Flt Warn System Flashcards

1
Q

Warnings and information about the nature of a situation are provided by _____ signals.

A

visual, aural, and tactile

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2
Q

Immediate attention warning lights are _____.

A

red

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3
Q

Red warning lights may indicate ____.

A
  • engine, wheel well, and APU fires
  • A/P, A/T disconnects
  • landing gear unsafe conditions
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4
Q

Amber annunciator lights alert the flight crew of conditions which ____.

A

require timely attention

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5
Q

Informational alerts such as electrical power availability, valve position, equipment status, and flight attendant or ground communications are indicated by lights that are _____ in color.

A

blue

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6
Q

Some lights have a bright blue and a dim blue setting. The bright blue indicates a valve _____ and the dim blue indicates a valve _____.

A

moving to its selected position/in the selected position

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7
Q

Green lights indicate an extended configuration of ____.

A

both landing gear and leading edge devices

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8
Q

Pushing the fire warning (FIRE WARN) lights or BELL CUTOUT for an engine fire ____.

A
  • extinguishes both FIRE WARN lights
  • silences the Fire Warning Bell
  • resets the system for additional warnings
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9
Q

Pushing a MASTER CAUTION light after it illuminates ____.

A

resets the system for additional master caution conditions

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10
Q

An illuminated amber light on the System Annunciator Panel is on because of a malfunction outside of the primary viewing area of the pilots. To extinguish it, ____.

A

push either MASTER CAUTION light

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11
Q

The Landing Gear Warning Cutout Switch silences the landing gear configuration warning at flaps UP through ____ degrees.

A

10

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12
Q

The GPWS Inoperative (INOP) Light illuminates amber for ____.

A

a GPWS malfunction

  • a power loss
  • invalid inputs
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13
Q

Generally, aural warnings will silence ____.

A

automatically when the associated non-normal condition no longer exists

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14
Q

The System Annunciator Light Panels monitor system indications located on ____.

A

the Overhead and Fire Control panels

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15
Q

The _____ annunciator panel monitors the following systems: flight controls, IRS, fuel, electrical, APU, and overheat/detection.

A

left

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16
Q

The _____ annunciator panel monitors the following systems: anti-ice, hydraulics, doors, engines, overhead panel, and air conditioning.

A

right

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17
Q

The takeoff configuration intermittent warning can be cancelled only ____.

A

when the configuration is corrected

18
Q

Landing gear light indications are ____.

A
  • green light - gear is down and locked
  • red light - gear is in disagreement with lever position, gear is not down and locked (below 800 ft RA and a thrust lever at idle.)
  • extinguished - gear up and locked
19
Q

The Proximity Switch Electronic Unit (PSEU) monitors ____.

A
  • takeoff and landing configuration warnings
  • air/ground sensing
  • landing gear
20
Q

Two independent Mach/airspeed warning systems sound a clacker when maximum speed is exceeded. The clacker will only be silenced when ____.

A

airspeed is reduced below Vmo/Mmo

21
Q

The PSEU light is inhibited ____.

A

in flight

22
Q

The stall warning stick shaker consists of ____.

A

two separate motors, one on each control column

23
Q

The stick shakers are designed to alert the pilots ____.

A

just before a stall develops

24
Q

On the fire test panel, we can test for ____.

A
  • APU, engines, and wheel well fire
  • engine overheat
  • operational fire bottle squibs
25
Q

A valve that is not in its selected position will show up as a(an) _____ light.

A

bright blue

26
Q

The MASTER CAUTION Lights will remain illuminated ____.

A

until reset or as long as the caution condition exists

27
Q

Single faults in certain redundant systems or some simple faults do not illuminate the MASTER CAUTION or the System Annunciator Light until _____.

A

recall of the system

28
Q

When performing the Before Taxi/Taxi checklist, the PSEU light illumination on recall indicates _____.

A

a simple fault exists in the PSEU system

29
Q

____ will activate the takeoff warning system.

A

SPEED BRAKE lever is not in the DOWN position

30
Q

The red gear indicator light will be illuminated for ____.

A

landing gear in transit

31
Q

The flaps are set at 10 degrees, the landing gear is up, and you are above 800 feet RA. Which of the following statements is true about the landing gear horn?

A

The horn will not sound.

32
Q

The Mach/airspeed warning will sound the clacker anytime _____ is exceeded.

A

Vmo/Mmo

33
Q

The SMYD computers receive input from _____.

A
  • anti-ice controls
  • ADIRUs
  • FMCs
34
Q

A momentary altitude alert tone will activate ____.

A

approaching 900 feet of the altitude selected on the mode control panel

35
Q

Deviations from the altitude selected on the mode control panel will cause a ____.

A

momentary altitude horn at 200 feet off altitude and an amber flashing box around the current altitude

36
Q

A flashing amber box around the current altitude signifies ____.

A

an altitude deviation of 200 feet or more

37
Q

Normal engine indications on the upper engine display are ____ in color.

A

white

38
Q

Maximum engine limits are displayed in ____.

A

red

39
Q

Upon engine shutdown on the ground at the end of the flight, an inflight exceedence will be ____.

A

shown by a red box

40
Q

A start valve failed to close on engine start. Which of the following will alert the crew?

A

Blinking start valve open alert for 10 seconds

41
Q

Some minor cautions or faults do not illuminate the MASTER CAUTION lights or system annunciator lights but are stored and presented later during ____.

A

RECALL

42
Q

The landing gear configuration warning horn will activate at any altitude and cannot be silenced if a gear is not down and locked with the flaps set to ____ degrees with one or both throttles set to idle.

A

15