RST 2 Tech Examination PDF

29/12/2023, 21:35 Technical Examination Welcome  Blaithin Wilson Search Home / Courses / Flight Crew Training / Recurrent Training / RST 2 2022/23 / Started on State Completed on Time taken Question 1 Correct / Technical Examination Thursday, 30 March 2023, 9:39 PM Finished Thursday, 30 Mar...

29/12/2023, 21:35 Technical Examination Welcome  Blaithin Wilson Search Home / Courses / Flight Crew Training / Recurrent Training / RST 2 2022/23 / Started on State Completed on Time taken Question 1 Correct / Technical Examination Thursday, 30 March 2023, 9:39 PM Finished Thursday, 30 March 2023, 10:03 PM 23 mins 38 secs Which statement is correct when on the ground, with the BAT switch positioned to OFF and the STANDBY POWER Switch positioned to BAT? Marked out of 4.00 Select one: The Switched Hot Battery Bus is powered by the Battery. The Switched Hot Battery Bus is not powered.  The Switched Hot Battery Bus is powered by TR 3. The Switched Hot Battery Bus is powered by the Hot Battery Bus. Question 2 Which bus supplies electrical power to the main battery charger? Correct Marked out of 4.00 Select one: Transfer bus 1 Transfer bus 2 AC ground service bus 1 AC ground service bus 2  Question 3 Under normal conditions, from where is the AC standby bus powered? Correct Marked out of 4.00 Select one: a. The batteries via the static inverter. b. TR1, TR2 and TR3. c. AC transfer bus 2. d. AC transfer bus 1.  https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 1/7 29/12/2023, 21:35 Question 4 Technical Examination Which statement is true when the STANDBY POWER Switch is selected to OFF (the center position)? Correct Marked out of 4.00 Select one: The Static Inverter provides 28 volt DC power to Transfer Bus No 1. The 'STANDBY PWR OFF' light will extinguish. Automatic switching is provided from normal power sources to alternate power sources. The 'STANDBY PWR OFF' light will illuminate (amber).  Question 5 Where is the GROUND SERVICE Switch located? Correct Marked out of 4.00 Select one: On the Aft Attendant´s panel On the Forward Attendant´s panel  In the external AC power receptacle located on the lower right side of the fuselage. On the Aft Overhead panel on the Flight Deck https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 2/7 29/12/2023, 21:35 Question 6 Technical Examination When will the ELEC Light illuminate on the ground? Correct Marked out of 4.00 Select one: When a fault exists in the AC or standby power system. When a fault exists in the AC, DC or the standby system. When a fault exists in the DC or standby system.  The ELEC light only operates in flight. Question 7 Under what conditions can the APU generator can supply both transfer busses? Correct Marked out of 4.00 Select one: a. Both on the ground or in flight.  b. On the ground only. c. It cannot supply both transfer busses simultaneously. d. In flight only. Question 8 After the loss of all generators, how long can two fully charged batteries provide standby power for? Correct Marked out of 4.00 Select one: a. A minimum of 60 minutes.  b. Maximum of 30 minutes. c. A minimum of 120 minutes. d. A minimum of 12 minutes per battery. https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 3/7 29/12/2023, 21:35 Question 9 Technical Examination With the AUTO BRAKE select switch positioned to RTO, when will autobraking be initiated? Correct Marked out of 4.00 Select one: a. When wheel speed is 88 knots or more and the thrust levers are retarded to IDLE.  b. When the AUTO BRAKE DISARM light is illuminated, wheel speed is 88 knots or more and the thrust levers are retarded to IDLE. c. Automatically when the thrust levers are retarded to IDLE d. When wheel speed is 60 knots or less and the thrust levers are retarded to IDLE. Question 10 Correct In the event of a total loss of pressure in a Hydraulic System A, B and the Standby System in flight, will the brakes function on landing? Marked out of 4.00 Select one: No, as the brakes are supplied by Hydraulic system A. No, as the brakes are supplied by Hydraulic System B Yes, the hydraulic power will be supplied by the Brake System Accumulator  No, unless the Ram Air Turbine has been deployed Question 11 Correct When disarming the Autobrake System which of the following does NOT cause the AUTO BRAKE DISARM light to illuminate? Marked out of 4.00 Select one: a. Applying manual brakes. b. Positioning the AUTO BRAKE select switch to OFF.  c. Advancing the forward thrust levers after the first 3 seconds after touchdown. d. Moving the SPEED BRAKE lever to the DOWN detent. Question 12 Which of the following conditions must exist to arm the RTO mode prior to takeoff? Correct Marked out of 4.00 Select one: a. AUTO BRAKE select switch OFF. b. Wheel speed greater than 60 knots. c. Forward thrust levers positioned to IDLE.  d. AUTOBRAKE switch to MAX. https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 4/7 29/12/2023, 21:35 Question 13 Technical Examination What is the result if the thrust lever(s) are advanced during the first 3 seconds after touchdown? Correct Marked out of 4.00 Select one: The AUTO BRAKE DISARM light will not illuminate.  