Flight Controls Flashcards
The following primary flight controls are hydraulic: _____.
-Elevators
-Rudder
-Roll Spoilers (MFS)
In a right and left hydraulic failure condition, the elevators are operated by _____.
Manual Reversion (cables) via trapped pres-
sure in the PCUs
In a right and left hydraulic failure condition, the rudder is operated by _____.
the lower rudder PCU via the Aux Hydraulic
System
Is the yaw damper active on the ground?
Yes—ON until 60 kt where it is disabled, then
re-enabled with weight off wheels.
Is there a trim tab on the rudder?
No, the rudder surface is deflected directly.
Ground spoilers are enabled when (5) _____
-The switch is set to ARM
-Thrust levers idle
-2 of 3: WOW
-Radar alt. less than 7 ft
-Wheel speed is above 16 kt
The stick pusher can be disabled in three ways: _____, _____, and _____.
-MSW (press and hold)
-Stall Pusher PBA OFF
-CB1 #B-12
The maximum altitude with the YD off is _____ ft.
31,000
If the right EDP fails, what operation concerns and indications are present?
First 5° of flaps are extremely slow and the
cyan CAS message FLAPS RATE LOW is
present.
Turn off the roll spoilers by selecting _____.
The Roll Spoilers PBA to the OFF position as
directed by the checklist for a Roll Control Jam
on the left side
When the roll disconnect is activated, the pilot in the _____ seat controls the roll spoilers and the pilot in the _____ seat controls
the ailerons.
Left - Spoilers
Right - Ailerons
When the pitch disconnect is activated, _____.
The right and left control columns are separated. The pilot without the jam will fly that
respective side elevator
The controls secured by the gust lock include _____. PCUs trap pressure for elevator and rudder dampening for _____ hr after
hyd pressure is removed.
-Ailerons and thrust levers
-Approximately 12 hours
The _____ flight controls have trim tabs on the _____ side only.
-Ailerons
-Left
Which 3 systems use primary trim?
-AP
-Configuration trim
-Mach trim
