.
The aircraft is below the glide slope [G/S]; and you must decrease the ROD in order to come back to the G/S; in addition; you must increase the bank angle in order to prevent the 'overturn'
The aircraft is presently on the G/S; but you must decrease the ROD in order to maintain the G/S; in addition; you must decrease the bank angle in order to prevent the 'under turn'
The aircraft is above the glide slope [G/S]; and you must increase the ROD in order to come back to the G/S; in addition; you must increase the bank angle in order to prevent the 'overturn'
The HSI and FD readings are contradictory
1
2
3
4
170 Degrees [C]
160 Degrees [C]
200 Degrees [C]
190 Degrees [C]
Read zero ft/min rates of climb or descent
Over read
Under read
Read normally
Prevent drift/topple of the spin axis
Sense topples of the spin axis
Provide current for the fast erect circuit
Prevent the gyro from toppling when power is removed from the instrument
Altitude 195' ft
Altitude 186' ft
Altitude 223' ft
Altitude 205' ft
Static pressure fed to an open capsule
Pitot pressure fed to an open capsule
Static pressure fed into a gas tight casing; but outside a partially evacuated capsule
Static pressure fed outside a completely evacuated aneroid capsule
Pilot and copilot altimeters is more than 75 feet in flight
Pilot and copilot altimeters is more than 75 feet on the ground
Known field elevation and the indicated altitude is more than 75 feet
Indicated altitude and the altitude reported by ATS is more than 100 feet
OAT corrected for altitude
Ambient temperature minus the ram rise from adiabatic compression of the boundary layer
SAT +100% ram rise when TA probe recovery factor is equal to 1.0
When the airplane is stationary
When the airplane is stationary
At airplane speeds above mach 0.30
At ISA conditions
At low flight altitude
0.5 Degrees from localizer center line; and 2.5 Degrees from VOR radial
10 Degrees from localizer center line; and 5 Degrees from VOR radial
1.25 Degrees from localizer center line; and 5 Degrees from VOR radial
5 Degrees from localizer center line; and 10 Degrees from VOR radial
There will be significant errors in both pitch and roll
The indications will be correct for a given TAS and rate of turn
The indications will be correct in pitch only
The indications will be correct in roll only
Descent at 500 FT/MIN
Climb at 500 FT/MIN
Descent at 250 FT/MIN
Zero
The ratio of IAS to local sound speed
The ratio of TAS to local sound speed
The speed at which compressibility correction must be calculated
The ratio of EAS to local sound speed at that temperature
A descending turn to the left
A climbing turn to the left
A descending turn to the right
A climbing turn to the right
Height
Altitude above the airport
Flight level above TDZN
Elevation above AMSL
A bank to the right
A bank to the left
A level attitude
Will not move
A bank to the right
A bank to the left
A level attitude
Will not move
Dynamic pressure minus pitot excess
Dynamic pressure plus pitot excess
Atmospheric pressure
Pitot excess pressure
A temporary increase in lag error
A lower pressure error than with normal sources
An increase in position error
No change in position error
Change of electrical resistance of the two metals
Change of electrical resistance with temperature
Change of electrical resistance with change in pressure
Change of electrical capacitance with change In temperature
Real wander only; in the horizontal plane
Wander; real or apparent; in the vertical plane
Apparent wander only; in the horizontal plane
Wander; real or apparent; in the horizontal plane
Rotation of the earth
Clear air turbulence
Gimbal friction
External torque
The aircraft will turn faster than indicated
The instrument will over-read
The rate of turn indicated will be unaffected
The radius of the turn will decrease
The captain's CRT only
The co-pilot CRT only
A special screen
On both the captain's and the co-pilot's CRTs
Red; yellow; green
Yellow; green; red
Green; yellow; red
Red; green; yellow
Descends below 500ft radio altitude with gear retracted
Is below 1000ft radio altitude and more than 1.3 dots below the ILS glide path
Descend below 200ft radio altitude with flaps retracted
Sinks more than approximately 10% of accumulated altitude
500 ft
