(b)  
Turn the OGV until the outboard end is toward you.

 (c)  
Lift the OGV out of the aft fairing recess.

 S 214-005-C00
 (4)  Examine the seal on the OGV inner shroud. If it is necessary, remove the seal.
 TASK 72-33-01-404-006-C00
 3. Fan Outlet Guide Vanes and Seals Installation (Fig. 401)
_____________________________________________
 A. General
 (1)  There are three different OGV types used in a set. You must compare the part numbers of the initial and replacement OGV's.
 B. Consumable Materials
 (1)  D00601 Grease, graphite (CP2101) - GP460 Aeroshell 8
 C. References
 (1)  
AMM 71-11-02/201, Fan Cowl Panels

 (2)  
AMM 78-31-00/201, Thrust Reverser System

 D. Access
 (1)  Location Zones
 506 Engine No. 1 - Fan Frame
 606 Engine No. 2 - Fan Frame

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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)  Access Panels 5738L/5739R Engine No. 1 - Fan Duct Cowl and Thrust Reverser Halves
 5838L/5839R  Engine No. 2 - Fan Duct Cowl and ThrustReverser Halves
 E. Procedure
 S 434-007-C00
 (1)  
If it is necessary, install the seal on the inner shroud.

 S 424-008-C00

 (2)  
Install the OGV.

 NOTE:____Look at the part number of the OGV. This will tell you if the OGV is aluminum or composite.
 (a)  
Engage the OGV inner platform into the aft fairing recess.

 (b)  
Push the OGV outer platform forward and lift the OGV against the interior surface of fan inlet case.

 S 644-011-C00
 (3)  
Lightly lubricate the threads of the bolts with grease, GP460 Aero shell 8.

 S 434-014-C00

 (4)  
COMPOSITE OGV'S (ENGINES WITH CFMI SB 72-713); Install the bolts and washers that attach the OGV to the fan inlet case.

 (a)  Tighten the bolts to 170-185 pound-inches (19-21 Newton meters).
 S 434-013-C00
 (5)  ALUMINUM OGV'S (ENGINES WITH AND WITHOUT CFMI SB 72-796); Install the bolts and saddles that attach the OGV to the fan inlet case.
 (a)  Tighten the bolts to 170-185 pound-inches (19-21 Newton meters).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(6)  S 414-015-C00Do this task:  Close the Thrust Reverser (AMM 78-31-00/201).
 (7)  S 864-016-C00Do this task: Thrust Reverser Activation after Ground Maintenance (AMM 78-31-00/201).
 (8)  S 414-017-C00Do this task:  Close the Fan Cowl Panel (AMM 71-11-02/201).

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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ACOUSTICAL PANELS - REMOVAL/INSTALLATION
________________________________________
 1.  General
_______
 A.  This procedure gives the tasks to remove and install the acoustical panels. The acoustical panels are installed in the fan case, fan frame and fan case extension ring.
 B.  Separate tasks are given for these acoustical panels that follow:
 (1)
Forward acoustical panels

 (2)
Mid acoustical panels
　
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