• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/10

Click to flip

Use LEFT and RIGHT arrow keys to navigate between flashcards;

Use UP and DOWN arrow keys to flip the card;

H to show hint;

A reads text to speech;

10 Cards in this Set

  • Front
  • Back
What does 'Aileron Lockout' refer to?
The system locking the OUTBOARD ailerons during high speed flight to minimize some of the roll effect.
At what stages of flight are the inboard ailerons active?
At all stages of flight.
What other device assists the aileron in rolling the aircraft?
Spoilers - rise up on the down-going wing.
What is 'Spoiler Blowdown'?
The design of spoilers to be progressively blown down by increasing air loads on them.
Describe "Spoiler Walk Down"
The tendency for the aircraft to pivot around the flap area of the wing with spoiler activated - increasing drag and increasing altitude loss.
What purpose does a rudder ratio changer serve?
Varies the amount of rudder travel that is applied at various speeds, to minimize rick of over-stressing.
On an aircraft with a split rudder, what happens if one rudder ratio changer were to fail.
Both rudders would be out of whack, a comparator would pick this up, and "rudder ratio" warning would be displayed in cockpit.
Yaw dampers are a device installed to combat what aerodynamic tendency?
Dutch Roll.
What is the difference between a series type and a parallel type yaw damper?
Series does not move rudder pedals, can be used in all stages of flight.

Parallel moves rudder pedals, must be OFF for take-off and landing.
What are 4 reasons for the use of a moveable stabilizer in a large jet aircraft?
1. Using elevator trim for larger periods causes trim drag.
2. Need to be able to cater for large change in C o G.
3. Need to be able to cater for changes in C o P at high mach numbers.
4. To counter changes in pitch trim as leading and trailing edge flaps are deployed.