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TECH GENERAL — CH.10

Aircraft ControlsAircraft & Engines — DGCA CPL practice questions

Question 1 of 6

The elevator controls movement about the:

A.Longitudinal axis
B.Lateral axis
C.Normal axis
D.Drag axis

All 6 questions — Aircraft Controls

Aircraft & Engines · DGCA CPL. The correct option is marked on each.

  1. Q1. The elevator controls movement about the:

    • A.Longitudinal axis
    • B.Lateral axis
    • C.Normal axis
    • D.Drag axis

    Why: Elevator → pitch about the lateral axis; ailerons → roll about the longitudinal axis; rudder → yaw about the normal axis.

  2. Q2. An anti-balance tab moves:

    • A.Opposite to the control surface, reducing stick force
    • B.In the same direction as the control surface, increasing stick force
    • C.Only when selected by the pilot
    • D.Only on the ground

    Why: Anti-balance tabs move WITH the surface to add feel (stick force) and effectiveness; balance tabs move opposite to lighten the controls.

  3. Q3. With a servo tab system, the pilot's controls are connected to:

    • A.The main control surface directly
    • B.The tab only
    • C.Both surface and tab
    • D.A hydraulic actuator

    Why: The pilot moves only the tab; the aerodynamic force on the tab then drives the main surface.

  4. Q4. Adverse aileron yaw is caused by:

    • A.More induced drag on the down-going aileron's wing
    • B.More induced drag on the up-going aileron's wing
    • C.Rudder deflection
    • D.Propeller torque

    Why: The down-going aileron (rising wing) makes more lift AND more induced drag, yawing the nose away from the turn; differential or Frise ailerons reduce it.

  5. Q5. When spoilers are used for roll control they:

    • A.Cause strong adverse yaw
    • B.Do not cause adverse yaw
    • C.Increase lift on the down-going wing
    • D.Can only be used on the ground

    Why: Raising a spoiler dumps lift AND adds drag on the down-going wing, so the yaw is into the turn — no adverse yaw.

  6. Q6. Ground spoilers (lift dumpers) are deployed on landing to:

    • A.Increase lift for a gentle touchdown
    • B.Dump lift so the full weight is on the wheels for effective braking
    • C.Assist nose-wheel steering
    • D.Reduce engine noise

    Why: Dumping all wing lift transfers the aircraft's weight to the wheels, maximising brake effectiveness.