EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITHOUT VIBRATION ISOLATORS ú

 54-42-13
 ú ú B05 Page 206 ú Nov 12/00
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F11414
A 737-300/400/500MAINTENANCE MANUAL

Center Thrust Reverser Hinge Fitting Installation
Figure 203 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH CROSS RODS ú

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 ú ú B04 Page 207 ú Jul 15/95
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F11435
A
737-300/400/500MAINTENANCE MANUAL
34. HINGE FITTING SEE A33. WASHER 32. BOLT
31. BOLTSEE B 35. CROSS BEAM
SEE C
A
43. WASHER 36. WASHER
42. JUMPER
37. NUT
A
41. BUSHING
39. WASHER
40. ISOLATOR
38. NUT
34. CENTER
45. BUSHING  A
HINGE
(2 LOCATIONS) FITTING
48. BUSHING (2 LOCATIONS)
42. JUMPER
38. NUT
31. BOLT
39. WASHER
43. WASHER 45. BUSHING
44. BUSHING (2 LOCATIONS)
35. CROSS  40. ISOLATOR (2 LOCATIONS)
BEAM

41. BUSHING
 (2 LOCATIONS)

B
A-A
47. BUSHING
 (2 LOCATIONS)

48. BUSHING
46. RETAINER  (2 LOCATIONS)(2 LOCATIONS)
49.
 RACE (2 LOCATIONS)

50.
 BALL (2 LOCATIONS)

C
Center Thrust Reverser Hinge Fitting Installation
Figure 203 (Sheet 3)

F11631
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH CROSS BEAMS ú

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 ú ú B06 Page 208 ú Jul 15/98
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A 737-300/400/500MAINTENANCE MANUAL
A
A
B
B
RIGHT SIDE OF STRUT OPPOSITE LEFT SIDE OF STRUT SHOWN
0.16 MINIMUM  GAP0.032 0.005  0.16 MINIMUM 
0.12 MINIMUM  FWD  0.12 MINIMUM  FWD  0.032 0.005 GAP 
A-A  B-B 
Figure 203 (Sheet 4) Thrust Reverser Cowl Installation 

G67768
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú B06 Page 209 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

FWD

Aft Thrust Reverser Hinge Fitting Installation
Figure 204

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F11399
A 737-300/400/500MAINTENANCE MANUAL
 TASK 54-42-13-012-043-B00
 2. Get Access to the the Hinges for the Thrust Reverser (Fig. 201)
____________________________________________________
 A. References
 (1)  
AMM 78-31-00/201, Thrust Reverser System

 (2)  
AMM 78-31-01/401, Thrust Reverser

 B. Access
 (1)  
Location Zones
 500 Left Nacelle
 600 Right Nacelle

 (2)  
Access Panels
 5783L - Left Thrust Reverser
 5883R - Right Thrust Reverser

 C. Procedure
 S 042-006-B00
 WARNING: DO THE DEACTIVAION 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).
　
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