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CPL Test Series
Question Bank
Questions for R* B*LI GYRO
Answer the following questions
Test Mode
Training Mode
1. An a/c turns left from Hdge 045° to 315° at rate 1. Time taken will be. Bank = TAS/10 + 7
90 sec
30 sec
45 sec
2. The basic properties of a gyroscope are: 1. The gyro's weight 2. The rigidity in space 3. The inertia 4. The high RPM 5. The precession. The combination of correct statements is
2, 5
3, 4
2, 3, 5
3. What should a turn and slip indicator show in a right turn on the ground?
Needle left and ball left
Needle left and ball right
Needle right and ball left
4. Gyro rigidity improve with?
Increasing RPM and mass but decreasing radial displacement of mass
Increasing RPM, mass and radial displacement of mass
Decreasing RPM but increasing mass and radial displacement of mass
5. When, in flight, the needle of a needle-and-ball indicator is on the right and the ball on the left, the aircraft is
turning left with too much bank
turning left with not enough bank
turning right with not enough bank
6. To maintain same rate of turn, if CAS is increased, bank should be
Same
Increased
Decreased
7. The maximum directional gyro error to the earth rotation is
4°/hour
15°/hour
20°/hour
8. The rate-of-turn is the
aircraft speed in a turn
pitch rate in a turn
change-of-heading rate of the aircraft
9. The number of degrees of freedom of a gyro is?
One more than the number of gimbals
One less than the number of gimbals
The same as the number of gimbals
10. In comparison to low level, to maintain same rate of turn, RAS at higher level is to be
Increased
Same
Decreased
11. A turn indicator is built around a gyroscope with
1 degree of freedom
3 degrees of freedom
0 degree of freedom
12. How many degrees of freedom and what is the spin axis of an attitude indiciator?
Local earth vertical two degrees of freedom
Aircraft lateral axis two degrees of freedom
Aircraft horizontal axis one degree of freedom
13. When turning at constant bank angle the rate of turn is?
Determined by weight
Determined by weight and TAS
Determined by TAS
14. How will a basic AI respond if an aircraft performs a 270 degree turn at constant bank angle and ROT?
Nose down and bank
Noise level and bank
Nose up and bank
15. An aircraft if flying at a 120kt true airspeed, In order to achieve a rate 1 turn, the pilot will have to bank the aircraft at an angle of
12°
19°
30°
16. Rigidity in a gyroscope is
the reaction 90° in the direction of rotation when applying force to the spinning wheel
a way to express the stability of the inner and outer gimbal rings
the tendency it has to remain in its plane of rotation and resist attempts to alter its position.
17. The properties of a gyro are? 1. Mass 2. Rigidity in space 3. Inertia 4. Precession 5. Rigidity with reference to the earth
1,2,3,5
1,2,3,4
1,3,4,5
18. On a TSI what does it indicate when the turn needle is out to the left and the ball out to the right?
Right turn with too much bank
Left turn with too little bank
Left turn with too much bank
19. What are the errors in a DGI? 1. Transport wander 2. Earth rate 3. Heading errors when banking and pitching, 4. Mechanical imperfections
1,2,4
All of the above
1,2,3
20. What factors affect the turn indicator? 1. AofA 2.AOB 3. TAS 4. Weight
2,3
1,2
1,3
21. Sources of power for Gyroscopic operations in an aircraft are
Vaccum, gravity and rigidity
Rigidity, rotor speed and movement of inertia
Vaccum, pressure and electrical
22. What type of gyro has a horizontal spin axis and one degree of freedom?
Rate integrating gyro
Displacement gyro
Rate gyro
23. Increasing altitude at constant TAS will ____ the angle of Bank required to achieve a rate 1 turn
Increase
Not affect
Decrease
24. When both the needle and ball of a turn and slip indicator are displaced to the right the aircraft is?
Turning right with insufficient TAS
Turning right with too much TAS
Turning left with too much TAS
25. On the ground, during a right turn, the turn indicator indicates
needle in the middle, ball to the right
needle to the right, ball to the right
needle to the right, ball to the left
26. What corrective action is required if the ball is out to the right in a left turn?
More right ruder
More left rudder
More left bank
27. What angle of bank is required to conduct a balanced rate 1 turn in an aircraft at 125 kts TAS at a mass of 55000 Kg?
