S 822-033
 (2)  
Adjust the cables to the correct loads if it is necessary.

 S 712-034

 (3)  
Do the operational test of the primary and the secondary control systems as follows:

 (a)  
The Aileron and Aileron Trim Control Systems, Systems Test (AMM 27-11-00/501)

 (b)  
The Rudder and Rudder Trim Control System, Systems Test (AMM 27-21-00/501)

 (c)  
The Flight Controls Hydraulic Modular Package, Test (AMM 27-09-21/501)

 (d)  
The Elevator and Tab Control System, Operational Test (AMM 27-31-00/501)

 (e)  
The Stall Warning System, Operational Test (AMM 27-32-00/501)

 (f)  
The Horizontal Stabilizer Trim Control System, Operational Test (AMM 27-41-00/501)

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737-300/400/500MAINTENANCE MANUAL
 (g)  
The Trailing Edge Flap System, Operational Test (AMM 27-51-00/501)

 (h)  
The Trailing Edge Flap Position Indicating System, Operational Test (AMM 27-58-01/501)

 (i)  
The Spoiler/Speed Brake Control System, Operational Test (AMM 27-61-00/501)

 (j)  
The Auto-Speed Brake Control System, Operational Test (AMM 27-62-00/501)

 (k)  
The Leading Edge Slat System, Operational Test (AMM 27-81-00/501)

 (l)  
The Leading Edge Slat Position Indicating System, Operational Test (AMM 27-88-00/501)

 S 022-035
 (4)  
Remove unwanted lubricant applied for storage, but do not use caustic solvents, or cleaning agents.

 S 642-036

 (5)  
If it has been more than one month since the last control cable lubrication, examine, replace as necessary, and lubricate all control cables (AMM 20-10-91/401).

 G. External Surface and Doors
 S 862-037
 CAUTION:_______OBEY THE PRECAUTIONS FOR ARDROX 302N REMOVER. DO NOT PERMIT THE REMOVER TO BECOME DRY. DO NOT PERMIT THE REMOVE TO TOUCH THE ACRYLIC MORE THAN 60 MINUTES. DO NOT PERMIT THE REMOVER TO TOUCH THE HIGH-STRENGTH STEEL PARTS (180,000 PSI AND OVER). IF YOU DO NOT OBEY THESE INSTRUCTIONS, DAMAGE TO COMPONENTS CAN OCCUR.
 (1)  
Apply a layer approximately 20 mils thick of Ardrox 302N remover and permit a dwell time of at least 10 minutes.

 (2)
Use high pressure water that is less than 140°F to rinse the area.

 S 162-038
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A 737-300/400/500MAINTENANCE MANUAL
 S 022-039
 (3)  
Remove the tape from the control cabin windows and windshields, external openings, doors, hatches and nose radome.

 S 642-040

 (4)  
Lubricate all the external doors (AMM 12-25-11/301,
 AMM 12-25-21/301, AMM 12-25-31/301, AMM 12-25-41/301,
 AMM 12-25-51/301, and AMM 12-25-91/301).

 S 212-041

 (5)
Visually examine the door seals for flat spots or deterioration.

 S 212-042

 (6)  
Do a check of the internal and external door handles on the entry and service doors for the correct torque loads.

 S 862-043

 (7)  
Operate the internal and the external handle many times.

 NOTE: Use the internal and the external handle to make sure the
____
 operation of the handles are smooth.

 H. Hydraulic System
 S 282-044
 (1)  Do a check of all the hydraulic system components and replace them if it is necessary.
 NOTE: To replace a component, follow the applicable maintenance
____
 manual procedure.

 S 282-045
 (2)  Supply pressure to the hydraulic system and do a check for leaks (AMM 29-00-00/201, AMM 29-15-00/201).
　
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