Flight Controls Flashcards
Name the Powered Flight Control Surfaces (PFCS)
elevators, spoilers, rudder
What is the FCECU?
Flight Control Electronic Control Unit, located under the passenger floor, single electronic unit divided into two channels which send electrical outputs to primary and secondary flight control systems, flight data recording systems, advisory systems, and caution indicating systems
What is the FCECU powered by?
left channel - left essential DC bus
right channel - right essential DC bus
How is the elevator controlled and powered?
mechanically controlled by two fully independent cable and pulley control circuits (left control column controls left elevator, right control column controls right elevator), hydraulically powered by three identical Power Control Units (PCUs)
Which elevator PCUs are powered by which hydraulic system?
outboard - hyd system 1
center - hyd system 2
inboard - hyd system 3
What prevents an elevator PCU runaway?
input bungees
What prevents damage to the elevator control circuit in the event of a PCU jam?
two overload bungees installed in the horizontal stabilizer, one in each elevator circuit
What provides gust lock protection and elevator flutter suppression?
elevator PCU compensator installed in the return line of the No. 3 hydraulic system
What provides elevator artificial feel and pitch trim inputs?
two identical Pitch Feel and Trim Units (PFTUs) located in the upper section of the vertical stabilizer
ELEVATOR PRESS caution light
all 3 hydraulic systems are supplying pressure to elevator
ELEVATOR ASYMMETRY caution light
position mismatch between the left and right elevator control surfaces
ELEVATOR FEEL caution light
one of the FCECU channels is not able to control the pitch trim actuator
PITCH TRIM caution light
one of the FCECU channels is not able to control its related pitch trim actuator or Pilot and Copilot pitch trim input commands are different
How is the rudder controlled and powered?
mechanically controlled by rudder pedals which are connected by an interconnect rod, hydraulically powered by 2 PCUs
How is artificial feel for the rudder provided?
mechanical feel spring unit
What rudder PCUs are powered by which hydraulic system?
lower PCU - hydraulic system 1
upper PCU - hydraulic system 2
Deflection of rudder sections
full deflection, aft section - 36 degrees
full deflection, fore section - 18 degrees
flap 0 limited, aft section - 24 degrees
flap 0 limited, fore section - 12 degrees
What is rudder deflection limited by?
regulated by FCECU in response to airspeed
What does the Rudder Feel/Trim and Summing Unit do?
provides artificial feedback forces on rudder pedals and sums rudder trim and yaw damper inputs and then commands a single input to the rudder PCUs
RUD 1 switchlight
mechanical jam in lower rudder PCU, depressurizes PCU when pushed