TCH.1C-27J-2-27JG
2-91
LIFT DUMPER CONTROL VALVE - 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 913H, 913I, 913B, 913A and
621N.
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
1
15,00
Removal
AFM
1
10,00
Installation
AFM
1
15,00
Follow
Maintenance
AFM
1
15,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 55 (Min.)
Total Time Detention System:
55 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00074
Kit, aircraft assy platform
G0005100001
27-60-25
2-695