Ch. 6 Airplane Attitude Instrument Flying Flashcards
What is attitude instrument flying?
Attitude instrument flying is defined as the control of an aircraft’s spatial position by using instruments rather than outside visual references.
What are the two basic methods utilized for learning attitude instrument flying?
“Control performance” and “Primary Supporting” methods.
How is aircraft performance managed?
By controlling attitude and power.
What is the instrument that displays the attitude of the airplane when utilizing the “control performance” method?
Attitude indicator
Which instrument(s) display the power output when utilizing the “control performance” method?
The manifold pressure and tachometer.
The performance instruments in the “control performance method” most directly reflect a change of what?
Acceleration.
What are the performance instruments when utilizing the “control performance method”?
Altimeter Airspeed Indicator VSI Heading Indicator Slip/skid Indicator Pitch Attitude Indicator
Which instruments indicate the position of the aircraft relative to a selected navigation facility or fix?
Navigation instruments.
What is the four step process to change attitude?
- Establish
- Trim
- Cross-check
- Adjust
Any time the attitude of the aircraft requires changing, the pilot must adjust what?
Attitude and power in order to achieve the desired performance.
What should the pilot do to ease workload when it comes to getting the desired performance from the aircraft?
The pilot should become familiar with the approximate pitch and power changes necessary to establish a specified attitude.
How will you know the aircraft is trimmed appropriately?
The pilot is able to relax pressure on the control yoke and momentarily divert attention to another task at hand without deviating from the desired attitude.
What reference should be used when adjusting pitch changes?
The pitch should be made in reference to bar widths on the miniature airplane.
What should be referenced when adjusting changes to bank?
Roll index
What should be referenced when adjusting power in the “control performance method”?
Manifold pressure gauge and tachometer.
What is the difference between the “control performance” and the “primary supporting” methods
It focuses more on the instruments that depict the most accurate indication for the aspect of the aircraft attitude being controlled
In straight-and-level flight what is the primary pitch instrument?
Altimeter
What vertical speed should you use when correcting for altitude deviations in straight-and-level flight?
Double your deviation not to exceed 500 fpm.
An increase in 2.5 degrees of pitch equals approximately what climb performance?
450 fpm climb.