Flt Warn System Flashcards
Warnings and information about the nature of a situation are provided by _____ signals.
visual, aural, and tactile
Immediate attention warning lights are _____.
red
Red warning lights may indicate ____.
- engine, wheel well, and APU fires
- A/P, A/T disconnects
- landing gear unsafe conditions
Amber annunciator lights alert the flight crew of conditions which ____.
require timely attention
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.
blue
Some lights have a bright blue and a dim blue setting. The bright blue indicates a valve _____ and the dim blue indicates a valve _____.
moving to its selected position/in the selected position
Green lights indicate an extended configuration of ____.
both landing gear and leading edge devices
Pushing the fire warning (FIRE WARN) lights or BELL CUTOUT for an engine fire ____.
- extinguishes both FIRE WARN lights
- silences the Fire Warning Bell
- resets the system for additional warnings
Pushing a MASTER CAUTION light after it illuminates ____.
resets the system for additional master caution conditions
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, ____.
push either MASTER CAUTION light
The Landing Gear Warning Cutout Switch silences the landing gear configuration warning at flaps UP through ____ degrees.
10
The GPWS Inoperative (INOP) Light illuminates amber for ____.
a GPWS malfunction
- a power loss
- invalid inputs
Generally, aural warnings will silence ____.
automatically when the associated non-normal condition no longer exists
The System Annunciator Light Panels monitor system indications located on ____.
the Overhead and Fire Control panels
The _____ annunciator panel monitors the following systems: flight controls, IRS, fuel, electrical, APU, and overheat/detection.
left
The _____ annunciator panel monitors the following systems: anti-ice, hydraulics, doors, engines, overhead panel, and air conditioning.
right
The takeoff configuration intermittent warning can be cancelled only ____.
when the configuration is corrected
Landing gear light indications are ____.
- 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
The Proximity Switch Electronic Unit (PSEU) monitors ____.
- takeoff and landing configuration warnings
- air/ground sensing
- landing gear
Two independent Mach/airspeed warning systems sound a clacker when maximum speed is exceeded. The clacker will only be silenced when ____.
airspeed is reduced below Vmo/Mmo
The PSEU light is inhibited ____.
in flight
The stall warning stick shaker consists of ____.
two separate motors, one on each control column
The stick shakers are designed to alert the pilots ____.
just before a stall develops
On the fire test panel, we can test for ____.
- APU, engines, and wheel well fire
- engine overheat
- operational fire bottle squibs