Xiaomi 13t

(ATA 32) What controls the MLG extension speed?. Actuator rod end snubber by the end of the extension stroke. Alternate extension system pressure in retract actuator. Actuator rod end snubber by the end of the extension stroke.

(ATA 32) Which sensor is using by PFCs for auto speedbrake operation?. MLG down proximity sensor. MLG truck tilt sensor. weight-On-Wheel System sensor.

(ATA 32) Which proximity sensor electronic unit (PSEU) has the flight lock and cargo control functions. PSEU 1 only. Both PSEU Simultaneously. PSEU 2 only.

(ATA 32) What must be removed in main electronic compartment to get access to NLG spring broken cable compensator?. Main battery. Crew oxygen bottle. ADIRU with its cover.

(ATA 32) When do the normal and alternate brake metering valves get pressure together. During gear retract braking. During normal braking. During alternate braking.

Normal brake metering valve use wich pressure system?. Right hydraulic system and acumulator pressure. Left hydraulic system only. Center/reserve and acumulator pressure.

Alternate brake metering valve use wich hydraulic system?. Center/reserve hydraulic system. Left hydraulic system only. Right hydraulic system and accumulator pressure.

(ATA 32) Can tail skid be retracted after tail strike?. No, due to tail skid cartrige being crushed. Yes, if just the fuse pin is broken. Yes, if just tail skid cartrige is crushed.

(ATA 32) The MLG drag brace-operated sequence valve controls the: MLG door close operation during landing gear extension. MLG side brace down lock actuator during landing gear extension. MLG drag brace down lock actuator during landing gear retraction.

(ATA 32) What does Weigh-ON-Wheels (WOW) system monitor for air/ground indication. MLG beam bending. MLG shock strut compression. MLG truck tilt positioner extension.

(ATA 32) When are the semi-levered gear hydraulic struts commanded to unlock. The airplane on the ground. The flaps are in a takeoff position. The airplane is in the air.

(ATA 32) How is the hottest brake on each main gear truck indicated on the synoptic page. Flashing brake symbol. Solid white brake symbol. Brake temperature indication in red.

(ATA 32) What does the ELMS auto-off relay execute?. Operate the control lever lock solenoid on the ground to lock lever in down position. Operates the control lever lock solenoid during the air/ground changeover. Removes the power of the UP solenoid and the selector moves to OFF to remove pressure.

(ATA 32) MLG steering operates: Simultaneously with NLG steering. When NLG turns more than 13 degrees. Independently from NLG steering.

(ATA 32) What are the degrees that moves the NLG steering and the MLG steering operates?. NLG steering up to 70 degrees left or right and MLG Steering When nose turns more than 13 degrees. NLG steering up to 50 degrees left or right and MLG Steering When nose turns more than 20 degrees. NLG steering up to 100 degrees and MLG Steering When nose turns 15 degrees.

(ATA 29) GE 90. Which of the following statements is true about the engine drive pump (EDP)?. When the Engine drive pump (EDP) is switched OFF, the depressurization solenoid gets electrical power. The depressurization solenoid is not part of the engine driven pump (EDP). C. When the depressurization solenoid is energized, the pump pressure output goes to the hydraulic system.

(ATA 29) How is an Air Driven Pump (ADP) overspeed condition reset?. By switching the pump switch to OFF and back to ON position. By operation of reset switch on the Logic Speed Control Unit (LSCU). By performing the appropriate Maintenance Access Terminal (MAT) test.

(ATA 29) RR RB211 Trent 800. Access to the EDP is through which cowling?. Right Fan cowling. Left Thrust Reverser half. Right Thrust Reverser half.

(ATA 29) PW 4000. Access to the EDP is through which cowling?. Right Thrust Reverser half. Left Thrust Reverser half. Right Fan cowling.

(ATA 29) GE90. Access to the EDP is through which cowling?. Left Thrust Reverser half. Right Thrust Reverser half. Left Fan cowl.

(ATA 29) What you have to do, to keep the movement of fluid between the right and center hydraulic systems to a minimum?. Pressurize the center hydraulic system first. Remove the pressure from the center hydraulic system last. Pressurize the right hydraulic system first. Remove the pressure from the right hydraulic system last. B. Pressurize the center hydraulic system first. Remove the pressure from the center hydralic system last.

(ATA 29) The RAT PRESSURE indication stay on after ground RAT monitoring until?. The RAT stow valve handle will be set to the STOW position. The internal laekage in the RAT module causes the pressure to decrease. The RAT monitoring valve will be released back to the FLIGHT position.

(ATA 29) When the depressurization solenoid valve gets electrical power?. turn off the pump. pump pressure output goes. the engine turns.

(ATA 29) Send the data to the AIMS for flight deck indication and also control the fault lights and the RAT indication lights on the hydraulic/RAT panel?. ACMP. HYDIM cards. PSEU.

(ATA 32) the function of the alternate Extend hydraulic pressure switch is to. turn off the alternate extend power pack after the completion of the alternate extend cycle. Supply pressure indication to the AIMS. turn on the alternate extend power pack when there is a failure on the Center hydraulic system.

(ATA 32) During landing gear up operation. Gear retract pressure goes through the alternate braking system to reduce the Main gear wheel speed. The normal brake metering valve supplies brake pressure to reduce the Main gear wheel speed. The accumulator pressure is used to reduce the Main gear wheel speed.

(ATA 32) the signal of the pedal position switches not applied position is. Make the BRAKE OFF lights comes on. Deactivate the alternate anti skid system only ground. Make the red BRAKE ON light come on when the brake pedals are applied.

(ATA 32) the signal of the pedal position switches when is applied. Make the BRAKE OFF lights comes on. Deactivate the alternate anti skid system only ground. Make the red BRAKE ON light come on when the brake pedals are applied.

