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Frontier Airbus > Switches and Light Guide - Feb 21 Update > Flashcards

Switches and Light Guide - Feb 21 Update Flashcards

1
Q

LIGHTS & SWITCHES -

ADIRS ADR 1/2/3 Push Button

A
  • Fault Light - Fault in Air Data Reference computer
  • OFF Light - Selected ADR is off
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2
Q

LIGHTS & SWITCHES -

ADIRS IR 1/2/3 Push Button

A
  • OFF
    • Inertial data output disconnected
  • Fault Light
    • Steady Fault Light - Fault in IR
    • Flashing Fault Light - Attitude and Heading may be recoverable in ATT mode.
  • Align Light (Older Aircraft only)
    • Steady Align Light - Normal during align (10min)
    • Flashing Align Light -
      • No position entered in 10 min
      • Bad position (1 degree difference between shutdown and entered)
      • Fault
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3
Q

LIGHTS & SWITCHES -

ADIRS IR 1/2/3 Rotary Selector

A
  • Off - ADIRU is deactivated, both ADR and IR are unavailable
  • NAV - Normal mode supply full inertial data
  • ATT - Attitude and Heading only supplied
    • Enter mag heading using keyboard
    • Should be entered every 10 minutes
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4
Q

LIGHTS & SWITCHES -

ADIRS ON BAT Light

A
  • Self test during alignment
  • One or more IRs are on battery power
    • IR2 and IR3 are lost after 5 min on bat power only.
      • If CAPT3 is selected IR1 and IR2 are lost.
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5
Q

LIGHTS & SWITCHES -

AIR COND Panel APU BLEED push button

A
  • ON light (white)
    • Opens valve when pushed and
      • N>95%
      • No leak
  • OFF
    • APU Valve closes
  • FAULT light (amber)
    • Leak detected
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6
Q

LIGHTS & SWITCHES -

AIR COND Panel ECON FLOW push button

A
  • ON
    • ECON flow is selected. 80% of normal flow. Will automatically go to 100% if it cannot meet the cooling demand.
  • OFF
    • 100% of the normal flow.

The system goes to 120% of normal in single pack operation or APU bleed supply.

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7
Q

LIGHTS & SWITCHES -

AIR COND Panel ENG 1/2 BLEED push button

A
  • Pushed
    • Opens bleed valve unless
      • Leak
      • Overheat
      • Overpressure
      • Start valve open
      • APU bleed valve open (or pb ON)
      • Air 8psi or less (15psi for NEO)
      • FIRE push button released
      • At least one bleed consumer is on (NEO/722/23)
  • FAULT light (amber) (LOOSA-BFH)
    • Leak
    • Overheat
    • Over pressure downstream
    • Start in progress and valve not closed
    • APU Bleed on and valve not closed
    • Dual BTS Failure (NEO/722/23)
    • Single BTS failure or fault on ground (NEO)
    • Fan duct burst (NEO)
    • HP Valve failed open on ground (NEO)
  • OFF light (white)
    • Bleed valve closed
    • HP valve closed
    • Fan air valve closed (NEO)
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8
Q

LIGHTS & SWITCHES -

AIR COND Panel HOT AIR push button

A
  • FAULT light (amber)
    • Overheat detected, and automatically closes:
      • Hot air valve
      • Trim valves
  • OFF light (white)
    • Hot air valve closed
    • Trim air valves closed
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9
Q

LIGHTS & SWITCHES -

AIR COND Panel PACK 1/2 push button

A
  • Pushed
    • Opens pack valve unless:
      • Ditching switch selected
      • Overheat in compressor outlet
      • Start in progress
      • Air pressure low
      • FIRE push button released
  • FAULT light (amber)
    • Overheat of compressor outlet or pack outlet
    • Disagreement if valve position
  • OFF light (white)
    • Pack flow control valve closed
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10
Q

LIGHTS & SWITCHES -

AIR COND Panel PACK FLOW selector

A
  • LO
    • 80% - Select if less than 115 passengers
    • Will automatically go to 100% if the cooling demand cannot be met.
  • NORM
    • 100% - Select if 115 or more
  • HI
    • 120% - Select if abnormally hot and/or humid
    • In single pack or with APU Bleed supply the system goes to HI automatically.
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11
Q

