R **ON A/C 106-149, 301-399, 401-499,
C. Test Running (Ref. Fig. 001A, 002A) If a failure occurs prior to the acceptation phase, the test is refused as mentioned above. If a failure occurs after the acceptation phase, the FMGCs remain in LAND TEST condition since the aircraft is on ground with engines shut down. From AFS/LAND TEST-4 page, the operator must answer questions by YES or NO via the MCDU. NOTE: Please answer by YES if agree with sentence, NO if disagree. If the answer is YES, the test continues until the last page is displayed (AFS/LAND TEST-9) with XXX LAND TEST OK final message. If the answer is NO :
-an analysis is made at the level of the AFS BITEs in order to detect and isolate the failure, and
-a failure message is displayed on the AFS/LAND TEST REPORT page requesting to check the system concerned by the analysis. NOTE: Each AFS/LAND TEST page displays an END OF TEST indication. Pressing the line key adjacent to this indication results in the transmission of an END OF TEST FIDS command to the four FG BITEs.
1EFF : ALL 1 22-97-00Page 2 1 1 Aug 01/05 1 1 1CES 1R Land Test (Accepted) R Figure 001
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 22-97-00Page 3/4 1201-299, 1May 01/05 1 1 1CES
INTENTIONALLY BLANK
R 1 1
22-97-00Page 5
1 1 May 01/04 1 1 1CES 1
Land Test (Accepted)
Figure 001A (SHEET 1)
Land Test (Accepted)
Figure 001A (SHEET 2)
Land Test (Accepted)
Figure 001A (SHEET 3)
Land Test (Accepted)
Figure 001A (SHEET 4)
Land Test (Refused)
Figure 002
Land Test (Refused) Figure 002A
R 1EFF : 1 1 1CES 106-149, 301-399, 401-499, 1 111 22-97-00 Page 11 Aug 01/05
Reception of this command causes loss of the LAND TEST ACCEPTATION
condition for each BITE.
The LAND TEST introduces the capability to test MLS and GLS (provision) landing systems in addition to ILS system (AFS/LAND TEST-0 page).
NOTE : AFS/LAND TEST-0 page will be displayed only if another landing
____ system than ILS is installed.
In addition, a test Close-Up page is added in order to replace the A/C systems in their initial states.
LAND CAT III CAPABILITY TEST - ADJUSTMENT/TEST
______________________________________________
TASK 22-97-00-710-001
Operational Test of the LAND CAT III Capability
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 APPR mode operates correctly and to put the aircraft
back to CAT III capability.
R NOTE : The purpose of the Land CAT III test is to check the aircraft
____ R capability to perform a CAT III DUAL automatic landing.
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 with a Ground
Power Supply 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 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
Menu Page
31-60-00-860-001 EIS Start Procedure
31-60-00-860-002 EIS Stop Procedure
34-10-00-860-004 IR Alignment Procedure
34-10-00-860-005 ADIRS Stop Procedure
1EFF : ALL 1 22-97-00Page 501 1 1 Feb 01/04 1 1 1CES 1
3. Job Set-up
__________
Subtask 22-97-00-860-051
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure
(Ref. TASK 31-60-00-860-001).
(3)
Align the three ADIRS
(Ref. TASK 34-10-00-860-004).
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