ATP 04 Gerard 2020
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- 1.According with the Noise abatement T.O and climb procedure B , as establish in DOC 8168 Ops Volume 1 , part V A/C must climb at V2 + 10 to 20 Kt , until :
- A.
1500 ft
- B.
3000 ft
- C.
1000 ft
- D.
500 ft
- 2.To use passengers oxygen in case of severe cabin smoke is :
- A.
Useless because breathing oxygen would explode under smoke conditions
- B.
Possible and recommended
- C.
Useless because the topical cabin smoke is mixed with the breathing oxygen
- D.
Useless because the oxygen units do not operate under smoke conditions
- 3.During an A/C de icing / anti icing procedure
- A.
The anti-icing fluid is applied without heating and de --icing fluid is applied hot.
- B.
The anti-icing and de -icing fluids are applied hot.
- C.
The anti-icing and de -icing fluids are applied cold
- D.
The de--icing fluid is applied without heating and the anti-icing fluid is applied hot
- 4.A category III A precision approach (CAT III A) is an app wich may be carried out with a Wry visual range of at least :
- A.
200 m
- B.
100 m
- C.
250 m
- D.
50 m
- 5.For purpose of wake turbulence separation , what is the ICAO minimum radar separation time if a light aeroplanos (7000 kg ) is following a medium aeroplane (less than 136000 kg but more than 7000 kg ) on the approach to landing
- A.
4 min
- B.
5 min
- C.
2 min
- D.
3 min
- 6.A category II precision app ( CAT II) is an app with :
- A.
A decision height of at least 100 ft
- B.
A decision height of at least 200 ft
- C.
A decision height at least 50 ft
- D.
No decision height
- 7.At wich levels may Reduce Vertical Separation Minimum (RVSM ) be used within NAT region ¿?
- A.
Below FL 290
- B.
Between FL290 and FL 410
- C.
Between FL 275 and FL 400
- D.
Between Fl 245 and FL 410
- 8.A category I precision app ( CAT I ) is an app with may be carried out with visual range of at least :
- A.
500 m
- B.
550 m
- C.
350 m
- D.
800 m
- 9.According DOC 4444 (ICAO) a wake turbulence nonreader separation minima of 2 minutes shall be applied to :
- A.
LIGHT a/c landing behind a MEDIUM a/c
- B.
MEDIUM a/c landing behind a HEAVY a/c
- C.
MEDIUM a/c taking off behind a HEAVY a/c from an intermediate part of a parallel by less than 760m
- D.
LIGHT a/c taking off behind a MEDIUM a/c from an intermediate part of the same rwy.
- 10.According to the recommended noise abatement take off and climb procedure A ICAO DOC 8168 thrust redaction to climb power has to be done as soon as the a/C reaches :
- A.
3000 ft
- B.
2000 ft
- C.
1000 ft
- D.
1500 ft
- 11.Wind shear is :
- A.
A vertical or horizontal wind velocity and / or wing direction over a large distance
- B.
A vertical or horizontal wing velocity and / or wind direction over a short distance
- C.
A horizontaal wind velocity variation ove a short distance
- D.
A vertical wind velocity variation over a short distance
- 12.The greatest possibility of ice buildup , while flying under icing conditions occurs on:
- A.
The a/C front areas
- B.
The upper and lower wing surfaces
- C.
The upper and lower rudder surfaces
- D.
Only the pilot and static probes
- 13.In the JAR OPS a rwy is considered damp when
- A.
Surface moisture gives it a shiny appearance
- B.
It is covered with a film of water of less than 3 mm
- C.
It is covered with a film of water of less than 1mm
- D.
Its surface is not dry and when surface moisture does not give it a shiny appearance
- 14.An a/c wich experience a headwind of 40 kt while making its way towards the centre of a microburst may expect , when crossing the microburst to face a wind shear of :
- A.
80 kt
- B.
40 kt
- C.
60 kt
- D.
20 kt
- 15.For a/c with more than 44 seats can be evacuated the plane in :
- A.
60 seconds
- B.
90 seconds
- C.
132 seconds
- D.
120 seconds
- 16.The velocity of sound at the sea level in standard atmosphere is :
- A.
644 kt
- B.
322 kt
- C.
661 kt
- D.
1059 kt
- 17.The error in altimeter ratings caused by the variation of static pressure near the source is known as :
- A.
Position pressure error
- B.
Barometric error
- C.
Instrumente error
- D.
Hysteresis effect
- 18.The Ground Proximity Warning System (GPWS) is a system working according to a height span ranging
- A.
The ground to 500 ft
- B.
50 ft to 2500 ft
- C.
The ground to 1000 ft
- D.
30 ft to 5000 ft
- 19.If the static source of an altimeter becomes blocked during a descent the instrument will :
- A.
Continue to display the reading at wich the blockage occurred
- B.
Gradually indicate zero
- C.
under -- read
- D.
Indicate a height equivalent to the setting on the milibar subscale
- 20.A stall warning system is based on a measure of :
- A.
Airspeed
- B.
Attitude
- C.
Ground speed
- D.
Aerodynamic incident
- 21.If the static source to an airspeed indicator (ASI) becomes blocked during a descent the instrument will :
- A.
Continue to indicated the speed applicable to that at the time of the blockage
- B.
Under -read
- C.
Over - read
- D.
Read zero
- 22.A resolution advisory (RA)is represented on the display system of the TCAS 2 by a :
- A.
Red fulll circle
- B.
Red full square
- C.
Blue or white full lozenge
- D.
Blue or white empty lozenge
- 23.When flying from a sector of warm air into one of colder air the altimeter will :
- A.
Underread
- B.
Be just as correct as before
- C.
Show the actual height above ground
- D.
Overread
- 24.THe stall warning system receives information about the 1.- angle of attack 2.- airplane speed 3.- airplane back angle 4.- airplane configuration 5.- load factor
- A.
1, 2,3,4,5
- B.
2 ,3,4,5
- C.
1,3,5
- D.
1, 4
- 25.A pilot blockage of both the ram air input and the drain hole with the static port open causes the airspeed indicator to :
- A.
Freeze at zero
- B.
React like an altimeter
- C.
Read a little high
- D.
Read a little low
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