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Q400 > Crew Alerting System > Flashcards

Crew Alerting System Flashcards

1
Q

Name 10 warning tone conditions

A
  1. ENGINE FIRE-FIRE BELL
  2. TAKE OFF CONFIG
    3.AUTOPILOT DISENGAGEMENT
  3. PITCH TRIM IN MOTION
  4. OVERSPEED WARNING
  5. LANDING GEAR NOT DOWN & LOCKED
  6. ALTITUDE ALERT
  7. BETA LOCKOUT WARNING
  8. MASTER WARNING LIGHT ILLUMINATED
  9. MASTER WARNING CAUTION ILLUMINATED
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2
Q

How long can pitch trim be in motion for before a clacking tone can be heard?

A

3 seconds

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3
Q

What warnings do you get if you exceed VMO?

A

A warning tone & airspeed display changing to red colour

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4
Q

If the landing gear is not down and locked do you get a warning tone?

A

Yes

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5
Q

How many chimes for master warning and how many for a caution?

A

3 & 1

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6
Q

Take off Config warning conditions?

A

WITH BOTH POWER LEVERS ABOVE 50% TORQUE
& WEIGHT ON THE NOSE WHEEL
• ELEVATOR TRIM OUT OF TAKE-OFF RANGE
• LEFT OR RIGHT AILERON TRIM OUT OF RANGE
• PARKING BRAKE LEVER SET TO PARK
• ONE OR BOTH CONDITION LEVERS NOT AT MAX/1020
• FLAPS EXTENDED MORE THAN 20° OR LESS THAN 3.5°
• INBOARD OR OUTBOARD SPOILERS EXTENDED

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7
Q

Where is the take off warning test toggle switch?

A

Capt side panel

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8
Q

Stall Protection System (SPS) includes?

A

Visual indications (red speed tape)
Stick shaker and associated noise
Sticker pusher

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9
Q

AOA vanes number 1 and 2 what do they do for stalls?

A

AOA 1 & 2 provide info to the stall protection module (located avionics rack)

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10
Q

AOA sensor heated by?

A

L or R variable 115V AC Bus

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11
Q

What caution light do you get when you press the ‘Stick Pusher Shut Off’ switch light?

A

Pusher Syst fail

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12
Q

SPS caution lights?

A

1 or #2 STALL SYST FAIL

PUSHER SYST FAIL

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13
Q

Stall protection modules send signals to AFCS and GPWS to do what?

A

Disengage autopilot and inhibit audible PULL UP when stick shakers are activated

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14
Q

SPS enabled when?

A

Airspeed < 215kts and RA > 200ft

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15
Q

Stick pusher override by?

A

Press ‘STICK PUSHER SHUT OFF’ or manual override by applying opposing force to control column or 36kg

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16
Q

Turning REF SPEED SWITCH to INCR does what?

A

Changes the stick shaker and pusher activation to a lower AOA and the low speed cue on the airspeed indicator.
Eg. INCR on low speed cue is 120kts instead of 100kts if INCR is off

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17
Q

EGPWS how many basic modes and enhanced modes?

A

6 basic
2 enhanced modes

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18
Q

Yellow BELOW G/S switch light on glareshield does what?

A

Flashes if below G/S
Can be pressed to cancel the below G/S alerts

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19
Q

Too low flaps aural alert when?

A

The GPWS landing flap selector and the flap setting are in disagreement and aircraft is below 200ft

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20
Q

GPWS Flap override switch light on capt side panel used when?

A

Cancels the EGPWS flap alerts when doing a zero or partial flap landing

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21
Q

EGPWS envelope?

A

50ft RA to 2450ft RA

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22
Q

GPWS malfunction indications?

A

GPWS caution light
TERR FAIL on MFD

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23
Q

How to conduct EGPWS test on ground?

A

The EGPWS can be tested on the ground by pressing either of the red PULL UP - GPWS TEST switchlights.
Prior to performing the test check the following:
- #1 NAV is on and tuned to a VOR station
- FMS #1 is on and initialised
- Flaps are set at 0
- NAV and TERR selected on EFIS control panel
- GPS flap override is normal and guarded, and
- The GPS caution light is out

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24
Q

EGPWS ground test failed?

