S 434-063-C01
(34)
Tighten and install lockwire to the jamnut.
S 864-064-C01
(35)
Adjust the feedback cable (AMM 78-34-02/201).
S 864-065-C01
(36)
Move the sleeve to the extended position (AMM 78-31-00/201).
S 434-066-C01
(37)
Install the forward two hinge fitting seal supports (Fig. 401).
S 864-067-C01
(38)
Move the sleeve to the retracted position (AMM 78-31-00/201).
S 434-068-C01
(39)
Install the forward fairing (AMM 54-32-01/401).
S 434-069-C01
(40)
Install the forward segment of the sleeve-to-strut fairing of the thrust reverser.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C01 Page 426 ú Jul 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
S 864-070-C01
(41)
Remove, install and adjust the opening actuator of the thrust reverser (AMM 78-31-08/401).
S 434-071-C01
(42)
Remove the protective mat from the upper surface of the sleeve and (if used) from the wing leading edge.
S 864-072-C01
(43)
Examine the thrust reverser cascades by the part number to make sure they are installed in the correct location.
S 864-073-C01
(44)
Change the cascades if it is necessary (AMM 78-31-05/401).
NOTE: The left (right) half of the thrust reverser for
____ left engine is interchangeable with the left (right) half of the thrust reverser for the right engine. However, make sure the cascades are installed in the specified configuration for that engine (AMM 78-31-05/401).
S 434-074-C01
(45)
If you installed an inboard thrust reverser half, make sure that the deflectors of the flap seal door are installed (AMM 78-31-09/401).
S 434-075-C01
(46)
Install the fan cowl panel (AMM 71-11-02/401).
S 224-083-C01
(47)
IF YOU INSTALLED A DIFFERENT THRUST REVERSER HALF OR CHANGED THE ENGINE; Do a check for aerodynamic smoothness between the fan cowl and the thrust reverser sleeve (AMM 78-31-10/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C01 Page 427 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 414-005-C01
(48)
Supply hydraulic power (AMM 29-15-00/201).
S 414-006-C01
(49)
Supply hydraulic pressure from the reservoir (AMM 29-09-00/201).
S 714-078-C01
(50)
Do these tests in AMM 78-31-00/501 as follows:
(a)
Indicator lights test.
(b)
Normal Operation Test.
1) Operate the thrust reverser between the retract and the extend position until all the air is bled from reverser hydraulic system as evidenced by smooth translation of the sleeves.
(c)
Auto-Restow Test.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C01 Page 428 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST REVERSER - REMOVAL/INSTALLATION
______________________________________
1. General
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