17.5 degrees
15.5 degrees
19.5 degrees
28. The heading read on the dial of a directional gyro is subject to errors, one of which is due to the movement of the aircraft. This error
shows itself by an apparent rotation of the horizontal axis of the gyroscope which seems to turn at 15° per hour to the right in the northern hemisphere
is at its greatest valve when the aircraft follows a meridian track
is dependent on the ground speed of the aircraft, its true tack and the average latitude of the flight
29. The rate turn indicator uses a gyroscope: 1. with one degree of freedom 2. with two degrees of freedom 3. the frame of which is supported by two return springs 4. the spinning wheel axis of which is parallel to the pitch axis 5. the spinning wheel axis of which is parallel to the yawing axis 6. the spinning wheel axis of which is horizontal The combination of correct statements is
1,6
2,5
1,3
30. Following a left engine failure the pilot of a multi engine a/c uses rudder to oppose yaw and keeps the a/c on hdg while using bank to prevent side slip. The TSI will show
Needle central and ball to the right. Since a/c is maintained hdg; the a/c is not turning, so needle is central
Both needle and ball to the right
both needle and ball central
31. A/H indications are reliablie in
±85° pitch, ±90° roll
±85° pitch, ±180° roll
±55° pitch, ±85° roll
32. An a/c rolls out after 180° steep turn to the right with reference to natural horizon. A/H will show
Level and bank to the left
Climb and slight bank to the left
Climb and slight bank to the right
33. During an acceleration phase at constant attitude, the resetting principle of the artificial horizon results in the horizon bar indicating a
nose-down followed by a nose-up attitude
nose-up attitude
constant attitude
34. What are the essential properties of a turn indicator? 1. Two degrees of freedom 2. One degree of freedom 3. Horizontal spin axis 4. Vertical spin axis 5. Longitudinal spin axis
1,2
2,3
3,4
35. In a turn at constant rate, the turn indicator reading is
independent to the aircraft true airspeed
proportional to the aircraft true airspeed
inversely proportional to the aircraft true airspeed
36. Classic artificial horizon Indications turning through 180° at constant AOB?
Nose up and correct AOB
Nose up and AOB too high
Nose up and AOB too low
37. What will a classic artificial horizon indicate when turning through 90 degree at constant attitude and bank angle?
Too much bank and too much nose up attitude
Correct bank angle and attitude
Too little bank and too much nose up attitude
38. An a/c rolls out after 180° steep turn to the left with reference to natural horizon. A/H will show
Climb and slight turn to the right
Climb and slight bank to the left
Level and bank to the left
39. If the turn indicator needle is out to the right and the ball is out to the left, it indicates?
A left turn with too much bank
A right turn with too little bank
A left turn with too little bank
40. The ball in a serviceable slip indicator is _____ by _____ and _____ indicate the state of slip
Held central, gravity, does not always
Held central, gravity, always
Positioned, Acceleration, does not always
41. If the mass of the aircraft was decreased from 60000 Kg to 45000 Kg?
It would increase the required AOB
It would not affect the required AOB, but less power would be required
It would decrease the required AOB
42. What is the function of the altitude nut on a DI?
To correct Coriolis effect
To compensate for earth rate error
To compensate for latitude error
43. The characteristics of the directional gyro (DG) used in a gyro stabilized compass system are
two degrees of freedom, whose horizontal axis corresponding to the reference direction is maintained in the horizontal plane by an automatic erecting system
two degrees of freedom, whose axis aligned with the vertical to the location is maintained in this direction by an erecting system
one degree of freedom, whose vertical axis, aligned with the real vertical to the location is maintained in this direction by an automatic erecting system
44. In comparison to low level at higher level, if RAS is kept constant to maintain same rate. Bank is to be
Decreased
Same
Increased
45. Under normal operating conditions, when an aircraft is in banked turn, the rate-of-turn indicator is valuable gyroscopic flight control instrument; when it is associated with an attitude indicator it indicates: 1. the angular velocity of the aircraft about the yaw axis 2. the bank of the aircraft 3. the direction of the aircraft turn 4. the angular velocity of the aircraft about the real vertical The combination of correct statements is
1,2
1,3
3,4
46. For a coordinated rate 1 right turn at 250 Kts TAS, in clean configuration the correct AOB is approximately?
23 degrees
16 degrees
32 degrees
47. An airborne instrument, equipped with a gyro with 1 degree of freedom and horizontal spin axis is a
directional gyro
fluxgate compass
turn indicator
48. An airborne instrument, equipped with a gyro with 2 degrees of freedom and horizontal spin axis is
a directional gyro
a flux gate compass
a turn indicator
49. If the turn and slip indicator shows needle left and ball right in a banked turn, the aircraft is ____ and the required corrective actions is_____?
Skidding push left pedal forward
Skidding push right pedal forward
Slipping push left pedal forward
50. On the ground, during a left turn, the turn indicator indicates
needle to the left, ball to the right
needle in the middle, ball to the right
needle to the left, ball to the left
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