LIGHTS & SWITCHES -

AIR COND Panel RAM AIR push button

A
  • ON light (white)
    • If Delta P is less than 1 psi and DITCHING pushbutton is in the normal lights out position:
      • RAM AIR inlet opens
      • Outflow valve opens 50% if not being manually controlled
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12
Q

LIGHTS & SWITCHES -

AIR COND Panel COCKPIT/FWD/AFT Tempurature Selectors

A
  • Commands sent to Zone Controller or Air Conditioning System Controller depending on the aircraft which control the temperature via trim air valve.
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13
Q

LIGHTS & SWITCHES -

AIR COND Panel X BLEED rotary selector

A
  • SHUT
    • Closed
  • AUTO
    • Opens if:
      • APU Bleed valve is open
    • Closed if:
      • APU Bleed valve is closed
      • Wing, Pylon and APU leak (except during start)
  • OPEN
    • Open
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14
Q

LIGHTS & SWITCHES -

ANTI ICE Panel ENG 1/2 push button

A
  • OFF
    • Engine anti-ice valve closes
  • FAULT light (amber)
    • Valve disagreement
    • Breifly as valve transits
  • ON light (blue)
    • ENG A. ICE memo on ECAM
    • NAI appears on E/WD when in TOGA or FLX/MCT detents
    • Respective valve open if air available
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15
Q

LIGHTS & SWITCHES -

ANTI ICE Panel WING push button

A
  • OFF
    • Wing anti-ice valves close
  • FAULT light (amber)
    • Low Pressure
    • Either valve disagreement with push button
    • Breifly as the valves transit
  • ON light (blue)
    • WING A. ICE memo on ECAM and WAI on E/WD in TOGA/MCT/FLEX
      • In flight, both valves open if air available
      • On the ground, both valves open for 30 second test sequence
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16
Q

LIGHTS & SWITCHES -

APU Panel MASTER SW Push Button

A
  • FAULT Light (amber)
    • Auto shutdown for many reasons
    • Fire will only cause auto shutdown on ground
  • ON light (blue)
    • ECB self test
    • Flap opens
    • Fuel isolation valve opens and fuel pump on
    • ECAM page appears
  • OFF
    • MASTER SW ON light and START AVAIL light extinguish
    • Shutdown delay 60-120 seconds if APU bleed used
    • Flap closes at 7%
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17
Q

LIGHTS & SWITCHES -

APU Panel START Push Button

A
  • AVAIL light (green)
    • N> 99.5%
    • N> 95% for 2 seconds
  • ON light (blue)
    • APU starts
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18
Q

LIGHTS & SWITCHES -

CABIN PRESS Panel DITCHING push button

A
  • Closes
    • Avionics Ventiliation Inlet and Extract valves
    • Both Pack flow control valves
    • Ram Air inlet valve
    • Outflow valve
      • Only if under AUTO control
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19
Q

LIGHTS & SWITCHES -

CABIN PRESS Panel LDG ELEV selector

A
  • AUTO
    • Landing elevation from FMGS being used to control pressurization schedule
  • -2 through 14
    • Pull out and turn to select landing field elevation if not in FMGS database
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20
Q

LIGHTS & SWITCHES -

CABIN PRESS Panel MAN V/S CTL switch

A
  • UP/DN
    • Commands manual motor to modulate outflow valve according to V/S selected using switch (displayed on ECAM)
    • Operatesonly when MODE SEL in MAN
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21
Q

LIGHTS & SWITCHES -

CABIN PRESS Panel MODE SEL Push Button

A
  • AUTO
    • 2 Auto systems automatically transfer control
      • 70 sec after each landing
      • if operating system fails
    • Deselection for 10 seconds may switch system being used.
  • FAULT light (amber)
    • Both Auto systems have failed
  • MAN light (white)
    • Activates MAN V/S CTL toggle switch
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22
Q

LIGHTS & SWITCHES -

CALLS Panel EMER CALL from Flight Attendant Panel

A
  • ATT Light flashes on ACPs
  • CALL light in the EMER push button flashes
  • Three long buzzers sound

Inhibited during takeoff and landing.