A

RADIO ALTITUDE FAULT
- GLIDESLOPE FAULT
- BAROMETER RATE FAULT

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25
Q

TCAS surveillance area?

A

40nm max
The system monitors 14nm around the aircraft

26
Q

TCAS Aircraft tracking amount?

A

45 aircraft and 8 most dangerous intruder aircarft

27
Q

TPU stand for?

A

TCAS processor unit

28
Q

TCAS press key does what?

A

Changes TCAS display from continuous to pop up mode. Pop up mode is default

29
Q

TA only mode automatic when?

A

Below 1000ft RA during climb
Below 900ft RA during descent

30
Q

TCAS surveillance area (vertical)

A

Norm +/- 2700ft
Below +2700, -9000ft
Above +9000, -2700ft

31
Q

TCAS traffic symbols and colours?

A

Proximity intruder traffic blue solid diamond
TA yellow circle
RA red square

32
Q

Climb RAs inhibited when?

A

OEI

33
Q

TCAS aural advisories inhibited when?

A

<600ft during climb
<400ft during descent

34
Q

Increase climb RA inhibited when?

A

Landing config and flaps >15 and gears down
Take off config auto feather armed

35
Q

Which parameter below is NOT considered by the stall protection system when activating a stick shaker?

A

Aircraft weight

36
Q

Increase descent advisories are inhibited ?

A

Below 1,450 RA

37
Q

If operating with the REF SPEEDS switch selected to INCR ?

A

The low speed cue on the speed tape start at a higher lAS

38
Q

The rapid clacking tone when the pitch trim is in motion is produced ?

A

When the trim has been running in excess of 3 seconds

39
Q

During an engine-out condition TCAS resolution advisories ?

A

Will not order any climb instructions

40
Q

With TCAS operating in the relative (REL) mode an intruder showing -02 is ?

A

200 feet below

41
Q

The STICK PUSHER SHUT OFF switchlights are located ?

A

On the glareshield in front of the control columns

42
Q

The TCAS test function is accessed by using ?

A

The audio and radio control display unit (ARCDU)

43
Q

Switching TCAS between the pop-up and continuous display modes is performed on the ?

A

The associated EFIS control panel

44
Q

When TCAS is selected to TA/RA it will operate in TA ONLY mode when ?

A

Below 1,100 RA on climb, and below 900 RA on descent

45
Q

The stall protection system provides which of the following types of indications of an impending stall?

A

All of the above
Aural
Visual
Tactile

46
Q

A successful TCAS system test is indicated by ?

A

A TCAS SYSTEM TEST OKAY aural message

47
Q

The TCAS range ring on the MFD navigation page is displayed at ?

A

2nm

48
Q

The stick pusher activates when ?

A

The aircraft has stalled

49
Q

Activation of one stick shaker will ?

A

Cause both control columns to vibrate and shake

50
Q

If the selected flap does not match the GPWS LANDING FLAP the ‘TOO LOW, FLAPS warning will sound ?

A

Below 200’ RA

51
Q

Lifting the power lever gate release triggers in flight will ?

A

Produce a continuous chirping tone

52
Q

When TCAS is selected to BELOW the surveillance area displayed is ?

A

2700 feet above and 9000 feet below the aircraft

53
Q

The stall protection system includes ?

A

Two stick shakers and one stick pusher

54
Q

Above 150 feet AGL a BANK ANGLE warning from the EGPWS will sound the aircraft exceeds ?

A

40 degrees angle of bank

55
Q

When the master warning light illuminates which of the following will be heard?

A

A triple chime

56
Q

The default display mode for TCAS information is ?

A

The pop-up mode

57
Q

During descent the first radio altitude callout occurs at ?

A

2500 RA

58
Q

When the TCAS display is in the continuous mode and a traffic advisory is issued ?

A

The display is forced to 10NM AUTO RANGE

59
Q

Warning and caution alert tones are generated by ?

A

Warning Tone Generators (WTGs)

60
Q

The stall protection system is NOT available below ?

A

200 RA

61
Q

Which of the following will NOT trigger the take-off configuration warning horn?

A

Control lock engaged

62
Q

When a data tag is not present the target traffic is operating their transponder in mode?

A

A without altitude encoding.

Q400 (33 decks)

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