TCH.1C-27J-2-27JG
2-73
FLAP POSITION TRANSDUCER - 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.Position maintenance platform (AGE NO. 00074).
4.Open the access panel 532C (632C).
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
ELT
1
25,00
Removal
ELT
1
15,00
Installation
ELT
1
20,00
Follow
Maintenance
ELT
1
25,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 85 (Min.)
Total Time Detention System:
85 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054
Kit, torque wrenches
G0001200001-001**
00074
Kit, aircraft assy platform
G0005100001
27-50-40
2-587