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23
Q

LIGHTS & SWITCHES -

CALLS Panel EMER Push Button

A
  • When Pushed:
    • ON and CALL lights flash in push button
    • Illuminates EMERGENCY CALL Light on all F/A Panels
    • 3 High/Low Chimes sound
    • Pink Light at all F/A Call panels
  • CALL or ON light flashing
    • Emergency call from Cockpit to Cabin or vice versa
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24
Q

LIGHTS & SWITCHES -

CARGO HEAT Panel AFT ISOL VALVE push button

A
  • FAULT light (amber)
    • Inlet or Outlet valve disagreement
  • OFF light (white)
    • Inlet and outlet isolation valves close
    • Trim air valve closes
    • Extraction fan stops
  • AUTO (dark)
    • Inlet and outlet isolation valves open
    • Extraction fan on (if no smoke detected)
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25
Q

LIGHTS & SWITCHES -

CARGO HEAT Panel HOT AIR push button

A
  • FAULT light (amber)
    • Duct overheat
  • OFF light (white)
    • valve closes
  • AUTO (dark)
    • Valve regulates hot air pressure
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26
Q

LIGHTS & SWITCHES -

CARGO SMOKE panel DISCH switches

A
  • Pushed
    • Ignites squib and discharges single bottle into corresponding compartment.
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27
Q

LIGHTS & SWITCHES -

CARGO SMOKE Panel FWD/AFT push buttons

A
  • SMOKE light (red)
    • Smoke detected by
      • By both channels
      • By one channel and other failed
  • DISCH light (amber)
    • bottle pressure low
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28
Q

LIGHTS & SWITCHES -

COCKPIT DOOR Panel Light

A
  • OPEN light (amber)
    • Steady
      • Door not fully closed and not fully locked
    • Flashing
      • Cabin crew has begun the Emergency Access process. If no flight deck action is taken door will unlock after predetermined time (15-120 sec)
  • FAULT light (red)
    • System failure
      • Latch, control unit, pressure sensor, etc
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29
Q

LIGHTS & SWITCHES -

COCKPIT DOOR panel switch

A
  • UNLOCK
    • Pulled and held releases lock so door can be opened from cabin
  • NORM
    • Only EMERGENCY access available from cabin
  • LOCK
    • Emergency access, buzzer and keypad are inhibited for a predetermined time (5-20 min)
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30
Q

LIGHTS & SWITCHES -

ELEC Panel AC ESS FEED push button

A
  • FAULT light (amber)
    • AC ESS Bus not powered
  • ALTN light (white)
    • AC2 Bus supplies AC ESS BUS
  • Normal (dark)
    • AC1 Bus supplies AC ESS BUS
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31
Q

LIGHTS & SWITCHES -

ELEC Panel APU GEN push button

A
  • FAULT light (amber)
    • GCU Trip
    • Line contactor open
      • other than by push button or EXT PWR on
    • inhibited at low speed
  • OFF light (white)
    • Generator will not power electrical system
    • Fault circuit reset
  • Pushed (dark)
    • If EXT PWR and engine generators not in use, APU powers electrical system
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32
Q

LIGHTS & SWITCHES -

ELEC Panel BAT 1/2 push buttons

A
  • AUTO
    • Battery contactors are closed when:
      • APU start (max 3 min during EMER GEN operation)
      • Battery voltage <26.5 until <4 amps (after 30 min delay in flight)
      • AC1 and AC2 buses are unpowered and <100 kts or EMER GEN is not supplying power
    • Battery contactors are open if battery voltage is low (on the ground with no power supply)
  • FAULT light (amber)
    • Battery charger is out of limits
  • OFF light (white)
    • Battery contactors are open (light powered by DC BAT BUS)
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33
Q

LIGHTS & SWITCHES -

ELEC Panel BUS TIE push button

A
  • AUTO
    • Automatically closes one or both contactors to maintain power supply to AC1 and AC2 based on aircraft priority system
  • OFF light (white)
    • Both bus tie contactors open
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34
Q

LIGHTS & SWITCHES -

ELEC Panel COMMERCIAL push button

A
  • ON
    • Powers
      • Cabin and cargo lights
      • Toilets
      • Drain mast ice protection
      • Galleys
      • IFE (Not LiveTV)
  • OFF
    • Above equipment unpowered
35
Q

LIGHTS & SWITCHES -

ELEC Panel EXT PWR push button

A
  • AVAIL light (green)
    • Plugged in and power parameters are normal
  • ON light (blue)
    • EXT PWR push button is selected on
      • If engine generators are supplying system, ON light will be illuminated until the EXT PWR push button is deselected and removed from the tie bus.
  • External power has priorirty over the APU generator. Engine generators have priority over external power.
36
Q

