Hydraulics & Flight Controls Flashcards
Output from the cockpit controls is carried by ____, through Pilot assist servos, to the mixing unit.
Mechanical Linkage and Bell Cranks
Cyclic stick position is maintained by the ____.
Roll Trim Actuator
There are 2 tail rotor cables that connect the controls to the ____.
Aft Quadrant.
If both tail rotor cables fail, a centering spring will position the tail rotor servo linkage to provide enough pitch to allow trimmed flight at about __ KIAS and __ KIAS
25 KIAS and 145 KIAS
On the primary servos there are 2 pressure switches, 1 for each stage, located on top of each servo to illuminate first or second stage primary servo pressure caution light if pressure drops below ____ or a Pilot valve jams
2,000 ±50 psi
Mixing unit automatically provides ____ mechanical control mixing functions which reduce Pilot workload.
4
The TAIL SERVO switch is located on the ____.
miscellaneous switch (MISC SW) panel
The Pilot Assist Module has a pressure reducer with relief valve that reduces pressure to ____ psi for pitch trim actuator.
1,000 PSI
The Pilot Assist Module has a red indicator button on the trim pressure reducer that will pop up if trim pressure exceeds ____ psi.
1,500 PSI
Each hydraulic system is designed to provide ___ ±50 psi of pressure under no load conditions.
3,000 +/- 50
During normal operations, the Pilot Assist Module directs hydraulic pressure to the Pilot Assist Servos from which pump?
No. 2 Hydraulic Pump
In the event yaw boost servo jams or has a hardover, a force of ____ lbs would be necessary to move the flight controls with only a mechanical linkage.
250 Lbs
The ____ switch on the AFCS control panel only affects collective and yaw boost.
BOOST
Red indicator button on each filter on the No. 1 and No.2 hydraulic pump pops out when pressure goes to ____.
70 PSID ±10.
The delay on the depressurizing valve is 0.5 sec if main generators are on, or ___ if APU generator or external power is source of power.
3–5 sec