13694588
Descripción
Test por David Nunez, actualizado hace más de 1 año
|
Creado por David Nunez
hace casi 6 años
|
|
Pregunta 1
Pregunta
Q1. The possible classifications in a warning, according to the priority are:
Respuesta
-
Warning, Caution and Advisory
-
Warning, Caution and Peace
-
Fire Fire, Warning and Caution
-
All are false
Pregunta 2
Pregunta
Q2. The possible classifications in a warning, according to the presentation are:
Respuesta
-
Visual
-
Acoustic
-
Mechanical
-
All are true
Pregunta 3
Pregunta
Q3. The components of altimeter alerting system are:
Respuesta
-
Servo altimeter and alerting unit
-
Altimeter and alerting unit
-
Alerting unit and cancel button
-
All are false
Pregunta 4
Pregunta
Q4. The ground proximity warning systems has:
Respuesta
-
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)
Pregunta 5
Pregunta
Q5. The Mode 2 of the GPWS use:
Respuesta
-
Mode 2A, Mode 2B and Mode 2C
-
Mode 2A
-
Mode 2A and Mode 2B
-
Mode 2X and Mode 2Y
Pregunta 6
Pregunta
Q6. The TCAS, Traffic Collision Avoidance System, provides traffic information within approximately:
Respuesta
-
30 miles
-
8 miles
-
60 miles
-
45 miles
Pregunta 7
Pregunta
Q7. The levels of capability or TCAS are:
Respuesta
-
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
Pregunta 8
Pregunta
Q8. About the ACAS (Airborne Collision Avoidance System):
Respuesta
-
A. TCAS II + Software v7 = ACAS II
-
B. TCAS IV = ACAS III
-
C. TCAS III = ACAS III
-
D. A and B are true
Pregunta 9
Pregunta
Q1. TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS)...
Respuesta
-
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
Pregunta 10
Pregunta
Q2. Operation of TCAS:
Respuesta
-
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
Pregunta 11
Pregunta
Q3. MACH/AIRSPEED WARNING SYSTEM
Respuesta
-
It advises when exceeding Vmo or Mmo
-
It only uses aural (acoustic) warnings
-
It only uses visual warnings
-
All the above are true
Pregunta 12
Pregunta
Q4. FLIGHT DATA RECORDER
Respuesta
-
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
Pregunta 13
Pregunta
Q5. COCKPIT VOICE RECORDER (CVR) REQUIREMENTS ARE
Respuesta
-
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
Pregunta 14
Pregunta
Q6. CVR records, among other things,
Respuesta
-
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
Pregunta 15
Pregunta
Q7. Regarding directional aerials in TCAS:
Respuesta
-
There must be at least 1 at fuselage top
-
Can exist at fuselage bottom
-
A and B are true
-
A and B are false
Pregunta 16
Pregunta
Q8. Stall warning presentation methods are:
Respuesta
-
Visual (red lights)
-
Aural (beep or message "STALL")
-
Stick shakers
-
All of the above are true
Pregunta 17
Pregunta
Q1. Flight and navigation instrument regulation appears in
Respuesta
-
JAR 25
-
JAR 23
-
JAR 21
-
JAR OPS 1
Pregunta 18
Pregunta
Q2. The red color is used to
Respuesta
-
Max and min values
-
Normal operation values
-
Take off, caution or exceptional values
-
Certain limitations
Pregunta 19
Pregunta
Q3. The EPR Engine Pressure Ratio is used for
Respuesta
-
Measurement of the useful thrust
-
Horsepower developed
-
Measurement of the aircraft pressure
-
The interference between the front and rear wings
Pregunta 20
Pregunta
Q4. Magnetic drag is
Respuesta
-
A. Similar to car tachometers
-
B. Used in light aircrafts
-
C. Separated due to centrifugal force
-
D. A and B are correct
Pregunta 21
Pregunta
Q5. Load selector display unit
Respuesta
-
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
Pregunta 22
Pregunta
Q6. The flight warning computer
Respuesta
-
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
Pregunta 23
Pregunta
Q7. ECAM is
Respuesta
-
A. Designed by airbus
-
B. Displays corrective action to be taken during failures
-
C. Designed by boeing
-
D. A and B are correct
Pregunta 24
Pregunta
Q8. EICAS is
Respuesta
-
A. Designed by boeing
-
B. Data not always neccesarily shown
-
C. Designed by airbus
-
D. A and B are correct
Pregunta 25
Pregunta
Q1. Regarding EICAS crew alerting, alert message levels can be:
Respuesta
-
Level A (RED): Advisories
-
Level B (RED): Warnings
-
Level B (AMBER): Cautions
-
All of above are false
Pregunta 26
Pregunta
Q2. Regarding ECAM (E/W display), which information can be shown:
Respuesta
-
Primary engine parameters (N1, fuel flow, EGT,...)
-
Flaps and slats position
-
Warning and caution messages
-
All of the above are true
Pregunta 27
Pregunta
Q3. The ECAM (S/S display), which information can be shown:
Respuesta
-
A. Electrical
-
B. Hydraulic
-
C. Primary engine parameters (N1, EGT, ...)
-
D. A and B are true
Pregunta 28
Pregunta
Q4. ECAM system failure
Respuesta
-
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
Pregunta 29
Pregunta
Q5. About ECAM (a) and EICAS (b):
Respuesta
-
(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
Pregunta 30
Pregunta
Q6. About ECAM (a) and EICAS (b):
Respuesta
-
(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
Pregunta 31
Pregunta
Q7. About ECAM (a) and EICAS (b):
Respuesta
-
(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
Pregunta 32
Pregunta
Q8. About ECAM (a) and EICAS (b):
Respuesta
-
(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
¿Quieres crear tus propios Tests gratis con GoConqr? Más información.