LIGHTS & SWITCHES -

ELEC Panel GALLEY push button

A
  • AUTO
    • Powers
      • Main galley*
      • Secondary galley
      • IFE*

* Main Galley and IFE are shed when only one generator is operating. (Except only IFE is shed if on the ground with APU Gen or EXT PWR)

  • FAULT light (amber)
    • Any generator load > 100%
  • OFF light (white)
    • Both galleys and IFE are unpowered
37
Q

LIGHTS & SWITCHES -

ELEC Panel GEN 1/2 push button

A
  • FAULT light (amber)
    • GCU Trip
    • Line contactor open (other than by push button)
  • OFF light (white)
    • Generator will not power electrical system
    • Fault circuit reset
  • Pushed (dark)
    • Generator powers electrical system
38
Q

LIGHTS & SWITCHES -

ELEC Panel IDG 1/2 push button

A
  • FAULT light (amber)
    • High Oil Tempurature
    • Low Oil Pressure (inhibited below 14% N2)
  • Pushed
    • Disconnects IDG
    • Can only be reconnected on the ground
    • CAUTION the following may cause damage
      • Holding the push button for more than 3 seconds
      • Disconnecting an engine that is not running or windmilling
39
Q

LIGHTS & SWITCHES -

EMER ELEC PWR Panel RAT and EMER GEN TEST push button

A
  • Guarded
    • Used by MX to test the Emergency Generator connecting to the aircraft electrical system
40
Q

LIGHTS & SWITCHES -

EMER ELEC PWR Panel GEN 1 LINE push button

A
  • SMOKE light (amber)
    • Smoke detected in avionics compartment
  • OFF light (white)
    • GEN 1 is disconnected from AC 1 bus (GEN 2 then powers AC 1)
    • GEN 1 powers the number 1 fuel pump in each wing tank
41
Q

LIGHTS & SWITCHES -

EMER ELEC PWR Panel MAN ON push button

A
  • AUTO
    • Automatically extends the RAT which powers the Blue Hydraulic system which drives the emergency generator when:
      • AC1 and AC2 are unpowered
      • aircraft speed > 100kts
  • MAN ON
    • Manually extends the RAT and connects the emergency generator to electrical system.
    • Emergency generator coupling occurs 3 sec after RAT supplies the emergency generator.
42
Q

LIGHTS & SWITCHES -

EMER ELEC PWR Panel RAT and EMER GEN fault light

A
  • FAULT light (red)
    • The emergency generator is not supplying power when AC BUS 1 and 2 are not powered.
43
Q

LIGHTS & SWITCHES -

Engine Control Panel ENG 1/2 Fire/Fault Light

A
  • FIRE (red)
    • Illuminates when fire is detected in respective engine
  • FAULT (amber)
    • Automatic start abort
    • HP fuel valve disagreement
    • Thrust control malfunction
44
Q

LIGHTS & SWITCHES -

EVAC Panel COMMAND Button

A
  • EVAC Light - Flashes when COMMAND is pressed
  • ON Light -
    • EVAC Lights flash at FA panels
    • Evacuation tone sounds
45
Q

LIGHTS & SWITCHES -

FIRE Panel AGENT (1/2/APU) push buttons

A
  • SQUIB light (white)
    • Squib is armed (after FIRE push button is popped)
  • DISCH light (amber)
    • Bottle has lost pressure
46
Q

LIGHTS & SWITCHES -

FIRE Panel APU FIRE push button

A
  • Released (popped)
    • Shuts down APU
    • Silences CRC
    • Arms squib
    • Closes LP fuel valve
    • Shuts off APU fuel pump
    • Deactivates APU Generator
    • Closes APU Bleed Valve
    • Closes X Bleed valve
47
Q

LIGHTS & SWITCHES -

FIRE Panel APU TEST push button

A
  • Pushed
    • CRC + MASTER WARN light
    • ECAM
    • APU FIRE push button light*
    • SQUIB light*
    • DISCH light*
      • * If DC power only
48
Q

LIGHTS & SWITCHES -

FIRE Panel ENG 1/2 FIRE push buttons

A
  • Released (popped)
    • Silences CRC
    • Arms squibs
    • Closes hydraulic fire shutoff valve
    • Closes LP fuel valve
    • Deactivates Generator
    • FADEC power supply is removed
    • Closes the engine bleed valve
    • Closes Pack flow control valve
49
Q

