(a)  Do a check of the bushing flange for wear (if the flange rubs an adjacent part of the structure). 1) If the flange face thickness has greater than 25% wear,
 replace the bushing.
 NOTE: Refer to SRM 54-50-90 for bushings on the strut
____ structure or CMM 54-50-01 for bushings on the upper link or diagonal brace.
 (b)  
Remove the sealant.

 (c)  
Do a check for corrosion around the flange of the bushing. 1) If you see corrosion, replace the bushing.

 NOTE: Refer to SRM 54-50-90 for bushings on the strut
____ structure or CMM 54-50-01 for bushings on the upper link or diagonal brace.
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 (d)  
If you do not find corrosion or flange face thickness wear less than 25%, fillet seal the outside edge of the bushing flange with BMS5-95 sealant (AMM 20-30-11/201).

 (e)  
Do the inspection for migration again at the next "C" check.

 F. Put the Airplane Back to Its Usual Condition.
 S 416-009-B00
 (1)  
Install the applicable strut fairings (AMM 54-32-01/401).

 S 416-010-B00

 (2)  
Close the access doors of the aft fairing.

 S 416-011-B00

 (3)
Install the applicable strut access panels (AMM 54-33-01/201).

 S 446-012-B00

 (4)  
Do the activation procedure for the leading edge slats
 (AMM 27-81-00/201).

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 NACELLE STRUT DRAIN TUBE AND SEALANT - INSPECTION/CHECK
_______________________________________________________
 1.  General_______
 A.  There are four tasks in this procedure:
 (1)  
System disconnect box drainage check

 (2)  
Strut midspar drainage check

 (3)  
Strut midspar closeout web drainage check

 (4)  
Heat shield assembly drainage check

 B.  Apply the sealant to the heat shield and the interior of the nacelle strut. It prevents the leakage of the fuel or the hydraulic fluid between the strut compartments or to the engine. Do a check on the strut for the correct strut sealing.
 C.  The drain system supplied a way for fluids which leak from the system plumbing to route through the strut to a safe location outside the airplane. The procedures to clear the strut drain system of blockages, and includes the use of the compress air and water.
 TASK 54-11-00-206-001-B00
 2.  System Disconnect Box Drain Check_________________________________
 A.  General
 (1)  When you install the engine, do the strut drain check.
 B.  Equipment
 (1)  
Funnel and Hose

 (2)  
Container - Minimum of 2 U.S. gallons (8 liters) of water

 C.  References
 (1)  
AMM 54-31-01/401, Naceele Strut Access Panels

 (2)  
AMM 54-32-01/401, Nacelle Strut Forward Fairing

 D.  Access
 (1)  
Location Zone
 ZONE 5 LEFT NACELLE
 ZONE 6 RIGHT NACELLE

 (2)  
Access Panel
 5738R FAN COWL - RIGHT NACELLE
 5739R FAN COWL - RIGHT NACELLE

 NACELLE STRUT FORWARD FAIRING ACCESS PANEL
 E.  Procedure
 S 016-003-B00
 (1)  Remove the forward fairing (AMM 54-32-01/401).
 (a)  Use the procedure given in AMM 54-31-01/401 to remove and attach the clamp latch fasteners.
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