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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
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YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
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CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
1. Reason for the Job
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To make sure that the rudder travel limiting system No1 (No2) operates correctly.
2. Job Set-up Information
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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
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3. Job Set-up
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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
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4. Procedure
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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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