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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 121<br />

determined when the bearing pointer passes 90 degrees to the inbound course.<br />

7.6.2. TACAN. Station passage is determined when the range indicator stops<br />

decreasing.<br />

7.6.3. ADF. Station passage is determined when the bearing pointer passes 90° to the<br />

inbound course.<br />

7.6.3.1. NOTE: When established in an NDB holding pattern, subsequent station<br />

passage may be determined by using the first definite move by the bearing pointer<br />

through 45° index on the RMI.<br />

7.7. Time and Distance Check. To compute time and distance from a station, first turn the<br />

aircraft to place the bearing pointer on the nearest 90° index. Note the time and maintain<br />

heading. When the bearing pointer has moved 10°, note the elapsed time in seconds and<br />

apply the following formulas to determine time and distance:<br />

7.7.1. Divide the elapsed time in seconds by the degrees of bearing change to obtain<br />

minutes from the station: 120 divided by 10 = 12 minutes from the station.<br />

7.7.2. Multiply your groundspeed in nautical miles per minute by the minutes from the<br />

station.<br />

7.7.2.1. NOTE: The accuracy of time and distance checks is governed by the existing<br />

wind, the degree of bearing change, and the accuracy of timing. The number of<br />

variables involved causes the result to be an approximation. However, by flying an<br />

accurate heading and checking the time and bearing closely, you can get a reasonable<br />

estimate of time and distance from the station.<br />

7.8. Groundspeed Check. Groundspeed checks are done to aid in calculating ETAs to<br />

fixes, which are useful for position reports, fuel computations and other mission timing<br />

problems.<br />

7.8.1. Conditions. A groundspeed check can be made while maintaining a course to or<br />

from a TACAN/VORTAC station. As a guide, however, groundspeed checks should be<br />

performed only when the aircraft slant range distance is more than the aircraft altitude<br />

divided by 1,000. For example, if the aircraft is at FL 200, groundspeed checks should be<br />

performed when beyond 20 nautical miles. Checks made below 5,000 feet are accurate at<br />

any distance.<br />

7.8.2. Begin Timing. To perform the groundspeed check, begin timing when the range<br />

indicator shows a whole number. After the predetermined time has elapsed, check the<br />

range indicator and note the distance flown. Apply the following formula to determine<br />

groundspeed: Multiply the distance flown times 60 and then divide the product by the<br />

elapsed time in minutes. For example, if you fly 12 NM in 2 minutes, then your<br />

groundspeed is 360 knots. ((12 NM x 60)/2 min = 360 knots)<br />

7.8.2.1. NOTE: For precise computation, time for longer periods and solve the<br />

problems on a computer. To simplify computations, use a 2-minute time check and<br />

multiply the distance traveled by 30, a 3-minute time check, distance times 20; or a 6-<br />

minute time check, distance times 10. A rapid groundspeed check can be<br />

accomplished by timing the range indicator for 36 seconds and multiplying the<br />

distance traveled by 100.

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