Warning Systems Flashcards

1
Q

Where is the TCAS RA displayed

A

On the outer Rose of TA/VSI indicator

Accompanied by voice Alerts

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2
Q

What are the indications when departing an MCP selected altitude.

A
  1. Departing by more than 250’
  2. A steady ‘C’ chord
  3. Aural ALTITUDE
  4. flashing altitude advisory light
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3
Q

What are the indications when approaching an MCP selected altitude

A

At 750’ from the selected altitude,

  1. CAWS generates ‘C’ chord
  2. Altitude advisory light comes on steady
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4
Q

What conditions will activate the landing gear configuration warning system with the gear not down and locked

A
  1. Gear handle not down and flaps extended beyond 26°

2. Gear handle not down. Any throttle fully retarded, with airspeed less than 210 kn and altitude less than 1500 RA

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5
Q

What is the meaning of the different colors displayed by the EGPWS

Magenta
Dotted green
Dotted Amber
Dotted red
Solid Amber
Solid red
A

Color and density very based on terrain eight verse airplane altitude
Magenta - no terrain data available

Dotted green - to rain from 2000 below to 500 below(250 with gear down) The airplanes current altitude

Dotted Amber - terrain 500 feet below(250 with gear down) two 2000 above airplanes current altitude

Dotted red - to rain more than 2000 above the airplanes current altitude

Solid Amber - caution to rain. Approximately 60 seconds from impact

Solid red - warning to rain, approximately 30 seconds from impact

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6
Q

Describe the TCAS RA maneuver guidance

Autothrottle and autopilot usage?

A
  1. If maneuvering is required, disengage the auto pilot and auto throttle
  2. Smoothly adjust pitch and thrust to achieve/maintain the vertical guidance indicated by the green band on the TA/VSI.
  3. Follow the plan lateral flightpath unless visual contact with the conflicting traffic requires other action
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7
Q

What are windshear RWS indications on the PFD during take off or approach and landing

A

for take off after nose strut extension

  1. Increasing performance - Amber WINDSHEAR on both the PFD and glareshield. No aural warning.
  2. Decreasing performance - red WINDSHEAR on both PFD and glare shield. Aural warning tone and three cycles of “WINDSHEAR”
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8
Q

What are the windshear guidance during takeoff, after nose strut extension on FMA

A

Increasing performance -

  1. WIND SHR on FMA.
  2. Pitch guidance available through the auto pilot and or FD.
  3. WIND SHR Will flash five times on the FMA and then become steady.
  4. The roll window will remain on changed

Decreasing performance -

  1. WIND SHR on FMA pitch window.
  2. guidance is available through the auto pilot and/or FD.
  3. WND SHR. Will flash five times on the FMA and then become steady.
  4. roll guidance, wings level, will be provided on the FD and HDG HLD Will be displayed on the FMA
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9
Q

What is the wind shear guidance during approach or landing

A

Increasing performance -

  1. guidance is not activated during the approach mode unless the TOGA button is pressed or either engine EPR is 95% of max go around EPR.
  2. When WIND SHR is on FMA Pitch guidance is available for the auto pilot and or FD.
  3. The FMA Will flash five times then steady. The role window will remain unchanged

Decreasing performance -

  1. guidance is not activated unless the TOGA is pressed or 95% max EPR for go around.
  2. With these conditions windshear guidance is available to the auto pilot and or FD, when displayed on the FMA pitch window Pitch guidance is available to the auto pilot and or FD.
  3. Windshear will flash five times and then steady.
  4. Roll guidance will be provided on the FD and HDG HLD will be displayed on the FMA
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10
Q

How do you silence the overspeed warning system

A
  1. The CAWS Will generate a clacking sound, alternating with the spoken word “overspeed” or “slat overspeed”
  2. The warning indications remain active and cannot be silenced until the overspeed condition is corrected
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11
Q

What’s the function of the Pitch Limit Indicator (PLI)
When does it start?
Slats function

A
  1. The PLI appears when airplane reaches 60 kn and the airplane is at or below 1500 AGL
  2. If the slats are extended, the PLI Will be displayed at any altitude
  3. PLI indicates relationship of airplane angle of attack and stick shaker angle of attack
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12
Q

Where is the TCAS Target symbology displayed

A

On the TA/VSI indicator and the pedestal radar

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13
Q

Explain the symbol/color of a TCAS TA and other warning methods

A
  1. aural alert “TRAFFIC, TRAFFIC” calls attention to a display of a solid amber circle on the TA/VSI indicator and pedestal radar if mode selector is in TCAS or WX/TCAS.
  2. relative altitude with a climb or divert arrow may be displayed
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14
Q

Explain the symbol and color of a TCAS RA

A
  1. An RA is displayed as a solid red square on the traffic display,
  2. colored arcs are added on the VSI
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15
Q

Purpose of GPWS and The types of alerts it provides

Sink rate
Terrain
Don't sink
Too low gear
Too low flaps
Minimums
Glideslope
A

The GPWS alerts the crew when any one of the following occurs

SINK RATE, SINK RATE - excessive sink rate
TERRAIN TERRAIN - excessive terrain closure rate
DONT SINK - altitude loss after take off or go around
TOO LOW GEAR, or TOO LOW FLAPS - unsafe altitude while not in the landing configuration
GLIDESLOPE - dissent below glideslope below 1000 feet AGL
MINIMUMS - Decent below decision height

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16
Q

When is the minimums vocal inhibited

A

Below 50’ +/-15

So 50 feet is unreliable if used as a DH. You may not hear anything

17
Q

When do predictive windshear PWS, become available on take off or approach

A
  1. It’s active regardless of weather radar switch position on the weather radar indicator. The crew is alerted by way of annunciation and audio announcement
  2. During take off and landing new PWS CAUTION alerts are inhibited between 80 kn and 400 RA, and new WARNING alerts between 100 kts and 50’ RA landing
  3. Below 2300 feet RA Windshear operations use an alternate scan technique for radar and windshear detection
  4. Windshear operation is transparent to the Crew unless an alert is issued, however crews May notice that the radar update rate could be delayed by as much as 12 seconds due to sharing of processing between windshear and radar
  5. The PWS automatically begins scanning for windshear on the ground when…
    A. The right throttle is set for take off, approximately 80% N1
    B. One engine is running
  6. The PWS automatically begins scanning for windshear in the air when…
    A. Below 2300’ RA but alerts are only issued below 1200’ RA
18
Q

Can you shut off the gear horn

A

No for flap logic

Yes for speed and altitude logic

19
Q

When is predictive windshear system able to issue an alert on the ground

A

Right throttle set for takeoff

At least one engine running

20
Q

When does reactive windshear guidance become available on takeoff

A

After nose strut extension with WND SHR in the pitch window on the FMA

21
Q

When is the CENTER FUEL PRESS LO message/Master Caution inhibited

A

When the flaps are 6 degrees or greater