Canadian ATPL SARON Frequently Tested
Exam Questions With Verified Multiple Choice
and Conceptual Actual 100%
Correct Detailed Answers
Guaranteed Pass!!Current Update!!
1. In a pressurized aircraft, the outflow valve controls:
A. Oxygen flow
B. Fuel vapour pressure
C. Rate of air leaving the cabin
D. Temperature differential
2. Rapid cabin depressurization symptoms include:
A. Slow ear equalization
B. Fogging, loud noise, and rapid temperature drop
C. Increase in altitude reading
D. Autopilot disconnect
3. The point where the aircraft can divert with equal time to two airports is the:
A. PNR
B. ETP 3
C. ETP (Equal Time Point)
D. CPDLC point
,4. The critical point (CP) uses what primary factor?
A. Cost index
B. Magnetic variation
C. Fuel burn comparison between continuing and returning
D. Vertical wind shear
5. Which factor increases Vmcg?
A. Lower temperature
B. Lower thrust setting
C. Wet or contaminated runway
D. Forward CG position
6. Which factor increases Vmca?
A. Reduced bank angle
B. Aft centre of gravity
C. Lower aircraft weight
D. Higher density altitude
7. A jet aircraft increases its stall speed when:
A. Altitude increases
B. Weight increases
C. Flaps are extended
D. CG moves forward
8. The purpose of a Mach trimmer is to:
A. Control yaw at high altitude
B. Prevent flameouts
, C. Compensate for Mach tuck at high speed
D. Reduce trim drag during climb
9. Critical Mach number is defined as:
A. Mach at which lift equals drag
B. Mach at which airflow first becomes supersonic on the wing
C. Max cruise Mach
D. Mach at which buffet begins
10. A swept wing design generally results in:
A. Higher stall speed and weaker tip vortices
B. Lower drag at low speed
C. Higher critical Mach and delayed compressibility effects
D. No effect on stability
11. Routine fuel checks must be performed:
A. Every 30 minutes
B. Every 60 minutes or as directed by SOPs
C. Only before top of descent
D. Only when ATC requests
12. When taxiing in strong quartering tailwind, the correct control inputs are:
A. Neutral elevators, ailerons into wind
B. Ailerons downwind, elevators down
C. Ailerons into wind, elevators up
D. Level ailerons, elevators neutral
Exam Questions With Verified Multiple Choice
and Conceptual Actual 100%
Correct Detailed Answers
Guaranteed Pass!!Current Update!!
1. In a pressurized aircraft, the outflow valve controls:
A. Oxygen flow
B. Fuel vapour pressure
C. Rate of air leaving the cabin
D. Temperature differential
2. Rapid cabin depressurization symptoms include:
A. Slow ear equalization
B. Fogging, loud noise, and rapid temperature drop
C. Increase in altitude reading
D. Autopilot disconnect
3. The point where the aircraft can divert with equal time to two airports is the:
A. PNR
B. ETP 3
C. ETP (Equal Time Point)
D. CPDLC point
,4. The critical point (CP) uses what primary factor?
A. Cost index
B. Magnetic variation
C. Fuel burn comparison between continuing and returning
D. Vertical wind shear
5. Which factor increases Vmcg?
A. Lower temperature
B. Lower thrust setting
C. Wet or contaminated runway
D. Forward CG position
6. Which factor increases Vmca?
A. Reduced bank angle
B. Aft centre of gravity
C. Lower aircraft weight
D. Higher density altitude
7. A jet aircraft increases its stall speed when:
A. Altitude increases
B. Weight increases
C. Flaps are extended
D. CG moves forward
8. The purpose of a Mach trimmer is to:
A. Control yaw at high altitude
B. Prevent flameouts
, C. Compensate for Mach tuck at high speed
D. Reduce trim drag during climb
9. Critical Mach number is defined as:
A. Mach at which lift equals drag
B. Mach at which airflow first becomes supersonic on the wing
C. Max cruise Mach
D. Mach at which buffet begins
10. A swept wing design generally results in:
A. Higher stall speed and weaker tip vortices
B. Lower drag at low speed
C. Higher critical Mach and delayed compressibility effects
D. No effect on stability
11. Routine fuel checks must be performed:
A. Every 30 minutes
B. Every 60 minutes or as directed by SOPs
C. Only before top of descent
D. Only when ATC requests
12. When taxiing in strong quartering tailwind, the correct control inputs are:
A. Neutral elevators, ailerons into wind
B. Ailerons downwind, elevators down
C. Ailerons into wind, elevators up
D. Level ailerons, elevators neutral
