(2)
On the center pedestal, on the MCDU related to the replacement FMGC:
-adjust the brightness of the MCDU screen,
-
push the DATA mode key to obtain the DATA INDEX page,
-
push the line key adjacent to the A/C STATUS indication,
-make sure that the IDLE/PERF value are the same as the value you wrote during the removal. If not:
-enter ARM into brackets in the CHG CODE line (5L),
-write the IDLE/PERF value in the scratchpad,
-enter this value in line (6L),
-set the brightness to off.
**ON A/C 001-049, 101-105,
Subtask 22-83-34-710-051
D. Do these tests:
(1) Operational Test of the AFS (Ref. TASK 22-96-00-710-001).
NOTE : As an alternative, you can do this operational test without
____
the CFDS (Ref. TASK 22-10-00-710-002).
(2) Operational Test of the MCDU (Ref. TASK 22-70-00-710-001). On the A/C STATUS page:
-do a check of the active data base of the installed FMGC for correct dates and serial numbers shown (it is necessary to open the circuit breaker of the opposite FMGC). If not, do the loading of the correct data base (Ref. TASK 22-70-00-610-008).
NOTE : If the aircraft is operated in CAT 3 conditions, you must also
____ do this test: Land CAT 3 Capability Test (Ref. TASK 22-97-00-710-001).
**ON A/C 051-061,
Subtask 22-83-34-710-051-D
D. Do these tests:
(1) Operational Test of the AFS (Ref. TASK 22-96-00-710-001).
NOTE : As an alternative, you can do this operational test without____ the CFDS (Ref. TASK 22-10-00-710-002).
R R (2) Operational Test of the MCDU (Ref. TASK 22-70-00-710-001). On the A/C STATUS page: - do a check of the active data base of the installed FMGC for correct dates and serial numbers shown (it is necessary to open the circuit breaker of the opposite FMGC). If not, do the loading of the correct data base (Ref. TASK 22-70-00-610-008), or do the crossloading (Ref. TASK 22-70-00-610-009).
NOTE : If the aircraft is operated in CAT 3 conditions, you must also____ do this test: Land CAT 3 Capability Test (Ref. TASK 22-97-00-710-001).
**ON A/C 062-099,
Subtask 22-83-34-710-051-E
D. Do these tests:
(1) Operational Test of the AFS (Ref. TASK 22-96-00-710-001).
NOTE : As an alternative, you can do this operational test without____ the CFDS (Ref. TASK 22-10-00-710-002).
R R (2) Operational Test of the MCDU (Ref. TASK 22-70-00-710-001). On the A/C STATUS page: - do a check of the active data base of the installed FMGC for correct dates and serial numbers shown (it is necessary to open the circuit breaker of the opposite FMGC). If not, do the loading of the correct data base (Ref. TASK 22-70-00-610-008), or do the crossloading (Ref. TASK 22-70-00-610-009).
NOTE : If the aircraft is operated in CAT 3 conditions, you must also____ do this test: Land CAT 3 Capability Test (Ref. TASK 22-97-00-710-001).
1EFF : 051-099, 1 22-83-34Page 410 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499,
Subtask 22-83-34-710-051-B
D. Do these tests:
(1) Operational Test of the AFS (Ref. TASK 22-96-00-710-001).
NOTE : As an alternative, you can do this operational test without
____ the CFDS (Ref. TASK 22-10-00-710-002).
(2) Operational Test of the MCDU (Ref. TASK 22-70-00-710-001). On the A/C STATUS page:
-do a check of the active data base of the installed FMGC for correct dates and serial numbers shown (it is necessary to open the circuit breaker of the opposite FMGC).
R If not, do the loading of the correct data base (Ref. TASK 22-70-R 00-610-008), or do the crossloading (Ref. TASK 22-70-00-610-009).
NOTE : If the aircraft is operated in CAT 3 conditions, you must also
____ do this test: Land CAT 3 Capability Test (Ref. TASK 22-97-00-710-001).
**ON A/C ALL
Subtask 22-83-34-710-052
E. Additional check (CFDS available)
(1) Do the procedure to get the SYSTEM REPORT/TEST page (Ref. TASK 31-32-00-860-001).
NOTE : The actions and results of this procedure occur the MCDU you
____
use.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
Push the line key adjacent to the - The AFS MAIN MENU page comes into AFS indication. view.
2.
Push the line key adjacent to the - The AFS/LRU IDENTIFICATION page comes LRU IDENT indication. into view.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM AUTO FLIGHT 自动飞行4(95)
