Bus Guide Signs, Int Lts, Ant-Ice, Probe/Window Heat, C

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Author:
jsperry843
ID:
210886
Filename:
Bus Guide Signs, Int Lts, Ant-Ice, Probe/Window Heat, C
Updated:
2013-04-02 01:07:39
Tags:
Bus Guide
Folders:

Description:
SIGNS Panel, Int Lts, ANTI-ICE Panel, Probe/Window Heat, Cabin/Press, Air Condition
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  1. SIGNS Panel

    What signs illuminate with the NO PED switched to ON?
    • NO Personal Electronic Device (PED)
    • EXIT signs
  2. SIGNS Panel

    Why do we move the SEATBELT and NO PED switches together?

    Do we use the AUTO position?
    Creates the seatbelt chime - VX aircraft do not have a chime associated with the PED switch. A chime is associated with the SEATBELT switch, however. Moving both switches together our guest are alerted to fasten SEATBELT and to the NO PED requirement.

    We do not utilize the AUTO position.
  3. SIGNS Panel

    What lights illuminate when the EMER EXIT LT switch is placed ON?
    • Proximity emergency escape path marking system
    • Overhead emergency lights
    • EXIT signs
  4. SIGNS Panel

    When will the proximity emergency escape path marking system automatically illuminate?
    • With the EMER EXIT LT switch in ARM and:
    • Normal aircraft electrical power system failure or
    • DC ESS SHED BUS fail
  5. SIGNS Panel

    When will the overhead emergency lights automatically illuminate?
    • With the EMER EXIT LT switch in ARM and:
    • Normal aircraft electrical power system fails or
    • DC ESS SHED BUS fails or
    • AC BUS 1 fails (DC ESS SHED BUS powered)
  6. SIGNS Panel

    When will the EXIT signs automatically illuminate?
    • With the EMER EXIT LT switch in ARM and:
    • Normal aircraft electrical pwer system fails or
    • DC ESS SHED BUS fails
    • Excessive cabin altitude (>11,300')
    • NO PED signs illuminated
  7. SIGNS Panel

    What lights illuminate when normal aircraft electrical power fails?
    • Floor proximity emergency escape path marking system
    • Overhead emergency lighting
    • EXIT signs
  8. Signs Panel

    What lights illuminate when DC ESS SHED BUS fails?
    • Floor proximity emergency escape path marking system
    • Overhead emergency lighting
    • Exit signs
  9. SIGNS Panel

    What lights illuminate when AC Bus 1 fail if the DC ESS SHED BUS is powered?
    Overhead emergency lighting.
  10. SIGNS Panel

    What occurs when the EMER EXIT LT switch is placed to OFF?
    • All lights OFF
    • Amber EMER EXIT LT OFF light illuminates
  11. INT LTS Panel

    What flight deck lighting is available if normal electrical power is lost?
    • Captain's Instrument Panel (2 places)
    • Right Dome Light (with DOME switch in DIM or BRT position)
    • Standby Compass
  12. ANTI ICE Panel

    Is the engine anti-ice part of the normal pneumatic system?
    No - a seperate system independent of the pnuematic ducting
  13. ANTI-ICE Panel

    When do you use engine anti-ice?
    • OAT (Grnd) or TAT (Flt) 10 c or less and visible moisture is present.
    • Prior to and during descent in icing conditions including temperatures below -40C TAT

    *EXCEPTION - NOT DURING CLIMB & CRUISE WHEN THE TEMP IS <40C
  14. ANTI-ICE Panel

    What does an amber FAULT light in the ENG ANTI-ICE push button indicate?
    Switch and anti-ice valve disagreement
  15. ANTI-ICE Panel

    With ENG ANTI-ICE ON, what indications will you see?
    • Blue ENG ANTI-ICE light ON
    • ECAM: ENG ANTI ICE
    • N1 limit is reduced (amber tick on N1 indicator)
    • N1 idle is increased
  16. ANTI-ICE Panel

    What should you do if there is significant engine vibration due to ice?
    Increase N1 to 70% for a minimum of 15 secs. prior to selecting a higher thrust setting.
  17. ANTI-ICE Panel

    Is your descent affected with ENG ANTI-ICE ON?
    Yes - N1 idle is increased
  18. ANTI-ICE Panel

    Wing ANTI-ICE ON for ground use?
    No
  19. ANTI-ICE Panel

    What happens if the wing ANTI-ICE is selected ON when on the ground?
    The wing anti-icing valves will open for a 30 sec test
  20. ANTI-ICE Panel

    What part of the wing is heated?
    Outboard 3 slats
  21. ANTI-ICE Panel

    When do the wing anti-ice valves automatically close?
    • Upon landing
    • Bleed leak detected
    • Loss of electrical power (fail closed)
  22. ANTI-ICE Panel

