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

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142<br />

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

Figure 8.2. Example 2 - Off-scale Altimeter Settings.<br />

8.1.3.1. Subtracting Corrections. In example one (Figure 8.1), you have been cleared<br />

to fly the HI-TACAN RWY 22 at Gander INTL. The local altimeter setting is 31.20<br />

inches. Your altimeter's maximum range is 31.00 inches. First, determine the<br />

difference between the actual ALSTG (31.20) and the value set in your altimeter<br />

(31.00). Take this result (.20) and multiply by 1,000. This will give you your<br />

correction factor (200 ft). Because the altimeter setting exceeds the altimeter's<br />

maximum range, the correction (200 ft) will be subtracted from all approach altitudes.<br />

These corrections are indicated on the approach.<br />

8.1.3.2. Adding Corrections. In example two (Figure 8.2), you have been cleared to<br />

fly the TACAN RWY 10 at Shemya AFB. The local altimeter setting is 27.90 inches.<br />

Your altimeter's minimum range is 28.10 inches. First, determine the difference<br />

between the actual ALSTG (27.90) and the value set in your altimeter (28.10). Take<br />

this result (.20) and multiply by 1,000. This will give you your correction factor (200<br />

ft). Because the altimeter setting is less than the altimeter's minimum range, the<br />

correction (200 ft) will be added to all approach altitudes. These corrections are<br />

indicated on the approach.<br />

8.1.3.2.1. NOTE: Because high pressure is usually associated with fair weather<br />

(VMC), the use of correction factors where the actual altimeter setting exceeds<br />

the altimeter upper limit does not present a serious problem. On the other hand,<br />

low ceilings and visibilities are often associated with extremely low pressure (low<br />

altimeter settings). Aircraft that must execute an actual instrument approach<br />

(IMC) under these conditions should consider this situation an emergency. It is<br />

further recommended that all available approach and navigation aids (radar<br />

altimeters, Ground Controlled Approach (GCA) monitored approach, etc.) be<br />

used to determine aircraft position and altitude.<br />

8.1.4. Cold Weather Altimeter Corrections. Pressure altimeters are calibrated to indicate<br />

true altitude under International Standard Atmospheric (ISA) conditions. Any deviation<br />

from these standard conditions will result in an erroneous reading on the altimeter. This

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