LIGHTS & SWITCHES -

FIRE Panel ENG 1/2 TEST push buttons

A
  • Pushed
    • CRC + MASTER WARN light
    • ENG FIRE ECAM
    • ENG FIRE push button light
    • SQUIB light
    • DISCH light
    • FIRE light on ENG Panel
50
Q

LIGHTS & SWITCHES -

FUEL Panel CTR TK PUMP 1/2 push buttons

A
  • Pushed (dark)
    • Pump is operating if MODE SEL in MAN
    • Pump is operating if MODE SEL in AUTO as shown below
  • OFF
    • Not operating
  • FAULT light (amber)
    • Delivery pressure drops
51
Q

LIGHTS & SWITCHES -

FUEL Panel CTR TK XFR push buttons

A
  • Pushed (dark)
    • Valve is automatically controlled.
    • Transfer valve opens if in MAN mode
  • OFF
    • Valve is closed.
  • FAULT light (amber)
    • The associated wing tank overflows
52
Q

LIGHTS & SWITCHES -

FUEL Panel LTK PUMPS 1/2 and RTK PUMPS 1/2 push buttons

A
  • Pushed (dark)
    • Pump is on
    • For the older CEO aircraft: Only feeds when the center tank pump deilvery pressure drops below threshold.
  • OFF
    • Pump is off
  • FAULT light (amber)
    • Delivery pressure drops (low pressure)
53
Q

LIGHTS & SWITCHES -

FUEL Panel MODE SEL push button

A
  • AUTO (dark)
    • OLDER CEO Aircraft:
      • Center Tank Pumps operate:
        • For 2 minutes after first engine start
        • Slats are retracted
        • 5 minutes after CTK TK low level is reached (550lbs)
    • Aircraft with Center XFR Valves:
      • Center tank XFR valve control is automatic.
        • Open when associated inner tank is not full.
        • Close automatically 5 minutes after CTK TK low level is reached
  • FAULT (amber)
    • Center Tank > 550 lbs and
    • Left or Right Wing Tank < 11000 lbs
  • MAN (white)
    • Manual mode selected allowing manual control of the center tank transfer valves or pumps
54
Q

LIGHTS & SWITCHES -

FUEL Panel X FEED push button

A
  • OPEN (green)
    • Valve fully open
  • ON
    • Push button selected ON to open valve
  • OFF
    • Valve is closed
55
Q

LIGHTS & SWITCHES -

GPWS Panel FLAP MODE Push Button

A

“TOO LOW FLAPS” Mode inhibited

56
Q

LIGHTS & SWITCHES -

GPWS Panel G/S MODE Push Button

A

Off - Glide Slope Mode Inhibited

57
Q

LIGHTS & SWITCHES -

GPWS Panel LDG FLAP 3 Push Button

A
  • LDG MEMO changed to display FLAPS 3
    • Used when Landing Flaps will be 3 instead of FULL
    • Inhibits TOO LOW FLAPS
58
Q

LIGHTS & SWITCHES -

GPWS Panel SYS Push Button

A
  • Fault Light - Modes 1-5 malfunction
  • OFF - Modes 1-5 of GPWS inhibited
59
Q

LIGHTS & SWITCHES -

GPWS Panel TERR Push Button

A
  • Fault Light -
    • EGPWS Fault (Database)
    • Basic modes 1-5 still functional
  • OFF - Terrain function inhibited
60
Q

LIGHTS & SWITCHES -

Gravity GEAR EXTN Handle

A
  • Pulled and turned clockwise
    • 1st turn isolates landing gear from Green Hyd system
    • 2nd turn opens the landing gear doors
    • 3rd turn released landing gear
  • Note gear doors remain open
61
Q

LIGHTS & SWITCHES -

HYD Panel Blue ELEC PUMP push button

A
  • AUTO (dark)
    • Pump operates when electrical power availalbe and
      • In flight
      • On the ground after first engine start
      • On the ground with the BLUE PUMP OVRD pb ON
  • OFF light (white)
    • Pump de-energized
  • FAULT light (amber)
    • Reservoir Problem
    • Low Level
    • Fluid overheat
    • Low Air Pressure
    • Pump Problem
    • Low pump pressure (Inhibited on ground with engine off)
    • Overheat
62
Q

