Embraer 190 - Page 351

PERFORMANCE
AIRPLANE
FLIGHT
MANUAL
5-10
CTA APPROVED
Page 12 code 01
ORIGINAL
AFM-1912
-50
-40
-30
-20
-10
0
10
20
30
40
50
60
70
80
80 100 120 140 160 180 200
INDICATED AIRSPEED - kt
CORRECTION - ft
CORRECTED ALTITUDE = INDICATED ALTITUDE - DH
20000
10000 AND BELOW
ALTITUDE POSITION ERROR CORRECTION
AIR DATA SYSTEM 3 - FLAPS FULL
190cta22 - 30MAR2005
PRESSURE ALTITUDE - ft