Annunciators Flashcards

1
Q

FADEC 1

A

One of the FADECs has Failed
Look on EIED #2 msgs to see which one

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2
Q

Pitch Feel

A

Arther Unit has failed
Reduce Speed below 260 kgs or 0.76M
AP use is OK

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3
Q

T/O CONFIG (RED)

A

Slats, Flaps, Brakes set, Airbrakes deployed, Stab Trim out of green, or AP engaged

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4
Q

Aileron Feel

A

Arther Unit has failed
Reduce Speed below 260 kgs or 0.76M
AP use is OK

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5
Q

FADEC 2

A

One of the FADECs has failed.
Look on EIED #2 msgs to see which one

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6
Q

START 1

A

The Start valve is stuck open.
Pneumatic ISOL Valve Closed
Bleed 1 and APU Bleed Closed

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7
Q

AUTO SLATS

A

Slat Monitoring System inop
Reduce Speed Below 270 kts
If below 180 kts, extend Slats and Flaps

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8
Q

FLAP ASYM

A

GPWS or Flap O’Ride On
VREF Adjustment

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9
Q

AIL ZERO

A

Retrim w/ Emergency Aileron Trim Buttons

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10
Q

START 2

A

The Start Valve is Stuck Open
Pneumatic ISOL valve closed
Bleed 2 Closed

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11
Q

OIL 1 (RED)

A

Check Oil Pressure on EIED
If less than 25 PSI, retard engine lever to idle for 2 min.
Shutdown Engine

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12
Q

LH PROBES

A

Current to Probes is INOP

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13
Q

STB PROBES

A

Current to Probes is INOP

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14
Q

RH PROBES

A

Current to Probes is INOP

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15
Q

OIL 2 (RED)

A

Check Oil Pressure on EIED
If less than 25 PSI, retard engine lever to idle for 2 min
Shutdown Engine

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16
Q

A/P TRIM FAIL

A

Failure of Automatic Pitch Trim
Hold Wheel
Click off AP
Retrim Airplane
1 Reengage attempt

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17
Q

A/P (RED)

A

AP Failure
Try to Reengage
One Attempt

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18
Q

MISTRIM

A

Pitch is out of trim
Hold Wheel
Disconnect AP
Retrim and reengage
1 reengage attempt

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19
Q

TR 1

A

TR Malfunction
If no buffeting and not idle, monitor
If engine is idle, move power lever to idle

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20
Q

APU GEN

A

APU GEN contactor is open
One Reset Allowed

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21
Q

APU FAULT

A

On EIED, Check APU Parameters

22
Q

APR

A

APR System Fault
APR O’ride may still be available

23
Q

TR 2

A

TR Malfunction
If no buffeting and not idle, monitor
If engine is idle, move power lever to idle

24
Q

GEN 1

A

Gen 1 Contactor is open or generator output is <24V +/- 1V for 40 sec
If the switch is not tripped, tie the bus

25
BAT
BAT Connector is Open 2 Resets Allowed
26
GEN 2
Gen 2 Contactor is open or generator output is <24V +/- 1V for 40 sec If the switch is not tripped, tie the bus
27
FUEL 1
Low Booster Pump pressure (<5 PSI) X BP Open, Associated Booster Pump Off
28
LH BUS ISOL
Non Normal Position
29
HOT BAT (RED)
BAT is at 160 degrees F or more Turn off to cool down Check ESS bus volts are in green range
30
RH BUS TIED
Non Normal Position
31
FUEL 2
Low Booster Pump (<5 PSI) X BP Open, Associated Booster Pump Off
32
LO FUEL 1
<250 lbs Fuel Transfer Fuel X BP and low tank booster off
33
NOSE CONE OVHT
Temp greater than 70 degrees C Switch off as much equipment as possible Turn off Avionics if on ground
34
ECU OVHT
ECU reached temp of at least 220 degrees C Turn on COND'G EMERG This closes the cold air valves, shutting down the ECU Cold air into the cabin is lost
35
AFT COMPT OVHT
Temp is greater than 90 degrees C Probably have a bleed leak in the forward compartment Bleed 1, 2, and APU off ISOL Valve On Try Bleeds one at a time
36
LO FUEL 2
<250 lbs Fuel Transfer Fuel X BP and low tank booster off
37
PUMP 1 HYDR 1
Failure of a Hydraulic Pump, Less than 1,500 PSI Expect Longer Times for Gear, Slats, etc.
38
HYDR # TK PRESS
Depressurization of Hydraulic Tank Expect a leak in the system If pressure drops, slow to 260 KIAS/0.76 M Descend below FL200
39
HYDR #2 ISOL
Valve Malfunction If slats are extended, open ISOL If slats are retracted, close ISOL
40
PUMP 2 HYDR #1
Failure of a Hydraulic Pump, Less than 1,500 PSI Expect Longer Times for Gear, Slats, etc.
41
PUMP HYDR #2
Hydraulic System #2 is less than 1,500 PSI The ST BY Pump is operating when this light is illuminated Expect Less Pressure If loss of fluid, slow to 260 KIAS/0.76 M Elevator and Rudder are Protected
42
FUELING
Either fueling door issue or venting issue. May be venting fuel overboard
43
BRAKE (RED)
Both Brake Systems are INOP Use Parking Brake The Accumulator allows up to 6 Applications
44
BRAKE (not red)
Loss of Brakes on ONE side Increase Landing Distance by 10%
45
BRAKE PRESS
Brake Pressure Sensed without brakes being applied PB Forward Cycle Brake Computer CBS Increase Landing Distance by 10%
46
ST BY PUMP
ST BY Pump has been running continuously for more than 1 min
47
DOORS (RED)
Door Unlocked Indication
48
BRAKE ACCU
This means there is no parking brake pressure
49
ANTI-ICE
Verify wing and engine anti ice blue and amber lights are on
50
RECIR ISOL
Recirc Valve Malfunction Normally Closes at 15,000 ft There is a manual control lever in the Lavatory
51
CABIN (RED)
Cabin Pressure is above 10,500 ft