Entry of the Thrust Reverser Hydraulic Shut-off Valve Status through the MCDU [CFMI]

TASK 73-21-60-740-025-A
Entry of the Thrust Reverser Hydraulic Shut-off Valve Status through the MCDU

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 31-32-00-860-012-A	Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page
Shut-off Valve Status Entry - MCDU Screens ** ON A/C NOT FOR ALL
Shut-off Valve Status Entry - MCDU Screens ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 73-21-60-861-061-A ** ON A/C NOT FOR ALL

A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).

Subtask 73-21-60-869-064-A ** ON A/C NOT FOR ALL

B. Preparation for test
(1) On the overhead maintenance panel 50VU, push then release the ENG/FADEC GND PWR/1(2) pushbutton switch. The ON legend comes on.
(2) On the left or right MCDU get the SYSTEM REPORT/TEST ENG page (Ref. AMM TASK 31-32-00-860-012).

4. Procedure
Subtask 73-21-60-740-057-B ** ON A/C NOT FOR ALL

A. Enter the T/R hydraulic isolation valve status.
(1) Do this procedure for the ECU 1(2) channel A.

NOTE: This test is for the system 1. For the other system(s), use the indications between the parentheses.

ACTION	RESULT
1.On the MCDU:
Push the line key adjacent to the FADEC 1A (2A) indication.	The ENGINE 1(2) MAIN MENU page comes into view.
2.Push the line key adjacent to the LRU IDENT REPORT indication.	The LRU IDENTIFICATION page comes into view. If there is a NVM failure, the NVM FAULT: DATA NOT RETRIEVABLE indication comes into view.
3.If necessary change the thrust reverser isolation valve status as follows:
A.Push the line key adjacent to the CONFIGURATION CHANGE indication.	The T/R SOV status comes into view.
B.Push the line key adjacent to the T/R SOV STATUS CHANGE indication.	The T/R SOV INSTALLED ENTRY menu comes into view.
C.On the MCDU keyboard enter "Y" corresponding to the T/R SOV status (Y: T/R SOV installed)
D.Push the line key adjacent to the new status

(2) Do this procedure for the ECU 1(2) channel B.
(3) On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view.
(4) Stop the MCDU.

5. Close-up
Subtask 73-21-60-860-062-A ** ON A/C NOT FOR ALL

A. On the overhead maintenance panel 50VU:

Push the ENG/FADEC GND PWR 1(2) pushbutton switch. The ON legend goes off.

Subtask 73-21-60-862-061-A ** ON A/C NOT FOR ALL

B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).

[Rev.10 from 2021] 2026.04.01 02:56:52 UTC