08.01.2015 Views

BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE ...

BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE ...

BY ORDER OF THE SECRETARY OF THE AIR FORCE AIR FORCE ...

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

AFMAN 11-217V1 3 JANUARY 2005 47<br />

instruments. However, it is equally important for you to know what to change and how<br />

much pitch, bank, or power change is required.<br />

3.3.10.1. What to Change. Pitch attitude primarily controls airspeed and the rate of<br />

change in airspeed. Bank attitude control is used to maintain a heading or desired<br />

angle of bank during turns. Collective inputs control altitude changes and the rate of<br />

altitude change. Remember that power is used primarily to maintain your altitude and<br />

control the rate of climb or descent and cyclic inputs are used primarily to maintain<br />

airspeed and bank angle.<br />

3.3.10.2. How Much to Change. How much to adjust the attitude or power is,<br />

initially, an estimate based on familiarity with the aircraft and the amount you desire<br />

to change on the performance instruments. In a UH-1N for example, 2% of torque<br />

approximates 100 feet per minute of climb or descent or 5 knots of increase or<br />

decrease in airspeed. After you make a change in attitude or power, observe the<br />

performance instruments to see if the desired change occurred. If not, further<br />

adjustment of attitude or power is required. Remember, even though changes are<br />

estimates, they must be made in exact increments.<br />

3.4. Display of Flight Instrumentation. The advent of electronic displays has given the<br />

pilot the ability to optimize cockpit instrumentation for a particular mission by adding,<br />

removing, or relocating presentations on multi-function displays. This new dimension in<br />

cockpit management can be an asset if the selection of instrument displays is based on the<br />

requirement that, regardless of the type of mission, the pilot must always be aware of the<br />

aircraft's attitude. No mission can be safely or effectively executed if attitude awareness is<br />

lost.<br />

3.4.1. Primary Flight Instrumentation. Primary flight instrumentation must always be<br />

present and must provide full-time attitude, altitude, and airspeed information; an<br />

immediately discernible attitude recognition capability; an unusual attitude recovery<br />

capability; and complete fault indications.<br />

3.4.2. Position of Flight Instrumentation. The elements of information of Primary<br />

Flight Instrumentation must be positioned and arranged in a manner that enables the<br />

pilot to perform a natural crosscheck.<br />

3.4.3. Standardization of Flight. Primary flight instrumentation will be standardized in<br />

terminology, symbology, mechanization, and arrangement. Standardization of<br />

instrumentation display elements provides a common training base and allows the<br />

retention of good flying habits during transition to different aircraft. This standardization<br />

can only be effective when the pilot acknowledges attitude awareness as a full-time<br />

requirement and manages the cockpit accordingly.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!