An illuminated amber standby hydraulic LOW PRESSURE light indicates low output pressure, and is:
a)
armed only when the standby hydraulic pump operation has been selected or automatic standby pump operation is activated
b)
deactivated when Engine 2 fire switch has been pulled
c)
always armed
armed only when the standby hydraulic pump operation has been selected or automatic standby pump operation is activated
On the PFD/ND, hydraulic system quantity is displayed:
a)
on the Upper Display Unit
b)
at all times with the secondary engine indications
c)
by pushing the MFD System (SYS) switch
by pushing the MFD System (SYS) switch
The autobrake system uses _______ to provide maximum deceleration for rejected takeoff.
a)
Hydraulic System A pressure
b)
Hydraulic System B pressure
c)
Hydraulic System A or B pressure
Hydraulic System B pressure
After the autobraking has started, any of the following pilot actions disarm the system immediately and illuminate the AUTO BRAKE DISARM light:
a)
moving speed brake lever to full forward or applying manual brakes
b)
advancing the forward thrust lever(s), except during the first 3 seconds after touchdown
c)
all answers are correct
all answers are correct
When the LANDING GEAR lever is moved to DN, hydraulic system___ pressure is used to release the uplocks. The landing gear extends by:
a)
A; hydraulic pressure, gravity, and air loads
b)
STBY; hydraulic pressure, gravity, and air loads
c)
B; gravity, and air loads
A; hydraulic pressure, gravity, and air loads
With the AUTO BRAKE Select Switch in RTO, maximum brake pressure is automatically applied when the thrust levers are retarded to idle at or above ___ knots.
a)
60
b)
90
c)
120
90
Antiskid protection is provided:
a)
on both brake systems (normal and alternate)
b)
with normal brakes only
c)
with alternate brakes only
on both brake systems (normal and alternate)
An illuminated red landing gear indicator indicates the related landing gear is in disagreement with the LANDING GEAR lever position (in transit or unsafe), or:
a)
landing gear is not down and locked (with either or both forward thrust levers retarded to idle and below 800 feet AGL)
b)
landing gear is up
c)
the landing gear manual extension must be used
landing gear is not down and locked (with either or both forward thrust levers retarded to idle and below 800 feet AGL)
Hydraulic power for retraction, extension, and nose wheel steering is normally supplied by:
a)
standby system
b)
hydraulic system A
c)
hydraulic system B
hydraulic system A
Placing the Nose Wheel Steering Switch to ALT allows _______ to provide power for nose wheel steering.
a)
the standby hydraulic system
b)
hydraulic system A
c)
hydraulic system B
hydraulic system B