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ECES E a "Y" must be displayed if the thrust reverser shut-off valve
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is installed.
b "N" must be displayed if the thrust reverser shut-off valve
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is not installed.
c Change the installation status through the MCDU menu if
_ required according to instructions of the procedure (Ref. TASK 73-21-60-740-006).
(e) If you operate the aircraft in actual CAT III conditions, do these tests:
- Make sure that there is no CAT 3 DUAL INOP message on the lower ECAM DU with FADEC GND PWR 1 & 2 pushbutton switches (maintenance panel 50VU) pushed (ON legends on) and 3 IR'S aligned (Ref. TASK 34-10-00-860-004)
- Do the operational test of the LAND CAT III Capability (Ref. TASK 22-97-00-710-001).
Subtask 71-00-00-710-129
T. Do an operational test:
(1) Do an operational test of the FADEC with engine motoring (Ref. TASK 73-29-00-710-040)
(a) Do an operational test of the hydraulic pump during the FADEC test: FOR 1000EM1 (Ref. TASK 29-11-00-710-001) FOR 1000EM2 (Ref. TASK 29-13-00-710-002)
(2) Do a check for leaks on the hydraulic and fuel lines.
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
Subtask 71-00-00-710-133
U. Do an operational test:
(1) Do an operational test of the thrust reverser system (Ref. TASK 78-31-00-710-042).
NOTE : As an alternative procedure you can do this operational test
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without the CFDS.
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(2) Start the engine 1(2) (Ref. TASK 71-00-00-710-003).
(3) Do an operational test of the ice protection of the engine air intake (Ref. TASK 30-21-00-710-002).
(4) Do a minimum idle check and a check for leaks (Ref. TASK 71-00-00-710-006).
(5) Do a check of the IDG system as follows:
(a) On the lower ECAM DU select the ELEC page.
(b) Make sure that the frequency and voltage indications are correct with engine running.
(6) Do a leak check of the fuel return valve (Ref. TASK 73-11-50-360-002) to make sure that there are no leaks at pylon connection.
(7) Stop the engine (Ref. TASK 71-00-00-710-028). R **ON A/C 106-149, 229-299, 303-399, 401-499,
Subtask 71-00-00-710-133-A
U. Do an operational test:
(1) Do an operational test of the thrust reverser system (Ref. TASK 78-31-00-710-042).
NOTE : As an alternative procedure you can do this operational test
____
without the CFDS.
(2) Start the engine 1(2) (Ref. TASK 71-00-00-710-003).
(3) Do an operational test of the ice protection of the engine air intake (Ref. TASK 30-21-00-710-002).
(4) Do a minimum idle check and a check for leaks (Ref. TASK 71-00-00-710-006).
(5) Make sure that the IDG is connected:
(a) If the IDG is not connected, make sure that the maintenance message "IDG1(2) (E1(2)-4000XU) RECONFIG" is shown on the EPGS GROUND REPORT page.
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E 56-5B E E E R 1_ Make sure that the related GCU is energized.
R 2_ Reset the GCU:
R - On the ELEC control panel 35VU, release (OFF) then push the
R related ELEC/GEN pushbutton switch 3XU.
R 3_ On the ELEC page of the lower ECAM DU, make sure that the line
R connection between the IDG1(2) and the related busbar is shown
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