Aeroversity Random Mock Exam 2 Flashcards
The ICAO PANS-OPS Doc 8168 gives guidelines for flight procedures to be used:
A
For all normal procedures, contingency procedures for abnormal occurrences are expected to be formulated by the operator
B
For all normal and abnormal and emergency procedures for flight crew in commercial operations
C
For aeroplanes and helicopters to be used in instrument conditions
D For RNAV(GNSS) operations only
A
For all normal procedures, contingency procedures for abnormal occurrences are expected to be formulated by the operator
In which situation is advection fog most likely to form?
A
A light breeze blowing colder air out to sea
B
A warm moist air mass on the windward side of the mountains
C
An air mass moving inland from the coast in winter
D
Warm moist air settling over a warmer surface under no-wind conditions
C
An air mass moving inland from the coast in winter
The formation of morning fog before sunrise is possible if
(1 mark)
A
there is moderate turbulence in the lower layers of the atmosphere
B
air temperature and dew point are close to one another
C
warm, moisture laden air is carried over cold coastal waters or coastal headlands
D
the sky is overcast
B
air temperature and dew point are close to one another
A benefit of an Electronic Flight Display for instrument flying is that:
(1 mark)
A
The tendency for a pilot to over control is minimized
B
Its larger size makes very small pitch corrections possible
C
Information is presented in less concentrated form
D
A 45° bank angle marking has been added to the roll index
E
Airspeed indications are more readable in analogue format
B
Its larger size makes very small pitch corrections possible
C
Information is presented in less concentrated form
An aeroplane leaving ground effect will:
A
experience a decrease in the thrust required
B
experience a decrease in stability and a nose up change in moments
C
require a lower angle of attack to attain the same lift coefficient
D
experience a decrease in induced drag
B
experience a decrease in stability and a nose up change in moments
In a mountain-valley wind circulation, the mountain wind blows
A
at night up from the valley
B
at night down from the mountains
C
during the day down from the mountains
D
during the day up from the valley
B
at night down from the mountains
For a pressurised aircraft, the first-aid oxygen is designed to:
A
protect all the occupants against the effects of accidental depressurisation
B
provide oxygen to 10% of passengers at a cabin altitude exceeding 13000 ft after 30 minutes
C
provide undiluted oxygen for passengers who, for physiological reasons, might require oxygen following a cabin depressurisation
D
protect the flight crew and cabin attendants against fumes and noxious gases
C
provide undiluted oxygen for passengers who, for physiological reasons, might require oxygen following a cabin depressurisation
Aerodrome lights may be turned off provided they can be brought into operation within ___ of the expected arrival of an aeroplane. Which answer correctly fills in the blank space?
A
15 mins
B
30 mins
C
1 hour
D
1 hour 30 mins
C
1 hour
When the intruding aircraft is equipped with a transponder without altitude reporting capability, the TCAS II issues a:
A
“traffic advisory”, vertical and horizontal “resolution advisory”
B
“traffic advisory” and horizontal “resolution advisory”
C
“traffic advisory” and vertical “resolution advisory”
D
“traffic advisory” only
D
“traffic advisory” only
The airspeed indicator of a twin-engine aircraft comprises different sectors and color markings. The blue line corresponds to the:
A
minimum control speed or Vmc
B
optimum climbing speed with one engine inoperative or Vyse
C
speed not to be exceeded or Vne
D
best rate of climb speed or Vy
B
optimum climbing speed with one engine inoperative or Vyse
At the commencement of final approach, if the controller possesses wind information in the form of components, significant changes in the mean surface wind direction and speed shall be transmitted to aircraft. The mean tailwind component significant change is:
A
3 KT
B
2 KT
C
4 KT
D
5 KT
B
2 KT
Given:
AD = Air distance
GD = Ground distance
TAS = True Airspeed
GS = Groundspeed
Which of the following is the correct formula to calculate ground distance (GD) gone?
A
GD = (AD X GS)/TAS
B
GD = AD X (GS -TAS)/GS
C
GD = TAS/(GS X AD)
D
GD = (AD - TAS)/TAS
A
GD = (AD X GS)/TAS
An aeroplane is loaded with its centre of gravity towards the rear limit. This will result in:
A
An increased risk of stalling due to a decrease in tail plane moment
B
A reduced fuel consumption as a result of reduced drag
C
An increase in longitudinal stability
D
A reduction in power required for a given speed
A
An increased risk of stalling due to a decrease in tail plane moment
What is the deviation per dot on the HSI when using an EFIS 2-dot RNAV system in the EN ROUTE (ENR) mode?
A
10 NM
B
2 NM
C
1 NM
D
5 NM
B
2 NM
Which of the following lists information required to input a waypoint or ‘Phantom Station’ into a basic VOR/DME-based Area Navigation System?
A
Radial and distance from a VOR/DME to the waypoint or ‘Phantom Station’
B
Magnetic track and distance from the aircraft to the waypoint or ‘Phantom Station’
C
Magnetic track and distance to a VOR/DME from the waypoint or ‘Phantom Station’
D
Radials from a minimum of two VORs to the waypoint or ‘Phantom Station’
A
Radial and distance from a VOR/DME to the waypoint or ‘Phantom Station’
