(a)
Prepare the Airplane for the Removal of the Power Plant.
(b)
Engine Core Disconnects on the Right Side
(c)
Engine Core Disconnects on the Left Side
(d)
Fan Case Disconnects on the Left Side
(e)
Fan Case Disconnect on the Right Side
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)
Container - 5 gallon (20 liter) capacity,
approved for fuel
(4)
Electrical Connector Wrench - C71009
NOTE: Electrical connector wrench is only
____ required on engines with electrical connector (D1204) at strut firewall.
(5)
ENGINES WITH THE SQUARE-TOOTHED CONNECTOR
(4-GAGE WIRE) ON THE W200 WIRE BUNDLE;
Electrical Connector Tool - MT0011,
Daniels Manufacturing Corp., Orlando,FL
C.
Consumable Materials
(1)
Petrolatum, Pure Mineral - CP2102
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71-00-02
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ú ú ú C01B.101 ú BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. Page 404Jul 12/02
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Prepare For the Removal of the Power Plant
__________________________________________ ú
D. Parts
(1) Refer to the AIPC for the part numbers and effectivities of the items in the table that follows:
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 408 | 1 | O-ring | 73-11-01 | 01 | 520 | | | 2 | Drain Plug | | | 515 | 2......…........…...................................…..........….....….........1
E. References
(1)
AMM 08-11-00/201, Level Airplane
(2)
AMM 20-40-11/201, Static Grounding
(3)
AMM 24-22-00/201, Electrical Power
(4)
AMM 27-81-00/201, Leading Edge Flap and Slat Control System
(5)
AMM 29-09-00/201, Hydraulic Reservoir Pressurization System
(6)
AMM 54-32-01/401, Forward Fairing
(7)
AMM 71-11-02/401, Fan Cowl Panels
(8)
AMM 78-31-00/201, Thrust Reverser System
F.
Access
(1)
Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
501/601 Inlet Cowl
502/503 Fan Cowl Panels - Engine No. 1
602/603 Fan Cowl Panels - Engine No. 2
504/505 Thrust Reversers - Engine No. 1
604/605 Thrust Reversers - Engine No. 2
506 Engine No. 1
606 Engine No. 2
(2)
Access Panels 5739L/5738L Thrust Reversers - Engine No. 1 5839R/5838R Thrust Reversers - Engine No. 2
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 動力裝置 POWER PLANT 1(108)
