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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MAINTENANCE MANUAL
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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