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Airbus A320 CBT

A320

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Airbus A320 CBT

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  1. Flight controls Normal Operation (A) MENU

  2. As part of the preliminary cockpit preparation, you will check that : • the flap position agrees with the lever position, • the speed brake lever is in the RET position. WARNING: If a flight control surface position does not agree with the lever position, check with the maintenance crew before applying hydraulic power. MENU

  3. During the walk-around, you should ensure that all the flight control surfaces are undamaged, and free of any contamination e.g. snow or ice. The same check is performed on each side of the aircraft. MENU

  4. During cockpit preparation, the only check associated with the flight controls is to ensure that all flight control computers are in the lights out configuration. MENU

  5. Amber bank angle protection indicators Notice that before engine start, the bank angle protection indicators are displayed in amber on the PFD. The side sticks are inoperative because there is no hydraulic power. Moving the side sticks will not affect the control surfaces. MENU

  6. Captain seat Seat controls Armrest control knob Before pushback, for your own comfort, it may be necessary to adjust the position of the seats and the armrests to easily handle the side stick. This is done by using the seat electrical controls and the armrest control knob. MENU

  7. In the same way, it may be necessary to adjust the position of the rudder pedals. This is done using the rudder pedal adjuster. MENU

  8. After engine start, the ground spoilers are armed by pulling the lever out. Lift the Speed Brake lever... MENU

  9. After engine start, the ground spoilers are armed by pulling the lever out. No, click on the Speed Brake lever...

  10. After engine start, the ground spoilers are armed by pulling the lever out. No, click on the Speed Brake lever...

  11. A white band appearing around the base of the speedbrake lever and the green memo GND SPLRS ARMED on the E/WD indicate that the spoilers are now armed. MENU

  12. Next, the rudder trim is zeroed by pushing the reset pb. Reset the rudder trim. MENU

  13. Next, the rudder trim is zeroed by pushing the reset pb. No, click on the RESET pb.

  14. Next, the rudder trim is zeroed by pushing the reset pb. No, click on the RESET pb.

  15. The trim is now reset to zero. This is checked on the RUD TRIM panel. It can also be seen on the ECAM F/CTL page via a blue line displayed below the rudder scale. Note: the RUD TRIM rotary switch is isolated during flight with the autopilot engaged. MENU

  16. The Take off memo normally appears during taxiing. For training purposes, we have displayed it now. The flaps should be set to their take-off position (1+F, 2 or 3) . While the flaps are deploying, we will be looking at their indications on the E/WD. To set the flaps, you need to lift up the lower part of the flap lever, and then position it to the appropriate setting. Here, as an example, we will select Flap 3. Select FLAP 3. MENU

  17. The Take off memo normally appears during taxiing. For training purposes, we have displayed it now. The flaps should be set to their take-off position (1+F, 2 or 3) . While the flaps are deploying, we will be looking at their indications on the E/WD. To set the flaps, you need to lift up the lower part of the flap lever, and then position it to the appropriate setting. Here, as an example, we will select Flap 3. No, click on the flap lever.

  18. The Take off memo normally appears during taxiing. For training purposes, we have displayed it now. The flaps should be set to their take-off position (1+F, 2 or 3) . While the flaps are deploying, we will be looking at their indications on the E/WD. To set the flaps, you need to lift up the lower part of the flap lever, and then position it to the appropriate setting. Here, as an example, we will select Flap 3. No, click on the flap lever.

  19. As soon as a flap selection is made: • blue markers appear on the E/WD to show the selected flap and slat positions, • A blue number shows which flap position has been selected (here 3), • The word FLAP appears in blue. MENU

  20. Also as soon as a flap selection is made: • The current flap and slat position green markers move, • The green labels S and F appear. MENU

  21. When the flaps and slats have reached their selected positions: • All position indications turn from blue to green, • The word FLAP changes from blue to white, • The FLAPS T.O memo on the E/WD turns to green. MENU

  22. Take-off trim is set manually using the trim wheels. The pitch trim values are indicated on the scales beside the trim wheels. The take off trim has to be in the green range. Select either pitch trim wheel. MENU

  23. Take-off trim is set manually using the trim wheels. The pitch trim values are indicated on the scales beside the trim wheels. The take off trim has to be in the green range. No, click on either pitch trim wheel.

  24. Take-off trim is set manually using the trim wheels. The pitch trim values are indicated on the scales beside the trim wheels. The take off trim has to be in the green range. No, click on either pitch trim wheel.

  25. The pitch trim position set may be seen on the ECAM F/CTL page during the flight control check when taxiing, if required. The after start sequence for flight controls is complete. MENU

  26. When the flaps are extended, the ailerons are dropped by about 5 degrees in order to increase lift. The aileron indices are now pointing to a small white square which represents the new neutral position. MENU

  27. A flight control check is completed at a convenient stage while taxiing, as on a conventional aircraft. MENU

  28. Bank angle protection indicators On the PFD, the combined side stick deflection indicator is displayed as a white cross. The cross only indicates side stick deflections and does not indicate control surface position. The green bank angle protection Indicators have also appeared indicating Normal law as the aircraft is hydraulically powered. Combined side stick deflection indicators MENU

  29. The side sticks become operable after first engine start, as soon as hydraulic power is available. On ground, the control surfaces respond in direct relationship to movements of the side sticks. This is the ground mode. MENU

  30. As it is not possible to see the flight control surfaces from the cockpit, the reaction to side stick or rudder pedal movement is monitored on the ECAM F/CTL page. The page is automatically called when either of the side sticks, or either of the rudder pedals are moved. MENU

  31. We will start the flight control check with the elevators by moving the side stick to its full back position. Move the side stick. MENU

  32. The pilot non flying checks on the ECAM page that the elevators have moved to their full up position. Move the side stick fully forward. MENU

  33. The elevators have now moved to their full down deflection. Move the side stick back to neutral. MENU

  34. With the side stick neutral, ensure that the elevators have returned to the neutral position. The flight controls are working in pitch. MENU

  35. We will continue by checking the roll control. Move the side stick full left. MENU

  36. You can see on the ECAM that: • The left aileron has moved fully up, • The right aileron has moved fully down, • The roll spoilers on the left wing have extended. Move the side stick full right. MENU

  37. Now, you can see that: • The left aileron is fully down, • The right aileron is fully up, • The right roll spoilers are extended. Move the side stick back to neutral. MENU

  38. With the side stick neutral, ensure that the ailerons return to the neutral position and the spoilers are back in their stowed position. Now, we will check the rudder. MENU

  39. Before testing the rudder pedals, you need to press and hold the rudder PEDALS DISC button on the nose wheel steering handle, to prevent any unwanted steering inputs. Press the pedal disc button. MENU

  40. Before testing the rudder pedals, you need to press and hold the rudder PEDALS DISC button on the nose wheel steering handle, to prevent any unwanted steering inputs. No, click on the pedal disc button.

  41. Before testing the rudder pedals, you need to press and hold the rudder PEDALS DISC button on the nose wheel steering handle, to prevent any unwanted steering inputs. No, click on the pedal disc button.

  42. Now the rudder pedal movements will have no effect on the nose wheel steering. The right rudder pedal should now be pushed. Push the right rudder pedal. MENU

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