TCH.1C-27J-2-27JG
2-30
RUDDER QUADRANT - 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 212AZ, 212BZ, 214BZ,
213AZ, 130AH and 130AD.
4.Remove Pilot Seat (refer to manual
).
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
60,00
Removal
AFM
1
40,00
Installation
AFM
1
50,00
Follow
Maintenance
AFM
2
60,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 330 (Min.)
Total Time Detention System:
210 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054
Kit, torque wrenches
G0001200001-001**
27-20-35
2-250