TCH.1C-27J-2-27JG
2-85
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
maintenance.
PROCEDURE:
2-85.1 CHECK OF FLAP ASYMMETRY CONTROL
SYSTEM (refer to figure
) , (refer to
figure
) and (refer to figure
(Cont'd)
27-50-65
2-623