Embraer EMB145 - Page 677

AIRPLANE
OPERATIONS
MANUAL
PERFORMANCE
EMB-145 LB
REVISION 40
1-04-20
Page
5
Code
02
GRADIENT LOSS DUE TO A STEADY TURN
ONE ENGINE INOPERATIVE
TAKEOFF FLAPS 9°
0,0
0,2
0,4
0,6
0,8
1,0
1,2
1,4
1,6
1,8
2,0
2,2
2,4
2,6
0 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30
BANK ANGLE - deg
GRADIENT LOSS - %
ALL ENGINES MODELS
GRLOSS_TO - MAY 14, 2001
Φ
ΔV (KIAS)
0 0
15 0
20 5
25 10
30 15
AOM-145/1114