Frontier Lights and Switches FAULTS Flashcards

1
Q

ADIRS

IR 1/2/3 = FAULT (light steady amber)

A

Fault in IR

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2
Q

ADIRS

IR 1/2/3 = FAULT (light flashing amber)

A

Attitude and Heading may be recovered using ATT mode

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3
Q

ADIRS

ADR 1/2/3 = FAULT (light amber)

A

Fault in ADR

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4
Q

FLT CTL

ELAC 1/2 = FAULT (light amber)

A

ELAC Self test during Power up

Fault

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5
Q

FLT CTL

SEC 1/2/3 = FAULT (light amber)

A

Fault

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6
Q

FLT CTL

FAC 1/2 = FAULT (light amber)

A

Fault

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7
Q

GPWS

TERR = FAULT (light amber)

A

EGPWS Failure

Turn off airborne if airport not in database

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8
Q

GPWS

SYS PB = FAULT (light amber)

A

Modes 1-5 Failed

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9
Q

APU

MASTER SW = FAULT (light amber)

A

Auto Shutdown for many reasons.

Fire will only cause auto shutdown on the ground.

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10
Q

APU

Start pb (AVAIL light green)

A

N > 99.5%

N > 2s after N is reaches 95%

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11
Q

CABIN PRESS

MODE SEL = FAULT (light amber)

A

Both Auto Systems Failed

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12
Q

CABIN PRES

DITCHING pb = ON

A

Closes:

  • Avionics Ventilation inlet valve
  • Avionics Ventilation extract valve
  • Both Pack flow control valves
  • Ram Air Inlet valve
  • Outflow valve (if under Auto control)
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13
Q

ANTI ICE

WING PB = FAULT (light amber)

A

Low pressure

Either Valve Disagreement with PB

Either Valve in Transit

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14
Q

ANTI ICE

ENG 1/2 PB = FAULT (light amber)

A

Valve Disagreement

Valve in Transit

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15
Q

AIR COND

PACK 1/2 PB = FAULT (light amber)

A

Overheat of Comp Outlet or Pack Outlet

Disagreement of Valve position

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16
Q

AIR COND

ENG 1/2 BLEED PB = FAULT (light amber)

A
LOOSA 
Leak
Overheat
Overpressure downstream
Start In Process and Valve not closed
APU Bleed On and Valve not closed
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17
Q

AIR COND

APU BLEED PB = FAULT (light amber)

A

Leak

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18
Q

AIR COND

HOT AIR PB = FAULT (light amber)

A

Overheat detected, and closes:

  • Hot Air Valve
  • Trim Air Valve.
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19
Q

ELEC

GALLEY CAB PB = FAULT (light amber)

A

Any Generator Load >100%

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20
Q

ELEC

BAT 1/2 PB = FAULT (light amber)

A

Battery Charger current is out of limits

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21
Q

ELEC

IDG 1/2 PB = FAULT (light amber)

(IDG = Integrated Drive Generator)

A

High Oil Temp

Low Oil Pressure (inhibited below 14% N2)

22
Q

ELEC

GEN 1/2 PB = FAULT (light amber)

A

GCU Trip

Line contactor is open (other than by pb)

23
Q

ELEC

APU GEN PB = FAULT (light amber)

A

GCU Trip

Line contactor open (other than by pb or EXT PWR selected on)

Inhibited at low speed

24
Q

ELEC

AC ESS FEED PB = FAULT (light amber)

