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Quiz von David Nunez, aktualisiert more than 1 year ago
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Erstellt von David Nunez
vor mehr als 6 Jahre
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Frage 1
Frage
Q1. The possible classifications in a warning, according to the priority are:
Antworten
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Warning, Caution and Advisory
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Warning, Caution and Peace
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Fire Fire, Warning and Caution
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All are false
Frage 2
Frage
Q2. The possible classifications in a warning, according to the presentation are:
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Visual
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Acoustic
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Mechanical
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All are true
Frage 3
Frage
Q3. The components of altimeter alerting system are:
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Servo altimeter and alerting unit
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Altimeter and alerting unit
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Alerting unit and cancel button
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All are false
Frage 4
Frage
Q4. The ground proximity warning systems has:
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4 Modes (compulsory by JAR-OPS 1.665)
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3 Modes (compulsory by JAR-OPS 1.665)
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6 Modes (compulsory by JAR-OPS 1.665)
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5 Modes (compulsory by JAR-OPS 1.665)
Frage 5
Frage
Q5. The Mode 2 of the GPWS use:
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Mode 2A, Mode 2B and Mode 2C
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Mode 2A
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Mode 2A and Mode 2B
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Mode 2X and Mode 2Y
Frage 6
Frage
Q6. The TCAS, Traffic Collision Avoidance System, provides traffic information within approximately:
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30 miles
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8 miles
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60 miles
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45 miles
Frage 7
Frage
Q7. The levels of capability or TCAS are:
Antworten
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TCAS I, TCAS II and TCAS IV
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TCAS I, TCAS II and TCAS III
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TCAS X and TCAS Y
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TCAS I, TCAS II, TCAS III and TCAS IV
Frage 8
Frage
Q8. About the ACAS (Airborne Collision Avoidance System):
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A. TCAS II + Software v7 = ACAS II
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B. TCAS IV = ACAS III
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C. TCAS III = ACAS III
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D. A and B are true
Frage 9
Frage
Q1. TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS)...
Antworten
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Provides traffic information within approximately 30 miles of the airplane
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Information can be shown in a display
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It usually uses acoustic warnings
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All of the above are true
Frage 10
Frage
Q2. Operation of TCAS:
Antworten
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An aircraft transmit its identifier once per second in the form of an omni- directional broadcast known as squitter
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When a squitter signal is detected, the identity of the transmitting aircraft is added to a List or Roll Call for subsequent interrogation
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A and B are true
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A and B are false
Frage 11
Frage
Q3. MACH/AIRSPEED WARNING SYSTEM
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It advises when exceeding Vmo or Mmo
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It only uses aural (acoustic) warnings
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It only uses visual warnings
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All the above are true
Frage 12
Frage
Q4. FLIGHT DATA RECORDER
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It is never compulsory for commercial aircrafts
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The data during at least 25 hours must be present
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It records the voice of the pilots and the ambient sounds
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All are true
Frage 13
Frage
Q5. COCKPIT VOICE RECORDER (CVR) REQUIREMENTS ARE
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Record with reference to a common time scale
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Retaining data recorded during at least the last 2 hours of operation
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Automatically starts to record
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All of the above and a device to assist location in water
Frage 14
Frage
Q6. CVR records, among other things,
Antworten
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Voice communications transmitted or received on the flight deck by radio
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Voice or audio signals identifying navigation or approach aids introduced into a headset or speaker
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Both A and B are true
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Both A and B are false
Frage 15
Frage
Q7. Regarding directional aerials in TCAS:
Antworten
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There must be at least 1 at fuselage top
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Can exist at fuselage bottom
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A and B are true
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A and B are false
Frage 16
Frage
Q8. Stall warning presentation methods are:
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Visual (red lights)
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Aural (beep or message "STALL")
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Stick shakers
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All of the above are true
Frage 17
Frage
Q1. Flight and navigation instrument regulation appears in
Antworten
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JAR 25
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JAR 23
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JAR 21
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JAR OPS 1
Frage 18
Frage
Q2. The red color is used to
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Max and min values
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Normal operation values
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Take off, caution or exceptional values
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Certain limitations
Frage 19
Frage
Q3. The EPR Engine Pressure Ratio is used for
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Measurement of the useful thrust
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Horsepower developed
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Measurement of the aircraft pressure
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The interference between the front and rear wings
Frage 20
Frage
Q4. Magnetic drag is
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A. Similar to car tachometers
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B. Used in light aircrafts
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C. Separated due to centrifugal force
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D. A and B are correct
Frage 21
Frage
Q5. Load selector display unit
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A. Digitally displays the amount of fuel
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B. Allows the crew to select the amount of fuel to be refueled
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C. Control the movements of the aircraft
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D. A and C are correct
Frage 22
Frage
Q6. The flight warning computer
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A. Acquire data, process and then distribute to the DMC
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B. Generate alert messages
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C. Generate the image displayed
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D. B and C are correct
Frage 23
Frage
Q7. ECAM is
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A. Designed by airbus
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B. Displays corrective action to be taken during failures
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C. Designed by boeing
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D. A and B are correct
Frage 24
Frage
Q8. EICAS is
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A. Designed by boeing
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B. Data not always neccesarily shown
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C. Designed by airbus
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D. A and B are correct
Frage 25
Frage
Q1. Regarding EICAS crew alerting, alert message levels can be:
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Level A (RED): Advisories
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Level B (RED): Warnings
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Level B (AMBER): Cautions
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All of above are false
Frage 26
Frage
Q2. Regarding ECAM (E/W display), which information can be shown:
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Primary engine parameters (N1, fuel flow, EGT,...)
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Flaps and slats position
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Warning and caution messages
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All of the above are true
Frage 27
Frage
Q3. The ECAM (S/S display), which information can be shown:
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A. Electrical
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B. Hydraulic
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C. Primary engine parameters (N1, EGT, ...)
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D. A and B are true
Frage 28
Frage
Q4. ECAM system failure
Antworten
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Flight crew can manually switch the display functions to other units
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Flight crew can't manually switch the display functions to other units
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Only the captain can manually switch the display functions to other units
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Only the first officer can manually switch the display functions to other units
Frage 29
Frage
Q5. About ECAM (a) and EICAS (b):
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(a) is designed by Airbus and presents a centralised monitoring of the aircraft
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(b) is designed by Boeing and presents engine indicators and crew alerts
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A and B are true
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A and B are false
Frage 30
Frage
Q6. About ECAM (a) and EICAS (b):
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(a) data is always shown in checklist and scheme
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(b) data may not be shown if it is not necessary
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A and B are true
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A and B are false
Frage 31
Frage
Q7. About ECAM (a) and EICAS (b):
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(a) shows a corrective action when there is a failure
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(b) does not show a corrective action when there is failure
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A and B are true
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A and B are false
Frage 32
Frage
Q8. About ECAM (a) and EICAS (b):
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(a) errors are presented to the pilot which disappear once it is solved
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(b) instrument readings are shown to the pilot, who has to interpret them
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A and B are true
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A and B are false
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