(b)
Install the slat inner skin, the coverplate, and the doubler.

 (c)
Install the seal in the end of the outer duct.

 (d)
Put the outer duct assembly over the inner duct.

 (e)
Tighten the cap nut to 250 to 370 pound-inches.

 S 434-036
 CAUTION: FOR SLATS 1 AND 6, INSTALL THE DOWNLOCK HARNESS AND CLAMPS FOR
_______ THE SLAT ACTUATOR SO THEY DO NOT TOUCH THE TELESCOPING DUCT (AMM 27-81-21/401). IF THE HARNESS AND CLAMPS ARE NOT IN THE CORRECT POSITION, RUB OR WEAR DAMAGE CAN OCCUR.
 (14)
 For the duct at slat 1 or 6: Install the access door for the outer duct and the slat inner skin.

 S 864-051

 (15)
 Make sure that the leading edge slats are extended (AMM 27-81-00/201).

 S 414-038

 (16)
 Attach the door (2) to the inner duct (Fig. 401).

 S 434-039

 (17)
 Lightly tighten the bolts (1), but do not tighten them too much.

 S 864-040

 (18)
 Retract the leading edge slats (AMM 27-81-00/201).

 S 824-041

 (19)
 Adjust the door (2) against the wing structure to get equal clearances on the inboard and outboard sides, and equal clearances and on the forward and aft sides.

 (20)
 Tighten the bolts (1).

 (21)
 Extend the leading edge slats (AMM 27-81-00/201).

 S 434-044

 (22)
 Tighten the bolts that attach the door to the inner duct (6 locations).

 S 434-042
 S 864-043
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 30-11-31
 ALL  ú ú 01 Page 409 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 434-045
 (23)
 Attach the bonding strap from the wing structure to the door.

 S 794-046

 (24)
 Do a check for the air leakage at the duct.

 S 864-047

 (25)
 Retract the slats to the full up position (AMM 27-81-00/201).

 S 414-048

 (26)
 Install the wing access panels (AMM 12-30-00/201).

 S 414-049

 (27)
 For the duct at slat 3 or 4: Install the forward fairing on the engine nacelle (AMM 54-32-01/401).

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 WING ANTI-ICE CONTROL MODULE (P5-11) - REMOVAL AND INSTALLATION
_______________________________________________________________
 1.  General
_______
 A.  This subject contains two tasks, one for the removal and one for the installation of the wing anti-ice control module (P5-11). The P5-11 module is located on the pilots' overhead panel.
 TASK 30-11-41-004-013
 2.  Wing Anti-Ice Control Module Removal
____________________________________
 A.  Access
 (1)  Location Zone
 101, 102 Control Cabin

 B.  Procedure
 S 864-001
 (1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
 (a)  P18 Panel
 1) ENG 1 & WING VALVE
 2) ENG 2 & WING VALVE
 3) ENG 1 & WING CONTROL
 4) ENG 2 CONTROL

 S 024-002
 (2)  
Disconnect the four fasteners and lower the module.

 S 034-015

 (3)
Disconnect the electrical connectors from the module.

 TASK 30-11-41-404-014
 3.  Wing Anti-Ice Control Module Installation
_________________________________________
 A.  References
 (1)  24-22-00/201, Manual Control
 B.  Access
 (1)  Location Zone
 101, 102 Control Cabin

 C.  Module Installation
 S 434-003
 (1)
Hold the module and connect the electrical connectors.

 S 424-004

 (2)  
　
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