Quiz by David Nunez, created more than 1 year ago

Quiz on UD4. L15-18 2015__2, created by David Nunez on 11/05/2018.

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	Created by David Nunez almost 6 years ago

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UD4. L15-18 2015__2

Question 1 of 32

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Q1. The possible classifications in a warning, according to the priority are:

Select one of the following:

Warning, Caution and Advisory
Warning, Caution and Peace
Fire Fire, Warning and Caution
All are false

Explanation

Question 2 of 32

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Q2. The possible classifications in a warning, according to the presentation are:

Select one of the following:

Visual
Acoustic
Mechanical
All are true

Explanation

Question 3 of 32

1

Q3. The components of altimeter alerting system are:

Select one of the following:

Servo altimeter and alerting unit
Altimeter and alerting unit
Alerting unit and cancel button
All are false

Explanation

Question 4 of 32

1

Q4. The ground proximity warning systems has:

Select one of the following:

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)

Explanation

Question 5 of 32

1

Q5. The Mode 2 of the GPWS use:

Select one of the following:

Mode 2A, Mode 2B and Mode 2C
Mode 2A
Mode 2A and Mode 2B
Mode 2X and Mode 2Y

Explanation

Question 6 of 32

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Q6. The TCAS, Traffic Collision Avoidance System, provides traffic information within approximately:

Select one of the following:

30 miles
8 miles
60 miles
45 miles

Explanation

Question 7 of 32

1

Q7. The levels of capability or TCAS are:

Select one of the following:

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

Explanation

Question 8 of 32

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Q8. About the ACAS (Airborne Collision Avoidance System):

Select one of the following:

A. TCAS II + Software v7 = ACAS II
B. TCAS IV = ACAS III
C. TCAS III = ACAS III
D. A and B are true

Explanation

Question 9 of 32

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Q1. TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS)...

Select one of the following:

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

Explanation

Question 10 of 32

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Q2. Operation of TCAS:

Select one of the following:

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

Explanation

Question 11 of 32

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Q3. MACH/AIRSPEED WARNING SYSTEM

Select one of the following:

It advises when exceeding Vmo or Mmo
It only uses aural (acoustic) warnings
It only uses visual warnings
All the above are true

Explanation

Question 12 of 32

1

Q4. FLIGHT DATA RECORDER

Select one of the following:

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

Explanation

Question 13 of 32

1

Q5. COCKPIT VOICE RECORDER (CVR) REQUIREMENTS ARE

Select one of the following:

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

Explanation

Question 14 of 32

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Q6. CVR records, among other things,

Select one of the following:

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

Explanation

Question 15 of 32

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Q7. Regarding directional aerials in TCAS:

Select one of the following:

There must be at least 1 at fuselage top
Can exist at fuselage bottom
A and B are true
A and B are false

Explanation

Question 16 of 32

1

Q8. Stall warning presentation methods are:

Select one of the following:

Visual (red lights)
Aural (beep or message "STALL")
Stick shakers
All of the above are true

Explanation

Question 17 of 32

1

Q1. Flight and navigation instrument regulation appears in

Select one of the following:

JAR 25
JAR 23
JAR 21
JAR OPS 1

Explanation

Question 18 of 32

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Q2. The red color is used to

Select one of the following:

Max and min values
Normal operation values
Take off, caution or exceptional values
Certain limitations

Explanation

Question 19 of 32

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Q3. The EPR Engine Pressure Ratio is used for

Select one of the following:

Measurement of the useful thrust
Horsepower developed
Measurement of the aircraft pressure
The interference between the front and rear wings

Explanation

Question 20 of 32

1

Q4. Magnetic drag is

Select one of the following:

A. Similar to car tachometers
B. Used in light aircrafts
C. Separated due to centrifugal force
D. A and B are correct

Explanation

Question 21 of 32

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Q5. Load selector display unit

Select one of the following:

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

Explanation

Question 22 of 32

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Q6. The flight warning computer

Select one of the following:

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

Explanation

Question 23 of 32

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Q7. ECAM is

Select one of the following:

A. Designed by airbus
B. Displays corrective action to be taken during failures
C. Designed by boeing
D. A and B are correct

Explanation

Question 24 of 32

1

Q8. EICAS is

Select one of the following:

A. Designed by boeing
B. Data not always neccesarily shown
C. Designed by airbus
D. A and B are correct

Explanation

Question 25 of 32

1

Q1. Regarding EICAS crew alerting, alert message levels can be:

Select one of the following:

Level A (RED): Advisories
Level B (RED): Warnings
Level B (AMBER): Cautions
All of above are false

Explanation

Question 26 of 32

1

Q2. Regarding ECAM (E/W display), which information can be shown:

Select one of the following:

Primary engine parameters (N1, fuel flow, EGT,...)
Flaps and slats position
Warning and caution messages
All of the above are true

Explanation

Question 27 of 32

1

Q3. The ECAM (S/S display), which information can be shown:

Select one of the following:

A. Electrical
B. Hydraulic
C. Primary engine parameters (N1, EGT, ...)
D. A and B are true

Explanation

Question 28 of 32

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Q4. ECAM system failure

Select one of the following:

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

Explanation

Question 29 of 32

1

Q5. About ECAM (a) and EICAS (b):

Select one of the following:

(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

Explanation

Question 30 of 32

1

Q6. About ECAM (a) and EICAS (b):

Select one of the following:

(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

Explanation

Question 31 of 32

1

Q7. About ECAM (a) and EICAS (b):

Select one of the following:

(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

Explanation

Question 32 of 32

1

Q8. About ECAM (a) and EICAS (b):

Select one of the following:

(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

Explanation