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

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AFMAN 11-217V1 3 JANUARY 2005 83<br />

and each dot is 1¼°. If the localizer course is 3° wide, then full-scale deflection is<br />

1½° and each dot is ¾° (Figure 5.7). The range indicator displays slant range<br />

distance in nautical miles to the selected DME transponder and may or may not<br />

operate when ILS modes have been selected depending on equipment installation.<br />

Additional displays available on electronic horizontal situation indicators include<br />

ARC formats to display a segment of the standard display as well as MAP formats<br />

used to pictorially display bearing and distance to NAVAIDS or waypoints.<br />

5.3.2.2. Course Selector Knob. The course selector knob on most flight directors<br />

may be used to select any of 360 courses. To select a desired course, rotate the head<br />

of the course arrow to the desired course on the compass card and check the course<br />

selector window for the precise setting. The TO-FROM indicator is a triangularshaped<br />

pointer. When the indicator points to the head of the course arrow, it indicates<br />

that the course selected, if properly intercepted and flown, will take the aircraft to the<br />

selected facility.<br />

5.3.2.3. Heading Set Knob. The heading set knob on most flight directors is used to<br />

set the heading marker to a desired heading. With the proper mode selected on the<br />

flight director control panel, the heading marker can be slaved to the flight director<br />

computer. Thus, when a heading is set, the command bars will command the bank<br />

attitude required to turn to and maintain the selected heading.<br />

5.3.3. Flight Director Computer.<br />

5.3.3.1. Flight Director Computer Information. The flight director computer receives<br />

navigation information from the navigation systems and attitude information from the<br />

attitude gyro. Depending on the modes available and selected, the computer supplies<br />

pitch or bank commands to the command bars of the ADI. The functions of the<br />

computer vary with systems, and a number of inputs (NAVAIDs, datalink, Doppler,<br />

etc.) may be electronically processed by the system.<br />

5.3.3.2. Flight Director Systems. In some flight director systems, the command bars<br />

can be used for other maneuvers such as intercepting VOR, TACAN, and Doppler<br />

courses or performing data link intercepts. Pitch command information can vary<br />

from terrain avoidance commands to commanding a selected altitude. In all cases,<br />

the command bars display command information and do not reflect actual aircraft<br />

position. This section is limited to command information pertaining to selected<br />

headings and ILS approaches and is common to most flight director systems. Refer<br />

to the appropriate flight manual for the specific capabilities of the system installed in<br />

your aircraft.<br />

5.3.4. Flight Director Modes.<br />

5.3.4.1. Heading Mode. The flight director usually has mode selectors that allow the<br />

pilot to select command steering to a heading or to various navigation systems.<br />

5.3.4.2. ILS Intercept Mode (Figure 5.10). This mode is designed to direct the<br />

aircraft to, place it upon, and maintain it on the localizer course. This is<br />

accomplished by positioning the bank steering bar to command the pilot to fly flight<br />

director computed headings.

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