. 03 ALT C OFF, CHECK VOLT M MIN 13.4 V
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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 Park Brake SET
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23 Engine FailureEngine Failure During Takeoff Run 3 punkter
  1. 01 Power Lever 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 Power 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 912iS EmergenciesLANE Warning Lamps 6 punkter
  1. 01 LANE A and B warning 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 912iS 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 912iS EmergenciesEmergency Engine Shut-Off 4 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.
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42 Rotax 912iS 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
43 Rotax 912iS 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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44 Rotax 912iS 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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45 Rotax 912iS 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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46 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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47 System EmergenciesAutopilot Malfunction 5 punkter
  1. 01 AP OFF Button (Stick) PRESS
  2. 02 Autopilot CB (Blue Marked) 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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48 System EmergenciesControl Upset (Trim or Flap Runaway) 12 punkter
  1. 01 For an electric flap, aileron or elevator trim system failure leading to runaway or uncontrollable positioning. The CBs of all systems susceptible to runaway are marked blue.
  2. 02 Flap Runaway
  3. 03 Speed REDUCE BELOW 84 KIAS (FLAP SPEED)
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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, a chain of mechanical connections, and the SLPC unit.
  2. 02 Power Lever ADJUST FOR SMOOTH RUNNING
  3. 03 If Engine Within Limits LAND AS SOON AS PRACTICAL
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54 System EmergenciesMain Battery Fault (MAIN BATT Warning) 9 punkter
  1. 01 A fault detected by the lithium battery management system shows the yellow MAIN BATT warning on the PFD together with the master caution light.
  2. 02 Slow Flashing Battery LED, Normal Voltage NO ACTION IN FLIGHT
  3. 03 Possible cell to cell charge imbalance. Report to maintenance; do not dispatch the aircraft.
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55 System EmergenciesSLPC System Malfunction 6 punkter
  1. 01 Power Lever ADJUST TO MAINTAIN SAFE FLIGHT
  2. 02 Most SLPC failures (EMU loss, display bus data loss, governor servo failure, servo blockage or end stop signal loss) leave the propeller RPM constant, at an end stop, or slowly decaying to the minimum RPM stop. Anticipate reduced climb rate...
  3. 03 Oscillating Propeller RPM
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56 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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