TCH.1C-27J-2-27JG
2-48
CONTROL WHEEL - REMOVAL AND
INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect external AC power supply from aircraft
(refer to manual
).
2.Remove the Chart Holder (refer to manual
) .
3.Open the access panels 711A, 712A, 130B and 130C.
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Removal
AFM
1
40,00
Installation
AFM
1
50,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 90 (Min.)
Total Time Detention System:
90 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054
Kit, torque wrenches
G0001200001-001**
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00020
KEY WASHER
68867-101
1,00
27-30-15
2-405