Operational Test of the FADEC on the Ground (with Engine non Motoring) [CFMI]
TASK 73-29-00-710-040-A-02
Operational Test of the FADEC on the Ground (with Engine non Motoring)
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 73-29-00-861-054-A ** ON A/C NOT FOR ALL Subtask 73-29-00-865-056-A ** ON A/C NOT FOR ALL
Subtask 73-29-00-710-054-B ** ON A/C NOT FOR ALL
Subtask 73-29-00-860-059-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:57:13 UTC
Operational Test of the FADEC on the Ground (with Engine non Motoring)
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | WARNING NOTICE(S) |
| 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) |
Subtask 73-29-00-861-054-A ** ON A/C NOT FOR ALL Subtask 73-29-00-865-056-A ** ON A/C NOT FOR ALL
B. Make sure that this(these) circuit breaker(s) is(are) closed:
Subtask 73-29-00-860-058-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | ENGINE/1 AND 2/IGN/SYS A | 1JH | A03 |
| FOR FIN: 1000EM1 (ENGINE1) | |||
| 49VU | ENGINE/1/FADEC A/AND EIU 1 | 2KS1 | A04 |
| 121VU | ENGINE/IGN/ENG1/SYS B | 3JH1 | P41 |
| 121VU | ENGINE/IGN/ENG1/SYS A BAT | 2JH1 | P39 |
| 121VU | ENGINE/ENG1/FADEC B/AND EIU 1 | 4KS1 | R41 |
| FOR FIN: 1000EM2 (ENGINE2) | |||
| 49VU | ENGINE/2/FADEC A/AND EIU 2 | 2KS2 | A05 |
| 121VU | ENGINE/IGN/ENG2/SYS B | 3JH2 | P42 |
| 121VU | ENGINE/IGN/ENG2/SYS A BAT | 2JH2 | P40 |
| 121VU | ENGINE/ENG2/FADEC B | 4KS2 | Q40 |
C. Aircraft Maintenance Configuration
(1) On the ENG section of the maintenance panel 50VU:
(a) Push the FADEC GND PWR 1(2) pushbutton switch.
(b) The ON legend of this pushbutton switch comes on.
(2) On the AIR COND panel 30VU:
(a) Make sure that the APU BLEED pushbutton switch is released (ON legend off).
(b) Install a WARNING NOTICE(S) to tell the persons not to use it.
(3) Put a WARNING NOTICE(S) on the HP ground connector to tell the persons not to pressurize the pneumatic system.
(4) On the overhead panel, on the ADIRS CDU, set the three OFF/NAV/ATT selector switches to NAV.
(5) On the left or right MCDU, get the SYSTEM REPORT/TEST ENG MENU PAGE
4. Procedure(1) On the ENG section of the maintenance panel 50VU:
(a) Push the FADEC GND PWR 1(2) pushbutton switch.
(b) The ON legend of this pushbutton switch comes on.
(2) On the AIR COND panel 30VU:
(a) Make sure that the APU BLEED pushbutton switch is released (ON legend off).
(b) Install a WARNING NOTICE(S) to tell the persons not to use it.
(3) Put a WARNING NOTICE(S) on the HP ground connector to tell the persons not to pressurize the pneumatic system.
(4) On the overhead panel, on the ADIRS CDU, set the three OFF/NAV/ATT selector switches to NAV.
(5) On the left or right MCDU, get the SYSTEM REPORT/TEST ENG MENU PAGE
Subtask 73-29-00-710-054-B ** ON A/C NOT FOR ALL
A. Do this test:
5. Close-upNOTE: This test is for the system 1. For the other system(s), use the indications between the parentheses.
| ACTION | RESULT |
|---|---|
| 1.Push the line key adjacent to the FADEC 1A(2A) indication. |
|
| 2.Push the line key adjacent to the FADEC TEST indication. |
|
| 3.Push the line key adjacent to the PUSH BUTTON TO START THE TEST indication. |
|
| 4.On the ENG panel 115VU, make sure that the ENG MODE CRK/NORM/IGN/START selector switch is set to NORM. | |
| 5.On the ENG panel 115VU set the ENG MASTER 1(2) control switch to ON. |
NOTE: You can see the TEST ACTIVE warning during all the time you do the test (approx. 1 min. 45 sec.) |
| 6.On the MCDU push the line key adjacent to the DISPLAY NON MOTORING TEST RESULTS. |
|
| 7.Push the line key adjacent to the RETURN pushbutton switch |
|
| 8.Set ENG MASTER 1(2) control switch to OFF. | |
| 9.Push the line key adjacent to the RETURN indication until the SYSTEM REPORT / TEST ENG MENU |
|
| 10.Do the procedure for channel B of the FADEC 1(2) | |
| 11.On the MCDU, push the line select key adjacent to the RETURN indication until the CFDS menu page comes into view. | |
| 12.Push the MCDU MENU mode key. |
|
Subtask 73-29-00-860-059-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Remove the WARNING NOTICE(S).
(2) On the ENG section of the maintenance panel 50VU:
(a) Release the FADEC GND PWR 1(2) pushbutton switch.
(b) The ON legend goes off.
Subtask 73-29-00-862-054-A ** ON A/C NOT FOR ALL (1) Remove the WARNING NOTICE(S).
(2) On the ENG section of the maintenance panel 50VU:
(a) Release the FADEC GND PWR 1(2) pushbutton switch.
(b) The ON legend goes off.
FADEC Ground Test