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CPL Test Series
Question Bank
Questions for REVISION
Answer the following questions
Test Mode
Training Mode
1. What does a radio altimeter, for an aircraft in the landing configuration, measure
height of the aircraft above the ground
altitude of the aircraft wheels
height of aircraft wheels above the ground
altitude of the aircraft
2. What is the speed of sound at 25,000 ft and -28 degrees C
601kts
624kts
618kts
610kts
3. What will the altimeter read if the layers beneath the aircraft are all colder than standard?
read higher then the real altitude
readings will fluctuate
read the correct altitude
read lower than the real altitude
4. What is the principle of operation of a VSI
static pressure in a capsule
differential pressure across a capsule
total pressure in a capsule
dynamic pressure in a capsule
5. During a descent at constant CAS and total temperature, the mach no:
increases
decreases
remains constant
increases if SAT is greater than standard temperature and decreases if it is lower
6. If an aircraft climbs, at constant mach No, in ISA conditions what happens to the TAS and the CAS?
TAS decreases and CAS decreases
TAS remains constant and CAS decreases
TAS increases and CAS increases
TAS decreases and CAS increases
7. QNH is
the equivalent sea level pressure at the airfield
the setting that will give zero indication on the airfield
the airfield barometric pressure
the setting that will indicate airfield height
8. The flux valve in a RIMC
is fed with DC.
is supplied with AC current (usually 487.5 Hz).
is made of perm-alloy magnetic steel.
has its own self exciter unit.
9. A compass swing is used to
get true north and lubber line aligned.
align compass north with magnetic north.
align magnetic north with true north
align compass north with true north.
10. The white arc on the ASI indicates
VS0 at the lower end and VLE at the upper end
VS0 at the lower end and VFE at the upper end
VS1 at the lower end and VFE at the upper end
VS1 at the lower end and VLE at the upper end
11. Descending from FL390 at maximum groundspeed, what will the pilot be limited by
VMO initially then MMO at a specified altitude
VNE initially then MMO at a specified altitude
VNO initially then VNE at a specified altitude
MMO initially then VMO at a specified altitude
12. What is the input to a VSI?
static pressure
differential pressure
dynamic pressure
total pressure
13. If an aircraft is descending at constant mach number, and the total air temperature remains constant, what happens to the CAS?
remains constant
increases
decreases
increases if the temperature is below standard, and decreases if the temperature is above standard
14. What is the speed of sound at 30,000 ft and -40 degrees C.
562kts
590kts
595kts
661kts
15. An aircraft is flying at constant indicated altitude, over a cold airmass. The altimeter reading will be
less than the real altitude
greater than the real altitude
standard altitude
same as the real altitude
16. In a gyro magnetic compass, where does the torque motor get its information from?
the flux gate
the rotor gimbal
amplifier
error detector
17. What is the normal operating range of a low altitude Radio Altimeter?
0 to 2,500ft
50ft to 2500ft
0 to 7,500ft
0 to 10,000ft
18. A direction gyro gets its directional information from
direct reading magnetic compass
flight director
air data computer
flux valve
19. A radio altimeter is
ground based and measures true height.
a/c based and measures true height
a/c based and measures true altitude.
ground based and measures true altitude.
20. In a Gyro magnetic Compass the flux gate transmits information to the
error detector
erecting system
heading indicator
amplifier
21. A standby artificial horizon must have the following properties: 1. a remote gyro 2. its own power supply 3. only to be used in emergency 4. its own gyro 5. one for each certified pilot
2 & 4
2, 3, & 4
all the above
1,3, & 5
22. The pendulous type correction detector fitted to the DGI provides
pendulous internal nozzle on the outer gimbal
one torque motor
torque on the sensitive axis
two torque motors on the horizontal axis
23. A 2 axis gyro, measuring vertical changes will have
one degree of freedom, horizontal axis
two degrees of freedom, horizontal axis
two degrees of freedom, vertical axis
one degree of freedom, vertical axis
24. The Primary Flying Display (PFD) displays information dedicated to
weather radar
engine data and alarms
aircraft systems
flight path
25. In an altimeter what is fed to: the capsule (i) and to the case (ii)?
(i) static input (ii) vacuum
(i) total input (ii) ambient input
(i) pitot input (ii) static input
(i) vacuum (ii) static input
26. What is the maximum drift of a gyro, due to earth rate
15° per hour
5° per hour
90° per hour
180° per hour
27. In a turn at constant angle of bank ... the rate of turn is
independent of weight and proportional a to TAS
dependant on weight and proportional to TAS
independent of weight and inversely proportional a to TAS
dependant on weight and inversely proportional to TAS
28. An RMI rose is mechanically stuck on 090 degrees. The ADF pointer indicates 225 degrees. What is the relative bearing to the beacon?
