ATP 04 GERARD 2020

1. The use of TCAS for avoiding an A/C in flight is now general TCAS uses for its operation

The replies from the transponders of the other A/C

The echos from the ground air traffic control radar system

The ecos of c.a.sys installed on board

Both the replies from the transponder of the other a/c and the ground radar echoes

2. A category II precision app ( CAT II) is an app with :

A decision height of at least 100 ft

A decision height of at least 200 ft

A decision height at least 50 ft

No decision height

3. At wich levels may Reduce Vertical Separation Minimum (RVSM ) be used within NAT region ¿?

Below FL 290

Between FL290 and FL 410

Between FL 275 and FL 400

Between Fl 245 and FL 410

4. According DOC 4444 (ICAO) a wake turbulence nonreader separation minima of 2 minutes shall be applied to :

LIGHT a/c landing behind a MEDIUM a/c

MEDIUM a/c landing behind a HEAVY a/c

MEDIUM a/c taking off behind a HEAVY a/c from an intermediate part of a parallel by less than 760m

LIGHT a/c taking off behind a MEDIUM a/c from an intermediate part of the same rwy.

5. Wind shear is :

A vertical or horizontal wind velocity and / or wing direction over a large distance

A vertical or horizontal wing velocity and / or wind direction over a short distance

A horizontaal wind velocity variation ove a short distance

A vertical wind velocity variation over a short distance

6. 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 :

80 kt

40 kt

60 kt

20 kt

7. The Ground Proximity Warning System (GPWS) is a system working according to a height span ranging

The ground to 500 ft

50 ft to 2500 ft

The ground to 1000 ft

30 ft to 5000 ft

8. 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 :

200 m

100 m

250 m

50 m

9. A resolution advisory (RA)is represented on the display system of the TCAS 2 by a :

Red fulll circle

Red full square

Blue or white full lozenge

Blue or white empty lozenge

10. A stall warning system is based on a measure of :

Airspeed

Attitude

Ground speed

Aerodynamic incident

11. 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 :

3000 ft

2000 ft

1000 ft

1500 ft

12. The greatest possibility of ice buildup , while flying under icing conditions occurs on:

The a/C front areas

The upper and lower wing surfaces

The upper and lower rudder surfaces

Only the pilot and static probes

13. For a/c with more than 44 seats can be evacuated the plane in :

60 seconds

90 seconds

132 seconds

120 seconds

14. The velocity of sound at the sea level in standard atmosphere is :

644 kt

322 kt

661 kt

1059 kt

15. During a climb after T.O from contaminated rwy , if the total pressure probe of the airspeed indicator is blocked the pilot finds that indicated airspeed :

Increase steadily

Increase abruptly toward VNE

Decrease stadily

Decreases abruptly towards zero

16. If the static source of an altimeter becomes blocked during a descent the instrument will :

Continue to display the reading at wich the blockage occurred

Gradually indicate zero

Under -- read

Indicate a height equivalent to the setting on the milibar subscale

17. In the JAR OPS a rwy is considered damp when

Surface moisture gives it a shiny appearance

It is covered with a film of water of less than 3 mm

It is covered with a film of water of less than 1mm

Its surface is not dry and when surface moisture does not give it a shiny appearance

18. 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

4 min

5 min

2 min

3 min

19. 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 :

1500 ft

3000 ft

1000 ft

500 ft

20. A category I precision app ( CAT I ) is an app with may be carried out with visual range of at least :

500 m

550 m

350 m

800 m

21. If the static source to an airspeed indicator (ASI) becomes blocked during a descent the instrument will :

Continue to indicated the speed applicable to that at the time of the blockage

Under -read

Over - read

Read zero

22. 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

1, 2,3,4,5

2 ,3,4,5

1,3,5

1, 4

23. A pilot blockage of both the ram air input and the drain hole with the static port open causes the airspeed indicator to :

Freeze at zero

React like an altimeter

Read a little high

Read a little low

24. During an A/C de icing / anti icing procedure

The anti-icing fluid is applied without heating and de --icing fluid is applied hot.

The anti-icing and de -icing fluids are applied hot.

The anti-icing and de -icing fluids are applied cold

The de--icing fluid is applied without heating and the anti-icing fluid is applied hot

25. At sea level on a typical servo altimeter the tolerance in feet from indicated must not exceed :

+/- 70 feet

+/- 60 feet

+/-75 feet

+/- 30 feet

26. When flying from a sector of warm air into one of colder air the altimeter will :

Underread

Be just as correct as before

Show the actual height above ground

Overread

27. A pitot tube covered by ice wich blocks the ram air inlet will affect the following instruments

Air speed indicator only

Altimeter only

Vertical speed indicator only

Air speed ,altimeter and vertical speed ind

28. To use passengers oxygen in case of severe cabin smoke is :

Useless because breathing oxygen would explode under smoke conditions

Possible and recommended

Useless because the topical cabin smoke is mixed with the breathing oxygen

Useless because the oxygen units do not operate under smoke conditions

29. The error in altimeter ratings caused by the variation of static pressure near the source is known as :

Position pressure error

Barometric error

Instrumente error

Hysteresis effect

30. Which a pitot probe blocked due to ice build up the a/c airspeed ind will indicate in descent a :

Decreasing speed

Constant speed

Increasing speed

Fluctuating speed

ATP 04 Gerard 2020