Embraer EMB145 - Page 699

AIRPLANE
OPERATIONS
MANUAL
PERFORMANCE
EMB-145 A1 FAA
REVISION 39
1-04-25
Page
3
Code
02
AOM-145/1114
FLAP MANEUVERING SPEED
These speeds allow for an inadvertent 15° overshoot beyond the
normal 30° bank over stick shaker actuation.
FLAP MANEUVERING SPEED (KIAS)
BELOW MSLW* ABOVE MSLW*
FLAPS GEAR
NO ICING
CONDITIONS
WITH ICING
CONDITIONS
NO ICING
CONDITIONS
WITH ICING
CONDITIONS
0° UP 180 200 180 200
9° UP/DN 160
18°/22° UP/DN 140 150
45° DN 140
*Maximum Structural Landing Weight as specified on Limitations
Section.
FINAL APPROACH SPEED
V
APP
= V
REF
+ wind correction.
Wind correction = ½ steady headwind component + gust increment
above steady wind.
For Flaps 45° landing, the minimum wind correction is 5 KIAS and the
maximum is 15 KIAS.
For Flaps 22° landing:
- Performing CAT I approaches, the minimum wind correction is
5 KIAS and the maximum is 20 KIAS.
- Performing CAT II or CAT III approaches, the minimum wind
correction is 0 KIAS and the maximum is 20 KIAS.
For Emergency and Abnormal procedures using Flaps 0°, 9° and 18°,
the minimum wind correction is 0 KIAS and the maximum is 20 KIAS.
For Flaps 22°, the minimum wind correction is 0 KIAS and the
maximum is 15 KIAS. When there is wind and abnormal operation
speed additives, use the sum of both corrections.