Warning Systems Flashcards

1
Q

Annunciator intensity may be changed by:

  • Resetting the master caution system
  • Positioning the TEST switch to CAUT.
  • Using the lighting dimmer.
  • Positioning the dimming switch to BRT or DIM as appropriate.
A
  • Positioning the dimming switch to BRT or DIM as appropriate.
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2
Q

A gear warning horn sounds:
- Any time the gear does not lock down.
- When the gear fails to up-lock at retraction.
- Only when the HORN switch is positioned to TEST.
- When the gear is not down and locked with the airplane in the landing
configuration.

A
  • When the gear is not down and locked with the airplane in the landing
    configuration.
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3
Q

The warning lights are:

  • Amber and flash until the master warning is reset.
  • Red and flash until the master warning is reset.
  • Amber and indicate appropriate action is required.
  • Red and illuminate in a steady state when a fault is detected.
A
  • Red and flash until the master warning is reset.
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4
Q

The stall warning computer on the Dash 8 (200) provides:
- Stick pusher activation upon detection of a stall condition.
- Stick shaker warning of an impending stall and visual indication of speed
relative to stall speed during low speed maneuvers.
- Guaranteed protection against impending stall.
- Protection against controlled flight into terrain.

A
  • Stick shaker warning of an impending stall and visual indication of speed
    relative to stall speed during low speed maneuvers.
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5
Q

The conditions that cause the take-off warning horn to sound are (There maybe more than one correct

response) :
- One or both condition levers not at MAX.
- Landing gear not down and locked, flaps selected to 15° or greater.
- Engine ECU rating selector not at take-off power (TOP).
- Elevator trim out of the take-off range.
- Flaps extended more than 20 degrees or less than 5 degrees.
- Parking brake lever selected to PARK.

A
  • One or both condition levers not at MAX.
  • Engine ECU rating selector not at take-off power (TOP).
  • Elevator trim out of the take-off range.
  • Flaps extended more than 20 degrees or less than 5 degrees.
  • Parking brake lever selected to PARK.
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6
Q

When the TEST switch is set to the ADVSY position, all:

  • Advisory lights illuminate provided DC power is available.
  • Advisory lights illuminate provided 115 vAC power is available.
  • Caution annunciators illuminate
  • Caution/warning annunciator and both master indicators illuminate
A
  • Advisory lights illuminate provided DC power is available.
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7
Q

When a malfunction occurs, the caution / warning system activates:

  • The pilots ejection seat.
  • A master indicator and an aural tone.
  • A system annunciator.
  • A system annunciator and the associated master indicator.
A
  • A system annunciator and the associated master indicator.
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