Flight Controls Flashcards
How will the rotor discs react to a right pedal input?
the forward swashplate tilts right and the aft tilts left
How will the rotor discs react to a right cyclic input?
tilts both rotor discs to the right
How is the collective pitch in the forward and aft rotors affected when the cyclic is moved forward?
forward rotor disc pitch is decreased with an increase in the aft
DCP (Differential Collective Pitch)
What control movements must be made for a hovering turn about:-
a. Center hook?
b. Forward rotor?
c. Aft rotor?
a. apply pedal input only
b. Pedal and cyclic movements in opposite directions
c. Pedal and cyclic movements in the same direction
DAFCS DASH ILCA CCDA LVDT CPT
digital advanced flight control system Differential airspeed hold Integrated lower control actuator Cockpit control drive actuator Linear variable differential transducer Control position transducer
What environmental flight condition shall be avoided when the thrust brake is inoperative?
do not enter forecast turbulence
Which control axes have magnetic brakes that are released when the centering device release switch is pressed?
Pitch, roll, and yaw
What is the function of the DAFCS extensible link portion of the ILCA?
So that the DAFCS can make inputs into the flight control system
Pulling the cyclic aft increases pitch in the forward blades and decreases pitch in the aft blades, this is an example of?
differential collective pitch
What component improves control feel by reducing control sensitivity?
viscous damper
What is the preset tilt of the forward and aft transmissions?
forward: 9 degrees
Aft: 4 degrees
What ILCA does not have an extensible link portion?
The thrust ILCA
thrust CCDA components
mag brake, electric actuator, slip clutch
What are the functions of the boost potion of the ILCA?
Hydraulic assist (1500 psi) Prevent feedback provide hydraulic assist for cockpit control inputs, and prevents control feedback
What is the function of the DAFCS extensible link portion of the ILCA?
Electric signals to mechanical inputs in the upper portion of the flight controls