700 ft
200 ft
790 ft
Is another name for an autopilot system
Applies flight data to the auto pilot system
Is automatically disengaged by a GPWS alert
Can only be used in EFIS equipped aircraft
208 Degrees [C]
175 Degrees [C]
155 Degrees [C]
185 Degrees [C]
The nose of the aircraft; downwards; deviation
The north magnetic pole; downwards; variation
The nearest pole; downwards; declination
The north magnetic pole; downwards; dip
Varies with the heading of the aircraft
Increases as the magnetic variation increases
Increases as magnetic latitude increases
Is greatest at the magnetic equator
Acceleration error; turning error; altitude error; transport wander; rotor speed error
Gimballing error; random wander; apparent wander; rotor speed error; transport wander
Gimballing error; looping error; rolling error; rotor speed error; transport wander
Transport wander; apparent wander; latitude error; turning error; acceleration error
You are at an altitude of more than 12;000' ft AMSL
You maintain an altitude of 12;000'ft AMSL
You are at an altitude of less 12;000'ft AMSL
No answer is correct
This topple is sensed by a mercury switch lying in the fore and AFT plane; and energizes a torque motor which applies a force about the athwartships axis
This topple is sensed by a mercury switch lying in the athwartships plane; and energizes a torque motor which applies a force-about the fore and AFTaxis
This topple is sensed by a mercury switch lying in the fore and AFT plane; and energizes a torque motor which applies a force about the fore and AFT axis
This topple is sensed by a mercury switch lying in the athwartships plane; and energizes a torque motor which applies force about the athwartshipsaxis
Static pressure fed outside a sealed capsule and pitot pressure fed in to a second open capsule
Static pressure fed outside a sealed capsule
Pitot pressure fed in to an open capsule and static pressure fed outside the capsule
Static pressure fed out side a restrictive choke
Before the desired heading is reached
After the desired heading is passed
When the desired heading is reached
When the desired heading is reached; if the turn bank less than 30 Degrees
Correct indications with an Increase in residual dip
Correct indications with a decrease in residual dip
Will cause the compass to indicate a turn toward North
Will cause the compass to indicate a turn toward South
The strength of the calibrated springs
The speed of rotation and the plane of rotation of the rotor
The speed; radius and mass of the rotor
The precession and moment of inertia of the rotor
Over-read
Under-read
Return to zero
Over read for short time; than return to zero
Iron; steel; carbon-fibre
Nickel; iron; steel
Copper; iron; carbon steel
Iron; cobalt steel; chromium steel
Corrected outside air temperature
The ram rise
The recovery factor
Hot ramp radiation
Causes over reading of the ASI at all levels whenever TAS exceeds 300kt
Causes over reading of the ASI whenever CAS exceeds 300kt
Is calibrated out of the ASI at MSL ISA conditions and only causes overreading when air density is decreased and CAS exceeds 300kt
Is calibrated out of the ASI at MSL ISA conditions and only causes overreading when air density is decreased and TAS exceeds 300kt
CAS will decrease
EAS will increase
TAS will Increase
TAS will decrease
The ramp position has been inserted and checked
The platform is levelled
The gyros and accelerometers are in the 'null' position
The green 'ready NAV' light has been illuminated and the mode selector switch has been set to the 'NAV' position
Is attached to the aircraft such; that It is free to rotate to align itself with the earth's magnetic field
Is fed with an exciting current; which Is DC
Supplies current directly to the stator coils of the magnetic synchronizing unit
Supplies current directly to the precession coils on the gyro compass units
When the air is warmer than standard; you are lower than your altimeter indicates
When the air is warmer than standard; you are higher than your altimeter indicates
When the air is cooler than standard; you are higher than your altimeter indicates
No any effect
223 ft
106 ft
425 ft
160 ft
Quiz Review Timeline (Updated): Apr 7, 2018 +
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.