737-300 400 500 AMM 飞机维护手册 EXHAUST(81)

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 WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1)  Do the deactivation procedure for the thrust reverser for ground maintenance (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 C01 Page 416 (AIRPLANES POST-BOEING-SB 737-54-1036) 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 044-033-C03
 (2)  Open the circuit breakers and attach the DO-NOT-CLOSE tags for the applicable engine as follows:
 (a)  P6 Load Control Center
 1) ENG 1 THR REV IND SYS
 2) ENG 2 THR REV IND SYS
 3) ENG 1 SYNC LOCK
 4) ENG 2 SYNC LOCK
 5) ENG 2 SYNC LOCK - ALTN

 S 864-035-C03
 (3)  Make sure you remove the forward two hinge seal supports from the upper bifurcation of the thrust reverser.
 S 434-036-C03
 CAUTION: MAKE SURE THAT THE THRUST REVERSER HALVES DO NOT CLOSE AT THE
_______ SAME TIME BEFORE THE FINAL ADJUSTMENT. THIS CAN CAUSE STRUCTURAL DAMAGE TO THE THRUST REVERSER HALVES.
 (4)  
Adjust the compression rods (Fig. 404) to the length shown.

 S 864-037-C03

 (5)  
Make sure that the rods move freely in the strut fittings.

 S 644-047-C03

 (6)  
Lubricate the shank on the two hinge fitting bolts (Views C and D, Fig. 402) with bearing grease.

 NOTE: Do not lubricate the bolt threads.
____
 S 434-048-C03
 (7)  
If the sling and fittings are not attached to the thrust reverser half, connect the upper attach fittings of the sling to the clevis fittings on upper bifurcation (View B, Fig. 403).

 S 434-049-C03

 (8)  
Install the lower attach fittings of the sling at the holes in the lower bifurcation of the thrust reverser (View C, Fig. 403).

 (9)  
Attach the sling to the fittings.

 S 434-050-C03
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú  78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C03 Page 417 (AIRPLANES POST-BOEING-SB 737-54-1036) 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////

UPPER COMPRESSION PAD
NAC STA 209.75
A-A

 

315A1000-3 B-B 
 315A1000-40 SHIMS 315A1000-39 AND B-B 
LAMINATED SHIM BONDED TO STRUCTURE 
SOLID SHIM (-39) BONDED TO LAMINATED SHIM (-40) AND THEN BONDED TO STRUCTURE
Figure 404 (Sheet 1) Upper Compression Pad Adjustment 

 

E69286
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
 VIBRATION ISOLATOR SUSPENSION AND  ú  CONFIG  3
 WITH CROSS BEAMS  ú  C01  Page 418
 (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 ////////////////////////

PAD JAMNUT
FORWARD COMPRESSION ROD
NAC STA 233.38
C-C

PAD JAMNUT
AFT COMPRESSION ROD
NAC STA 246.70
D-D

Upper Compression Pad Adjustment
Figure 404 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
　
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