
Commercial Pilot Instrument Rating Test
Authored by MUHAMMAD FARIDH
Professional Development
Professional Development
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21 questions
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1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
The following are the rules governing Air operator certification (AOC), except:
CASR Part 135
CASR Part 121
CASR Part 119
CASR Part 91
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the minimum visibility required for VFR flight in controlled airspace?
10 statute miles
1 statute mile
3 statute miles
5 statute miles
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How does weight affect aircraft performance during takeoff?
Increased weight improves takeoff speed and reduces distance.
Weight has no effect on takeoff performance.
Increased weight requires a longer takeoff distance and reduces climb performance.
Lighter aircraft require longer takeoff distances.
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the purpose of the Aircraft Performance Charts?
The purpose of the Aircraft Performance Charts is to provide data for evaluating aircraft performance under different conditions.
To determine the color scheme of the aircraft.
To calculate fuel consumption during flight.
To provide maintenance schedules for the aircraft.
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the difference between true airspeed and indicated airspeed?
Indicated airspeed accounts for wind speed, while true airspeed does not.
Indicated airspeed is the speed shown on the airspeed indicator, while true airspeed is the actual speed of the aircraft through the air.
True airspeed is measured on the ground, while indicated airspeed is in the air.
Indicated airspeed is always higher than true airspeed.
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What are the primary navigation systems used in modern aircraft?
Visual Flight Rules
GPS, Inertial Navigation Systems (INS), Flight Management Systems (FMS)
Ground-Based Navigation Systems
Radio Navigation Systems
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How do you calculate the wind correction angle for a flight?
WCA = wind speed + ground speed
WCA = arcsin((wind speed / ground speed) * sin(wind angle))
WCA = (ground speed - wind speed) * cos(wind angle)
WCA = tan(wind angle / ground speed)
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