preparar

(ATA 32) When doesthe DOORS amber warning light on the P3-1 panel come on?. A. When system 1 or system 2 sensor is not open. B. When system 1 and system 2 door sensor is not open. C. When system 1 and system 2 door sensor is not closed.

(ATA 32) What does the PSEU TARGET TEST do?. A. Checks if the selected sensor is operational. B. Makes sure the sensor installation is correct. C. Provides a way to calibrate the sensor.

(ATA 32) How many degrees must the nose steering tiller be rotated to cause maximum nose wheel steering angle?. A. 360 degrees. B. 65 degrees. C. 180 degrees.

(ATA 32) Which one of the following inputs can provide Nose Wheels steering 65 degree?. A. Tiller. B. Control wheel. C. Pedais.

(ATA 32) Which of the following statements indicates that the auto brak armed and operative?. A. The Auto Brakes selector latches at the selected deceleration position. B. The Auto Brakes ARMED light is on. C. The Auto Brakes EICAS message is displayed.

(ATA 32) Where is the brake temperature indication displayed?. A. EICAS Elec/hyd page. B. EICAS ECS/MSG page. C. EICAS Status page.

(ATA 32) The "BRAKE SOURCE light (P1-3) and an EICAS message is ON. What does it. A. The right hydraulic system has Low Pressure. B. No active "Brake Source" is available. C. The selected "Brake Source" haslow hydraulic pressure strut?.

(ATA 32) Which of the following components is used to pressurize the nose gear shock. A. The charging valve at the top of the strut. B. Port on the lower left side of the outer cylinder. C. A check valve assembly at the bottom of the strut.

(ATA 32) What isthe function of NG steering cable compensator mechanism?. A. Protect the NG lower steering cable loop from one side hardover if upper steering cable loop breaks. B. Center the steering drum when the NG is extended to make the NG wheels straight. C. Compensate the NG steering cables tension variations with temperature changes.

(ATA 27) The primary flight controls are moved by: A. 14 electrically operated power control units with no manual reversion. B. 21 hydraulically operated power control units with manual reversion. C. 29 hydraulically operated power control units with no manual reversion.

(ATA 27) Which control mode of the horizontal stabilizer does not utilize the SAM?. A. Speed trim. B. Alternate electric trim. C. Manual electric trim.

(ATA 27) What is used for detection of flap asymmetry?. A. 8 flap position transmitters. B. 8 proximity sensors. C. 2 flap position sensors.

(ATA 27) The lockout mechanism prevents operation of?. A. OUTBOARD AILERON DURING HIGH SPEED CONDITIONS THROUGH ELECTRONIC CONTROL. B. INBOARD AILERONS DURING HIGH SPEED CONDITIONS BY BLOCKING HYDRAULIC FLUID TO THE PCAS. C. OUTBOARD AILERONS WHEN TRAILING EDGE FLAPS ARE BEING RETRACTED THOUGH THE GEARBOX.

(ATA 27) What is the elevator travel in autopilot mode with two channels engaged?. A. 10º up and 8.3° down. B. 28º up and 20º down. C. 8.3° up and down.

(ATA 27) What is the meaning of advisory EICAS message FLAP LOAD RELIEF?. A. Flap Load Relief occurred - flaps retracted as they should. B. Flap Load Relief speed approaching. C. Flap Load Relief system failed - flaps did not retract at a retraction speed.

(ATA 27) What isthe purpose of the aileron lockout mechanism?. A. Lock out a faulty aileron. B. Lock out the inboard ailerons at low speed. C. Lock out the outboard ailerons at high speed.

(ATA 32) When is the NG door position monitored?. A. When the gear retracts. B. When the gear extends. C. When the gear lever is in the down position.

(ATA 27) FSEU (flap/slat electronic unit) receives slat position fault data from: A. PSEU (proximity switch electronics unit). B. FSPM (flap stabilizer position module). C. LSPM (limit switch and position transmitter module).

(ATA 27) Which of the following is NOT a function of the control surface electronics unit (CSEU)?. A. Yaw damping. B. Spoiler deployment. C. Elevator control.

(ATA 27) What is the neutral position of the stabilizer?. A. 2 units. B. 2 degrees. C. 0 units.

(ATA 27) What is the autopilot control authority to the rudder?. A. 23° during autoland. B. 16.8º at low speed. C. 26.5º at low speeds.

(ATA 27) The horizontal stabilizer operates in full trim rate: A. In auto trim mode. B. In manual trim mode. C. In mach trim mode.

(ATA 27) RH elevator position pointer on EICAS status page disappeared. What is the. A. F/O's instrument transfer bus unpowered. B. RH elevator position transmitter failed. C. RH engine oil pressure reference power lost.

(ATA 27) If a jam occurs in the right elevator control system, what forces will be felt on. A. Override forces from aft quadrant override and half of hydraulic feel force. B. All hydraulic feel force, override forces from column and aft quadrant overrides. overrides. C. All hydraulic feel forces, all mechanical forces, override forces from column and aft quadrant.

(ATA 27) Flap position indicator needles are at 1 unit. What is the position of high lift devices?. A. LE slats are retracted, TE flaps are in 1 unit position. B. LE slats are in take off position, TE flaps are in 1 unit position. C. LE slats are in take off position, TE flaps are retracted.

(ATA 27) SCM management monitor(MM) card detected error in model card only. What is the MM card decision?. A. Shutdown decision, PCA is shutdown, causing to shutdown the symmetric PCA. B. Inhibit decision, PCA continues to operate with active channel. C. Switch decision, PCA continues to operate with standby channel.

(ATA 27) Horizontal stabilizer position indicator displays indication tape in black. What does it mean?. A. Input signal from drive synchro to indicator is lost. B. Stabilizer position signal voltage is not valid. C. No power to stabilizer position indicator.

(ATA 27) How do you initiate Yaw Damper System test?. A. By activating test switch on yaw damper module. B. By activating switch on P5. C. By activating test switch on P61 panel.