Flight Controls Flashcards
what system helps break the jammed rudder
Rudder system anti/jam breakout mechanisms
airleon flutter dampers prevetn
control surface flutter when HYD power is lost by the PCU
take off flaps are 8 and 20
both with stops
primary flight controls are
elevators rudder and ailerons that re manually contorledd and hyd actuated and spoileron
aileron bungee breakout switch provided automatic oneside
MFS and operable curcuit during a PCU runaway
the captain overrides all Horizontal stab trim controls
str trim will disc the AP too those limits are 2 - -13
Spolierons ROLL caution single chime and amber ROLL SEL lights
indicates a roll DISC handle has been pulled BUT the pilot had not EST the use of the second spolieron
0 1 8 20 30 45
flaps posistion 1 not flaps just slats max performance at 20
Flaps Half speed message on the EICAS shows that a motor
has failed
WOW is the only difference forget MFS and the deploy logic of the ground spoilers logic
needed is 16 knots 7 ft ra and WOW on the L or R Main LNG gear
each elevator has 3 pcus
on disc same side control to each elevator 2 for the ailerons and 1 pcu each spoiler or MFS
there are 4 circuit breaker panels
CA FO AFT Equip Nose compartment
GCU will give fire protection when a overcurrent of the gen bus
other fault protection is over under freq and volts and gen phase non fire driven issues
secondary flight controls electively driven
slaps flaps and spoilers aileron rudder horizontal stabtrim and MFS
ailerons protection has shock absorbers and hyd pressure
for gust lock on shut down with inboard brakes pressure