What is the function of the lock up solenoid. To will lock the floating piston in the SLG actuator. Will lock the SLG in alternate extension. Hold the gear in the retracted position and release hydraulic pressure up actuator.

(ATA 27) PFCS in direct mode, speedbrake lever placed to UP position. Which spoilers will move to UP position?. All, except 4 and 11. All, except 5 and 10. All, except 4,5.10,11.

(ATA 27) The elevator off-load function automatically sets the position of which flight controls? and in which flight mode?. Stabilizer, during manual flight or in autoflight. Stabilizer, during an autoflight mode. Elevator, during manual flight or in autoflight.

(ATA 27) Which spoilers have a mechanical signal for roll control?. 4 and 11. 5 and 10. 6, 7, 8 and 9.

(ATA 27) In which modes flaperon PCU may operate?. Normal, bypass and blocking/damped. Normal and bypass only. Normal and damped only.

(ATA 27) When is autospeedbrake function not available?. If R ACE defective only. If center hydraulic system is failed only. If R ACE defective or center hydraulic system is failed.

(ATA 27) When does PFCS select secondary mode?. When PFC disconnects switch in DISC position. When two ACEs are in direct mode. When one ACE is in direct mode.

(ATA 27) Control surface pointer does not shows on synoptic display. W. Control surface position unknown. Control surface does not operate. Control surface operates normally.

(ATA 27) Is it possible to put ACEs to direct mode?. Yes, using ACE mode select switch. No, only automatic mode selection available. Yes, using PFC disconnect switch.

(ATA 27) Which information is required to have elevator speed stability function available in flight, during autopilot operation?. Speed stability function is not available during autopilot operation. Computed air speed from ADIRU and SAARU and pitch trim signal from ACE or AIMS. Computed air speed from ADIRU or SAARU and pitch trim signal from ACE and AIMS.

(ATA 27) Which flight control surface is used for roll control at cruise speed?. Flaperons normally and ailerons using limited trim control only. Ailerons and flaperons. Flaperons only, ailerons locked in faired position.

(ATA 27) What is the function of the autoslat priority valve during landing gear operation?. It gives priority of the centre hydraulics to the flaps and slats. It has no effect during landing gear operation. It gives priority the left hydraulic system to the slats.

12. (ATA 27) What will happen when the aircraft is in the air with the autopilot engaged and the pilot operates the control column pitch trim switches?. Stab trim will be corrected and autopilot takes control after trim correction. The trim signal is ignored and the autopilot stays engaged. Pilot will take take full control of the aircraft.

(ATA 27) During autopilot operation, the aileron trim does not work. What is the problem?. The Ailerons trim actuator is faulty. No fault - its normal operation of the system. The actuator control electronics (ACE) is faulty.

(ATA 27) What is the necessary condition for right STCM operation?. R and L2 ACEs available. R and C ACEs available. C and L1 ACEs available.

(ATA 27) What is the indication for sheared primary pin of the inboard support fap?. Flaps caution message shows on the status display. Spring loaded door at inboard fap outboard fairing opens. Flaps status message shows on the status display.

(ATA 27) Which flight control surfaces are made of aluminum skins and ribs7. Flaps and slats. Elevators. Slats.

(ATA 32) Where is the MGSCU, (Main Gear Steering Control Unit), located?. On the E6 rack in the Aft Cargo Hold. In the RH MLG Bay. On the E5 rack in the MEC.

(ATA27) Which of the listed flight controls surfaces skin is reinforced graphite/epoxy bonded to a core of Nomex honeycomb?. Slats and Rudder. Elevators and Rudder. Elevators and slats.

(ATA 32) How can the MLG steering system be disabled: A manual shutoff valve handle on the main landing gear steering PCA. An action through the MAT. Inserting a pin in the MLG steering torsion bar.

(ATA 32) What does the P1 amber brake source indication show?. Brake accumulator pressure low. The braking system is in the alternate mode of operation. Normal and alternate brake system pressures low.

(ATA 32) Which of the following statements is correct? The Nose Gear steering tiller inputs turn the Nose Gear up to. 65 degrees in each direction and rudder pedals up to 15 degrees in each direction. 72 degrees in each direction and NO rudder pedal input is available. 70 degrees in each direction, the rudder pedals up to 7 degrees in each direction.

(ATA 32) Which of the following statements is correct? The MLG steering manual shut of valve permits the system to be: Hydraulically powered on the ground. Hydraulically unpowered. Electrically disabled on the steering control valves.

(ATA27) Airplane on the ground. Which conditions are required for the flaps/slat secondary mode becomes active?. Override function on the MAT. One lane is faulty. Secondary mode not available on ground.

(ATA 27) When one hydraulic motor operates, What is the speed of the ballscrew of the speed when both hydraulic motors operate?. 50 percent. 75 percent. 100 percent.

(ATA 27) What sensor use The FSEUs for to shutdown the primary mode?. Flap skew sensors. Flap position sensors. The flap/slat priority valve.

(ATA 32) Where do the weight on wheel, (WOW), cards receive their information from?. Weight On Ground switches on the shock struts. Truck Levelling sensors. Load sensors on each MLG structure beams.

(ATA 32) With center hydraulic system low quantity, how is the reserve brakes and Nose wheel steering systems protected?. Reserve brakes and Nose wheel steering uses brake accumulator pressure. The hydraulic system control isolates the output of C1 ACMP for brakes. The RAT will auto deploy.

(ATA 32) What does the ELMS auto- off relay execute?. Removes the power of the UP solenoid and the selector moves to OFF to removed. Operates the control lever lock solenoid during the air/ground changeover. Operate the control lever lock solenoid on the ground to lock lever in down position.