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UD4. L15-18 2015__2

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Quiz on UD4. L15-18 2015__2, created by David Nunez on 11/05/2018.
David Nunez
Quiz by David Nunez, updated more than 1 year ago
David Nunez
Created by David Nunez almost 6 years ago
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Resource summary

Question 1

Question
Q1. The possible classifications in a warning, according to the priority are:
Answer
  • Warning, Caution and Advisory
  • Warning, Caution and Peace
  • Fire Fire, Warning and Caution
  • All are false

Question 2

Question
Q2. The possible classifications in a warning, according to the presentation are:
Answer
  • Visual
  • Acoustic
  • Mechanical
  • All are true

Question 3

Question
Q3. The components of altimeter alerting system are:
Answer
  • Servo altimeter and alerting unit
  • Altimeter and alerting unit
  • Alerting unit and cancel button
  • All are false

Question 4

Question
Q4. The ground proximity warning systems has:
Answer
  • 4 Modes (compulsory by JAR-OPS 1.665)
  • 3 Modes (compulsory by JAR-OPS 1.665)
  • 6 Modes (compulsory by JAR-OPS 1.665)
  • 5 Modes (compulsory by JAR-OPS 1.665)

Question 5

Question
Q5. The Mode 2 of the GPWS use:
Answer
  • Mode 2A, Mode 2B and Mode 2C
  • Mode 2A
  • Mode 2A and Mode 2B
  • Mode 2X and Mode 2Y

Question 6

Question
Q6. The TCAS, Traffic Collision Avoidance System, provides traffic information within approximately:
Answer
  • 30 miles
  • 8 miles
  • 60 miles
  • 45 miles

Question 7

Question
Q7. The levels of capability or TCAS are:
Answer
  • TCAS I, TCAS II and TCAS IV
  • TCAS I, TCAS II and TCAS III
  • TCAS X and TCAS Y
  • TCAS I, TCAS II, TCAS III and TCAS IV

Question 8

Question
Q8. About the ACAS (Airborne Collision Avoidance System):
Answer
  • A. TCAS II + Software v7 = ACAS II
  • B. TCAS IV = ACAS III
  • C. TCAS III = ACAS III
  • D. A and B are true

Question 9

Question
Q1. TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS)...
Answer
  • Provides traffic information within approximately 30 miles of the airplane
  • Information can be shown in a display
  • It usually uses acoustic warnings
  • All of the above are true

Question 10

Question
Q2. Operation of TCAS:
Answer
  • An aircraft transmit its identifier once per second in the form of an omni- directional broadcast known as squitter
  • When a squitter signal is detected, the identity of the transmitting aircraft is added to a List or Roll Call for subsequent interrogation
  • A and B are true
  • A and B are false

Question 11

Question
Q3. MACH/AIRSPEED WARNING SYSTEM
Answer
  • It advises when exceeding Vmo or Mmo
  • It only uses aural (acoustic) warnings
  • It only uses visual warnings
  • All the above are true

Question 12

Question
Q4. FLIGHT DATA RECORDER
Answer
  • It is never compulsory for commercial aircrafts
  • The data during at least 25 hours must be present
  • It records the voice of the pilots and the ambient sounds
  • All are true

Question 13

Question
Q5. COCKPIT VOICE RECORDER (CVR) REQUIREMENTS ARE
Answer
  • Record with reference to a common time scale
  • Retaining data recorded during at least the last 2 hours of operation
  • Automatically starts to record
  • All of the above and a device to assist location in water

Question 14

Question
Q6. CVR records, among other things,
Answer
  • Voice communications transmitted or received on the flight deck by radio
  • Voice or audio signals identifying navigation or approach aids introduced into a headset or speaker
  • Both A and B are true
  • Both A and B are false

Question 15

Question
Q7. Regarding directional aerials in TCAS:
Answer
  • There must be at least 1 at fuselage top
  • Can exist at fuselage bottom
  • A and B are true
  • A and B are false

Question 16

Question
Q8. Stall warning presentation methods are:
Answer
  • Visual (red lights)
  • Aural (beep or message "STALL")
  • Stick shakers
  • All of the above are true

Question 17

Question
Q1. Flight and navigation instrument regulation appears in
Answer
  • JAR 25
  • JAR 23
  • JAR 21
  • JAR OPS 1

Question 18

Question
Q2. The red color is used to
Answer
  • Max and min values
  • Normal operation values
  • Take off, caution or exceptional values
  • Certain limitations

Question 19

Question
Q3. The EPR Engine Pressure Ratio is used for
Answer
  • Measurement of the useful thrust
  • Horsepower developed
  • Measurement of the aircraft pressure
  • The interference between the front and rear wings

Question 20

Question
Q4. Magnetic drag is
Answer
  • A. Similar to car tachometers
  • B. Used in light aircrafts
  • C. Separated due to centrifugal force
  • D. A and B are correct

Question 21

Question
Q5. Load selector display unit
Answer
  • A. Digitally displays the amount of fuel
  • B. Allows the crew to select the amount of fuel to be refueled
  • C. Control the movements of the aircraft
  • D. A and C are correct

Question 22

Question
Q6. The flight warning computer
Answer
  • A. Acquire data, process and then distribute to the DMC
  • B. Generate alert messages
  • C. Generate the image displayed
  • D. B and C are correct

Question 23

Question
Q7. ECAM is
Answer
  • A. Designed by airbus
  • B. Displays corrective action to be taken during failures
  • C. Designed by boeing
  • D. A and B are correct

Question 24

Question
Q8. EICAS is
Answer
  • A. Designed by boeing
  • B. Data not always neccesarily shown
  • C. Designed by airbus
  • D. A and B are correct

Question 25

Question
Q1. Regarding EICAS crew alerting, alert message levels can be:
Answer
  • Level A (RED): Advisories
  • Level B (RED): Warnings
  • Level B (AMBER): Cautions
  • All of above are false

Question 26

Question
Q2. Regarding ECAM (E/W display), which information can be shown:
Answer
  • Primary engine parameters (N1, fuel flow, EGT,...)
  • Flaps and slats position
  • Warning and caution messages
  • All of the above are true

Question 27

Question
Q3. The ECAM (S/S display), which information can be shown:
Answer
  • A. Electrical
  • B. Hydraulic
  • C. Primary engine parameters (N1, EGT, ...)
  • D. A and B are true

Question 28

Question
Q4. ECAM system failure
Answer
  • Flight crew can manually switch the display functions to other units
  • Flight crew can't manually switch the display functions to other units
  • Only the captain can manually switch the display functions to other units
  • Only the first officer can manually switch the display functions to other units

Question 29

Question
Q5. About ECAM (a) and EICAS (b):
Answer
  • (a) is designed by Airbus and presents a centralised monitoring of the aircraft
  • (b) is designed by Boeing and presents engine indicators and crew alerts
  • A and B are true
  • A and B are false

Question 30

Question
Q6. About ECAM (a) and EICAS (b):
Answer
  • (a) data is always shown in checklist and scheme
  • (b) data may not be shown if it is not necessary
  • A and B are true
  • A and B are false

Question 31

Question
Q7. About ECAM (a) and EICAS (b):
Answer
  • (a) shows a corrective action when there is a failure
  • (b) does not show a corrective action when there is failure
  • A and B are true
  • A and B are false

Question 32

Question
Q8. About ECAM (a) and EICAS (b):
Answer
  • (a) errors are presented to the pilot which disappear once it is solved
  • (b) instrument readings are shown to the pilot, who has to interpret them
  • A and B are true
  • A and B are false
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