2) Connect the aft end of the fuse [100] to the 'T' fitting [102]. a) Tighten the nut [101].
(b)
Install the hydraulic tube [96]. 1) Connect the nut of the tube [96] to the aft bulkhead. a) Tighten the nut.
2) Connect the nut [95] to the 'T' fitting [103]. a) Tighten the nut [95].
(c)
Install the tube bracket [97].
1) Install the two screws that hold the bottom bracket to the top bracket.
(d)
Install the elbow fitting [98].
1) Connect the nut [102] to the 'T' fitting [103]. a) Tighten the nut [102].
(e)
Install the air conditioning duct [91]. 1) Install the V-band clamp [94] on each end of the air conditioning duct [91].
2) Install the bonding jumper [93] to the air conditioning duct [91]. a) Tighten the nut [92].
(f)
Close the access panel 3303L.
E. Put the Airplane Back to Its Usual Condition
S 864-014-C00
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL
_______ SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Supply hydraulic power (AMM 29-15-00/201).
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78-34-07
ALL ú ú C01 Page 412 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2) S 734-013-C00If you installed the primary or return line fuses, do the Normal Operation Test (AMM 78-31-00/501).
(3) S 734-017-C00If you installed the standby fuses, do the Standby Operation Test (AMM 78-31-00/501).
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78-34-07
ALL ú ú C01 Page 413 ú Jul 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST REVERSER SYNC LOCK - REMOVAL/INSTALLATION
________________________________________________
1. General
_______
A. This procedure contains the tasks to remove and install a thrust reverser sync lock on the upper hydraulic actuator of each thrust reverser sleeve. There are two sync locks installed on each engine.
TASK 78-34-10-004-001-C00
2. Thrust Reverser Sync Lock Removal
_________________________________
A. References
(1)
AMM 71-11-04/201, Fan Cowl Panels
(2)
AMM 78-31-00/201, Thrust Reverser System
B.
Access
(1)
Location Zones
101 Control Cabin - Left
102 Control Cabin - Right
506 Left Engine
606 Right Engine
(2)
Access Panels
5746L/5846R Fan Cowl - Left
5737L/5837R Fan Cowl - Right
5738L/5838R Thrust Reverser Cowl - Left
5739L/5839R Thrust Reverser Cowl - Right
C.
Prepare to Remove the Sync Lock
S 864-002-C00
(1) For the left engine, open this circuit breaker on the load control center, P6, and attach a DO-NOT-CLOSE tag:
(a) ENGINE 1 SYNC LOCK
S 864-003-C00
(2) For the right engine, open these circuit breakers on the load control center, P6, and attach DO-NOT-CLOSE tags:
(a)
ENGINE 2 SYNC LOCK
(b)
ENGINE 2 SYNC LOCK ALTN
S 044-005-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3) Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
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