(2)
Install new packings (25) (P/N S9413-010) and (P/N S9413-014) on tubes (21).
(3)
Examine oil tube (7) for blockage due to oil coking. If tube (7) is blocked, do the steps paras. (4) to (7).
(4)
Withdraw shield tube (6) from bearing housing.
(5)
Use the TUBE - INSTALLATION FIXTURE, remove tube (7) from bearing housing.
(6)
Clean tubes (7) and (6) externally and internally using 1,1,1-trichloroethane. Make sure that the spray fluid flows freely through the tubes.
(7)
Dry tubes (6) and (7) with compressed air.
(8)
Blank the ends of tubes (6) and (7) with plastic caps or plugs.
Subtask 49-91-53-420-050
B. Installation of the Turbine Bearing Cavity Vent
(1)
If tubes (6) and (7) were previously removed for cleaning, remove the plugs/caps from them and do the steps in paras. (2) thru (4).
(2)
Use the TUBE - INSTALLATION FIXTURE, install tube (7) and torque tighten it to 0.68 m.daN (60.17 lbf.in).
(3)
Install the new gasket (5) (P/N 3846496-1) on the engine casing and align the bolt holes.
(4)
Install and locate tube (6) on tube (7). NOTE : The alignment tabs on the end of tube (6) must engage the
____
slots of tube (7).
(5)
Install the new packing (4) (P/N 561-515-0022) in vent fitting (3).
(6)
Install the new gasket (5) (P/N 3846496-1) on tube (6) and align the bolt holes.
(7)
Install vent fitting (3) and check valve (8) as one unit with washers
(2) and bolts (1).
(8)
Connect tube (9) to check valve (8).
(9)
Hold the check valve (8) with a wrench to prevent torque transfer, TORQUE the tube (9) B-nut to between 5.31 and 5.76 m.daN (39.15 and
42.47 lbf.ft).
(10)
Install the new gasket (12) (P/N 3846496-1) on shield tube (17) and align the bolt holes.
(11)
Install the new packing (13) (P/N 561-515-0022) in the adapter assembly (14).
(12)
Install the adapter assembly (14) with washers (16) and bolts (15).
(13)
Install the tubes (21) in adapter (14).
(14)
Install the tube retainers (20) on tubes (21) and secure with bolts (19).
Subtask 49-91-53-210-052
C. Do a visual check of the oil quantity. Add oil if the oil level is on or less than the ADD mark on the sight glass (Ref. TASK 49-90-00-600-001). 49-90-00-600-001).
Subtask 49-91-53-865-052
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
Subtask 49-91-53-410-050
E. Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001). Subtask 49-91-53-710-050
F. Do the Operational Test of the APU and do a Leak Check
(1)
Do the operational Test of the APU (Ref. TASK 49-00-00-710-004).
(2)
Allow the APU to run for 5 minutes then check the exhaust for smoke. NOTE : No smoke is permitted.
____
(3)
Select APU ECS mode, check for smoke/fumes in the cabin. NOTE : No smoke or oil fumes are permitted.
____
(4)
Open the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-010-001).
(5)
Examine vent fitting (3), check valve (8)/tube (9) connection, adapter assembly (14) and tubes (21) for oil leaks.
NOTE : No leaks are permitted.
____
________
5. Close-up
Subtask 49-91-53-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Set the LIGHT SW 11LJ to the OFF position.
(3)
Close the APU access doors 315AL, 316AR (Ref. TASK 52-41-00-410-001).
(4)
Remove the access platform(s). Subtask 49-91-53-865-055
B.
Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41
Subtask 49-91-53-860-052
C. Aircraft Maintenance Configuration
(1)
Pressurize the reservoirs of the hydraulic systems.
(Ref. TASK 29-14-00-614-002).
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