(7)  
If a latch adjustment is necessary, refer to 71-11-03/501.

 S 432-014-C00 CAUTION: DO NOT USE MORE THAN 60 POUNDS (270 NEWTONS) OF FORCE TO PUSH
_______ THE LATCH HANDLE CLOSED. TOO MUCH FORCE CAN CAUSE DAMAGE TO THE LATCH.
 (8)  
Engage the latch hooks to latch the keepers along the fan cowl panel mating halves, and push the latch handles closed.

 S 822-016-C00

 (9)  
If a latch adjustment is necessary, refer to 71-11-03/501.

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 ALL  ú ú C02 Page 207 ú Nov 15/98
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 862-019-C00
 (10)
 Make sure the manual starter guide opening is aligned with the manual starter value.

 S 442-017-C00

 (11)
 Do the activation procedure of the leading edge flaps as follows:

 (a)  
If the deactivation procedure was done on only the leading edge devices, refer to AMM 27-81-00/201.

 (b)  
Remove the circuit breaker lockset, and close these circuit breakers: 1) P6-2 Circuit Breaker Panel

 a) FLAP
 2) P6-11 Circuit Breaker Panel
 a) STBY HYD PUMP NORMAL
 3) P6-12 Circuit Breaker Panel
 a) STBY HYD PUMP (ALT)

 (c) Remove the DO-NOT-OPERATE tag from the flap control lever.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-11-02
 ALL  ú ú C02 Page 208 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FAN COWL PANELS - REMOVAL/INSTALLATION
______________________________________
 1.  General
_______
 A.  This procedure contains four tasks. The first task is to remove the fan cowl panels manually. The second task is to remove the fan cowl panels with the sling configuration. The third task is to install the fan cowl panels manually. The fourth task is to install the fan cowl panel with the sling configuration.
 B.  The fan cowl panel removal and installation are done manually or with a boom and sling arrangement. The boom attaches to the forward strut mount fittings, and the sling attaches to a fishpole hoist.
 TASK 71-11-02-004-001-C00
 2.  Remove the Fan Cowl Panel (Manually)
____________________________________
 A.  References
 (1)
AMM 27-81-00/201, Leading Edge Device Deactivation

 (2)
AMM 71-11-08/401, Vortex Control Device

 (3)
AMM 71-11-02/201, Fan Cowl Panel

 B.  
Access

 (1)  
Location Zones
 506 No. 1 Engine
 606 No. 2 Engine

 (2)  
Access Panel
 5746 Fan Cowl Panel (LH) - Engine No. 1
 5846 Fan Cowl Panel (LH) - Engine No. 2
 5737 Fan Cowl Panel (RH) - Engine No. 1
 5837 Fan Cowl Panel (RH) - Engine No. 2

 C.  
Manually Remove the Fan Cowl Panel (Fig. 401).

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 71-11-02
 ALL  ú ú C01 Page 401 ú Jul 15/93
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 044-002-C00
 WARNING: DO NOT TRY TO REMOVE THE FAN COWL PANEL DURING AN ENGINE
_______ OPERATION BECAUSE THE FORWARD LATCHES/HINGES ARE IN THE ENGINE INLET HAZARD AREA ZONE. IF YOU GO INTO THE HAZARD AREA, YOU CAN BE PULLED INTO THE ENGINE WITH POSSIBLE FATAL RESULTS.
 BE CAREFUL WHEN YOU REMOVE THE FAN COWL PANEL IN HIGH WINDS OR GUST CONDITIONS. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
　
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