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Question 1/101/10
Performance Class B - Theory
Performance Class B - Theory
Performance Class B - Theory
Refer to figure or CAP698 file 4.1.
Calculate the relative direction of the wind to the runway. i.e. (wind direction - runway direction) or (runway direction - wind direction).
Example: W/V 330/30
Runway 0
Wind angle = 50°
Select the answer:Select the answer
1 correct answer
A.
Head wind 10 crosswind 12 kt
B.
Head wind 15 kt crosswind 15 kt
C.
Head wind 20 kt crosswind 20 kt
D.
Head wind 19 kt crosswind 23 kt
.
Right Answer: D
Quiz
Question 2/102/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Departing SID requires 6.1% gradient with T/O flaps, speed 130 kts to 1800ft and thereafter a 5% gradient to FL80 clean at 230 kts. What is the ROC required to 1800ft?
Select the answer:Select the answer
1 correct answer
A.
600 fpm to 1800 ft with non-standard speed change altitude.
B.
1150 fpm with standard speed change altitude
C.
800 fpm to 1800 ft with non-standard speed change altitude.
D.
1250 fpm with standard speed change altitude.
The Rate of Climb (ROC) required to climb to 1800ft is 800 fpm with a non-standard speed change altitude when departing on the Standard Instrument Departure (SID) that requires a 6.1% gradient with takeoff flaps and a speed of 130 kts.
Right Answer: C
Quiz
Question 3/103/10
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Refer to the annex or CAP 698 Figure 4.5. Given the following information what is the Climb Limited Take-Off Mass?OAT + 35°CPressure altitude 2000 ftFlaps 5°A/C packs OFFAnti-icing OFFPMC OFF
Select the answer:Select the answer
1 correct answer
A.
52800 kg
B.
53700 kg
C.
57900 kg
D.
57000 kg
.
Right Answer: C
Quiz
Question 4/104/10
Performance Class A - Theory
Performance Class A - Theory
Performance Class A - Theory
With regard to the FMC and reduced thrust take-off’s which of the following statements is correct.
Select the answer:Select the answer
1 correct answer
A.
Reduced thrust cannot be used on a contaminated
runway.
B.
Reduced thrust is not recommended at very low
temperatures (OAT).
C.
Reduced thrust can lower VMCG and VMCA
D.
Reduced thrust cannot be used on a wet runway
Reduced thrust take-off cannot be used on a contaminated runway.
Right Answer: A
Quiz
Question 5/105/10
Performance Class B - Theory
Performance Class B - Theory
Performance Class B - Theory
A single engine aircraft has a gross glide gradient of 8%. Determine the net glide distance from 10 000 ft to 2 000 ft:
Select the answer:Select the answer
1 correct answer
A.
15.5 NM
B.
16.5 NM
C.
17 NM
D.
94 120 NM
The net glide distance can be calculated by multiplying the gross glide gradient (8%) by the difference in altitude (8000 ft), and then dividing by 100 to convert it to nautical miles. Therefore, the net glide distance from 10 000 ft to 2 000 ft is 15.5 NM.
Right Answer: A
Quiz
Question 6/106/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Please refer to the annex or to CAP 698, Figure 3.7. What is the time required by a multi-engined piston aeroplane to climb 2400 ft? Assume that the rate of climb is constant throughout the climb and equals the rate of climb at 6000 ft pressure altitude. Use the following data:2 engines operating at maximum continuous power,Gear retracted,Pressure altitude: 6000 ft,OAT: +17° C,Mass: 4000 lb.
Select the answer:Select the answer
1 correct answer
A.
8 minutes 0 seconds
B.
3 minutes 55 seconds
C.
1 minute 33 seconds
D.
1 minute 55 seconds
.
Right Answer: C
Quiz
Question 7/107/10
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Performance Class A - Use Of Data
Refer to figure 032-62.Given:
Airport elevation:
1 998 ft
Temperature (OAT):
+38 ⁰C
Tailwind:
8 kt
Tyres:
225 mph
Flaps:
5⁰
Aircraft:
medium range jet
Power management computer (PMC):
ON
Determine the tyre speed limited take-off mass for a departure from Madrid, Spain:
Select the answer:Select the answer
1 correct answer
A.
79 100 kg
B.
78 850 kg
C.
84 300 kg
D.
73 900 kg
.
Right Answer: D
Quiz
Question 8/108/10
Performance Class A - Theory
Performance Class A - Theory
Performance Class A - Theory
What is the effect of an inoperative anti-skid system on aeroplane performance?
Select the answer:Select the answer
1 correct answer
A.
The Regulated Take-Off Mass (RTOM) is only affected on a wet runway.
B.
The performance remains unaffected when using an auto-brake system and thrust reversers.
C.
It increases the landing distance required due to a reduced braking capability.
D.
V1 remains the same, but the Regulated Take-Off Mass (RTOM) decreases.
An inoperative anti-skid system on an aeroplane increases the landing distance required as it results in reduced braking capability.
Low temperatures, high pressure altitudes, low humidity.
C.
High temperatures, high pressure altitudes, high humidity.
D.
High temperatures, low pressure altitudes, high humidity.
VMC (Minimum Control Speed) would be lowest under conditions of high temperatures, high pressure altitudes, and high humidity.
Right Answer: C
Quiz
Question 10/1010/10
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Performance Class B - Use Of Data
Refer to figure or CAP697 file 2.1.
Given the following information, what is the required fuel to climb?
Airport Pressure Altitude: 4000 ft
Airport OAT: +10°C
Climb to: FL100
OAT at FL100: -5°C T
Take-Off Mass: 3400 lb
Gear: up
CPL (A / IR) Performance practice exam Practice test unlocks all online simulator questions
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Info quiz:
Quiz name:CPL (A / IR) Performance practice exam
Total number of questions:422
Number of questions for the test:100
Pass score:70%
Number of topics:4 Topics
Study topics:Number of questions:
Performance Class A - Theory:222 Questions
Performance Class A - Use Of Data:55 Questions
Performance Class B - Theory:102 Questions
Performance Class B - Use Of Data:43 Questions
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