TCH.1C-27J-2-27JG
2-31
FCS 1 CONTROL PANEL (103VE) RUDDER
TRIM - FUNCTIONAL TEST
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
None
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Test
ELT
1
30,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 30 (Min.)
Total Time Detention System:
30 (Min.)
AGE Required:
None
Consumable Material Required:
None
Safety Conditions:
None
PROCEDURE:
2-31.1
CHECK OF FCS 1 CONTROL PANEL (103VE)
RUDDER TRIM (refer to figure
1.Check that the following circuit breakers are closed:
A.FLAP ASYM (1CA) (8) located on Rear Mid Circuit
Breakers Panel (451VE) (9) in position L 5 (refer to
figure
(Cont'd)
27-20-40
2-258