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ADF - GROUND SCANNING and Trouble Shooting Data
Figure 011
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ADF - GROUND SCANNING and Trouble Shooting Data
Figure 011A
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ADF - CLASS 3 FAULTS and Ground Report
Figure 012
R 1EFF : 001-049, 051-051, 053-099, 101-149, 1 34-53-00Page 49 1151-199, 201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Allows to present the class 1, 2 or 3 internal failures detected on ground. These failures differ from those displayed on the LAST LEG REPORT and CLASS 3 FAULTS. By pressing the line key adjacent to the failure message, the operator is allowed to access to the corresponding Trouble Shooting Data.
-TEST (Ref. Fig. 013) Allows a check of the correct operation of the ADF on the ground. This test can be performed by:
-either selecting the test function on the face of the ADF receiver by pressing the TEST pushbutton switch
- or through the Centralized Fault Display System (CFDS) by selecting, on the MCDU, the test function on the ADF main menu page.
All the information displayed on the MCDU during the BITE TEST configuration can be printed by the printer (Ref. 31-35-00).
R **ON A/C ALL
C. Power-up Tests Initialization and Cockpit Repercussions
(1)
Conditions of power-up tests initialization
-How long the computer must be de-energized: 2 s.
-A/C configuration:
-whatever the A/C configuration on ground
(2)
Progress of power-up tests
(a)
Duration: 2 s.
(b)
Cockpit repercussions directly linked to power-up test accomplishment (some other repercussions may occur depending on the A/C configuration but these can be disregarded):
-
if ADF selected on FCU
-ND
ADF 1 or 2 in red
-
if ADF RMI option available
-ADF RMI display
ADF flag during 2 s.
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(3) Results of power-up tests (cockpit repercussions, if any, in case of tests pass/tests failed).
(a)
Tests pass:
-
if ADF selected on FCU
-ND
ADF 1 or 2 in green
-
if ADF RMI option available
-ADF RMI display
ADF flag no longer displayed
(b)
Tests failed:
-
if ADF selected on FCU
-ND
ADF 1 or 2 red indications flash
-
if ADF RMI option available
-ADF RMI display
ADF flag
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ADF - TEST Figure 013 (SHEET 1)
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ADF - TEST Figure 013 (SHEET 2)
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_____________________
TASK 34-53-00-740-003
BITE Test of the ADF
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1.
Reason for the Job
__________________
Self Explanatory
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 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV
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