    Can APU bleed air be utilized for wing anti-ice?
    No
  23. ANTI-ICE Panel

    What does the amber FAULT light in the WING ANTI-ICE push button indicate?
    • Switch/anti-ice valve disagreement
    • Low pressure is detected
  24. ANTI-ICE Panel

    In what position do the Wing and Engine Anti-Ice valves fail if electrical power is lost?
    • Wing - fail closed
    • Engine - fail open
  25. PROBE/WINDOW HEAT Panel

    Which exterior aircraft components utilize electical heating?
    • Cockpit windshields (2 ea) - heated
    • Sliding and side windows (4 ea) - demisted
    • AOA, TAT, pitot probes & static ports
    • Waste water drain masts
  26. PROBE/WINDOW HEAT Panel

    On the ground with PROBE/WINDOW HEAT push button in AUTO, when are the probe and mast heaters activated?
    • LOW with at least one engine running (except the TAT probe - not heated on grnd)
    • NORMAL is automatically selected after takeoff
  27. PROBE/WINDOW HEAT Panel

    What does the PROBE/WINDOW HEAT push button do?
    • Manually activates the:
    • Probe
    • Drain mast &
    • Window heaters.
  28. PROBE/WINDOW HEAT Panel

    With the PROBE/WINDOW HEAT push button ON will the heaters automatically switch to AUTO?
    No
  29. CABIN/PRESS Panel

    Which valves will reeeive a close command when the DITCHING push button is depressed (ARPO)?
    • Avionics inlet and extract valves
    • Ram air inlet
    • Pack flow control valve
    • Outflow valve (only if in AUTO mode)
  30. CABIN/PRESS Panel

    Will the DITCHING push button always close the outflow valve?
    No - not if the outflow valve is under MANUAL control
  31. CABIN/PRESS Panel

    Can the pilot control the outflow valve?
    Yes - select MAN on the MODE SEL and use the MAN V/S CTL switch.
  32. CABIN/PRESS Panel

    Approx what rate of cabin change does 1 click of the MAN V/S CTL switch produce?
    50 FPM
  33. CABIN/PRESS Panel

    How many controllers are in the pressurization system?
    2 - only one is used at a time and they swap roles after each landing
  34. CABIN/PRESS Panel

    How do you manually switch controllers?
    Switch MODE SEL to MAN for 10 secs then back to AUTO
  35. CABIN/PRESS Panel

    What does an amber FAULT light in the MODE SEL push button indicate?
    Both automatic pressure controllers are faulty
  36. CABIN/PRESS Panel

    The LDG ELEV selector in the AUTO position does what?
    The press sys uses the GMGS data to construct an optimized pressurization schedule
  37. CABIN/PRESS Panel

    From what source does the pressurizatoin sys obtain landing elevation?
    FMGC database
  38. CABIN/PRESS Panel

    when out of the AUTO position, what is different?
    The press sys uses the manually selected landing elevation
  39. CABIN/PRESS Panel

    what is the max cabin rate of descent with the press in AUTO?
    750 fpm
  40. CABIN/PRESS Panel

    What protects the airframe from excessive cabin differential pressure?
    2 press relief valves
  41. CABIN/PRESS Panel

    How many outflow valve motors are installed?
    One for ea auto controller and one for manual control
  42. CABIN/PRESS Panel

    Describe what occurs when cabin pressure altitude exceeds: 8800, 9550, 11300, 14000
    • 8800' CAB ALT flashes
    • 9550' EXCESS CABIN ALT warning
    • 11300' All cabin signs illuminate
    • 14000 All passenger masks deploy
  43. AIR CONDITION Panel

    The pnuematic system is monitored and controlled by?
    2 bleed monitoring computers (BMC)
  44. AIR CONDITION Panel

    If one BMC fails, can the other take over?
    Yes - they are interconnected. If BMC 1 fails:

    • APU and ENG 1 leak detection are not monitored
    • ECAM APU BLEED LEAK warning is lost
  45. AIR CONDITIONING Panel

    On the ECAM Bleed page, how do you know if the GND HP air supply is connected?
    The GND unit temp. and press are indicated on the ECAM BLEED PRECOOLER 1
  46. AIR CONDITIONING Panel

    How can you tell if the GND LP air supply is removed before selecting the APU BLEED push button to ON?
    • Turn off the CAB FANS push button
    • Open the air vent on the instrument panel and confirm no airflow.
  47. AIR CONDITIONING Panel

    The PACK FLOW selector has LO, NORM and HI positions. What does this allow us to do?
    Select flow rate is automatically selected when APU bleed air is in use or during single pack operation.
  48. AIR CONDITIONING Panel

    What flow rate is automatically selected when APU bleed air is in use or during single pack operation?
    Hi
  49. AIR CONDITIONING Panel

