Question 1
Question
109) Maximum and minimum values of V1 are limited by :
Answer
-
VR and VMCG
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V2 and VMCA
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VR and VMCA
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V2 and VMCG
Question 2
Question
99) During the certification flight testing of a twin engine turbojet aeroplane, the real take-off distances are equal to:
- 1547 m with all engines running
- 1720 m with failure of critical engine at V1, with all other things remaining unchanged.
The take-off distance adopted for the certification file is:
Answer
-
1547 m.
-
1720 m.
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1779 m.
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1978m.
Question 3
Question
The minimum value of V2 must exceed "air minimum control speed" by:
Question 4
Question
102) With regard to a take-off from a wet runway, which of the following statements is correct?
Answer
-
Screen height cannot be reduced.
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The screen height can be lowered to reduce the mass penalties.
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When the runway is wet, the V1 reduction is sufficient to maintain the same margins on the runway length.
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In case of a reverser inoperative the wet runway performance information can still be used.
Question 5
Question
103) On a reciprocating engined aeroplane, to maintain a given angle of attack, configuration and altitude at higher gross mass
Answer
-
an increase in airspeed is required but power setting does not change.
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requires an increase in power and decrease in the airspeed.
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an increase in airspeed and power is required.
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a higher coefficient of drag is required.
Question 6
Question
104) The first segment of the take-off flight path ends
Answer
-
at completion of gear retraction.
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at completion of flap retraction.
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at reaching V2.
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at 35 ft above the runway.
Question 7
Question
105) Which of the following factors favours the selection of a low flap setting for the take-off?
Answer
-
High field elevation, no obstacles in the climb-out path, low ambient temperature and short runway.
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Low field elevation, no obstacles in the climb-out path, short runway and a low ambient temperature.
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High field elevation, distant obstacles in the climb-out path, long runway and a high ambient temperature.
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Low field elevation, close-in obstacles in the climb-out path, long runway and a high ambient temperature.
Question 8
Question
106) Balanced V1 is selected
Answer
-
for a runway length limited take-off with a clearway to give the highest mass.
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if it is equal to V2.
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if the accelerate stop distance is equal to the one engine out take-off distance.
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for a runway length limited take-off with a stopway to give the highest mass.
Question 9
Question
108) For jet-engined aeroplanes, what is the effect of increased altitude on specific range?
Question 10
Question
96) The speed for best rate of climb is called:
Question 11
Question
110) Two identical aeroplanes at different masses are descending at idle thrust. Which of the following statements correctly describes their descent characteristics ?
Answer
-
At a given angle of attack, both the vertical and the forward speed are greater for the heavier aeroplane.
-
There is no difference between the descent characteristics of the two aeroplanes.
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At a given angle of attack the heavier aeroplane will always glide further than the lighter aeroplane.
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At a given angle of attack the lighter aeroplane will always glide further than the heavier aeroplane.
Question 12
Question
111) ETOPS flight is a twin engine jet aeroplane flight conducted over a route, where no suitable airport is within an area of
Answer
-
75 minutes flying time at the approved one engine out cruise speed.
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60 minutes flying time in still air at the approved one engine out cruise speed.
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60 minutes flying time in still air at the normal cruising speed.
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30 minutes flying time at the normal cruising speed.
Question 13
Question
112) For a take-off from a contaminated runway, which of the following statements is correct?
Answer
-
Dry snow is not considered to affect the take-off performance.
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A slush covered runway must be cleared before take-off, even if the performance data for contaminated runway is available.
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The performance data for take-off must be determined in general by means of calculation, only a few values are verified by flight tests.
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The greater the depth of contamination at constant take-off mass, the more V1 has to be decreased to compensate for decreasing friction.
Question 14
Question
113) If the thrust available exceeds the thrust required for level flight
Answer
-
the aeroplane accelerates if the altitude is maintained.
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the aeroplane descends if the airspeed is maintained.
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the aeroplane decelerates if it is in the region of reversed command.
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the aeroplane decelerates if the altitude is maintained.
Question 15
Question
114) Which statement regarding the relationship between traffic load and range is correct?
Answer
-
The maximum landing mass is basically equal to the maximum zero fuel mass.
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The maximum traffic load is not limited by the reserve fuel quantity.
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The traffic load can be limited by the desired range.
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The maximum zero fuel mass limits the maximum quantity of fuel.
Question 16
Question
115) The induced drag of an aeroplane
Answer
-
is independent of the airspeed.
-
increases with increasing airspeed.
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decreases with increasing airspeed.
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decreases with increasing gross weight.
Question 17
Question
116) Which statement, in relation to the climb limited take-off mass of a jet aeroplane, is correct?
Answer
-
50% of a head wind is taken into account when determining the climb limited take-off mass.
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On high elevation airports equipped with long runways the aeroplane will always be climb limited.
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The climb limited take-off mass decreases with increasing OAT.
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The climb limited take-off mass is determined at the speed for best rate of climb.
Question 18
Question
117) How is V2 affected if T/O flaps 20° is chosen instead of T/O flaps 10°?
Answer
-
V2 increases in proportion to the angle at which the flaps are set.
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V2 has no connection with T/O flap setting, as it is a function of runway length only.
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V2 decreases if not restricted by VMCA.
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V2 has the same value in both cases.
Question 19
Question
118) Which of the jet engine ratings below is not a certified rating?
Question 20
Question
107) Which statement regarding the influence of a runway down-slope is correct for a balanced take-off? Down- slope...
Answer
-
increases V1 and reduces the accelerate stop distance required (ASDR).
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reduces V1 and increases the accelerate stop distance required (ASDR).
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increases V1 and increases the take-off distance required (TODR).
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reduces V1 and reduces take-off distance required (TODR).