Email
info@vayudootaviation.com
Phone No
+91 7276526726
become a pilot
Home
About us
courses
CPL
ATPL
RTR(A)
Airline Cadet Program
IGRUA Entrance Prep
B.Sc. Aviation
Pilot Training
INDIA
USA
CANADA
SOUTH AFRICA
NEW ZEALAND
EUROPE
Aircraft Type-Rating
Airbus A320
Boeing 737
Blogs
contact
CPL Test Series
Question Bank
Questions for R* B*LI GYRO
Answer the following questions
Test Mode
Training Mode
1. To maintain same rate of turn, if CAS is increased, bank should be
Same
Decreased
Increased
2. The gimbal error of the directional gyro is due to the effect of
an apparent weight and an apparent vertical
a bank or pitch attitude of the aircraft
two slow procession on the horizontal gimbal ring
3. An airborne instrument, equipped with a gyro with 1 degree of freedom and horizontal spin axis is a
directional gyro
turn indicator
fluxgate compass
4. 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
5. When both the needle and ball of a turn and slip indicator are displaced to the right the aircraft is?
Turning left with too much TAS
Turning right with too much TAS
Turning right with insufficient TAS
6. ROT indications are?
Proportional to CAS
Proportional to mass
Proportional to TAS
7. The dither motor in a ring laser gyroscope?
Prevents or minimizes transport wander
Prevents laser lock
Stabilizes the frequency or the laser source
8. 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 little bank
A left turn with too much bank
A right turn with too little bank
9. What type of gyro has a horizontal spin axis and one degree of freedom?
Displacement gyro
Rate gyro
Rate integrating gyro
10. 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 right pedal forward
Slipping push left pedal forward
Skidding push left pedal forward
11. What would be the indication on an attitude indicator in a right turn?
Descent due to pendulous vanes
Climb due to pendulous vanes
No climb
12. What factors affect the turn indicator? 1. AofA 2.AOB 3. TAS 4. Weight
1,2
2,3
1,3
13. For a coordinated rate 1 left turn at an AOB of 27 degrees, the TAS should be?
200 Kts
250 kts
270 Kts
14. 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 right
Climb and slight bank to the left
15. What will be the immediate turn and slip indications when a left engine fails in climbing flight
Needle left and ball right
Needle and ball right
Needle and ball left
16. What corrective action is required if the ball is out to the right in a left turn?
More left bank
More right ruder
More left rudder
17. Sources of power for Gyroscopic operations in an aircraft are
Vaccum, pressure and electrical
Rigidity, rotor speed and movement of inertia
Vaccum, gravity and rigidity
18. The number of degrees of freedom of a gyro is?
The same as the number of gimbals
One more than the number of gimbals
One less than the number of gimbals
19. In comparison to low level, to maintain same rate of turn, RAS at higher level is to be
Increased
Same
Decreased
20. 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
1,3,4,5
1,2,3,4
21. Increasing altitude at constant TAS will ____ the angle of Bank required to achieve a rate 1 turn
Not affect
Increase
Decrease
22. A turn indicator is built around a gyroscope with
0 degree of freedom
3 degrees of freedom
1 degree of freedom
23. 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
24. The maximum directional gyro error to the earth rotation is
20°/hour
15°/hour
4°/hour
25. The rate-of-turn is the
pitch rate in a turn
change-of-heading rate of the aircraft
aircraft speed in a turn
26. If the mass of the aircraft was decreased from 60000 Kg to 45000 Kg?
It would decrease the required AOB
It would not affect the required AOB, but less power would be required
It would increase the required AOB
27. Classic artificial horizon Indications turning through 180° at constant AOB?
Nose up and AOB too low
Nose up and correct AOB
Nose up and AOB too high
28. When an aircraft has turned 270 degrees with a constant attitude and bank the pilot observes the following on a classic artificial horizon
attitude and bank correct
too much nose-up and bank too low
too much nose-up and bank correct
29. A turn indicator is an instrument which indicates rate of turn. Rate of turn depends on: 1. bank angle 2. aero plan speed 3. aero plane weight The combination of correct statements is
1,2
1,3
2,3
30. 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 dependent on the ground speed of the aircraft, its true tack and the average latitude of the flight
is at its greatest valve when the aircraft follows a meridian track
31. If the turn and slip indicator shows needle left and ball left in a banked turn, the aircraft is ____ and the required corrective action is ___?
Skidding push left pedal forward
Slipping push left pedal forward
Skidding push right pedal forward
32. 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?
19.5 degrees
15.5 degrees
17.5 degrees
33. A directional gyro is: 1. a gyroscope free around two axis 2. a gyroscope free around one axis 3. capable of self-orientation around an earth-tied direction 4. Incapable of self-orientation around an earth -tied direction. The combination of correct statements is
2,3
1,4
2,4
34. 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
1,2,3
All of the above
35. 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
36. When an aircraft has turned 360 degrees with a constant attitude and bank, the pilot observes the following on a classic artificial horizon
attitude and bank correct
too much nose-up and bank correct
too much nose-up and bank too high
37. When, in flight, the needle of a needle-and-ball indicator is on the left and the ball on the right, the aircraft is
turning left with not enough bank
turning left with too much bank
turning right with not enough bank
38. During take off roll an a/c fitted with vacuum driven A?H will show
Will read correct as a/c on ground (Irrespective of a/c position, indications will be the same)
Climb and bank to right
Only climb and no bank as a/c is on ground
39. 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
30°
12°
19°
40. 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
41. A turn indicator used in conjunction with an attitude indicator will show? 1. Turn direction 2. Rate of turn, 3. Angular velocity about the true vertical axis 4. Angular velocity about the aircraft vertical axis 5. Angular velocity about the longitudinal axis
1,2,4
1,3
1,2
42. Rigidity in a gyroscope is
the reaction 90° in the direction of rotation when applying force to the spinning wheel
the tendency it has to remain in its plane of rotation and resist attempts to alter its position.
a way to express the stability of the inner and outer gimbal rings
43. In a Turn-indicator, the measurement of a rate - of -turn consists of
high bank angles, in measuring the yaw rate
high bank angles, in measuring the roll rate
low bank angles, in measuring the yaw rate
44. 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
1,3
1,6
2,5
45. In the building principle of a gyroscope, the best efficiency is obtained through the concentration of the mass
on the periphery and with a high rotation speed
close to the axis and with a low rotation speed
on the periphery and with a low rotation speed
46. What is the function of the altitude nut on a DI?
To compensate for latitude error
To compensate for earth rate error
To correct Coriolis effect
47. An airborne instrument, equipped with a gyro with 2 degrees of freedom and horizontal spin axis is
a turn indicator
a directional gyro
a flux gate compass
48. The ball in a serviceable slip indicator is _____ by _____ and _____ indicate the state of slip
Held central, gravity, always
Positioned, Acceleration, does not always
Held central, gravity, does not always
49. When an aircraft has turned 90 degrees with a constant attitude and bank, the pilot observes the following on a classic artificial horizon
too much nose-up and bank too high
too much nose-up and bank too low
too much nose-up and bank correct
50. When, in flight, the needle and a ball of a needle-and-ball indicator are on the right, the aircraft is
turning left with not enough bank
turning right with too much bank
turning left with too much bank
Submit
Make New Set