737-300 400 500 AMM 飞机维护手册 EXHAUST(84)

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 COWL/REVERSERS USED ON STRUTS WITH ú  78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C01 Page 423 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
3)  If binding is apparent, or if thrust reverser closure shows restricted to all degree, stop the closure and adjust the sliders inboard.
 WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
 CAUTION: WHEN CLOSING THE LEFT THRUST REVERSER HALF, MAKE SURE YOU
_______ HAVE ADEQUATE CLEARANCE BETWEEN THE MAIN ENGINE CONTROL BOX (MEC) AND THE THRUST REVERSER INNER VEE BLADE AND THE FAIRLEAD BRACKET FOR THE ACTUATOR HYDRAULICS TUBES AT APPROXIMATELY NAC WL 85. THIS CAN CAUSE DAMAGE TO THE EQUIPMENT.
 (j)  Close and open the thrust reverser (AMM 78-31-00/201).
 NOTE: The above close and open sequence makes sure that you
____
 install the sliders correctly.

 (k)  
Apply the torque to the two nuts to connect the slider forward half to the aft hinge fitting.

 (l)  
Make sure the slider does not move while you tighten the nuts.

 (m)  
Remove the tape from the turbine exhaust sleeve seal segments.

 S 434-113-C03
 (29) Connect the electrical connector D1008 (D1016) to the sync lock (View B, Fig. 402).
 (a)  
Install the lacing tape to tie the sync lock wiring harness to the thrust reverser wiring harness.

 (b)  
Install the sync lock wiring harness (W1412) through the clamps that are attached to the thrust reverser.

 S 434-076-C03
 (30) Connect the thrust reverser electrical connector (View B and F, Fig. 402).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú  78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C03 Page 424 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 434-103-C03
 (31)
 Install the lockwire on the electrical connectors.

 S 434-077-C03

 (32)
 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 864-078-C03

 (33)
 Do all the applicable steps again to install the opposite thrust reverser half.

 S 974-079-C03

 (34)
 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 forward compression pad, at NAC
 STA 209.75, on the left and right thrust reverser halves 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
 these items:
 1)  The compression pads from which the shims have been
 removed.
 2)  The two aft upper compression pads , at NAC STA 233.38 and
 NAC STA 246.70 on each thrust reverser half.
 (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 THE PROCEDURE 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).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C03 Page 425 (AIRPLANES POST-BOEING-SB 737-54-1036) ú Jul 12/00
　
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