Embraer EMB145 - Page 437

AIRPLANE
OPERATIONS
MANUAL
EMERGENCY
PROCEDURES
REVISION 40
1-03-20
Page
3
Code
03
AOM-145/1114
CONTINUED FROM PREVIOUS PAGE
If it is necessary to reduce airspeed below 160 KIAS, extend
flaps to 22°.
NOTE: Turning the airplane and extending the landing gear
helps to maintain minimum airspeed with unwanted
pitch up tendency.
Pitch Trim Command.......................................... CHECK ALL
SWITCHES
If pitch trim is recovered, re-trim the airplane and proceed with
flight normally.
If pitch trim is not recovered:
Consider landing at the nearest suitable airport.
Approach and landing configuration:
Landing Gear ........................................... DOWN
Flaps......................................................... 22°
Airspeed ................................................... V
REF 45
+
10 KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE
LANDING DISTANCE, MULTIPLY THE
UNFACTORED LANDING DISTANCE FOR
FLAPS 45° BY 1.45.
If pitch trim command is not reestablished and the airplane
presents a NOSE DOWN tendency:
Airspeed ............................................................. REDUCE
Below 250 KIAS:
Flaps (at 20000 ft maximum) ........................ 9°
Below 200 KIAS:
Flaps.............................................................. 22°
Approach and landing configuration:
Landing Gear................................................. DOWN
NOTE: Gear extension should be delayed as long as
possible.
Flaps.............................................................. 22°
Airspeed ........................................................ V
REF 45
+
25 KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 1.75.