AS411 Test 2 With 100% Verified
Answers Graded A+
The elevators, rudder and ailerons are:
"fly by wire".
manually controlled and electrically actuated.
manually controlled and hydraulically actuated.
mechanically controlled. - CORRECT ANSWER-manually controlled and hydraulically
actuated.
The FWD/AFT cargo bays have both Smoke Detection and Fire Protection. -
CORRECT ANSWER-True
The slats/flaps are
electrically powered
hydro-mechanically powered
hydraulically powered
hydro-electrically powered - CORRECT ANSWER-electrically powered
What happens when the LH or RH ENGINE FIRE PUSH switchlight is pushed?
The Fuel Power Crossflow Pump closes.
The Fire Warning light extinguishes.
Fire Bottle squibs are armed.
Halon is released into the engine compartment. - CORRECT ANSWER-Fire Bottle
squibs are armed.
,The APU Halon bottle will automatically discharge in flight if an APU fire is detected.
True
False - CORRECT ANSWER-False
During landing or rejected takeoff, how does multi function spoiler deploy logic differ
from the ground spoilers deploy logic?
Multifunction spoiler deployment occurs only below 100 kts wheel speed.
Multifunction spoilers do not deploy on landing. Only ground spoilers deploy on landing.
Multifunction spoiler deployment requires both main landing gear WOW.
Multifunction spoiler deployment requires radio altimeter < 10'. - CORRECT ANSWER-
Multi function spoiler deployment requires both main landing gear WOW.
The fire detection system for the engines use:
Two loops mounted in series.
A single loop sensing element mounted in series.
Two cross-crossing loops.
A duel loop sensing element mounted in parallel. - CORRECT ANSWER-A duel loop
sensing element mounted in parallel.
Flap position indications are always available on the:
Hydraulic Synoptic page.
EICAS Primary Page.
Flight Control Synoptic page.
EICAS Status Page. - CORRECT ANSWER-Flight Control Synoptic page.
, The components of the lavatory fire protection system are: (select one)
a single fire bottle that discharges into the lavatory compartment.
a smoke detector unit and a fire bottle that discharges into the waste disposal.
two fire bottles that discharge at different rates into the waste disposal.
overheat sensing elements and a fire bottle that discharges into the lavatory
compartment. - CORRECT ANSWER-a smoke detector unit and a fire bottle that
discharges into the waste disposal.
In flight, if the aircraft descends below 300' radio altitude or if any engine thrust lever is
advanced to the climb detent (or above) with the MFS deployed, what caution message
will display?
FLT SPLR DEPLOY
CONFIG WARNING
RETRACT SPLR
CONFIG SPLRS - CORRECT ANSWER-FLT SPLR DEPLOY
When the respective CARGO FIREX BOTTLE ARMED PUSH TO DISCH switch is
pressed:
One bottle will discharge completely; the larger bottle discharges over 60 minutes.
The first bottle discharges. The second bottle is the backup.
The bottle squibs are armed.
Both cargo bottles immediately discharge. - CORRECT ANSWER-One bottle will
discharge completely; the larger bottle discharges over 60 minutes.
Each rudder and elevator assembly is powered by ______ PCUs.
3
Answers Graded A+
The elevators, rudder and ailerons are:
"fly by wire".
manually controlled and electrically actuated.
manually controlled and hydraulically actuated.
mechanically controlled. - CORRECT ANSWER-manually controlled and hydraulically
actuated.
The FWD/AFT cargo bays have both Smoke Detection and Fire Protection. -
CORRECT ANSWER-True
The slats/flaps are
electrically powered
hydro-mechanically powered
hydraulically powered
hydro-electrically powered - CORRECT ANSWER-electrically powered
What happens when the LH or RH ENGINE FIRE PUSH switchlight is pushed?
The Fuel Power Crossflow Pump closes.
The Fire Warning light extinguishes.
Fire Bottle squibs are armed.
Halon is released into the engine compartment. - CORRECT ANSWER-Fire Bottle
squibs are armed.
,The APU Halon bottle will automatically discharge in flight if an APU fire is detected.
True
False - CORRECT ANSWER-False
During landing or rejected takeoff, how does multi function spoiler deploy logic differ
from the ground spoilers deploy logic?
Multifunction spoiler deployment occurs only below 100 kts wheel speed.
Multifunction spoilers do not deploy on landing. Only ground spoilers deploy on landing.
Multifunction spoiler deployment requires both main landing gear WOW.
Multifunction spoiler deployment requires radio altimeter < 10'. - CORRECT ANSWER-
Multi function spoiler deployment requires both main landing gear WOW.
The fire detection system for the engines use:
Two loops mounted in series.
A single loop sensing element mounted in series.
Two cross-crossing loops.
A duel loop sensing element mounted in parallel. - CORRECT ANSWER-A duel loop
sensing element mounted in parallel.
Flap position indications are always available on the:
Hydraulic Synoptic page.
EICAS Primary Page.
Flight Control Synoptic page.
EICAS Status Page. - CORRECT ANSWER-Flight Control Synoptic page.
, The components of the lavatory fire protection system are: (select one)
a single fire bottle that discharges into the lavatory compartment.
a smoke detector unit and a fire bottle that discharges into the waste disposal.
two fire bottles that discharge at different rates into the waste disposal.
overheat sensing elements and a fire bottle that discharges into the lavatory
compartment. - CORRECT ANSWER-a smoke detector unit and a fire bottle that
discharges into the waste disposal.
In flight, if the aircraft descends below 300' radio altitude or if any engine thrust lever is
advanced to the climb detent (or above) with the MFS deployed, what caution message
will display?
FLT SPLR DEPLOY
CONFIG WARNING
RETRACT SPLR
CONFIG SPLRS - CORRECT ANSWER-FLT SPLR DEPLOY
When the respective CARGO FIREX BOTTLE ARMED PUSH TO DISCH switch is
pressed:
One bottle will discharge completely; the larger bottle discharges over 60 minutes.
The first bottle discharges. The second bottle is the backup.
The bottle squibs are armed.
Both cargo bottles immediately discharge. - CORRECT ANSWER-One bottle will
discharge completely; the larger bottle discharges over 60 minutes.
Each rudder and elevator assembly is powered by ______ PCUs.
3
