ATTITUDE INDICATOR – Air – DGCA Question Bank For Politics

#1. Local earth vertical two degrees of freedom.

Aircraft lateral axis two degrees of freedom.

Aircraft horizontal axis one degree of freedom

aircraft longitudinal axis three degrees of freedom.

#2. What would be the indication on an attitude indicator in a right turn?

Climb due to pendulous vanes.

No climb.

Descent due to pendulous vanes.

Correct pitch and bank at all times.

#3. What will a classic artificial horizon indicate when turning through 90 degrees at constant attitude and bank angle?

Correct bank angle and attitude.

Too much bank and too much nose up attitude.

Too little bank and too little nose up attitude.

Too little bank and too much nose up attitude.

#4. An AI has?

One degree of freedom and a lateral spin axis.

Two degree of freedom and a vertical spin axis.

Two degree of freedom and a horizontal spin axis.

One degree of freedom and a vertical spin axis.

#5. How will a basic AI respond if an aircraft performs a 270 degree turn at constant bank angle and ROT?

Nose up and bank.

Nose down and bank.

Nose level and bank.

Correct bank and pitch.

#6. Aircraft attitude is indicated on?

EICAS/ECAM primary display.

EFIS ND.

EFIS PFD.

All of the above.

#7. When turning through 90° at constant AOB and pitch attitude, what will a classic artificial horizon indicate?

Too much nose up and too little bank angle.

Too much nose up and too much bank angle.

Too little nose up and too little bank angle.

Too little nose up and too much bank angle.

#8. When turning through 270° at constant AOB and pitch attitude, what will a classic artificial horizon indicate?

Too much nose up and too little bank angle.

Too much nose up and too much bank angle.

Too little nose up and too little bank angle.

#9. An artificial horizon has?

Two degrees of freedom and a vertical spin axis.

Two degrees of freedom and a longitudinal spin axis.

Two degrees of freedom and a lateral spin axis.

No degrees of freedom because it is earth tied.

#10. The latitude nut _____________ an artificial horizon?

Compensates for transport error.

Is not fitted to.

Compensates for latitude error.

Compensates for earth rate errors.

#11. The gravity sensing unit in an artificial horizon is used to?

Prevent tilting of the gyro.

Prevent precession of the gyro.

Erect the gyro.

Provide signals to the autopilot.

#12. Classic artifical horizon indications turning through 180° at constant AOB?

Nose up and AOB too low.

Nose up and AOB too high.

Nose up and correct AOB.

Pitch attitude and AOB correct.

#13. An artificial horizon has degrees of freedom in the __ axis?

Two vertical.

Two horizontal.

One vertical.

One horizontal.

#14. Which or the following properties are possessed by a standby artificial horizon? 1. Independent power supply. 2. Integral gyro. 3. Remote (external) gyro. 4. Used only in emergencies. 5. At least one per pilot in JAR 25 aircraft.

1, 2.

2, 3.

3, 4.

4, 5.

#15. If an aircraft turns through 270° at a constant rate of turn and AOB, the indications on its classic artificial horizon will be?

Bank left nose up.

Bank right nose up.

Wings level nose up.

AOB and pitch attitude correct.

Dgca Question Bank For Pilots

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