    When should the PACK FLOW selector not be in the NORMAL position?
    • < 115 guests, select LO
    • Hot and humid conditions, select HI
    • During Smoke/Fumes removal, select HI as per the procedure
  50. AIR CONDITIONING/ Panel

    If PACK FLOW is selected to HI, will it automatically shift lower?
    No
  51. AIR CONDITIONING Panel

    If the engine bleed air in-flight is too low what will occur?
    Engine speed is automatically increased to provide adequate bleed air pressure.
  52. AIR CONDITIONING Panel

    What would cause an amber FAULT light to illuminate in the PACK 1 and/or PACK 2 push button (OOD)
    • Overheat - Pack outlet
    • Overheat - Compressor outlet
    • Discontinuity - Switch position disagreement with pack flow control valve

    Note - FAULT light will be illuminated when no bleed air is supplied.
  53. AIR CONDITIONING Panel

    What does the amber FAULT light in the APU BLEED push button indicate?
    Bleed leak (APU bleed leak valve closes)
  54. AIR CONDITIONING Panel

    What causes the amber FAULT light on the ENG 1 BLEED and/or ENG 2 BLEED push button? (OOLD)
    • Over pressure - downstream the bleed valve
    • Overheat
    • Leak - low pressure
    • Discontinuity - APU bleed valve open and engine bleed valve not closed or Engine Start with bleed valve not closed
  55. AIR CONDITIONING Panel

    What are the two functions of the engine bleed valves?
    • Pressure regulation
    • Shut off valves
  56. AIR CONDITIONING Panel

    What is the RAM AIR push button used for?
    • Smoke removal in cabin
    • Ventilation of cabin with a dual pack failure.
  57. AIR CONDITIONING Panel

    At what cabin differential pressure does the RAM AIR valve open
    1 psi deltaP or less
  58. AIR CONDITIONING Panel

    What logic controls the X-Bleed valve when the X-BLEED switch is in AUTO?
    • APU Bleed valve is OPEN = X-Bleed valve is OPEN
    • APU Bleed valve is CLOSED = the X-Bleed is CLOSED
    • X-Bleed CLOSED = wing, pylon or APU duct leaks (except during engine start)
  59. AIR CONDITIONING Panel

    What causes the PACK FLOW CONTROL valve to automatically close?
    • Upstream press < the minimum
    • Pack overheat
    • Engine start sequence
    • Engine Fire push button on the related side pressed
    • DITCHING push button is selected
  60. AIR CONDITIONING Panel

    What does an amber FAULT light in the HOT AIR push button indicate?
    Duct overheat - the HOT AIR and TRIM AIR valves close automatically.
  61. AIR CONDITIONING Panel

    What is the function of the HOT AIR push button?
    Controls the hot air pressure regulating valves which controls the flow of hot air to the trim air valves. This hot air is mixed with the pack-conditioned air for zone temperature control.
  62. Air Conditioning Panel

    How many Air Conditioning Sys Controllers are installed?
    2 Ea Air Conditioning Sys Controller has 2 lanes - active & standby
  63. AIR CONDITIONING Panel

    Describe how the Air Conditioning Sys Controllers regulate temperature:
    Basic temperature reg: Both packs produce the required outlet temperature determined by the lowest demand zone temperature.

    Optimized temperature reg: Hot air is added to the individual zones by the trim air valves to maintain the desired zone temperatures.
  64. Air Conitioning Panel

    What occurs when an active lane of an Air Conditioning Sys Controller fails?
    The second lane takes over.
  65. Air Conditioning Panel

    What occurs when both lanes of an Air Conditioning Controller fails?
    The related pack is lost. The hot air pressure-regulating valve and associated trim air valve(s) close.
  66. Air Conditioning Panel

    How dose the Air Conditioning System Controller configure it's associated pack ram air inlet flap for takeoff and landing to avoid the ingestion of foreign matter?
    Takeoff: Ram air inlet flap closes when takeoff power is set and the main landing gear struts are compressed. Ram air inlet flap reopens after main landing grear strut extension.

    Landing: Ram air inlet flap closes as soon as the main landing gear struts are compressed and speed is > 70 kts. Ram air inlet flap opens 20 secs after speed <70 kts.
  67. Air Conditioning Panel

    What occurs when an (ACM) air cycle machine fails?
    The affected pack will operate as a heat exchanger.
  68. Air Conditioning Panel

    What effect will the engine start sequence have on the pack flow control valves?
    The pack flow control valve will cloe automatically.
  69. Air Conditioning Panel

    After engine start with the APU BLEED push button ON, what source is supplying bleed air to the packs?
    APU Bleed Air
  70. Air Conditioning Panel

    When does the Lav/Galley Extract Fan operate?
    Continuously when electrical power is available.
  71. Air Conditioning Pack

    If the Lav/Galley Extract Fan fails, what occurs?
    Cabin temperature defaults to a set value.

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