The AUTO BRAKE DISARM light will illuminate. The AUTO BRAKE SELECT switch will move to OFF. The AUTO BRAKE DISARM light will illuminate after 5 seconds . Question 14 What protection is provided during alternate brake operation? Correct Marked out of 4.00 Select one: a. Skid, locked wheel, touchdown and hydroplane.  b. Skid, locked wheel and hydroplane only. c. No protection is provided during alternate brake operation. d. Skid, and hydroplane only. Question 15 Correct Marked out of 4.00 Which statement is correct when selecting a landing autobrake setting after touchdown? Select one: a. Autobrakes will initiate if selected prior to decelerating through 30 knots of groundspeed.  b. Autobrake action will occur only when both thrust levers are retarded to reverse thrust range. c. Autobrakes will arm after decelerating through 60 knots groundspeed. d. The AUTO BRAKE DISARM light will illuminate and autobrake application will not occur. Question 16 Which statement is correct when selecting a landing autobrake setting after touchdown? Correct Marked out of 4.00 Select one: Autobrake action will occur only when thrust reverse is selected. Autobrakes will initiate if selected prior to decelerating through 30 knots of groundspeed.  Autobrakes will arm immediately at any groundspeed. The AUTO BRAKE DISARM light will illuminate and autobrake application will not occur. Question 17 Will Yaw Damper inputs to the rudder cause the rudder pedals to move? Correct Marked out of 4.00 Select one: Yes - but only if the standby rudder PCU is operating No  Yes - but only if rudder trim is applied Yes - but only when the yaw damper switch is off. https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 5/7 29/12/2023, 21:35 Question 18 Technical Examination What protection does the flap/slat electronics unit (FSEU) provide? Correct Marked out of 4.00 Select one: a. LE skew detection for slats 1 through 8. b. Slat and skew protection during auto-slat operation c. Protection from uncommanded motion, for LE devices if two or more slats on one wing move from the commanded position.  d. Skew detection for LE flaps Question 19 What is the maximum permitted lever position of the speed brake lever in flight? Correct Marked out of 4.00 Select one: FLIGHT DETENT  DOWN (Speed brake use is prohibited in flight). ARMED UP Question 20 Which statement is true for the Autoslat system? Correct Marked out of 4.00 Select one: a. The Autoslat system drives the slats to the full extended position when the LE slats are in the extend position as the aircraft approaches the stall angle.  b. The Autoslat system uses the FSEU to protect the slats from excessive air loads. c. The Autoslats are normally powered by hydraulic system A. d. The Autoslats are operated electrically in the event that hydraulic system B fails. Question 21 Why are mechanical gates installed at Flap 15 and Flap 1 on the flap selector unit? Correct Marked out of 4.00 Select one: a. To hinder inadvertent flap lever movement beyond Flaps 1 and Flaps 15 during a go-around.  b. To hinder flap movement beyond Flaps 15 until gear down is selected. c. To hinder flap movement to the UP position when speed is too low. d. Has no particular function. Question 22 Above what speed will the Mach Trim System operate? Correct Marked out of 4.00 Select one: a. Mach .615  b. Mach .505 c. Mach .555 d. Mach .455 https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 6/7 29/12/2023, 21:35 Question 23 Technical Examination With reference to the illumination of the LE FLAPS TRANSIT light, which statement is correct? Correct Marked out of 4.00 Select one: a. Indicates LE Slats are fully extended. b. Indicates that TE Flaps asymmetry protection is being provided. c. Indicates all LE Devices are fully extended. d. Is inhibited during Autoslat operation in flight.  Question 24 Correct Which statement is correct for a loss of hydraulic system B (system A operating normally), and no switches have been repositioned yet? Marked out of 4.00 Select one: a. Standby Yaw Damper functions with "A" FLT CONTROL switch in STDY RUD and Yaw Damper switch ON. b. Standby Yaw Damper is available. c. Main and Standby Yaw Dampers are not available.  d. Main Yaw Damper function is available. Question 25 In addition to Hydraulic System A and B, how else can the rudder be powered? Correct Marked out of 4.00 Select one: Standby hydraulic system through the Standby Rudder PCU.  Standby hydraulic system through the Main Rudder PCU. System B powering the Standby Rudder PCU. System A powering the Standby Rudder PCU. https://fopstraining.ryanair.com/mod/quiz/review.php?attempt=1683178&cmid=9121 7/7