5861270
Question 1
Question
77 To obtain the maximum possible range when flying into a headwind, the speed should:
Answer
-
O be higher than the optimum speed for still air,
-
O be the same as the optimum speed for still air
-
O proceed an appropriate fuel management.
-
O be lower than the optimum speed for still air
Question 2
Question
78 If the aircraft's C.G. is moved into a more forward position
Answer
-
O the drag and lift will be increased and the range will be decreased
-
O the drag and lift will be increased and the range will be increased
-
O the drag will be increased, lift will be decreased and the range will be decreased
-
O the drag will be decreased, the lift will be increased and the range will be increased.
Question 3
Question
79 For a given aircraft mass, as altitude increases, the minimum total drag will;
Answer
-
O remain the same and the Vmd will remain the same .
-
O decrease, and the Vmd will decrease
-
O increase, and the Vmd will increase
-
O remain the same and the Vmd will be diminished.
Question 4
Question
80 The maximum speed that can be achieved in level flight, will occur:
Answer
-
O when the drag is equal to the maximum thrust available,
-
O when the drag is a minimum
-
O when CL / CD is a minimum
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O when CD is a minimum
Question 5
Question
81 The scheduled landing distance required, is the distance :
Answer
-
O from a screen of a designated height to the point at which the aircraft has come to a complete stop,
-
O from touch down to the point at which the aircraft has vacated the runway in use.
-
O from touch down to the point at which the aircraft has come to a complete stop
-
O from the point at which the aircraft is 50 metres above the runway to the point at which the aircraft has come to a complete stop, with brakes full.
Question 6
Question
82 The landing distance required will be increased as a result of all of the following';
Answer
-
O increased temperature, increased pressure altitude, downhill runway slope,
-
O increased temperature, increased pressure altitude, uphill runway slope.
-
O decreased temperature, decreased pressure altitude, uphill runway slope
-
O increased temperature, decreased pressure altitude, downhill runway slope.
Question 7
Question
83 Which of the following statements relating to hydroplaning is true :
Answer
-
O When the wheel begins to hydroplane the wheel drag decreases.
-
O Hydroplaning can only occur if the depth of the contaminant exceeds 5 mm.
-
O Hydroplaning can only occur if the brakes are applied and releasing the brakes will stop the hydroplaning.
-
O Hydroplaning can be reduced when tιre chambers are more flat, (reduced tιre pressure).
Question 8
Question
102 Given that the regulations applied and control requirement is met, the speed at the 50 ft. screen must not be less than :
Answer
-
O 30% above the stalling speed with landing flap.
-
O 20% above the stalling speed with landing flap
-
O 30% above the stalling speed with flaps up
-
O stall speed.
Question 9
Question
103 If the runway is wet, the landing distance required for a dry runway :
Answer
-
O must be increased by 15% (X1.15)
-
O may be used unfactored '
-
O must be considered unpredictable
-
O must be increased by 10% (X1.10)
Question 10
Question
104 The landing distance required must not exceed :
Answer
-
O 70% of the landing distance available at destination and alternate aerodromes.
-
O 70% of the landing distance available at a destination aerodrome; and 50% of the landing distance available at an alternate aerodrome.
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O 50% of the landing distance available at a destination aerodrome, and 70% of the landing distance available at an alternate aerodrome.
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O 50% of the landing distance available at destination and alternate aerodromes.
Question 11
Question
108 For a grass runway, the landing distance required for a paved runway should be :
Answer
-
O increased by 15%,
-
O decreased by 5%
-
O increased by 5%
-
O decreased by 15%
Question 12
Question
109 In comparison to the true airspeed in still air conditions, the TAS for the best range in a strong tailwind will be:
Answer
-
O slightly lower.
-
O the same.
-
O slightly higher.
-
O significantly lower, proportional to the tailwind component.
Question 13
Question
110 Consult Fig.4. Refering to this graph, the flight for maximum range in a piston engined aircraft is achieved by flying:
Answer
-
O at that speed which provides the minimum power/ airspeed ratio.
