S 214-016-C00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 434-017-C00
 (9)  Install the drain plug with a new O-ring lubricated with engine oil.
 (a)  
Tighten the drain plug to 43-48 pound-inches
 (4.8-5.5 Newton meters).

 (b)  
Safety the drain plug with a lockwire.

 E. Set the clogging indicator
 S 824-018-C00
 (1)  Do these steps to set the clogging indicator:
 (a)  
Manually remove the knurled retaining ring.

 (b)  
Remove the retaining ring and glass inspection bowl.

 (c)  
Push the red button on the clogging indicator to the retracted position.

 NOTE: The button must stay in the retracted position.
____
 (d)  
Install the glass inspection bowl.

 (e)  
Lightly lubricate the knurled retaining ring with engine oil.

 (f)  
Install the knurled retaining ring with your hand.

 (g)  
Make sure that you cannot see the red indicator button.

 (h)  
Safety the retaining ring to the clogging indicator body with a lockwire.

 S 614-019-C00
 (2)  
Do the Engine Oil Replenish procedure (AMM 12-13-11/301).

 S 794-020-C00

 (3)  
Do the Engine Leak Check - Idle Power
 (AMM 71-00-00/501, Test No. 3).

 (4)  
Close the fan cowl panels (AMM 71-11-02/201).

 S 414-021-C00
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SCAVENGE OIL FILTER ELEMENT - REMOVAL/INSTALLATION
__________________________________________________
 1.  General
_______
 A.  This procedure contains two tasks. The first task is to remove the Scavenge Oil Filter Element. The second task is to install the Scavenge Oil Filter Element.
 B.  The scavenge oil filter element in the screw-on bowl can be replaced.
 C.  The scavenge oil filter is attached to the accessory gearbox at the 7 o'clock position.
 TASK 79-21-04-004-001-C00
 2.  Remove the Scavenge Oil Filter Element
______________________________________
 A.  Equipment
 (1) Container - 1 quart (1 liter) capacity for oil.
 B.  References
 (1) AMM 71-11-02/201, Fan Cowl Panel
 C.  Access
 (1)  
Location Zones
 506 Engine No. 1
 606 Engine No. 2

 (2)  
Access Panels 5737L/5746L Engine No. 1 - Fan Cowl Assembly 5837R/5846R Engine No. 2 - Fan Cowl Assembly

 D.  Procedure (Fig. 401)
 S 014-002-C00
 (1) Open the left fan cowl panel (AMM 71-11-02/201).
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 ALL  ú ú C01 Page 401 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
CLOGGING INDICATOR 
SEE  A  "OIL IN" TUBE 
"OIL OUT" TUBE  O-RING ELECTRICAL CONNECTOR
FILTER ELEMENT 
FWD  O-RING 
BOWL 

A
Scavenge Oil Filter - Element Installation Figure 401 (Sheet 1)
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