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TCH.1C-27J-2-27JG
2-78
FLAP ASYMMETRY CONTROL SYSTEM -
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
40,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 40 (Min.)
Total Time Detention System:
40 (Min.)
AGE Required:
None
Consumable Material Required:
None
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para 
2-5
) before performing
maintenance.
PROCEDURE:
2-78.1
CHECK OF FLAP ASYMMETRY CONTROL
SYSTEM (refer to figure 
2-72, sheet 3/3
) , (refer to
figure 
2-72, sheet 1/3
) and (refer to figure 
2-72,
sheet 2/3
)
(Cont'd)
27-50-65
2-615