R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 013A)
**ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 014)
R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 014A)
**ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 015)
R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 015A, 016)
1EFF : ALL 1 23-13-00Page 37 1 1 Aug 01/05 1 1 1CES 1
BITE - LAST LEG REPORT
Figure 013
R 1EFF : 001-049, 051-099, 101-105, 1 23-13-00Page 38 1 1 May 01/05 1 1 1CES 1
BITE - LAST LEG REPORT
Figure 013A
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 39 1401-499, 1Aug 01/05 1 1 1CES 1
BITE - PREVIOUS LEGS REPORT
Figure 014
R 1EFF : 001-049, 051-099, 101-105, 1 23-13-00Page 40 1 1 May 01/05 1 1 1CES 1
BITE - PREVIOUS LEGS REPORT
Figure 014A
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 41 1401-499, 1Aug 01/05 1 1 1CES 1
BITE - LRU IDENTIFICATION
Figure 015
R 1EFF : 001-049, 051-099, 101-105, 1 23-13-00Page 42 1 1 May 01/05 1 1 1CES 1
BITE - LRU IDENTIFICATION
Figure 015A
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 43 1401-499, 1Aug 01/05 1 1 1CES 1
BITE - GROUND SCANNING
Figure 016
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 44 1401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 017)
R **ON A/C 106-149, 218-299, 301-399, 401-499,
(Ref. Fig. 017A)
**ON A/C 151-199, 201-217,
(Ref. Fig. 017B)
R **ON A/C 062-099, 106-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 018)
R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 019, 020)
**ON A/C ALL
To gain access to the BITE, it is necessary to use one MCDU (Ref. 31-32). The MCDUs 3CA1 and 3CA2 are installed in the cockpit, on the center pedestal.
**ON A/C 001-049, 051-060, 101-101,
D. 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 the ground.
(2)
Progress of power of power-up tests
-Duration: 2 s.
-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):
1EFF : ALL 1 23-13-00Page 45 1 1 Aug 01/05 1 1 1CES 1
BITE - TEST Figure 017
R 1EFF : 1 1 1CES 001-049, 051-099, 101-105, 1 111 23-13-00 Page 46 May 01/05
BITE - TEST Figure 017A
R 1EFF : 1 1 1CES 106-149, 218-299, 301-399, 401-499, 1 111 23-13-00 Page 47 Aug 01/05
R BITE - TEST Figure 017B
R 1EFF : 1 1 1CES 151-199, 201-217, 1 111 23-13-00 Page 48 May 01/05
BITE - TROUBLE SHOOTING DATA
Figure 018
R 1EFF : 062-099, 106-149, 151-199, 201-299, 1 23-13-00Page 49 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
BITE - CLASS 3 FAULTS
Figure 019
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 50 1401-499, 1Aug 01/05 1 1 1CES 1
BITE - GROUND REPORT
Figure 020
R 1EFF : 106-149, 151-199, 201-299, 301-399, 1 23-13-00Page 51 1401-499, 1Aug 01/05 1 1 1CES 1 . none.
(3) Results of power-up tests (cockpit repercussions, if any, in case of tests pass/tests failed).
-
Tests pass:
. none.
-
Tests failed:
. none except RMP functions not available.
1EFF : 001-049, 051-060, 101-101, 1 23-13-00Page 52 1 1 May 01/05 1 1 1CES 1
RADIO MANAGEMENT - ADJUSTMENT/TEST
__________________________________ TASK 23-13-00-710-001 Operational Test of the Radio Management WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
NOTE : You can do this test in the hangar.
____
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