- •10 "Refer to figure 032-09.
- •11 If the tas is 100 kts on the glide slope of 3°, what is the rate of descent?
- •12 "Refer to figure 032-07.
- •19 "Refer to figure 032-06.
- •21 "Refer to figure 032-06.
- •22 What is the effect of the centre of gravity on fuel consumption?
- •28 "Refer to figure 032-07.
- •29 "The climb gradient of an aircraft after take-off is 6% in standard atmosphere, no wind, at 0 ft pressure altitude. Using the following corrections:
- •30 "Refer to figure 032-06.
- •37 "The following parameters positively affect the take-off ground run:
- •38 "An obstacle is 5000 m from the end of the todr and is 160 m high. The screen height is 50 ft and the ground climb gradient is 5%. Which of the following statements is correct?"
- •39 When comparing VX to vy:
- •40 "Refer to figure 032-06.
- •42 Why is there a requirement for an approach climb gradient?
- •43 "Refer to figure 032-08.
- •46 "Refer to figure 032-10.
- •53"Refer to figure 032-09.
- •54 Which of the following provides maximum obstacle clearance during climb?
- •55 For take-off performance calculations, what is taken into account?
- •56 "Refer to figure 032-26.
- •57 "Refer to figure 032-07.
- •58 Which of the following is true with regard to vMca (air minimum control speed)?
- •59 "The take-off distance of an aircraft is 600 m in standard atmosphere, no wind at 0 ft pressure-altitude. Using the following corrections:
- •60 The critical engine inoperative:
- •78 "Refer to figure 032-09.
- •79 "Given:
- •80 "Refer to figure 032-06.
- •84 "Given:
- •86 "Refer to figure 032-07.
- •87 If the cg moves aft from the most forward position:
- •88 If the actual Landing Mass is higher than planned:
- •94 Moving the centre of gravity from the forward to the aft limit (gross mass, altitude and airspeed remain unchanged):
- •96 "Refer to figure 032-09.
- •98 What affect has a tailwind on the maximum endurance speed?
- •99 For an aeroplane in Performance Class в the net take-off flight path begins at a height of and ends at a height of .
- •100 The speed Vs is defined as:
- •101 "Refer to figure 032-05.
- •102 "Refer to figure 032-05.
- •103 "Refer to figure 032-05.
- •104 "An aeroplane with reciprocating engines is flying at a constant angle of attack, mass and configuration. With increasing altitude the drag:"
- •105 The maximum indicated air speed of a piston engine aeroplane without turbo charger, in level flight, is reached:
- •106 "Refer to figure 032-05.
- •116 Which of the following will probably result in the greatest increase in take-off distance for a single-engined piston aeroplane?
- •117 "Refer to figure 032-04.
- •118 "Refer to figure 032-03.
- •119 In a given configuration the endurance of a piston engined aeroplane only depends on:
- •120 "A climb gradient required is 3,3%. For an aircraft maintaining 100 kts tas (no wind), this climb gradient corresponds to a rate of climb (roc) of approximately:"
- •121 "Refer to figure 032-02.
- •122 "Refer to figure 032-05.
- •123 Decreasing take-off flap from 15° to 0° will probably result in vlOf-
- •124 "Refer to figure 032-05.
- •125 "Refer to figure 032-03.
- •126 "Refer to figure 032-05.
- •127 "According to the information in a light aircraft manual, which gives two power settings for cruise, 65% and 75%. If you fly at 75% instead of 65%:"
- •128 "Refer to figure 032-02.
- •129 "Refer to figure 032-02.
- •130 "Refer to figure 032-02.
- •131 "For an aeroplane in Performance Class в the following factors must be applied in determining the take-off distance from dry grass and wet pavement respectively;"
- •132"Refer to figure 032-03.
- •133 "Refer to figure 032-02.
- •134 Vref for a Class в aircraft is defined by:
- •135 "The landing reference speed vref has, in accordance with international requirements, the following margins above stall speed in landing configuration:"
- •136 "If a tod of 800 m is calculated at sea level, on a level, dry runway, with standard conditions and with no wind, what would the tod be for the conditions listed below?
- •137 "Refer to figure 032-04.
- •138 "The stalling speed or the minimum steady flight speed at which the aeroplane is controllable in landing configuration is abbreviated as:"
- •139 What margin above the stall speed is provided by the landing reference speed vref?
- •140 "Refer to figure 032-04.
1 Landing on a runway with 5 mm wet snow will:
a give a slightly reduced landing distance, due to increased impingement drag.
b increase landing distance.
c not affect the landing distance.
d decrease landing distance.
