- •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:
- •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:
- •30 "Refer to figure 032-06.
- •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.
40 "Refer to figure 032-06.
Given:
OAT: 24°C
Pressure Altitude: 3000 ft
RWY: 12L
Wind: 080°/12 kts
Take-off mass: 3800 lbs
Other conditions as associated in the header of the graph. What is the take-off distance over a 50 ft obstacle?"
a 1700 ft
b 1420 ft
c 1950 ft
d 1600 ft
42 Why is there a requirement for an approach climb gradient?
a So that an aircraft falling below the glide path will be able to re-intercept it.
b Adequate performance for a go-around in the event of an engine failure.
c To maintain minimum altitude on the approach.
d So that the aircraft will not stall when full flap is selected.
43 "Refer to figure 032-08.
With regard to the graph for the light twin aeroplane, will the accelerate and stop distance be achieved in a take-off where the brakes are released before take-off power is set?"
a No, the performance will be worse than in the chart.
b It does not matter which take-off technique is being used.
c Yes, the chart has been made for this situation.
d Performance will be better than in the chart.
44 Approaching in turbulent wind conditions during manual flight requires:
a no change.
b an increase in approach speed.
c a steeper approach path.
d an increase in VREF.
45 "Following a take-off, limited by the 50 ft screen height, a light twin climbs on a gradient of 5%. It will clear a 160 m obstacle in relation to the runway (horizontally), situated at 5000 m from the 50 ft point with an obstacle clearance margin of:"
a 105 m.
b 90 m.
c 75 m.
d it will not clear the obstacle.
46 "Refer to figure 032-10.
Given:
Flaps:40°
Aerodrome pressure altitude:sea level
Ambient temperature:+15°C
Landing weight:4000 lbs
Wind:calm
Runway:paved and dry
What is the Landing Distance?
a 2400 feet.
b 2040 feet.
c 1400 feet.
d 1240 feet.
47 What rate of climb will be achieved with a climb gradient of 3,3% and a groundspeed of 100 kts?
a 400 ft/min.
b 300 ft/min.
c 330 ft/min.
d 370 ft/min.
48 The correct sequence of speeds is:
a Vs, max range speed, max endurance speed.
b Vs,Vx,VY.
c max endurance speed, Vs, max range speed.
d v*vs,vY.
49 The best speed for obstacle clearance is:
a VY with optimum flap setting for runway length, take-off weight and atmospheric conditions.
b Vy with no flaps.
c Vx with optimum flap setting for runway length, take-off weight and atmospheric conditions.
d Vx and no high lift devices.
50 Heavy rain may temporarily cause:
a increased weight.
b increased stalling speed.
c reduced forward speed.
d all of the above.
51 The maximum angle of bank permitted after take-off below 50 feet for an aeroplane in Performance Class В is:
a 0°
b 5°
c 15°
d 10°
52 The combination of factors that most requires a low-angled flap setting for take-off is:
a High field elevation, no obstacles in the climb-out path, low ambient temperature and short runway.
b Low field elevation, close-in obstacles in the climb-out path, long runway and a high ambient temperature.
c High field elevation, distant obstacles in the climb-out path, long runway and a high ambient temperature.
d Low field elevation, no obstacles in the climb-out path, short runway and a low ambient temperature.