2 If there is no continuity:
_

 - do a check and repair the wiring between the: PRESS SW-FLT CTL, G (1151GN) connector A/C and FWC-1/ FWC-2 connector AA/06C (Ref. ASM 29-32/01) and (Ref. ASM 31-52/02).
 (b) If the rudder does not operate:
 - do a check for 28 VDC at the: the SOL VALVE-LEAKAGE MEAS, G (1150GP) connector A/A and the connector A/B. (Ref. ASM 29-19/01).
 NOTE : There is normally 0 VDC.
____

 1 If there is 28 VDC:
_

 - do a check of the wiring between: the pushbutton switch (1882GP) connector C2 and the connector C3 (Ref. ASM 29-19/01).
 a If there is continuity:
_ - replace the pushbutton switch 1882GP.

 b If there is no continuity:
_

 - do a check and repair the wiring between the: pushbutton switch (1882GP) connector C3 and the CB (1881GP) (Ref. ASM 29-19/01).
 (c) If the fault continues:
 - Replace the SOL VALVE-LEAKAGE MEAS, G (1150GP) (Ref. AMM TASK 29-19-51-000-001) and (Ref. AMM TASK 29-19-51-400-001).
 (2) If the pressure is less than 1450 psi:
 - do a check for external leakage and repair the components as necessary.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-058, 101-101, ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 223
 May 01/05 CES

R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
 A. If the fault confirmation gives:
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 - the system name and the flow arrow of the Green hydraulic system in amber on the lower ECAM DU:

 - do a check of the system pressure on the lower ECAM DU and on the system accumulator gage (1072GM).

 (1) If the system pressure is more than 1450 psi:
 - use the rudder pedals to operate the rudder.
 (a) If the rudder operates:
 - do a check for continuity between the: PRESS SW-FLT CTL, G (1151GN) connector A/A and the connector A/C (with the hydraulic system pressurized) (Ref. ASM 29-32/01).
 1 If there is continuity:
_

 - replace the PRESS SW-FLT CTL, G (1151GN) (Ref. AMM TASK 29-32-12-000-001) and (Ref. AMM TASK 29-32-12-400-001).
 2 If there is no continuity:
_

 - do a check and repair the wiring between the: PRESS SW-FLT CTL, G (1151GN) connector A/C and FWC-1/ FWC-2 connector AA/06C (Ref. ASM 29-32/01) and (Ref. ASM 31-52/02).
 (b) If the rudder does not operate:
 - do a check for 28 VDC at the: SOL VALVE-LEAKAGE MEAS, G (1160GP) connector A/A and the connector A/B. (Ref. ASM 29-19/01).
 NOTE : There is normally 0 VDC.
____

 1 If there is 28 VDC:
_

 - do a check of the wiring between: the pushbutton switch (1882GP) connector C2 and the connector C3 (Ref. ASM 29-19/01).
 a If there is continuity:
_

 - replace the pushbutton switch 1882GP.
 b If there is no continuity:
_ - do a check and repair the wiring between the:

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 059-099, 102-149, 151-199, 201-299, ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 224
 301-399, 401-499, Aug 01/05 CES

R R  pushbutton switch (1882GP) connector C3 and the CB (1881GP) (Ref. ASM 29-19/01). 
R R R  (c) If the fault continues: - replace the MANIFOLD,HP (1111GM) (Ref. AMM TASK 29-11-14-000-001) and (Ref. AMM TASK 29-11-14-400-001). 
R R R  (2) If the pressure is less than 1450 psi: - do a check for external leakage and repair the components as necessary. 
R  **ON A/C ALL
 B. Do the fault confirmation procedure as given in Para. 3. to make sure that the operation is correct.
 5. Close-up________
 A. Aircraft Maintenance Configuration
 (1) De-pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-23-00-864-001).
 (2) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
 (3) Connect the isolation coupling of the PTU (Ref. AMM TASK 29-23-00-860-002).

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞29-11-00∞∞∞∞∞∞∞∞∞∞Page 225
 Nov 01/04 CES
　
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