S 712-046
 (3)  Do a test of the hydraulic systems that follow:
 (a)  
The main (left, right and center) hydraulic systems
 (AMM 29-11-00/201).

 (b)  
The Ram Air Turbine (RAT) system (AMM 29-21-00/501).

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 (c)  
The Hydraulic Fluid Quantity Indicating system (AMM 29-33-00/501).

 (d)  
The Hydraulic Pressure Indicating System (AMM 29-31-00/501).

 (e)  
The Hydraulic Fluid Temperature Indicating System (AMM 29-32-00/501).

 (f)  
Power Transfer Unit System (AMM 29-22-00/501).

 (g)  
Hydraulic Reservoir Pressure Indication System (AMM 29-35-00/501).

 S 962-047
 (4)  Replace the hydraulic system filters that follow:
 (a)  
The System L and R EDP Pressure/Case Drain Filter Module (AMM 29-11-17/401).

 (b)  
The ADP Pressure/Case Drain Filter Module (AMM 29-11-19/401).

 (c)  
The System L and R Return Filter Module
 (AMM 29-11-15/401).

 (d)  
The PTU Pressure Filter (AMM 29-22-02).

 (e)  
The PTU Case Drain Filter Module
 (AMM 29-22-05).

 L. Flight Controls
 S 632-048
 (1)  Make the flight control system serviceable after a Short Term (0 - 30 days) storage (AMM 27-00-00).
 NOTE: The flight control system operational tests are identified in
____ the Long Term (more than 30 days) storage procedure given below.
 (a)  
Make sure the cable tension loads are correct in all primary control systems (AMM 27-00-01/201).

 (b)  
Make sure the cable tension loads are correct in all secondary control systems (AMM 27-00-01/201).

 S 632-049
 (2)  Make the flight control system serviceable after a Long Term (more than 30 days) storage.
 (a)  Examine all of the cables you can see visually, and lubricate them (AMM 20-10-03/401).
 NOTE: When the last control cable lubrication was more than
____ 30 days, examine the cables (AMM 20-20-02/601). If it is necessary, replace the defective cables that you find.
 (b)  
Extend all of the flaps (both leading edge [AMM 27-81-00/1] and trailing edge [AMM 27-51-00/1]) and the spoilers, and examine them for corrosion.

 (c)  
Lubricate all of the flap tracks (AMM 12-21-09/301).

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 S 712-050
 (3)  Do an operational test of the primary and secondary control systems that follow:
 (a)  
The Control System Electronics Unit (CSEU) (AMM 27-09-00).

 (b)  
The Aileron and Aileron Trim Control System (AMM 27-11-00/501).

 (c)  
The Aileron Position Indicating System (AMM 27-18-00/501).

 (d)  
The Rudder and Rudder Trim Control System (AMM 27-21-00/501).

 (e)  
The Rudder and Elevator Hydraulic Supply Shutoff (AMM 27-23-00/501).

 (f)  
The Rudder Position Indicating System (AMM 27-28-00/501).

 (g)  
The Elevator Control System (AMM 27-31-00).

 (h)  
The Stall Warning System (AMM 27-32-00/501).

 (i)  
The Elevator Position Indicating System (AMM 27-38-00/501).

 (j)  
The Horizontal Stabilizer Trim Control System (AMM 27-41-00/501).

 (k)  
The Stabilizer Trim Indicating System (AMM 27-48-00/501).

 (l)  
The Trailing Edge Flap System (AMM 27-51-00/501).

 (m)  
The Trailing Edge Flap Position Indicating System (AMM 27-58-00/501).

 (n)  
The Spoiler/Speedbrake Control System (AMM 27-61-00/501).
　
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