71-00-02
 ALL  ú ú C12B Page 480Q ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Put the Airplane Back To Its Usual Condition
____________________________________________
 TASK 71-00-02-844-109-C00
 6. Put the Airplane Back To Its Usual Condition
____________________________________________
 A. General
 CAUTION: THE ENGINE MUST BE PRESERVED PER CHAPTER AMM 71-00-03/201 TO
_______ PREVENT INTERNAL PARTS CORROSION OR FAILURES.
 (1)  
You must do these tasks to put the power plant back to its usual condition:

 (a)  
Core Area Connections on the Left Side

 (b)  
Core Area Connections on the Right Side

 (c)  
Fan Case Connections on the Left Side.

 (d)  
Fan Case Connections on the Right Side.

 (e)  
Put the Airplane Back To Its Usual Condition.

 B.
Equipment

 (1)  
ENGINES WITHOUT THE VIBRATION ISOLATORS FOR THE
 FORWARD MOUNT/THRUST REVERSER HINGES;
 Thrust Reverser Hold-Open Rods - C78001-13

 (2)  
ENGINES WITH THE VIBRATION ISOLATORS FOR THE
 FORWARD MOUNT/THRUST REVERSER HINGES;
 Thrust Reverser Hold-Open Rods - C78012-14

 NOTE: C78012-14 replaces C78012-1.
____
 (3)  Part Power Rig Pin - C76001-1 or -2,
 or equivalent 0.248 (+0.000/-0.003) inch [6.30
 (+0.000/-0.076) mm] diameter, 2.5 inch (64 mm)
 minimum long rod or bolt with warning streamer
 attached

 NOTE: Part power rig pin C76001-1 or C76001-2,
____ as applicable, is found in a fly-away kit located in electronics compartment (kit is attached to forward outboard leg of battery support).
 (4)  Electrical Connector Wrench - C71009
 NOTE: Electrical connector wrench is only
____ required on engines with electrical connector (D1204) at strut firewall.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-00-02
 ALL  ú ú C08B Page 480R ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Put the Airplane Back To Its Usual Condition
____________________________________________
 (5)  
ENGINES WITH THE SQUARE-TOOTHED CONNECTOR
 (4-GAGE WIRE) ON THE W200 WIRE BUNDLE;
 Electrical Connector Tool - MT0011,
 Daniels Manufacturing Corp., Orlando,FL

 (6)  
Strap wrench - TG70, Glenair Inc.
 Glendale, CA

 C.
Consumable Materials

 (1)  
Anti-Seize Compound - Bostik Never Seez Pure
 Nickel Special

 (2)  
Graphite Grease - CP2101

 (3)  
Pure Mineral Petrolatum - CP2102

 D.
Parts

 (1)  
Refer to the AIPC for the part numbers and effectivities of the items in the table that follow:

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 403 | 1 | Clamp | 77-21-00 | 01 | 110 | | | 2 | Bolt | | | 95 | | | 3 | Washer | | | 100 | | | 4 | Nut | | | 105 | | | 5 | Clamp | | | 110 | | | 6 | Clamp | | | 110 | | | 7 | Nut | 36-12-35 | 02 | 60 | | | | | | | 9 | | | 8 | Washer | | | 45 | | | | | | | 50 | | | | | | | 90 | | | 9 | Bolt | | | 70 | | | 10 | Bolt | | | 75 | | | 11 | Washer | | | 80 | | | 12 | Clamp | 77-21-00 | 01 | 110 | 2......…........…...................................…..........….....….........1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 71-00-02
 ALL  ú ú C14B Page 480S ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
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