________________________________________________________________________
 TASK 22-61-00-710-001
 Operational Test of the Rudder Travel Limiting Function
 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.

 1. Reason for the Job
__________________
 To make sure that the rudder travel limiting system No1 (No2) operates correctly.
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
 Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV Page 31-60-00-860-001 EIS Start Procedure R 34-13-00-740-002 INTERFACE TEST of the ADR
 1EFF : ALL 1 22-61-00Page 501 1 1 May 01/99 1 1 1CES 1

 3. Job Set-up
__________

 Subtask 22-61-00-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 On the overhead panel, on the ADIRS CDU:

 -set the OFF/NAV/ATT selector switch related to IR3 to NAV
 -
make sure that the OFF and FAULT legends on the ADR3 pushbutton switch are off

 -
make sure that the OFF/NAV/ATT selector switches related to IR1 and IR2 are set to OFF.

 (3)
 On the center pedestal, on the SWITCHING panel 8VU:

 -set the AIR DATA selector switch to CAPT 3.

 (4)
 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

 -make sure that the FAC1 and the FAC2 pushbutton switches are pushed (in) (FAULT and OFF legends off).

 (5)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (6)
 On the center pedestal, on the ECAM control panel:

 -get the F/CTL page.

 (7)
 Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-10-00-863-003).

 (8)
 Make sure that the aircraft is in the clean configuration (on the FLAPS panel 114VU, the lever is in the 0 notch position).

 Subtask 22-61-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 49VU CAPT/LOUD/SPKR 5WW F10 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU EIS/F/O/LOUD/SPKR 4WW P08
 1EFF : ALL 1 22-61-00Page 502 1 1 Feb 01/98 1 1 1CES 1

 4. Procedure
_________

 Subtask 22-61-00-710-054
 A. Operational Test of the Rudder Travel Limiting Function
R NOTE : This test is for the system 1. For the system 2, use the
____ R indications between the parentheses.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal, on the  On the MCDU:
 MCDU:

 -Get the SYSTEM REPORT TEST/NAV
 page (Ref. TASK 31-32-00-860-010).

 -Push the line key adjacent to  The ADR3 page comes into view. the ADR3 indication.
 -Get acess to the INTERFACE TEST
 of the ADR3 (Ref. TASK 34-13-00-740-002)

 -Push the line key adjacent to  - On the Captain's PFD, the speed scale the START TEST indication. moves up and stops at 367.7 KTS.
 NOTE : Ignore the RETARD (and
____
 associated) warning. To
 stop it, release the
 ENG/FADEC GND PWR 1 and 2
 pushbutton switches on the
　
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