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Commercial Pilot Instrument Rating Test

Authored by MUHAMMAD FARIDH

Professional Development

Professional Development

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Commercial Pilot Instrument Rating Test
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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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