GNAV ATPL EXAM QUESTIONS &
ANSWERS
According to Learning Objective 061.01.08.01.01, the average TAS for climb problems
is calculated at an altitude that is __________ of the cruising altitude. - Correct Answers
-2/3)
According to Learning Objective 061.01.08.01.02, the average TAS for descent
problems is calculated at an altitude that is __________ of the descent altitude. -
Correct Answers -1/2)
During a level turn, if the bank angle steadily increases, the aircraft is experiencing a
__________ instability. - Correct Answers -spiral)
The angle between the lateral axis and the horizontal plane is known as the
__________ angle. - Correct Answers -bank)
When flying in icing conditions, the lift is __________, and the drag is __________. -
Correct Answers -decreased, increased)
In the event of a yaw damper failure, pilots can counteract Dutch roll by __________
altitude and __________ Mach number. - Correct Answers -reducing, decreasing)
When an aircraft's IAS decreases, its maneuverability __________ for a given control
surface deflection. - Correct Answers -decreases)
if sunrise at E is 2:43 then at W
it will be 5h later - Correct Answers -hence the 7:43.
Drift formula - Correct Answers -Drift = Cross Wind Component x (60/TAS)
the rhumb line track and the great circle track are _____
At the mid point!! - Correct Answers -parallel.
1 Nm = ?? km - Correct Answers -1.852 km
ANSWERS
According to Learning Objective 061.01.08.01.01, the average TAS for climb problems
is calculated at an altitude that is __________ of the cruising altitude. - Correct Answers
-2/3)
According to Learning Objective 061.01.08.01.02, the average TAS for descent
problems is calculated at an altitude that is __________ of the descent altitude. -
Correct Answers -1/2)
During a level turn, if the bank angle steadily increases, the aircraft is experiencing a
__________ instability. - Correct Answers -spiral)
The angle between the lateral axis and the horizontal plane is known as the
__________ angle. - Correct Answers -bank)
When flying in icing conditions, the lift is __________, and the drag is __________. -
Correct Answers -decreased, increased)
In the event of a yaw damper failure, pilots can counteract Dutch roll by __________
altitude and __________ Mach number. - Correct Answers -reducing, decreasing)
When an aircraft's IAS decreases, its maneuverability __________ for a given control
surface deflection. - Correct Answers -decreases)
if sunrise at E is 2:43 then at W
it will be 5h later - Correct Answers -hence the 7:43.
Drift formula - Correct Answers -Drift = Cross Wind Component x (60/TAS)
the rhumb line track and the great circle track are _____
At the mid point!! - Correct Answers -parallel.
1 Nm = ?? km - Correct Answers -1.852 km
