Beech Beechcraft Bonanza V35 - Altimeter Correction - Normal System

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ALTIMETER CORRECTION - NORMAL SYSTEM
NOTE: INDICATED AIRSPEED AND INDICATED ALTITUDE ASSUME
-- ZERO INSTRUMENT ERROR
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IAS • INDICATED AIRSPEED .-v KNOTS
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INDICATED PRESSURE
70 KNOTS (80 MPH)
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ALTITUDE 4500 FT
ALTIMETER CORRECTION --12 FT
ACTUAL PRESSURE Al TITUDE:
= 4500-12 = 4488 FT
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IAS • iNOICATEO AIRSPEED .-v KNOTS
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IAS • INDICATED AIRSPEED .-v MPH
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