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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
2)  Tighten the screws that go through elastomer spacers (aft screws, near the extension ring) to 35-90 pound-inches (4-10 Newton meters). To align correctly aft panels to extension ring panels, see AMM 71-11-00/201 Aerodynamic Smoothness.
 (h)  Where it is possible, start at the screws in the center of the acoustical panels.
 S 394-044-C00
 (3)  Apply sealant, MIL-A-46106 at these locations (Ref CFMI Standard Practices Manual 70-66-12):
 (a)  
Between the OGV's and the aft acoustical panels

 (b)  
Between the aft acoustical panels and the fan frame struts

 (c)  
Between the aft acoustical panels.

 S 414-020-C00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
 (4)  
For the applicable thrust reverser, do this task: Close the Thrust Reverser (AMM 78-31-00/201).

 S 414-027-C00

 (5)  
For the applicable fan cowl panel, do this task: Close the Fan Cowl Panel (AMM 71-11-02/201).

 S 864-045-C00

 (6)  
Do this task, Thrust Reverser Activation After Ground Maintenance (AMM 78-31-00/201).

 S 864-035-C00

 (7)  
Remove the DO-NOT-OPERATE tags from the start levers.

 TASK 72-33-02-004-021-C00
 8.  Extension Ring Acoustical Panel Removal_______________________________________
 A.  References
 (1)  AMM 71-11-02/201, Fan Cowl Panels
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 72-33-02
 ALL  ú ú C02 Page 415 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2)  AMM 78-31-00/201, Thrust Reverser System
 B. Access
 (1)  
Location Zones
 502/602 Fan Cowl - Left
 503/603 Fan Cowl - Right
 504/604 Thrust Reverser - Left
 505/605 Thrust Reverser - Right
 506/606 Engine

 (2)  
Access Panels
 5737L/5746L Fan Cowl Panels - Left
 5837R/5846R Fan Cowl Panels - Right
 5739L/5738L Thrust Reverser - Left
 5839R/5838R Thrust Reverser - Right

 

 C. Remove the Acoustical Panel on the Extension Ring
 S 864-036-C00
 (1)  Make sure the start levers are in the CUTOFF position.
 (a)  Install the DO-NOT-OPERATE tags.
 S 014-029-C00
 (2)  Open the applicable fan cowl panel (AMM 71-11-02/201).
 S 014-022-C00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (3)  
Open the applicable thrust reverser (AMM 78-31-00/201).

 S 024-023-C00

 (4)  
Remove the acoustical panel as follows (Fig. 404):

 (a)  ENGINES WITH THE BONDED ACOUSTICAL PANELS; Remove the eight collars and bolts from the acoustical panel.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú C02 Page 416 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
EXTENSION RING
SEE A
A
A
FWD
COLLAR  A
(8 LOCATIONS) 
EXTENSION 
RING  1 

FWD  A-A PANEL ACOUSTICAL  (8 LOCATIONS) BOLT 
1  MA-25S INSULATION ONLY ON ACOUSTICAL PANELS 

INSTALLED ON UPPER 180` SEGMENT OF EXTENSION RING. ACOUSTICAL PANELS INSTALLED ON LOWER 180` SEGMENT OF EXTENSION RING MUST HAVE COLLARS FILLET SEALED WITH BMS5-63 SEALANT
Extension Ring Acoustical Panel Installation
Figure 404 (Sheet 1)
　
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