TCH.1C-27J-2-29JG
2-24
CHECK VALVE IN LH (RH) ENGINE NACELLE -
REMOVAL AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect external electrical power (refer to manual
2.Position maintenance platform (AGE NO. 00074).
3.Open the access panels 414J and 414D (424J and
424D).
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
20,00
Removal
AFM
1
9,00
Installation
AFM
2
36,00
Test
AFM
2
28,00
Follow
Maintenance
AFM
2
20,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 217 (Min.)
Total Time Detention System: 113 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054 Kit, torque wrenches
G0001200001-001**
00074 Kit, aircraft assy platform
G0005100001
29-10-35
2-171