TCH.1C-27J-2-27JG
2-31.1
)
(Cont'd)
B.FLAP ASYM (12CA) (7) located on Rear Upper
Circuit Breakers Panel (452VE) (6) in position H 4
(refer to figure
C.FLIGHT CONTROL FLAP IND (3CA) (2) located
on Overhead Circuit Breakers Panel (271VE) (1) in
position F 14 (refer to figure
2.Connect electrical power to aircraft (refer to manual
3.Provide hydraulic power to the aircraft (refer to
) .
4.Start up the avionics and check that there are no
ACAWS messages concerning the flight controls.
WARNING
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BEFORE PROCEED THROUGH THE
NEXT STEPS BE CAREFUL THAT
NOBODY IS WORKING ON THE RUDDER
AREA.
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CAUTION
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Ensure that the rudder area is free from
tools and other objects.
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5.On the FCS 1 control panel (103VE) (3) set and hold
momentarily the NORMAL TRIM selector (5) to NOSE
LH position and check that the rudder moves toward
left.
(Cont'd)
27-20-40
2-259