A

ACC ESS Bus not powered

25
EMER ELEC PWR RAT / EMER GEN = FAULT (light red)
Emergency Generator is not supplying power, but should be (AC1/2 are not powered)
26
FUEL LTK PUMPS 1/2 PB = FAULT (light amber) RTK PUMPS 1/2 PB = FAULT (light amber) CTK PUMPS 1/2 PB = FAULT (light amber)
Low output pressure
27
FUEL MODE SEL PB = FAULT (light amber)
Center Tank abov 550 lbs AND | Left or Right Wing Tank blow 11,000 lbs
28
HYD ENG 1/2 PUMP = FAULT (light amber)
PROLL ``` Pump Problem: -Low pump pressure (inhib on grnd with Eng off) Reservoir Problem: -OVERHEAT of fluid -LOW level -LOW air pressure ```
29
HYD PTU = FAULT (light amber)
ROLL Reservoir Problem: - OVERHEAT of fluid - LOW level - LOW air pressure
30
HYD PTU = AUTO
Automatically runs when Green & Yellow differential psi >500 -self test during second engine start. NOTE: PTU is inhibited: -for 40 seconds after cargo door is opened or closed -ONLY one ENG master switch on AND Tow Pin in -ONLY one ENG master switch on AND Parking Brake Set
31
HYD Blue ELEC PUMP = Fault Light (amber)
``` Reservoir problem: -Low level -Fluid Overheat -Low Air Pressure Pump problem -Low pump pressure (inhibited on the grd with engine off) -Overheat ```
32
HYD Yellow ELEC PUMP = Fault Light (amber)
``` Reservoir problem: -Low level -Fluid Overheat -Low Air Pressure Pump problem -Low pump pressure (inhibited on the grd with engine off) -Overheat ```
33
CARGO HEAT HOT AIR PB = FAULT (light amber)
Duct Overheat
34
CARGO HEAT AFT ISOL VALVE = FAULT (light amber)
Inlet or Outlet valve disagreement
35
VENTILATION BLOWER PB = FAULT (light amber)
SACO.... ``` S = Smoke A = Air Pressure is low (Blowing Air Pressure)* C = Computer Fault* O = Overheat* ``` *ACO = Horn on grnd + no engines running
36
VENTILATION EXTRACT PB = FAULT (light amber)
SAC ``` S = Smoke A = Air Pressure low (Extracting Air Pressure)* C = Computer fault ``` *A = Horn on grnd + no engines running
37
ENGINE FIRE ENG 1(2) FIRE pb = Released aka popped
Silences CRC Arms squibs Closes Hydraulic Shutoff valve Closes LP fuel valve De-energizes FADEC Deactivates IDG Closes Bleed valve Closes Pack flow control valve
38
ENGINE FIRE APU FIRE pb = Released aka popped
Silences CRC Arms squib Closes LP fuel valve (APU shuts down) Turns off APU fuel pump Deactivates APU generator Closes APU Bleed valve Closes X Bleed Valve
39
ENGINE FIRE AGENT 1(2) = SQUIB Light (white)
Squib is armed (after FIRE pb popped)
40
ENGINE FIRE AGENT 1(2) = DISCH Light (amber)
Bottle empty
41
ENGINE FIRE ENG 1(2) Test pb = Pushed
- CRC + MASTER WARN Light - ECAM - ENG FIRE pb Light - SQUIB Light - DISCH Light - FIRE Light on ENG panel
42
ENGINE FIRE APU Test pb = Pushed
-CRC + MASTER WARN Light -ECAM -APU FIRE pb Light* -SQUIB Light* -DISCH Light* (* If DC power only)
43
ENGINE CP Fault Light 1(2) = (amber)
- Automatic start abort | - HP fuel valve disagreement
44
COCKPIT DOOR Cockpit Door Fault Light = (red)
System Failure (i.e. latch, control unit, pressure sensor, etc)
45
RCDR GND CTL AUTO pb = Pushed
Voice and Data recorders operate: - 5 minutes after initial power up - On the ground from 1st engine start to 5mins after 2nd engine shutdown - In Flight
46
RCDR RCDR CVR ERASE pb = Pushed
Erases tape (2 hours) when: - Held for 2 seconds - On the ground - Parking Brake On
47
OXYGEN MASK MAN ON pb = AUTO
- Mask doors open when Cabin Altitude > 14,000' | - Prerecorded instructions broadcast
48
OXYGEN CREW SUPPLY OFF Light = (white)
Closes valve
49
SIGNS EMER EXIT LT Switch = ON
Overhead, EXIT signs and proximity marking system Lights illuminate
50
SIGNS EMER EXIT LT Switch = ARM
``` Loss of AC1 bus illuminates only: -Overhead Lights Loss of DC ESS SHED bus illuminates: -Overhead Lights -Exit Signs -Path Lighting ```
51
EFIS Controls GPWS Light = (red)
Illuminates for: -GPWS Modes 1-4 alert Mode 1 -Excessive Rate of Descent Mode 2 -Excessive Terrain Closure Rate Mode 3 -Altitude loss after takeoff or go around Mode 4 - Unsafe terrain clearance when not in ldg config -EGPWS alert
52
EFIS Controls G/S = (amber)
Illuminates for: | -GPWS Mode 5 alert - Too far below glide slope