Beech Beechcraft Bonanza V35 - Altimeter Correction - Emergency System

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ALTIMETER CORRECTION - EMERGENCY SYSTEM
NOTES: 1. INDICATED AIRSPEED AND INDICATED ALTITUDE ASSUME ZERO INSTRUMENT ERROR.
2. APPLICABLE FOR ALL WING FLA~ POSITIONS.
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STORM WINDOW CLOSED
60 70 80 90 100 110 120 130 140 150 160 170 180 190 200
IAS- tr-Jt>ICATEO AIRSPEED 'v KNOTS
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70 80 90 100 110 120 130 140 150 160 170 180 190 200 210 220 230
IAS- INUICATEO AIRSPEED...,, MPH
EXAMPLE:
lAS •••....
70 KTS (81 MPH)
OPEN
STORM WINDOW . . . , . •
INDICATED PRESSURE ALTITUDE.
5000FT
Al TITUDE COR-RECT!Oflt. . . .
ACTUAL PRESSURE ALTITUDE •
. -33 FT
. 5000-33 =-4967 FT
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IAS - INDICATED AIRSPEED"' KNOTS
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!AS- INDICATED AIRSPEED"' MPH
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