System Review PTM CH-15 (Flight Controls) Flashcards
Pitch control is provided by___ operated elevators.
Mechanically (cables)
Pulling the PITCH/ROLL Disconnect Handle separates the ___ and ___ systems.
Pitch and Roll
PITCH/ROLL Disconnect allows left yoke to control ___?
Left Elevator
Left Aileron
PITCH/ROLL Disconnect allows right yoke to control ___?
Right Elevator
Spoilers
PITCH/ROLL Disconnect can reconnect ___?
Pitch or Roll or BOTH
Primary Pitch Trim is accomplished by ___ controlled movable horizontal stabilizer.
Electrically
Secondary Pitch Trim travels at the normal rate, T/F?
FALSE, Slower
Autopilot is available with Secondary Pitch Trim activated, T/F?
FALSE
Mach trim system increases aircraft pitch ___ (up or down) forces at airspeed above Mach 0.77.
UP. Counters Mach Tuck
Roll control is provided how?
Mechanically operated ailerons and Hydraulically operated roll spoilers.
Spoiler panels number _______ operate as roll spoilers and speed brakes.
They deploy ___ (fully or incrementally).
2,3,4 and 7,8,9 (middle 3).
Incrementally
Spoiler panels number _______ operate as speed brakes only. They deploy ___ (fully or incrementally). Where is the speedbrake handle for full deployment?
1,5 and 6,10 (outboard 2)
Incrementally
EXT
What provides proportional roll spoiler deployment?
Spoiler mixer box
Aileron trim is through two ___ operated aileron trim tabs.
Electrically
Rudder is hydraulically controlled, T/F?
FALSE. Mechanically
Rudder bias uses ___ (air pressure or electric or hydraulic) forces to assist rudder control during single engine operations.
Bleed Air Pressure from engines
Rudder Trim is through a single, ___ (Electrically or hydraulically) operated trim tab.
Electrically
Yaw Damping is through the rudder ___ control.
Servo
Flaps are ___ (electrically or hydraulically) operated.
Electrically
Control Lock ___ (electrically or hydraulically or mechanically) locks the controls and restricts the ___ throttle to half travel.
Mechanically
Left
CONTROL LOCK CAS contributes to a ___ ________ warning.
NO TAKEOFF
Speed brakes should be stowed by ___ feet.
500 feet.
Flaps may be set only at Up (0 degrees), 1, 2 and Full (35 degrees).
NO. Any position between Up and Full
Flap/Stabilizer Interconnect trims the stab when flaps are in motion between 2 & Full with the Autopilot ______ (engaged or disengaged).
Disengaged
Fault in the aileron ratio changer causes a ______ CAS.
AILERON CNTRL FAULT