-
O significantly higher than the minimum drag speed (Vmd).
-
O at the lowest density altitude environment that is safely possible.
-
O at the same speed which provides the maximum power/airspeed ratio.
Question 14
Question
113 The best rate of climb is achieved.
Answer
-
O when there is a maximum excess of power above that required to maintain straight and level flight.
-
O when climbing into wind at the best angle of climb.
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O when cored into a thermal.
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O when the mixture is full rich and the throttle fully advanced and the aeroplane maintaining cruise speed.
Question 15
Question
114 (Refer to Fig.8). What is the effect of a temperature increase from -4?C to +10°C on the density altitude if the pressure altitude remains at 5,000 feet?
Answer
-
O 1,650-foot increase.
-
O 1,000-foot increase.
-
O 1,300-foot increase.
-
O 1950-foot increase.
Question 16
Question
115 (Refer to Fig.8). What is the effect of a temperature increase from +4?C to -15°C on the density altitude if the pressure altitude remains at 10,000 feet?
Answer
-
O 2,100-foot decrease.
-
O 1,800-foot increase.
-
O 1,500-foot decrease.
-
O 1,000-foot increase.
Question 17
Question
116 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,380 feet MSL with an altimeter setting of 28.22" at standard temperature.
Answer
-
O 3,010 feet MSL.
-
O 1,250 feet MSL.
-
O 1,373 feet MSL.
-
O 2500 feet MSL.
Question 18
Question
117 (Refer to Fig.8). Determine the pres¬sure altitude with an indicated altitude of 1,820 feet MSL with an altimeter setting of 30.58" at standard temperature.
Answer
-
O 1,200 feet MSL.
-
O 2,440 feet MSL.
-
O 2000 feet MSL.
-
O none of them.
Question 19
Question
118 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................29.25"
Runway temperature...........................................+27°C
Airport elevation......................................5,250 ft MSL
Answer
-
O 8,500 feet MSL.
-
O 4,600 feet MSL.
-
O 5,877 feet MSL.
-
O 6000 feet MSL.
Question 20
Question
119 (Refer to Fig.8). Determine the density altitude for these conditions:
Altimeter setting...................................................30.15"
Runway temperature........................................... -1°C
Airport elevation......................................4,610 ft MSL
Answer
-
O 3,500 feet MSL.
-
O 4,900 feet MSL.
-
O 4,000 feet MSL.
-
O 3,000 feet MSL.
Question 21
Question
120 (Refer to figure 8.) Determine the pressure altitude at an airport that is 4,563 feet MSL with an altimeter set¬ting of 29.96".
Answer
-
O 4,527 feet MSL.
-
O 4,236 feet MSL.
-
O 3,640 feet MSL.
-
O 4,600 feet MSL.
Question 22
Question
121 (Refer to figure 8.) What is the effect of a temperature increase from -1?C to 10°C on the density altitude if the pressure altitude remains at 3,000 feet MSL?
Answer
-
O 1,300-foot increase.
-
O 900-foot increase.
-
O 1,100-foot decrease.
-
O 1300-foot decrease.
Question 23
Question
122 (Refer to figure 8.) Determine the pressure altitude at an airport that is 1,386 feet MSL with an altimeter setting of 29.97".
Answer
-
O 1,341 feet MSL.
-
O 1,451 feet MSL.
-
O 1,562 feet MSL.
-
O 1,212 feet MSL.
Question 24
Question
123 (Refer to figure 8.) Determine the density altitude for these conditions:
Altimeter setting...................................................30.35"
Runway temperature........................................... -4°C
Airport elevation......................................3,894 ft MSL
Answer
-
O 2,000 feet MSL,
-
O 1,500 feet MSL
-
O 2,900 feet MSL,
-
O 3,500 feet MSL
Question 25
Question
124 (Refer to Fig.9) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220° at 30 knots?
Answer
-
O 23knots.
-
O 19 knots.
-
O 30 knots.
-
O 34 knots.
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