LIGHTS & SWITCHES -

HYD Panel ENG 1/2 PUMP push buttons

A
  • ON (dark)
    • Pump runs if engine is running
  • OFF light (white)
    • Stops pump
    • Turns off FAULT light except for overheat
  • FAULT light (amber)
    • Reservoir Problem
      • Low Level
      • Fluid overheat
      • Low Air Pressure
    • Pump Problem
      • Low pump pressure (inhibited on ground with engine off)
63
Q

LIGHTS & SWITCHES -

HYD Panel PTU push button

A
  • AUTO
    • Automatically runs when Green and Yellow differential pressure >500
    • Self test during second engine start
    • NOTE: PTU is inhibited:
      • For 40 sec after cargo door operation
      • ONLY one ENG master switch on AND tow pin in
      • ONLY one ENG master switch on AND parking brake set
  • OFF light (white)
    • Power transter stops
      • Turns off FAULT light except for overheat
  • FAULT light (amber)
    • Reservoir Problem
    • Low Level
    • Fluid overheat
    • Low Air Pressure
64
Q

LIGHTS & SWITCHES -

HYD Panel RAT MAN ON push button

A
  • Pushed
    • Extends RAT and powers Blue system (2500psi)
      • switch powered by HOT BAT BUS
65
Q

LIGHTS & SWITCHES -

HYD Panel Yellow ELEC PUMP push button

A
  • ON
    • Pump operates when electrical power available
  • OFF (dark)
    • Pump off
      • But pump will be turned on, regardless of switch, if Cargo Door Lever is moved to open/close
    • Turns off FAULT light except for overheat
  • FAULT light (amber)
    • Reservoir Problem
      • Low Level
      • Fluid overheat
      • Low Air Pressure
    • Pump Problem
      • Low pump pressure (Inhibited on ground with engine off)
      • Overheat
66
Q

LIGHTS & SWITCHES -

Landing Gear Indicator Panel AUTO/BRK push buttons

A
  • LO
    • Most Aircraft: 1.7 m/s - 4 seconds after full ground spoiler deployment
    • Newer NEOs: 2 m/s - 2 seconds after ground spoiler deployment
  • MED
    • 3 m/s - 2 seconds after full ground spoiler deployment
  • MAX
    • Maximum pressure as soon as full ground spoiler deployment
  • DECEL light (green)
    • Deceleration is 80% of selected rate.
  • ON light (blue)
    • Armed
67
Q

LIGHTS & SWITCHES -

Landing Gear Indicator Panel LDG GEAR lights

A
  • UNLK light (red)
    • Not locked in selected position (LGCIU 1)
  • Arrow (green)
    • Gear is down and locked (LGCIU 1)
68
Q

LIGHTS & SWITCHES -

Landing Gear Lever

A
  • UP
    • Normal brake system applies main wheel brakes
    • Retracts gear
  • DOWN
    • Extends gear
  • Down Arrow (red)
    • In the landing configuration and landing gear not locked down
    • ECAM warning also appears
69
Q

LIGHTS & SWITCHES -

AUTOLAND WARNING LIGHTS

A

Illuminate when, below 200ft until touchdown:

  • Excessive ILS deviation (1/4 dot LOC, 1 dot G/S)
  • Loss or disconnect of both AP
  • ILS transmitter failure (Loss of signal)
  • RA disagree of more than 15ft
  • FMGS detects long flare, or untimely flare

Immediate missed approach required.

Vol II 6.30 pg 13

70
Q

LIGHTS & SWITCHES -

OXYGEN Panel CREW SUPPLY OFF Light

A

Closes valve (no oxygen to flight deck masks)

71
Q

LIGHTS & SWITCHES -

OXYGEN Panel MASK MAN ON Push Button

A
  • Pushed
    • Mask Doors Open
  • AUTO
    • Mask Doors open when Cabin Altitude >14,000’
72
Q

LIGHTS & SWITCHES -

OXYGEN Panel PASSENGER SYS ON Light

A
  • Signal to open mask doors has been activated
  • Remains on until TMR RESET is pushed on MX Panel
73
Q

LIGHTS & SWITCHES -

PROBE/WINDOW HEAT Push Button

A
  • AUTO
    • Probes and windows heated
      • In flight
      • On the ground when one engine running (except TAT probe)
  • ON light (blue)
    • Continuous heating of probes and windows
74
Q