2 "If for aeroplane in Performance Class В the intended take-off flight path requires track changes of more than 15°, with the pilot unable to maintain visual navigation accuracy according to EASA AIR OPS regulations, the clearance of obstacles within of track need be considered."
a 500 m
b 600 m
c 900 m
d 300 m
3 "On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kts and the holding speed (minimum fuel burn per hour) is 95 kts. The best rate of climb speed will be obtained for a speed:"
a equal to 125 kts.
b equal to 95 kts.
c < 95 kts.
d between 95 and 125 kts.
4 An aircraft with a Centre of Gravity towards the aft limit will experience:
a a decreased range and decreased stalling speed.
b an increased range and decreased stalling speed.
c a decreased range and increased stalling speed.
d an increased range and increased stalling speed.
5 VY is defined as:
a speed for best rate of descent.
b speed for best rate of climb.
c speed for best angle of climb.
d maximum speed which should be used in a climb.
6 Vx is defined as:
a the speed for best rate of climb.
b the speed for best specific range.
c the speed for best angle of climb.
d the speed for best angle of flight path.
7 "Given:
Still Air climb gradient: 3.8%
TAS: 100 kts
GS: 130 kts
What is the effective wind climb gradient?"
a 4,20%
b 2,90%
c 4,90%
d 3,80%
8 "Refer to figure 032-07.
Given:
OAT: -10°C
Pressure Altitude:4000 ft
RWY:12R
Wind:180°/10 kts
Take-off Mass:4600 lbs
Heavy Duty Brakes installed
Other conditions as associated in the header of the chart. What is the Accelerate and Stop Distance under the conditions given?"
a 4600 ft
b 3800 ft
c 3550 ft
d 4300 ft
9 Other factors remaining constant, how does increasing altitude affect Vx and VY in terms of IAS?
a Vx will remain constant and VY will decrease.
b Vx will decrease and VY will increase.
c Both will increase.
d Both will decrease.
10 "Refer to figure 032-09.
Given:
OAT: 10°C
Pressure altitude: 2000 ft
Gross mass: 3750 lbs
Other conditions as associated in the header of the graph. What is the one engine inoperative rate of climb for the conditions given?"
a 890 ft/min.
b 500 ft/min.
c 200 ft/min.
d 430 ft/min.
11 If the tas is 100 kts on the glide slope of 3°, what is the rate of descent?
a 1000 ft/min.
b 500 ft/min.
c 250 ft/min.
d 300 ft/min.
12 "Refer to figure 032-07.
Given:
OAT:25°C
Pressure altitude:3000 ft
RWY:24L
Wind:310°/20 kts
Take-off mass:4400 lbs
Heavy Duty Brakes installed
Other conditions as associated in the header of the chart. What is the Accelerate and Stop Distance under the conditions given?"
a 4300 ft
b 3350 ft
c 3750 ft
d 4000 ft
13 For a piston-engined aeroplane at a constant altitude, angle of attack and configuration, an increased weight will require:
a the same power but higher speed.
b more power and the same speed.
c more power but lower speed.
d more power and higher speed.
14 What happens to the speeds, Vx and VY, when lowering the aircraft’s landing gear?
a Vx increases, VY increases.
b Vx decreases, VY increases.
c Vx increases, VY decreases.
d Vx decreases, VY decreases.
15 The take-off distance required increases:
a due to headwind because of the drag augmentation.
b due to slush on the runway.
c due to downhill slope because of the smaller angle of attack.
d due to lower gross mass at take-off.
16 "The flight manual of a light twin engine recommends two cruise power settings: 65% and 75%. The 75% power setting in relation to the 65% results in:"
a an increase in speed and fuel-burn/distance, but an unchanged fuel-bum per hour.
b same speed and an increase of the fuel-burn per hour and fuel-burn/distance.
c same speed and fuel-burn/distance, but an increase in the fuel-burn per hour.
d an increase in speed, fuel consumption and fuel-burn/distance.
17 Other factors remaining constant, how does increasing altitude affect Vx and VY in terms of TAS?
a VY remains constant and Vx decreases.
b VY remains constant and Vx increases.
c Both remain constant.
d Both will increase.
18 An aircraft is climbing at Vx. If the speed is increased, maintaining the power setting.
a the climb gradient will decrease and the rate of climb increase.
b the climb gradient will increase and the rate of climb increase.
c the climb gradient will increase and the rate of climb decrease.
d the climb gradient will decrease and the rate of climb decrease.
19 "Refer to figure 032-06.
Given:
OAT: -15°C
Pressure Altitude: 4000 ft
RWY:12R
Wind:080°/12 kts
Take-off Mass:4000 lbs
Runway Surface:
tarred and dry
What is the minimum runway length? No stopway or clearway is available."
a 1750 ft.
b 1550 ft.
c 1950 ft.
d 1250 ft.
20 "A runway is contaminated with 0.5 cm of wet snow. The flight manual of a light twin nevertheless authorises a landing in these conditions. The landing distance will be, in relation to that for a dry runway:"
a substantially decreased
b reduced
c increased
d unchanged