the stabilizer movement stops. 2) Make sure the captain's STAB TRIM indicator shows
 3.0 +/- 1.0 units of trim.
 3)  Move the two STAB TRIM switches on the captain's control wheel to the NOSE UP position.
 NOTE: You will measure how much time is necessary for
____ the stabilizer to move from the upper travel limit the lower travel limit.
 4) Hold the STAB TRIM switches in the NOSE UP position until the stabilizer movement stops. 5) Measure the time necessary for the stabilizer to move from
 the upper travel limit to the lower travel limit. 6) Release the two STAB TRIM switches. 7) Make sure the stabilizer moves from its upper travel limit
 to its lower travel limit in 43 - 57 seconds.
 S 825-034
 (4)  
Do this test: "M1452 and M1453 Circuit Cards (Flap Load Limiter System)" (AMM 32-09-20/401).

 (5)  
Do this task: "Passenger Sign Operation Test" (AMM 33-24-00/201).

 S 825-035
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A
737-300/400/500MAINTENANCE MANUAL
 H. Put the Airplane Back to Its Usual Condition
 S 415-026
 (1)
Install the switch cover on the flap control unit (Fig. 501):

 (a)  
Apply a thin layer of the grease to the switch cover.

 (b)  
Install the switch cover.

 S 865-027
 (2)  
Put the ALTERNATE FLAP arm switch in the OFF position.

 S 415-028

 (3)  
Do this task: "Inboard Flap Track Fairing Installation"
 (Ref 27-51-32/401).

 S 865-029

 (4)  
Do this task: "Hydraulic System B Pressurization"
 (Ref 27-51-00/201).

 S 865-030

 (5)  
Put the flap control lever in the UP detent to retract the trailing edge flaps.

 S 865-031

 (6)  
Do this task: "Hydraulic System B Depressurization"
 (Ref 27-51-00/201).

 (7)  
Do this task: "Remove Electrical Power" (Ref 24-22-00/201).

 S 865-032
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FLAP LOAD LIMITER AIRSPEED SWITCHES - REMOVAL/INSTALLATION
__________________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the flap load limiter airspeed switches.
 B.  The two airspeed switches are installed in the lower compartment below the floor of the flight compartment. The switch S560 is connected to the auxiliary pitot-static system No. 1. The switch S562 is connected to the auxiliary pitot-static system No. 2.
 TASK 27-51-89-004-001
 2.  Flap Load Limiter Airspeed Switch Removal_________________________________________
 A.  Access
 (1)  
Location Zone
 202 Lower Nose Compartment

 B.  
Procedure

 S 864-002
 (1)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6 Panel
 1) FLAP LOAD RELIEF

 S 024-003
 (2)  
Remove the airspeed switch:

 (a)  
Remove the pitot and the static lines from the airspeed switch.

 (b)  
Disconnect the electrical connector from the airspeed switch.

 (c)  
Remove the mounting bolts from the airspeed switch.

 (d)  
Remove the airspeed switch from the airplane.

 TASK 27-51-89-404-004
 3.  Flap Load Limiter Airspeed Switch Installation______________________________________________
 A.  References
 (1)  
27-51-89/501, Flap Load Limiter Airspeed Switches
　
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