(c)
Replace for the clay the applicable shim thickness.
NOTE: It is preferred to shim each thrust reverser half
____ equally, therefore the final computation is to half the gap requirement to find the required shim thickness.
Example: Clay thickness L 0.11 inch (2.79 mm) (plus) + Clay thickness R 0.09 inch (2.29 mm) ------------------
0.20 inch (5.08 mm)
(minus) - 2 X Gap requirement -0.06 inch (1.52 mm) -------------------
0.14 inch (3.56 mm) Divide by two /2 /2
-------------------Required shim = 0.07 inch (1.78 mm)
(d)
At each of the three lower compression pads (Fig. 404), replace for the clay the applicable shim with a thickness equal to the measured clay thickness minus the required distance (0.02 inch
(f)
Apply BMS 10-11 Type I primer after delamination.
(g)
Bond the solid shim to the laminated shim (315A1000-39 and -40, see Figure 404), then bond shims to pads with BMS 5-36 cement and install screws.
[0.51 mm]).
Example: Clay thickness (minus) - Gap requirement 0.09 inch -0.02 inch ---------- (2.29 mm)(0.51 mm)---------
Required shim = 0.07 inch (1.78 mm)
(e) Install new shims.
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO CLOSE THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(h) Close the thrust reverser (AMM 78-31-00/201).
S 434-082-C03
(37)
Engage the telescopic unit of the reverser feedback cable in the support bracket (View B, Fig. 402).
S 434-083-C03
(38)
Tighten and install lockwire to the jamnut.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3
WITH CROSS BEAMS ú C03 Page 428
(AIRPLANES POST-BOEING-SB 737-54-1036) 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 824-084-C03
(39)
Adjust the feedback cable (AMM 78-34-02/201).
S 864-085-C03
(40)
Manually extend the thrust reverser (AMM 78-31-00/201).
S 434-086-C03
(41)
Install the forward two hinge fitting seal supports (Fig. 401).
S 864-087-C03
(42)
Manually retract the thrust reverser (AMM 78-31-00/201).
S 434-088-C03
(43)
Install the forward fairing (AMM 54-32-01/401).
S 434-089-C03
(44)
Install the forward segment of the sleeve-to-strut fairing of the thrust reverser.
S 034-090-C03
(45)
Disconnect the upper end of the actuator rod.
S 434-091-C03
(46)
Adjust the opening actuator of the thrust reverser (AMM 78-31-08/401).
S 434-092-C03
(47)
Remove the protective mat from the upper surface of the sleeve and (if used) from the wing leading edge.
S 864-093-C03
(48)
Examine the thrust reverser cascades by the part number to make sure they are installed in the correct location.
(49)
Change the cascades if it is necessary (AMM 78-31-05/401).
S 864-094-C03
NOTE: The left (right) half of the thrust reverser for the 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 434-095-C03
(50)
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).
(51)
Install the left (right) fan cowl panel (AMM 71-11-02/401).
S 434-096-C03
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3
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