W DOC AIRBUS | AMM A320F

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)


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** ON A/C NOT FOR ALL
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)
 B. 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)
F FADEC Ground Test ** ON A/C NOT FOR ALL
F FADEC Ground Test ** ON A/C NOT FOR ALL
3. Job Set-up
Subtask 73-29-00-861-054-A ** ON A/C NOT FOR ALL
A. Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
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:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUENGINE/1 AND 2/IGN/SYS A1JHA03
FOR FIN: 1000EM1 (ENGINE1)
49VUENGINE/1/FADEC A/AND EIU 12KS1A04
121VUENGINE/IGN/ENG1/SYS B3JH1P41
121VUENGINE/IGN/ENG1/SYS A BAT2JH1P39
121VUENGINE/ENG1/FADEC B/AND EIU 14KS1R41
FOR FIN: 1000EM2 (ENGINE2)
49VUENGINE/2/FADEC A/AND EIU 22KS2A05
121VUENGINE/IGN/ENG2/SYS B3JH2P42
121VUENGINE/IGN/ENG2/SYS A BAT2JH2P40
121VUENGINE/ENG2/FADEC B4KS2Q40
Subtask 73-29-00-860-058-A ** ON A/C NOT FOR ALL
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
F FADEC Ground Test ** ON A/C NOT FOR ALL
F FADEC Ground Test ** ON A/C NOT FOR ALL
4. Procedure
Subtask 73-29-00-710-054-B ** ON A/C NOT FOR ALL
A. Do this test:
NOTE: 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.
F FADEC Ground Test ** ON A/C NOT FOR ALL
F FADEC Ground Test ** ON A/C NOT FOR ALL
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
  • The ENGINE 1(2) MAIN MENU page comes into view.
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.
  • The MCDU MENU page comes into view
5. Close-up
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
B. De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.01 02:57:13 UTC