TCH.1C-27J-2-27JG
2-73
FLAP TENSION REGULATOR - REMOVAL AND
INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Isolate hydraulic power (refer to manual
3.Open the access panels 130AG, 130AE, 711A, 712A,
130B, 130C and 220FZ.
4.Position maintenance platform (AGE NO. 00074).
5.Open the access panels 553A, 553B and 553C.
6.Position emergency stair.
7.Open emergency exit door 885A.
Recomended Personnel:
PROCEDURE
MECH.
CODE QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
1
45,00
Removal
AFM
1
30,00
Installation
AFM
1
35,00
Follow
Maintenance
AFM
1
45,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 155 (Min.)
Total Time Detention System: 155 (Min.)
27-50-15
2-562