78-31-13
ALL ú ú C01 Page 602 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TRANSLATING SLEEVE PANEL
TRANSLATING SLEEVE PANEL
INBD
Thrust Reverer Auxiliary Slider
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-13
ALL ú ú C01 Page 603 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
L22343
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 016-003-C00
(2)
Open the fan cowl panels (AMM 71-11-02/201).
S 986-017-C00
(3)
Manually extend the thrust reverser to the fully deployed position (AMM 78-31-00/201).
S 216-006-C00
(4)
Use a flashlight and a mirror to do a visual inspection of the upper and lower thrust reverser auxiliary sliders.
(a) Examine the forward and aft ends of the slider fitting in the track. Make sure the Rulon-J on both ends has not worn through (Fig. 601).
NOTE: On the forward end of the slider, you must use an
____ inspection mirror to see the Rulon-J in the slider track.
1) If the Rulon-J is missing or worn through, if you cannot see the Rulon-J, or if the Rulon-J appears to be worn to less than 0.010 inch (0.254 mm) thickness: a) Do this task: Dimensional Inspection Of The Thrust
Reverser Auxiliary Slider.
NOTE: The original thickness of the Rulon-J
____ surface is 0.030 inch (0.762 mm). If the Rulon-J is worn to less than 0.010 inch (0.254 mm) thickness, the slider should be replaced.
2) If you can see that the Rulon-J surface is not worn on both ends of the slider, do this task: Put The Airplane Back To Its Usual Condition. No further action is necessary.
TASK 78-31-13-206-007-C00
3. Dimensional Inspection Of The Thrust Reverser Auxiliary Slider
______________________________________________________________
A. General
(1) This task is a detailed dimensional inspection of the thrust reverser auxiliary slider, done with the slider removed.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-13
ALL ú ú C01 Page 604 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
B. References
(1)
AMM 71-11-02/201, Fan Cowl Panels
(2)
AMM 78-31-00/201, Thrust Reverser
C.
Access
(1)
Location Zones
504 Engine No. 1 - Thrust Reverser System
505 Engine No. 1 - Thrust Reverser System
604 Engine No. 2 - Thrust Reverser System
605 Engine No. 2 - Thrust Reverser System
(2)
Access Panels
5738L Engine No. 1 - Left Thrust Reverser
5739L Engine No. 1 - Right Thrust Reverser
5838R Engine No. 2 - Left Thrust Reverser
5839R Engine No. 2 - Right Thrust Reverser
D.
Procedure
S 046-008-C00
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1)
Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
S 986-009-C00
(2)
Manually extend the thrust reverser to the fully deployed position (AMM 78-31-00/201).
S 026-016-C00
(3)
With the sleeve installed on the thrust reverser, do the task to remove the auxiliary slider fitting (CMM 78-31-23).
S 226-010-C00
(4)
Do a dimensional inspection of the slider.
(a) Examine the slider fitting metal.
1) If the fitting metal is worn, cracked, or damaged, do the task to install a new slider fitting (CMM 78-31-23).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 EXHAUST(147)
