Embraer EMB145 - Page 526

ABNORMAL
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-57
Page
2
Code
03 REVISION 40
AOM-145/1114
STABILIZER ANTI-ICING FAILURE
EICAS WARNING: ICE COND-A/I INOP
EICAS CAUTION: STAB A/ICE FAIL
LIGHT: Master Warning and Master Caution
Ice Detection Override Knob ......................................... ALL
Thrust Levers ................................................................ ADVANCE
If failure persists:
Stabilizer Anti-Icing Button ....................................... CYCLE
If failure persists:
Stabilizer Anti-Icing Button ....................................... OFF
Avoid or exit icing conditions.
After exiting icing conditions:
Ice Detection Override Knob............................... AUTO
Maximum Bank Angle ................................................... 30°
Minimum Airspeed for
Flaps up or 9°........................................................... 190 KIAS
Landing configuration:
Flaps ........................................................................ 22°
Airspeed................................................................... V
REF 45
+
15 KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE
LANDING DISTANCE, MULTIPLY THE
UNFACTORED LANDING DISTANCE FOR FLAPS
45° BY 1.55.
If associated with Wing Anti-icing System failure and if in icing
conditions or if there is any uncertainty as to whether the wing surfaces
are clear of ice prior to approach and landing, proceed:
Landing configuration:
Flaps ................................................................... 22°
Airspeed.............................................................. V
REF 45
+
30 KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE
LANDING DISTANCE, MULTIPLY THE
UNFACTORED LANDING DISTANCE FORFLAPS
45° BY 1.85.