TCH.1C-27J-2-27JG
2-94.1 CHECK OF FCS1 CONTROL PANEL LIFT
DUMPER (refer to figure
) , (refer
to figure
) and (refer to figure
1.Check that the following circuit breakers are closed:
A.FLAP ASYM (1CA) (15) located on Rear Mid
Circuit Breaker Panel (451VE) (14) in position L 5.
B.FLAP ASYM (12CA) (13) located on Rear Upper
Circuit Breaker Panel (452VE) (12) in position H 4.
C.FLIGHT CONTROL FLAP IND (3CA) (11) located
on Overhead Circuit Breaker Panel (271VE) (10) in
position F 14.
2.Provide electrical power to the 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.
Perform the following steps for rudder trim:
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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(Cont'd)
27-60-05
2-675