225 degrees.
135 degrees.
Cannot be determined.
000 degrees.
29. If the needle and the ball of a Turn & Slip indicator both show right, what does it indicate
turn to right & too much bank
turn to left & too little bank
turn to left & too much bank
turn to right & too little bank
30. Density altitude is defined as
the altitude reading on the altimeter which has QNH set on it
the altitude showing on the altimeter with the lowest regional QNH set
the altitude corresponding to the standard atmosphere compensated for ambient density
the altitude of the airfield elevation corrected for Lapse Rate
31. An aircraft turns right, through 900, onto North, at 48N, using a direct indicating compass. The aircraft is turning at rate 2. What heading should the aircraft roll out on?
030°
010°
350°
330°
32. A low altitude Radio Altimeter, used in precision approaches, has the following characteristics: 1. 1540MHz to 1660 MHz range 2. pulse transmissions 3. frequency modulation 4. height range between 0 and 5,000ft 5. an accuracy of +/- 2ft between 0 and 500ft
3 and 5
3 and 4
1, 4 and 5
2, 3 and 5
33. What principle does the radio altimeter work on?
pulse modulation and carrier wave
frequency modulation and carrier wave
amplitude modulation
pulse modulation
34. What does the blue line on an ASI of a twin propeller engined aircraft indicate?
VMCA
VNO
VYSE
VFE
35. An aircraft is taking of on a runway heading 0450, in still air, with a compass having 00 deviation. The runway is on an agonic line. What are the northerly turning errors (northern hemisphere)?
compass stays on 045° if wings are kept level
compass moves to less than 045°
compass remains on 045°
compass moves to more than 045°
36. From where does the air data computer (ADC) obtain aircraft altitude?
OAT probe
IRS
absolute barometric sensor on aircraft fuselage
dynamic – absolute ambient pressure
37. In a Remote Indicating Compass, what component feeds the Amplifier?
annunciator
gyro precession signal
flux valve
error detector
38. A machmeter measures the ratio of;
pitot pressure to (static pressure times pitot pressure)
pitot pressure times static pressure
(pitot pressure minus static pressure) to static pressure
pitot pressure to static pressure
39. The Pitot tube comprises a mast to position it below the skin of the aircraft for
easy access for maintenance
position it outside the boundary layer
avoid disturbance from aerodynamic flow about the aircraft
anti-ice protection
40. What are the components of a Ring Laser Gyro?
mirrors and 2 cavities
2 beams of laser light
2 anodes and 2 cathodes
horizontal gryo axis and 1 degree of freedom
41. You are flying at a constant FL 290 and constant mach number. The total temperature increases by 50. The CAS will
decrease by 10 kts
increase by 10 kts
remain approximately constant
will increase or decrease depending on whether you are above or below ISA.
42. If an aircraft, fitted with a DRMC, takes off on a westerly heading, in the northern hemisphere, the DRMC will indicate
a turn to south
oscillates about west
a turn to the north
no turn
43. If a constant CAS is maintained in a climb, what happens to the mach number
increases
decreases
remains constant
44. The component(s) used to align an inertial strap-down unit in the horizontal plane is/are
Accelerometers and gyroscopes
Accelerometers
Flow inductors
Gyroscopes
45. In a DGI what error is caused by the gyro movement relative to the earth?
Earth Rate
Transport Wander
real wander
latitude error
46. An aircraft is flying a true track of 360° from 5° south to 5° north. What is the change in apparent wander rate
- 5° per hour
0° per hour
depends upon groundspeed
+ 5° per hour
47. The green arc on the ASI is used to identify which speed range
V S1 to V FE
V S1 to V NO
V S1 to V LO
V SO to V NO
48. What aircraft system uses a frequency of 4,400 MHz?
weather radar
ATC radar
SSR
radio altimeter
49. What are the advantages of a laser gyro compared to a conventional gyro?
takes longer to align
uses more power
has a longer cycle life
takes longer to set up/ spin up
50. When descending from FL230 to FL50 at maximum speed, the limitations which apply are
MMO then VMO
MMO
VMO
VMO then MMO
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