If you are a member of the air force, you need to be conversant with the ATPL systems and monitor them and notice changes; how attentive have you been in your training so far? Do you feel confident enough to take this trivia on airplane ATPL systems and performance? Do give it a try, and keep on revising!
Angle of climb and endurance
Angle of climb and range
Rate of climb and range
Rate of climb and endurance
Rate this question:
Most forward
Most rearward
At the CP position
Mid range
Rate this question:
The weight side force
The asymmetric thrust
The side slip force
The torque effect
Rate this question:
Trim tab
Servo tab
Spring loaded tab
Lagging tab
Rate this question:
Increase in chordwise airflow
Decrease in chordwise airflow
Decrease in spanwise airflow
Increase in spanwise airflow
Rate this question:
The flap load relief system
The flap lockout system
The flap asymmetry system
The flap brake
Rate this question:
CD by controlling chordwise airflow over the wings
CL by controlling chordwise airflow over the wings
CD by controlling spanwise airflow over the wings
CL by controlling spanwise airflow over the wings
Rate this question:
All systems at all times
One system at a time
Two systems at all times
The system with the highest pressure
Rate this question:
Decreases
Increases
Remains constant
Rate this question:
Increase pressure and temperature
Decrease pressure and temperature
Decrease pressure, increase temperature
Increase pressure, decrease temperature
Rate this question:
Isobaric and differential ranges
Positive and differential ranges
Positive and negative ranges
Negative and differential ranges
Rate this question:
An emergency plug for puncture inflicted on landing
For pressure relief during conditions of excessive tyre heat
As temperature cooling valve during conditions of excessive tyre heat
As an indicator of excessive hard braking during landing
Rate this question:
Shuttle valve
Check valve
Pressure relief valve
Hydraulic fuse
Rate this question:
Divergent passages
Axial force
Air foil sections
Convergent passages
Rate this question:
Equalise pressure and propagate fuel through all flame tubes
Equalise temperature and propagate fuel through all flame tubes
Equalise pressure and propagate combustion through all flame tubes
Equalise temperature and propagate flame through all flame tubes
Rate this question:
Exhaust gas discharge angle is aerodynamically limited
Engine is rpm limited
Turbine is not as effective due to building up of backpressure
Ingestion of exhaust gas causes loss of engine efficiency
Rate this question:
Gs, gyro and comp
Gs, vor/loc and comp
Vor/loc, compass and comp
Gyro, compass and comp
Rate this question:
Vertical speed
Approach speed
Descent speed
Engine rotation speed
Rate this question:
A coordinated turn
A set rate of climb and descent
Coordinated climb and descent
A level turn
Rate this question:
Increase rate and angle of climb
Increase angle of climb
Increase rate of climb
Not change angle or rate of climb
Rate this question:
The captain’s altimeter
The co-pilot’s altimeter
The Air Data Computer (ADC)
The autopilot aneroid
Rate this question:
1 AC/ DC system
2 AC/DC»systems
3 AC/ DC systems
4 AC/ DC systems
Rate this question:
Lift equals weight and thrust equals drag
Lift is greater than weight and thrust is greater than drag
Lift is less than weight and thrust is less than drag
Lift is less than weight and thrust is greater than drag
Rate this question:
Plan
Map
VOR
Rate this question:
It will be totally blank
It will switch to the display currently existing on the right EHSI
It will be unaffected
It will display a MAP failure flag
Rate this question:
High pressure compressor stages
Low pressure compressor stages
Turbine outlet
Compressor outlet
Rate this question:
Shorter charge time
Less Corrosive
Do not require venting
Higher load carrying capacity
Rate this question:
Each pilot's flight controls are powered from a separate hydraulic system; the third system is on standby, cutting in automatically if one of the first two systems fail
Both pilot's flight controls are powered from a primary hydraulic system; the other two systems are on standby, cutting in automatically if the primary system fails
Both pilot's flight controls are powered from all three systems simultaneously
Both pilot's flight controls are powered from two main hydraulic systems simultaneously; the third system is on standby; cutting in automatically if any of the two main systems fail
Rate this question:
Temperature
Density
Pressure altitude
Aerodrome altitude
Rate this question:
Minimum drag speed with zero flap
Minimum drag speed with takeoff flap
The minimum safe speed with zero flap
The minimum safe speed with takeoff flap
Rate this question:
Up
Down
Faired
Automatically adjusted by the autopilot
Rate this question:
Move left
Move right
Stay centered
Remain half a ball out to the right
Rate this question:
Overhead lights are too bright
The screens are overheating
The power source has failed
The symbol generator has failed
Rate this question:
As high as possible
As low as possible
Lower rather than higher
Higher rather than lower
Rate this question:
Simultaneously enter inputs to the FMC's subsystems
Enter the fuel on board and the required flight fuel reserves
Input the AUW and CG position
Change the original entered flight plan while in-flight
Specify ETA's for destination and enroute waypoints
Rate this question:
Landing airfield elevation and cabin rate of change
Cabin altitude and cruise altitude
Required differential pressure and landing altitude
Cruise altitude and cabin rate of change
Rate this question:
Up and left
Up and right
Down and left
Down and right
Rate this question:
Up and left
Up and right
Down and left
Down and right
Rate this question:
Up and left
Up and right
Down and left
Down and right
Rate this question:
EGT rise
Compressor surge
Compressor stall
Thrust increase
Rate this question:
1 kg of AVTUR
1L of AVTUR
Neither, the range is the same for both
Either, it depends on the temperature
Rate this question:
Fully closed until the desired cruise altitude is reached
Automatically controlled by the cabin pressure controller
Fully closed until the desired cabin altitude is reached
Pilot selects position with an outflow valve knob
Rate this question:
Smaller because of the smaller mass airflow
Larger because of the larger mass air flow
Larger because of the smaller mass airflow
Smaller because of the large mass air flow
Rate this question:
Engine-driven pumps
The hand pump
Boost pumps
The Accumulator
Rate this question:
Centralise the nose wheel
Limit the amount of turn
Allow the nose wheel to swivel
Prevents nosewheel shimmy
Rate this question:
Quiz Review Timeline (Updated): Mar 21, 2023 +
Our quizzes are rigorously reviewed, monitored and continuously updated by our expert board to maintain accuracy, relevance, and timeliness.
Wait!
Here's an interesting quiz for you.