Instruments Theory 2 Flashcards
(53 cards)
GYRO 43
A turn indicator is an instrument which indicates rate of turn. Rate of turn depends upon:
1. Bank angle.
2. Aeroplane speed.
3. Aeroplane weight.
The combination regrouping the correct statements is?
a) 1, 2, and 3
b) 1 and 2
c) 1 and 3
d) 2 and 3
Correct Answer:
[x) b) 1 and 2]
GYRO 44
During an acceleration phase at constant attitude, the resetting principle of the artificial horizon results in the horizon bar indicating a:
a) Nose-down attitude.
b) Constant attitude.
c) Nose-down followed by a nose-up attitude.
d) Nose-up attitude.
Correct Answer:
[x) d) Nose-up attitude]
GYRO 45
Heading information given by a gyro platform, is given by a gyro at?
a) 2 degrees-of-freedom in the vertical axis.
b) 1 degree-of-freedom in the horizontal axis.
c) 1 degree-of-freedom in the vertical axis.
d) 2 degrees-of-freedom in the horizontal axis.
Correct Answer:
[x) d) 2 degrees-of-freedom in the horizontal axis.
GYRO 48
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?
a) Is at its greatest value when the aircraft follows a meridian track.
b) 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.
c) Is dependent on the ground speed of the aircraft, its true track and the average latitude of the flight.
d) Is, in spite of this, insignificant and may be neglected.
Correct Answer:
[x) c) Is dependent on the ground speed of the aircraft, its true track and the average latitude of the flight.
GYRO 49
A gravity erector system is used to correct the errors on?
a) Artificial horizon.
b) A directional gyro.
c) A turn indicator.
d) A gyro-magnetic compass.
Correct Answer:
[x) a) Artificial horizon]
GYRO 49
A gravity erector system is used to correct the errors on?
a) Artificial horizon.
b) A directional gyro.
c) A turn indicator.
d) A gyro-magnetic compass.
Correct Answer:
[x) a) Artificial horizon]
ATTITUDE 1
How many degrees of freedom and what is the spin axis of an attitude indicator?
a) Local earth vertical — two degrees of freedom.
b) Aircraft lateral axis — two degrees of freedom.
c) Aircraft horizontal axis — one degree of freedom.
d) Aircraft longitudinal axis — three degrees of freedom.
⸻
Correct Answer:
[x) a) Local earth vertical — two degrees of freedom.
ATTITUDE 2
What would be the indication on an attitude indicator in a right turn?
a) Climb due to pendulous vanes.
b) No climb.
c) Descent due to pendulous vanes.
d) Correct pitch and bank at all times.
⸻
Correct Answer:
[x) a) Climb due to pendulous vanes]
ATTITUDE 3
What will a classic artificial horizon indicate when turning through 90 degrees at constant attitude and bank angle?
a) Correct bank angle and attitude.
b) Too much bank and too much nose up attitude.
c) Too much nose up and too little nose up attitude.
d) Too little bank and too much nose up attitude.
⸻
Correct Answer:
[x) d) Too little bank and too much nose up attitude]
ATTITUDE 4
An AI has?
a) One degree of freedom and a lateral spin axis.
b) Two degrees of freedom and a vertical spin axis.
c) Two degrees of freedom and a horizontal spin axis.
d) One degree of freedom and a vertical spin axis.
⸻
Correct Answer:
[x) b) Two degrees of freedom and a vertical spin axis]
ATTITUDE 5
How will a basic AI respond if an aircraft performs a 270 degree turn at constant bank angle and ROT?
a) Nose up and bank.
b) Nose down and bank.
c) Nose level and bank.
d) Correct bank and pitch.
⸻
Correct Answer:
[x) a) Nose up and bank]
ATTITUDE 7
When turning through 90° at constant AOB and pitch attitude, what will a classic artificial horizon indicate?
a) Too much nose up and too little bank angle.
b) Too much nose up and too much bank angle.
c) Too little nose up and too little bank angle.
d) Too little nose up and too much bank angle.
⸻
Correct Answer:
[x) a) Too much nose up and too little bank angle]
ATTITUDE 8
When turning through 270° at constant AOB and pitch attitude, what will a classic artificial horizon indicate?
a) Too much nose up and too little bank angle.
b) Too much nose up and too much bank angle.
c) Too little nose up and too little bank angle.
d) Too little nose up and too much bank angle.
⸻
Correct Answer:
[x) b) Too much nose up and too much bank angle]
ATTITUDE 9
An artificial horizon has?
a) Two degrees of freedom and a vertical spin axis.
b) Two degrees of freedom and a longitudinal spin axis.
c) Two degrees of freedom and a lateral spin axis.
d) No degrees of freedom because it is earth tied.
⸻
Correct Answer:
[x) a) Two degrees of freedom and a vertical spin axis]
ATTITUDE 10
The latitude nut ……….. an artificial horizon?
a) Compensates for transport error.
b) Is not fitted to.
c) Compensates for latitude error.
D) compensates for earth rate errors.
Correct Answer:
[x) b) Is not fitted to.
ATTITUDE 11
The gravity sensing unit in an artificial horizon is used to?
a) Prevent tilting of the gyro.
b) Prevent precession of the gyro.
c) Erect the gyro.
d) Provide signals to the autopilot.
⸻
Correct Answer:
[x) a) Prevent tilting of the gyro]
TURN/SLIP 5
A turn indicator has?
1. A horizontal spin axis.
2. A vertical spin axis.
3. One degree of freedom.
4. Two degrees of freedom.
5. A spin axis tied to the yawing plane of the aircraft.
6. A gravity erecting unit.
a) 1, 3
b) 1, 5
c) 3, 5
d) 4, 6
Correct Answer:
[x) a) 1, 3
ATTITUDE 12
Classic artificial horizon indications turning through 180° at constant AOB?
a) Nose up and AOB too low.
b) Nose up and AOB too high.
c) Nose up and correct AOB.
d) Pitch attitude and AOB correct.
⸻
Correct Answer:
[x) c) Nose up and correct AOB.
ATTITUDE 13
An artificial horizon has ….. degrees of freedom in the ……. axis?
a) Two — vertical.
b) Two — horizontal.
c) One — vertical.
d) One — horizontal.
⸻
Correct Answer:
[x) b) Two — horizontal]
ATTITUDE 14
Which of 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.
a) 1, 2
b) 1, 2, 3
c) 2, 3, 4
d) 3, 4, 5
⸻
Correct Answer:
[x) a) 1, 2]
TURN/SLIP 14
Following a left engine failure the pilot of a multi-engine aircraft uses rudder to arrest the yaw, whilst side slipping down track with the wings held level by the ailerons. What will the turn and slip indicator show in this condition?
a) Both needle and ball central.
b) Both needle and ball right.
c) Both needle and ball left.
d) Needle left and ball right.
Correct Answer:
[x) a) Both needle and ball central.
TURN/SLIP 1
The ball in a serviceable slip indicator is ………… by …………. and …………. Indicates the state of slip?
a) Held central — Gravity — Does not always.
b) Positioned — Acceleration — Does not always.
c) Held central — Gravity — Always.
d) Positioned — Acceleration — Always.
⸻
Correct Answer:
[x) b) Positioned — Acceleration — Does not always]
TURN/SLIP 2
The turn indicator is affected by?
1. AOB
2. Airspeed
3. Weight
4. Altitude
a) 1, 2
b) 2, 3
c) 3, 4
d) 4, 5
⸻
Correct Answer:
[x) a) 1, 2