TCH.1C-27J-2-27JG
2-75
FLAP DRIVE CONTROL UNIT - REMOVAL AND
INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
NOTE
Ensure that aircraft is not electrically and
hydraulic supplied.
1.Open the access panels 553A, 553B, 553C and
621Q.
2.Open the access panel 554A and remove life raft.
3.Loosen the panel located under the panel 554A.
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
1
35,00
Removal
AFM
1
60,00
Installation
AFM
1
70,00
Follow
Maintenance
AFM
1
35,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 200 (Min.)
Total Time Detention System: 200 (Min.)
AGE Required:
None
27-50-25
2-574