LIGHTS & SWITCHES -

RAIN RPLNT Push Button

A
  • Squirts a measured quantity of fluid on windshield.
  • Inhibited on the ground with engines not running.
75
Q

LIGHTS & SWITCHES -

RCDR Panel CVR ERASE Push Button

A
  • Erases tape (2 hours) when:
    • Held for 2 seconds
    • On the ground
    • Parking brake on
76
Q

LIGHTS & SWITCHES -

RCDR Panel CVR TEST Push Button

A
  • Activates test when:
    • CVR is powered
    • Parking Brake is on
77
Q

LIGHTS & SWITCHES -

RCDR Panel GND CTL Push Button

A
  • ON light (blue) - CVR/DFR are temporarily/manually on
  • AUTO (dark) - Voice and Data recorders operate:
    • 5 minutes after initial power up
    • On the ground from 1st engine start to 5 minutes after 2nd engine shutdown
    • In flight
78
Q

LIGHTS & SWITCHES -

Side Stick Takeover push button

A
  • Momentary push
    • Disconnects autopilot
  • Pushed and held
    • Establishes priority
  • Push and held for 40 seconds
    • Latches priority
79
Q

LIGHTS & SWITCHES -

SIGNS Panel EMER EXIT LT switch

A
  • ON
    • Overhead EXIT signs and proximity marking system lights illuminate
  • ARM
    • Loss of AC1 bus illuminates only:
      • Overhead lights
    • Loss of DC ESS SHED bus illuminates
      • Overhead lights
      • Exit signs
        • Path lighting
  • OFF
    • Off

NOTE: LIGHT EMER push button on pursers panel overrides cockpit switch.

80
Q

LIGHTS & SWITCHES -

Speed Brake Lever

A
  • RET
    • Retracts speed brakes
    • Pull up from this position to arm GND SPLR
  • 1/2
    • Extends speed brakes
    • Hard point at this position
  • FULL
    • Fully extends speed brakes
    • Full extension of gound spoilers will automatically occur when:
      • If armed:
        • both mains compressed and
        • both thrust levers at idle
      • If not armed
        • RTO above 72kts or
        • Both mains compressed and
        • reverse thrust is selected on at least one engine
    • Partial extension of ground spoilers (10 degrees) occurs automatically when:
      • Reverse is selected
      • only one main is compressed
  • Full retraction of ground spoilers automatically occurs when:
    • Disarmed
    • After landing
    • One TLA advanced > 20 degrees
81
Q

LIGHTS & SWITCHES -

Triple Indicator

A
  • ACCU PRESS
    • Pressure in Yellow Accumulator
    • Good for 7 parking brake applications
  • BRAKES
    • Yellow pressure being delivered to respective brake
82
Q

LIGHTS & SWITCHES -

VENTILATION Panel BLOWER and EXTRACT push buttons

A
  • Both in AUTO
    • On the ground
      • Prior to takeoff power, typically OPEN configuration
      • After takeoff power, CLOSED configuration
      • May be in closed config prior to takeoff if skin temperature is too cold.
    • In Flight
      • Typically in the CLOSED configuration
      • May be in INTERMEDIATE configuration if the skin temperature is too hot.
  • One in OVRD
    • Closed configuration
    • Air conditioned air is added
    • Blower fan stops (If BLOWER in OVRD)
  • Both in OVRD
    • SMOKE configuration
      • Air conditioning air added
      • Blower fan stops, Extract fan runs
      • Intermediate flap opens
83
Q

LIGHTS & SWITCHES -

VENTILATION Panel BLOWER push button

A
  • FAULT light (amber)
    • Air pressure low*
    • Computer fault*
    • Smoke
    • Overheat*

*horn sounds if on the ground and no engines running

  • OVRD (white)
    • Goes to closed configuration (inlet and extract valves close)
    • Air conditioning air added
    • Blower fan stops
84
Q

LIGHTS & SWITCHES -

VENTILATION Panel EXTRACT push button

A
  • FAULT light (amber)
    • Air pressure low*
    • Computer fault
    • Smoke

*horn sounds if on the ground and no engine running

  • OVRD (white)
    • Goes to closed configuration (inlet and extract valves close)
    • Air conditioning air added

Frontier Airbus (6 decks)

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