FLIGHT CONTROLS
Operation
Aircraft Operations Manual
8.2
PAGE
3
Apr 01/15
CONDITIONS
NORMAL PROCEDURES
2.5
RUDDER
SUBTAB TRIM
CURVES TEST
The following test is required by AMM section 27
−
22
−
25
−
2 Rudder Trim
Tab / Procedure 1
−
Adjust Rudder Sub Tab.
Flight conditions and aircraft configuration:
Altitude:
According to Table 201 in referenced AMM section.
Airspeed:
According to Table 201 in referenced AMM section.
Flaps/Gear:
According to Table 201 in referenced AMM section.
Yaw Damper:
OFF
Autopilot:
OFF.
Autopilot:
OFF.
The aircraft must be free of ice and the flight should be performed in stable
atmospheric conditions.
1.
Power
SET
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
−
Set power for level flight with equal torque on both engines.
2.
Trims
SET
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
−
Trim the aircraft at the conditions specified in AMM table 201 with wings
level, constant heading and slip ball centered.
3.
Yaw trim
RECORD
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
−
Record yaw trim indicator value at each airspeed and trim condition.