👩‍💻 |05| WT004: Instrument Test (Gyroscope, AH, DGI, RIMC)

wander, real or apparent, in the vertical plane

Artificial horizon

Correct answer is – 30° port bank, level flight

Skidding; push left pedal forward,

Artificial horizon,

through 90Degrees in the direction of spin of the rotor

Correct answer is – A bank or pitch attitude of the aircraft. Feedback – when the aircraft is pitching or rolling the gyro will start experiencing the precession force and read error. this error will get cancelled out once the aircraft level out.

Correct answer is – Nose-up attitude.

Needle central and ball central

An erection system is used.

22 degree

An AC voltage that varies with heading.

2 NM

decrease

Correct answer is – Two; vertical. uses vertical axis earth gyro. maintains always local vertical to earth due to rigidity. it has two degrees of freedom 1.- Pitch: about the lateral axis of aircraft- freedom in the horizontal axis. 2. Roll: about longitudinal Axis of aircraft – horizontal axis. in __ horizontal axis . about __ vertical plane

Correct answer is – it is less pendulous, has a higher rotor speed and a linear acceleration cut-out

Angular velocity about the vertical axis.

Correct answer is – horizontal axis tied gyro

make the gyro sensitive to banking of the aircraft as well as to turning

Correct answer is – Moving the compass housing around its vertical axis

Has a longer life cycle.

Correct answer is – Local earth vertical; two degrees of freedom. Artificial Horizon has 2 degrees of freedom, one in roll and 1 in pitch. so when the aircraft is pitching or rolling then the gyro will remain vertical. controlled by local gravity

Correct answer is – error detector

Correct answer is – Error detector.

4.2° per hour.

Correct answer is – 1,2.

Correct answer is – Is used to establish aircraft magnetic heading during a compass swing

Determined by TAS.

high rpm, high moment of inertia, rapid build-up of speed, constant RPM

An AC motor.

Correct answer is – Is dependent on the ground speed of the aircraft, its true track and the average latitude of the flight.

Correct answer is – 2, 3 and 5

Error Detector.

The erection system is cut out by sensing acceleration.

Correct answer is – 10.5°/hour to the right.

Proportional to TAS.

Correct answer is – Causes the directional gyro unit to precess.

Correct answer is – Too much nose-up and bank too low.

Correct answer is – Is not fitted to.

Skidding; push right pedal forward.

Torque motors and mercury switches.

Correct answer is – 10.6° clockwise

The rotorl is locked in yawing plane and the azimuth gear is connected to the knob for correction.

Horizontal Axis rate gyro; yaw rate,

Correct answer is – 1, 2, 3, & 5

Correct answer is – Nose up and bank.

Prevents laser lock.

200 Kts.

Correct answer is – Attitude and bank correct.

an inertial navigation system

Induce a real wander to cancel out drift due to earth’s rotation.

A horizontal axis and one degree of freedom.

change-of-heading rate of the aircraft

At the equator.

15 deg/hour at the pole.

Two gimbals, two degrees of freedom and a horizontal spin axis,

tied

Miniature aircraft relative to the horizon bar.

A right turn with too little bank.

Flux Valve.

Correct answer is – 0

Correct answer is – 2 degrees of freedom and horizontal spin axis.

1 & 4

a rate of turn to the left, slipping in

Correct answer is – mounting the detector unit in the wingtip

Correct answer is – Error detector.

Pitch and Roll.

vertical axis and has 2 degrees of freedom

Correct answer is – 1,4. Feedback – you have to manually correct it —- tied using knob

Correct answer is – attaching a bias weight to the inner gimbal which makes the gyro Precess in azimuth in the opposite direction to apparent wander . Feedback – Don’t get confuse- —————- Due to spring the precession is in the “”same direction” as yaw”. but due to latitude nut precession is in “‘opposite direction “” of earth rate drift wander

Acceleration errors are greatest on headings of 090 and 270 degrees.

Correct answer is – Too high pitch-up and correct banking.

The rate at which the aircraft is turning about the yaw axis.

The same as the number of gimbals.

Correct answer is – gimballing error, random wander, apparent wander, rotor speed error, transport wander

Slipping; push left pedal forward.

Correct answer is – increased nose-up attitude and right wing low

Correct answer is – It will tilt upwards at the front.

Is a torque motor type.

Correct answer is – Too much nose up and too much bank angle.

Correct answer is – the inner gimbal ring is pivoted laterally inside the outer gimbal ring and the outer gimbal ring is pivoted longitudinally inside the case

15° per hour.

rotation of the earth

One; one.

The vacuum pump.

Pendulous vanes and air jets.

Correct answer is – 1, 3 and 5

Increasing TAS.

Correct answer is – Is the resultant magnetic force in the horizontal plane in the position where the compass is installed

Correct answer is – Precess the directional gyro.

Correct answer is – (- 15 sine latitude in degrees per hour)

Correct answer is –the lag of the base of the rotor housing

Correct for apparent wander due to earth’s rotation.

A directional gyro.

A descent and a turn to the left.

Correct answer is – when flying south from 56°N the true heading will decrease Feedback – gyro is compensated for apparent wander at 56°N. in east west at 56 N – no error flying north form set latitude – ( -ve ) – under read – True heading increase. flying south from set latitude – ( +ve ) over read – true decrease.

1,2.

-6.67° per hour.

It would not affect the required AOB, but less power would be required.

Correct answer is – A torque motor