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Quiz
Question 1/101/10
Subsonic Aerodynamics
Subsonic Aerodynamics
Subsonic Aerodynamics
An aeroplane flying with an airspeed of 200 kt and CL is equal to 0.6. The pilot is requested to increase speed to 250 kt by the ATC. The new CL is…
Select the answer:Select the answer
1 correct answer
A.
0.47
B.
0.38
C.
0.2
D.
0.40
The lift coefficient (CL) is directly proportional to the airspeed of the aeroplane. Therefore, when the pilot increases the airspeed from 200 kt to 250 kt, the new CL decreases accordingly. In this case, with the new airspeed of 250 kt, the new CL is calculated to be 0.38.
Right Answer: B
Quiz
Question 2/102/10
Propellers
Propellers
Propellers
For a twin-engine aeroplane, a reason for limiting a propeller's diameter is to...
Select the answer:Select the answer
1 correct answer
A.
avoid excessive propeller-tip velocities at high RPMs.
B.
increase ground clearance.
C.
avoid a reduction in power absorption.
D.
reduce the aeroplane's minimum control speed.
Limiting a propeller's diameter for a twin-engine aeroplane is necessary to avoid excessive propeller-tip velocities at high RPMs.
Right Answer: A
Quiz
Question 3/103/10
Stall, Mach Tuck, And Upset Prevention And Recovery
Stall, Mach Tuck, And Upset Prevention And Recovery
Stall, Mach Tuck, And Upset Prevention And Recovery
An aeroplane has a stall speed of 100 kt. When the aeroplane is flying a level co-ordinated turn with a load factor of 1.5, the aeroplane will stall in this turn at:
Select the answer:Select the answer
1 correct answer
A.
150 kt.
B.
122 kt.
C.
82 kt.
D.
141 kt.
In a level co-ordinated turn with a load factor of 1.5, the stall speed will increase by the square root of the load factor. Therefore, the aeroplane will stall in this turn at approximately 122 kt.
Right Answer: B
Quiz
Question 4/104/10
Limitations
Limitations
Limitations
The speed VC in gust diagram...
Select the answer:Select the answer
1 correct answer
A.
equals 55 ft/s.
B.
equals 50 ft/s.
C.
equals 25 ft/s.
D.
equals 66 ft/s.
In a gust diagram, the speed VC represents the minimum speed required to maintain level flight in turbulent conditions.
Right Answer: B
Quiz
Question 5/105/10
High-speed Aerodynamics
High-speed Aerodynamics
High-speed Aerodynamics
Assuming ISA conditions and a climb above the tropopause at constant Mach number and aeroplane mass, the:
(note: assume maintaining constant thrust)
Select the answer:Select the answer
1 correct answer
A.
IAS increases.
B.
TAS decreases.
C.
lift coefficient increases.
D.
lift coefficient decreases.
When climbing above the tropopause at constant Mach number and aeroplane mass, the lift coefficient increases due to the reduction in air density which requires higher lift to maintain level flight.
Right Answer: C
Quiz
Question 6/106/10
Flight Mechanics
Flight Mechanics
Flight Mechanics
After suspecting a fuel leak, the aircrew flying a jet transport aircraft decides to divert to the nearest suitable airport. At what speed should they fly?
Select the answer:Select the answer
1 correct answer
A.
Maximum Range Speed
B.
Maximum Endurance Speed
C.
MMO
D.
Long Range Speed
The aircrew should fly at Maximum Range Speed when diverting to the nearest suitable airport after suspecting a fuel leak in a jet transport aircraft.
Right Answer: A
Quiz
Question 7/107/10
Control
Control
Control
Outboard ailerons are (1) at (2) speeds, to prevent (3) .
Outboard ailerons are locked at high speeds, to prevent aileron reversal.
Right Answer: A
Quiz
Question 8/108/10
Stability
Stability
Stability
Dihedral contributes positively to lateral stability by:
Select the answer:Select the answer
1 correct answer
A.
Increasing lift on the wing away from the wind.
B.
Increasing drag on the wing away from the wind.
C.
Increasing the lift on the wing into the wind.
D.
Increasing drag on the wing into the wind.
Dihedral contributes positively to lateral stability by increasing the lift on the wing into the wind.
Right Answer: C
Quiz
Question 9/109/10
Subsonic Aerodynamics
Subsonic Aerodynamics
Subsonic Aerodynamics
Refer to figure. What does line 3 represent?
Select the answer:Select the answer
1 correct answer
A.
Induced drag
B.
Parasite drag
C.
Total drag
D.
Profile drag
.
Right Answer: A
Quiz
Question 10/1010/10
Propellers
Propellers
Propellers
In twin engine aeroplanes with propellers turning clockwise as seen from behind:
Select the answer:Select the answer
1 correct answer
A.
the left engine is the critical engine.
B.
the ‘minimum control speed’ is determined by the failure of the right engine.
C.
the left engine produces a higher yaw moment if the right engine fails than vice versa.
D.
the right engine is the critical engine.
In twin engine aeroplanes with propellers turning clockwise as seen from behind, the left engine is considered the critical engine because it produces more yawing moment in the event of an engine failure.
CPL (A / IR) Principles of flight practice exam Practice test unlocks all online simulator questions
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Info quiz:
Quiz name:CPL (A / IR) Principles of flight practice exam
Total number of questions:1204
Number of questions for the test:100
Pass score:70%
Number of topics:8 Topics
Study topics:Number of questions:
Control:77 Questions
Flight Mechanics:150 Questions
High-speed Aerodynamics:117 Questions
Limitations:59 Questions
Propellers:104 Questions
Stability:98 Questions
Stall, Mach Tuck, And Upset Prevention And Recovery:146 Questions
Subsonic Aerodynamics:453 Questions
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