Beechcraft Duchess 76 - Altimeter Correction - Alternate System

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ALTIMETER CORRECTION .' ALTERNATE SYSTEM
EXAMPLE:
lAS .....•................................ 75 KTS
FLAPS , , DOWN (ON)
INDICATED PRESSURE ALTITUDE •..........• 4000 FT
STORM WINDOW iOPEN
ALTIMETER CORRECTION '.' - 25 FT
ACTUAL PRESSURE ALTITUDE .•............. 3975 FT
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ALTERNATE SYSTEM· INDICATED AIRSPEED - KNOTS
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ALTERNATE SYSTEM· INDICATED AIRSPEED - KNOTS
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