Altimeter Correction - Normal System - Beechcraft Debonair 35-33 Pilot Operating Handbook

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ALTIMETER CORRECTION - NORMAL SYSTEM
NOTE . INDICATE O AIRSPEEO AN O INDIC ATED ALTITUDE A SSUM E
- - ZERO INSTAUMENT ERROR
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IAS - INDICfEO AIRSPEED
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KNOTS
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60 70 80 90 100 1 10 120 130 140 150 160 170 180 190 200 210 220 230
IAS - INDICATEO A IRSPEED
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MPH
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EXAMPLE
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IN OICATEO PRESSUAE
ALTITUO E
ALTIMETER CORRECTl ON
A CTUA L PRESSUR E AL TITU OE
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112 KN OTS
UP
5000 FEET
10 FEET
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50 60 70 80 90 100 1 10 120 130 140
IAS - INOICATEO AIASPEED
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IAS - !NOICATED AIRSPEED
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