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时间:2011-04-02 05:45来源:蓝天飞行翻译 作者:航空
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 27-81-21
 ALL  ú ú 01 Page 609 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

A

T

T

A-A
NOTE: ALL DIMENSIONS ARE IN INCHES

65C26660-1,-3 OR 65C26661-1 UNLESS SHOWN DIFFERENTLY 65C26660-5 OR 65C2661-3 ONLY

ROLLER CONTACT-WEAR SURFACE
65C26660-1,-3,-5
Leading Edge Slats (3 and 4) Main Track Wear Limits Figure 601 (Sheet 9)
G60058
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 27-81-21
 ALL  ú ú 01 Page 610 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

TABLE 1
65C26660-1,-3,-5
Leading Edge Slats (3 and 4) Main Track Wear Limits
Figure 601 (Sheet 10)

G60077
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 27-81-21
 ALL  ú ú 01 Page 611 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

TABLE 1
65C26661-1,-3
Leading Edge Slats (3 and 4) Main Track Wear Limits
Figure 601 (Sheet 11)

G60081
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 27-81-21
 ALL  ú ú 01 Page 612 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LEADING EDGE FLAP ACTUATOR - REMOVAL/INSTALLATION
_________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the actuator of the leading edge flap. The procedure has these tasks:
 (1)  
The removal of the actuator from the leading edge flap

 (2)  
The removal of the actuator

 (3)  
The installation of the actuator

 (4)  
The installation of the actuator to the leading edge flap.


 TASK 27-81-31-004-001
 2.  Leading Edge Flap Actuator Removal (Fig. 401)__________________________________
 A.  Special Tools and Equipment
 (1)  
F80048-84, -89 or -90 - Leading Edge Flap Actuator Lock

 B.  
References

 (1)  
27-81-00/201, Leading Edge Flap and Slat Control System

 (2)  
29-09-00/201, Hydraulic Reservoir Pressurization System

 C.  
Access

 (1)  
Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH
 303 Wing Inboard Leading Edge with Slats, LH
 403 Wing Inboard Leading Edge with Slats, RH


 D.  
Prepare for Removal


 S 864-002
 (1)  
Do this task to pressurize hydraulic system B: "Leading Edge Flaps and Slats Hydraulic Systems A and B Pressurization" (Ref 27-81-00/201).

 S 864-021

 (2)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
PTU circuit breakers C1081 and C1085.


 S 864-022
 (3)  Move the flap control lever to the 1-unit detent to extend the leading edge flaps.
 S 494-032
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
_______ THE LEADING EDGE FLAP AND SLAT LOCKS. THE LEADING EDGE FLAPS AND SLATS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (4)  Do this task to install the leading edge flap actuator lock on the adjacent actuator: "Leading Edge Flap and Slat Locks Installation" (Ref 27-81-00/201).
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