- do the operational test of the LAND CAT III capability (Ref. AMM TASK 22-97-00-710-001)

 - do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).

 (1) If there is one or several CFDS messages related to the AFS: R - do the trouble shooting procedure related to the maintenance R message. R R For defective LRU(s), see the Fault Symptoms List..
 「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page A214
 Feb 01/05 CES

 (2) If there is no CFDS message: - do a check on the Post Flight Report for other CFDS messages related to:
 - Radio Altimeter System (via the FMGC), - ADIRS System, - Landing Gear Extension/Retractation System, - Slats/Flaps System.
R R R  (a) If there is one or several CFDS messages: - do the trouble shooting procedure related to the maintenance message. 
R  For defective LRU(s), see the Fault Symptoms List.. 
R R  (b) If there is no CFDS message, no trouble shooting is necessary except if the warning appears at the takeoff phase: - do the lubrification of the MLG (torque link and gland housing) (Ref. AMM TASK 12-22-32-640-001). If fault continues:
 - check the hydraulic level (A/C on jacks) and the pressurization of the MLG shock absorber (Ref. AMM TASK 12-14-32-614-003) and (Ref. AMM TASK 12-12-32-611-004).
 B. If the fault continues:
 - replace the FAC-1 (1CC1) or/and FAC-2 (1CC2) and (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
 (1) If the fault continues: - do a check and repair the wiring of the FAC OWN bus and the FAC HLTY MON (OWN & OPP) discretes between the FACs and the FWCs: (Ref. ASM 22-65/01) (Ref. ASM 22-69/01).
 C. Do the test gives in Para 3.

 Loss of Yaw Damper and Rudder Trim and Rudder Travel Limitation Functions on the FAC 1
 1. Possible Causes
_______________
 - FAC-1 (1CC1)

 - wiring

 - P/BSW - FLT CTL/FAC 1 (12CC1)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2)
 AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2)
 AMM 22-96-00-710-001 Operational Test of the AFS
 AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the

 External Power AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply
 AMM 29-23-00-863-001  Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
 AMM 29-24-00-863-001  Pressurize the Yellow Hydraulic System with the
 Electric Pump

 3. Fault Confirmation
__________________
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.

 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______ ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 A. Job Set-Up
 (1) Aircraft Maintenance Configuration
 (a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).

 (b) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-863-001), (Ref. AMM TASK 29-24-00-863-001) and (Ref. AMM TASK 29-10-00-863-003).

 「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page A216
 May 01/04R CES

 B. Make sure that this(these) circuit breaker(s) is(are) closed:

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04
 C. Test
 (1) Open the circuit breaker 5CC1 for more than 5 seconds.

 (2) After 10 seconds, close the circuit breaker 5CC1.

 (3) After 2 minutes, do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FAC 1.

 4. Fault Isolation
　
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