Embraer EMB145 - Page 127

LIMITATIONS
FAA
AIRPLANE
O
PERATIONS
MANUAL
1-01-10
Page
6
Code
01
REVISION 41
Copyright © by Embraer. Refer to cover page for details.
AOM
-
145/1114
FLIGHT CONTROLS
MAXIMUM FLAP EXTENDED SPEED (V
FE
) - FOR EMB-135,
ERJ-140 AND EMB-145 MODELS, EXCEPT EMB-145 XR
Flaps 9°......................................................................... 250 KIAS
Flaps 18°....................................................................... 200 KIAS
Flaps 22°....................................................................... 200 KIAS
Flaps 45°....................................................................... 145 KIAS
MAXIMUM FLAP EXTENDED SPEED (V
FE
) - FOR EMB-145 XR
MODEL
Flaps 9°......................................................................... 250 KIAS
Flaps 18°....................................................................... 200 KIAS
Flaps 22°....................................................................... 200 KIAS
Flaps 45°....................................................................... 160 KIAS
Above 10000 ft with Yaw Damper disengaged:
Flaps 22°....................................................................... 180 KIAS
Flaps 45°....................................................................... 145 KIAS
ELECTROMECHANICAL GUST LOCK
Each time electromechanical gust lock lever is set to unlocked (FREE)
position elevator movement must be checked. This check must be
performed at least 10 seconds after positioning the gust lock lever to
the unlocked (FREE) position by moving the control column from the
full up stop to the full down stop and back to the full up stop position.
MAXIMUM FLAP EXTENDED ALTITUDE
Maximum Altitude for Flap Extension ...........................20000 ft
PITCH TRIM
Maximum Airspeed after Takeoff/During Climb
without Retrimming..................................................160 KIAS