S 434-001-C01
(28)
Install the lockwire on the electrical connectors.
S 434-058-C01
(29)
Connect the hydraulic hoses to the fittings on the fan cowl panel (Views B and F, Fig. 402) and tighten to 255 inch-pounds (28.8 Newton meters).
S 424-059-C01
(30)
Do all the applicable steps again to install the other thrust reverser half.
S 424-060-C01
(31)
Do not do these steps if you are to install the same thrust reverser half or halves and you have not changed the engine.
(a) Remove the shims from the upper three compression pads on each left and right thrust reverser half and from the three lower compression pads on the left half (View A, Fig. 402).
NOTE: Do not remove the shims from the pads adjacent to the
____ five latch fittings on the left half.
(b)
Apply a piece of clay approximately 0.20 inch (5.1 mm) thick to the nine compression pads.
(c)
Apply bearing grease to the surfaces (or other suitable release agent) which will contact with the clay when the cowl/reverser halves are closed.
WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 TO OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(d)
Close the thrust reverser (AMM 78-31-00/201).
(e)
Make sure that the V-blade and groove surfaces on the extension ring of the fan frame and reverser are fully engaged.
(f)
Close all five latches.
NOTE:____Starts at the forward latch and continues to aft. Use a 50 to 55 pounds (22.7 to 25 kg) closing force as measured one inch (25.4 mm) from latch handle end. If it is necessary, use the hex key wrench to turn the adjustment screw, installed in the end of latch hook, to get the correct closing force.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C02 Page 420 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
B-B
LAMINATED SHIM BONDED TO STRUCTURE
SOLID SHIM (-39) BONDED TO LAMINATED SHIM (-40) AND THEN BONDED TO STRUCTURE
Upper Compression Pad Adjustment Figure 404 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C02 Page 421 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
D-D
315A1000-4 (-8 OPTIONAL)
315A1000-21 AND -22
COMPRESSION PAD AND SHIM
LAMINATED SHIM E-E E-E
LAMINATED SHIM BONDED TO STRUCTURE COMPRESSION PAD (-21) AND SOLID SHIM (-22) Thrust Reverser System - Inspection/Check Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C02 Page 422 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
NAC STA 246.70
F-F
BACS40R10E11F 315A1000-28 AND -20 SOLID SHIM COMPRESSION PAD AND SHIM
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