Q1. The possible classifications in a warning, according to the priority are:
Warning, Caution and Advisory
Warning, Caution and Peace
Fire Fire, Warning and Caution
All are false
Q2. The possible classifications in a warning, according to the presentation are:
Visual
Acoustic
Mechanical
All are true
Q3. The components of altimeter alerting system are:
Servo altimeter and alerting unit
Altimeter and alerting unit
Alerting unit and cancel button
Q4. The ground proximity warning systems has:
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)
Q5. The Mode 2 of the GPWS use:
Mode 2A, Mode 2B and Mode 2C
Mode 2A
Mode 2A and Mode 2B
Mode 2X and Mode 2Y
Q6. The TCAS, Traffic Collision Avoidance System, provides traffic information within approximately:
30 miles
8 miles
60 miles
45 miles
Q7. The levels of capability or TCAS are:
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
Q8. About the ACAS (Airborne Collision Avoidance System):
A. TCAS II + Software v7 = ACAS II
B. TCAS IV = ACAS III
C. TCAS III = ACAS III
D. A and B are true
Q1. TRAFFIC COLLISION AVOIDANCE SYSTEM (TCAS)...
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
Q2. Operation of TCAS:
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
Q3. MACH/AIRSPEED WARNING SYSTEM
It advises when exceeding Vmo or Mmo
It only uses aural (acoustic) warnings
It only uses visual warnings
All the above are true
Q4. FLIGHT DATA RECORDER
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
Q5. COCKPIT VOICE RECORDER (CVR) REQUIREMENTS ARE
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
Q6. CVR records, among other things,
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
Q7. Regarding directional aerials in TCAS:
There must be at least 1 at fuselage top
Can exist at fuselage bottom
Q8. Stall warning presentation methods are:
Visual (red lights)
Aural (beep or message "STALL")
Stick shakers
Q1. Flight and navigation instrument regulation appears in
JAR 25
JAR 23
JAR 21
JAR OPS 1
Q2. The red color is used to
Max and min values
Normal operation values
Take off, caution or exceptional values
Certain limitations
Q3. The EPR Engine Pressure Ratio is used for
Measurement of the useful thrust
Horsepower developed
Measurement of the aircraft pressure
The interference between the front and rear wings
Q4. Magnetic drag is
A. Similar to car tachometers
B. Used in light aircrafts
C. Separated due to centrifugal force
D. A and B are correct
Q5. Load selector display unit
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
Q6. The flight warning computer
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
Q7. ECAM is
A. Designed by airbus
B. Displays corrective action to be taken during failures
C. Designed by boeing
Q8. EICAS is
A. Designed by boeing
B. Data not always neccesarily shown
C. Designed by airbus
Q1. Regarding EICAS crew alerting, alert message levels can be:
Level A (RED): Advisories
Level B (RED): Warnings
Level B (AMBER): Cautions
All of above are false
Q2. Regarding ECAM (E/W display), which information can be shown:
Primary engine parameters (N1, fuel flow, EGT,...)
Flaps and slats position
Warning and caution messages
Q3. The ECAM (S/S display), which information can be shown:
A. Electrical
B. Hydraulic
C. Primary engine parameters (N1, EGT, ...)
Q4. ECAM system failure
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
Q5. About ECAM (a) and EICAS (b):
(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
Q6. About ECAM (a) and EICAS (b):
(a) data is always shown in checklist and scheme
(b) data may not be shown if it is not necessary
Q7. About ECAM (a) and EICAS (b):
(a) shows a corrective action when there is a failure
(b) does not show a corrective action when there is failure
Q8. About ECAM (a) and EICAS (b):
(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
