WorksheetsATRN215 FINAL EXAM 2025
Total questions: 50
Worksheet time: 25mins
Aircraft Instruments that use air pressure differential to provide indication.
Airspeed Indicator
Vertical Speed Indicator
Altimeter
All of the above
The barometric pressure in the local area.
Static Pressure
Dynamic Pressure
QFE
QNE
As air becomes less dense, __ reduces because the propeller is less efficient in thin air.
Power
Lift
Thrust
Drag
It compares the information given by the static port and the pitot tube.
Altimeter
Vertical Speed Indicator
Airspeed Indicator
All of the Above
Is defined as “Speed in a particular direction”.
Vitesse
Velocity
Vitese
V-Speed
The slowest speed a plane can fly to maintain a level flight.
Rotation Speed
Maneuvering Speed
Best Glide Speed
Stall Speed
To check your ASI before takeoff;
Airspeed increasing at the correct rate
Blowing wind gives slight indication
Needle will initially point to zero
Apply breaks during full power
The average pressure exerted by the weight of the atmosphere is approximately
14.7 psi
1013.2 hPa
29.92 inHg
All of the Above
Atmospheric pressure at sea level is _.
0 psi
1 inHg
15 inHg
14.7 psi
A Mercurial Barometer uses Mercury because mercury is _ times more dense than water.
13.6
14.7
15
15.2
Dynamic Pressure is equal to
Airspeed
Altitude
Vertical Rate
Gravity
Refers to the relationship of wing chord to direction of oncoming wind.
Pitch Angle
Bank Angle
Angle of Attack
Best Angle
Found 31 miles above the surface.
Troposphere
Stratosphere
Mesosphere
Ionosphere
The slowest speed a plane can fly to maintain a level flight.
Best Glide Speed
Stall Speed
Maneuvering Speed
Slow Speed
IAS corrected for installation error and instrument error
Indicated Airspeed
Calibrated Airspeed
True Airspeed
Groundspeed
The most vital instruments installed on an aircraft.
Altimeter
Vertical Speed Indicator
Airspeed Indicator
All of the Above
Thousands of Feet in an Altimeter;
Triangular Needle
Short Needle
Long Needle
Circular Needle
Vertical distance between mean sea level and a point on the ground.
Altitude
Height
Elevation
Distance
The altitude indicated when the altimeter is set to 29.92 in Hg the standard pressure.
QNH
QNE
QFE
QTE
If you fly from an area of higher pressure to an area of lower pressure without resetting your altimeter, you may fly at a _ altitude than you intended.
Higher
Lower
Same
Unsure
Rate of turn is too great for the angle of bank.
SLIP TURN
SKID TURN
SKIP TURN
COORDINATED TURN
_ counter overbanking tendency.
Rudders
Yoke Up
Yoke Down
Ailerons
Not enough rudder causes _ turns.
SLIP TURN
SKID TURN
SKIP TURN
COORDINATED TURN
Force that pulls us towards the direction of the turn.
Centrifugal
Centripetal
Gravity
G
Rate of turn and bank angle are proportionate to each other.
SLIP TURN
SKID TURN
SKIP TURN
COORDINATED TURN
Using your rudder counteracts _.
Overbanking
Underbanking
Adverse Yaw
Adverse Turn
If you constantly turn at a Half Standard Rate it will take you _ seconds to do a full 180.
90
120
180
360
Turn in which heading changes by 3 degrees per second.
SLIP TURN
SKID TURN
SKIP TURN
COORDINATED TURN
A liquid filled, curved tube with a ball inside. Indicates the quality of turn.
Insinometer
Invenometer
Inclinometer
Invinometer
The 30 degree inclination of the Turn Coordinator’s gyro allows the instrument to also measure the rate of _ as we enter the turn.
Turn
Bank
Roll
Pitch
The gyro of the AI is oriented horizontally, so that the plane of rotation is parallel to the _.
Sky
Ground
Clouds
Horizon
This AI does NOT indicate whether the aircraft is climbing or descending, it indicates only the _.
Turn Angle
Bank Angle
Roll Angle
Pitch Angle
The axis along the aircraft’s wings.
Horizontal
Lateral
Vertical
All of the above
Your heading indicator will indicate as much as _ degrees error in half an hour of operation.
3
7.5
15
30
The HI’s gyro is oriented vertically, so that the plane of rotation is _ to the horizon.
Parallel
Perpendicular
Equal
Uncertain
Connect points with equal variation.
Agonic Line
Amonic Line
Igonic Line
Isogonic Line
The Magnetic Compass’ pointer are called.
Luber Line
Lubber Line
Lover Line
Loober Line
Effect increases as you approach the poles.
Variation
Deviation
Compass Error
Magnetic Dip
Compass error due to the disturbances from the magnetic fields.
Variation
Deviation
Compass Error
Magnetic Dip
During _, the magnetic compass will slightly turn toward the north in the Northern Hemisphere.
Acceleration
Deceleration
Compass Error
Magnetic Dip
This computer, rather than individual instruments, can determine the calibrated airspeed, Mach number, altitude, and altitude trend data from an aircraft's Pitot Static System.
Air Data Computer
Attitude and Heading Reference System
Air Data Inertial Reference Unit
Air Data Processor
Consists of sensors on three axes that provide attitude information for aircraft, including roll, pitch, and yaw.
Air Data Computer
Attitude and Heading Reference System
Air Data Inertial Reference Unit
Air Data Processor
A key component of the integrated Air Data Inertial Reference System (ADIRS), which supplies air data (airspeed, angle of attack and altitude) and inertial reference (position and attitude) information to the pilots.
Air Data Computer
Attitude and Heading Reference System
Air Data Inertial Reference Unit
Air Data Processor
Consolidates key flight information for pilots onto a single screen.
Primary Flight Display
Multi Function Display
Electronic Flight Display
Can change the color or shape of the data to alert the aircrew.
Primary Flight Display
Multi Function Display
Electronic Flight Display
On a PFD, the Kollsman Window is called as;
Altitude Reference Bug
Altitude Reference Box
Barometric Setting Box
Barometric Reference Bug
Vx indication on the ASI is _.
Best Rate of Climb
Best Angle of Climb
Best Glide Speed
Rotation Speed
Vy indication on the ASI is _.
Best Rate of Climb
Best Angle of Climb
Best Glide Speed
Rotation Speed
LCD means _.
Liquid Conceptual Display
Liquid Cognitive Display
Liquid Crystal Display
Liquid Crystal Design
The Horizontal Situation Indicator is commonly found on the _ side of a PFD standard format.
Center
Right
Left
Bottom
