3. Push the line key adjacent to the START TEST indication.

4. Push the line key adjacent to the CONFIRM START OF TEST indication.

 NOTE : As soon this key is
____ pushed, you must move the throttle control lever in the 35 subsequent seconds.
 5. Put the throttle control lever in the MAX REVERSE position.
- The ECU 1(2) CHAN A page comes into
view.

- The THRUST REVERSER TEST ENGINE 1(2)
CHANNEL A menu comes into view.

- The CONFIRM START OF TEST indication
comes into view.

- The thrust reversers of the engine 1

(2) operate.
 On the upper display unit of the ECAM
 system:

 - The REV indication in the N1 indicator of the engine 1 (2) must be amber when the thrust reversers operate.

 - It must become green when the thrust reversers are deployed and locked.

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6. When the SET THROTTLE LEVER OF  - The thrust reversers of the engine 1
 OWN ENGINE TO FWD IDLE indication  (2) stow.
 shows, put the throttle control  On the upper display unit of the ECAM
 lever in the IDLE position (zero  system:
 on the scale).  - The REV indication must be amber when
 the thrust reversers operate.
 - It must go out of view when the
 thrust reversers are stowed and
 locked.
 On the MCDU:
 - TEST OK indication comes into view.
 7. Push the line key adjacent to the
 START RESTOW TEST indication and
 do the test again from step 4. to
 step 6.
 8. Push the line key adjacent to the
 RETURN indication until the
 SYSTEM REPORT/TEST ENG comes in
 view.
 9. Do the procedure again for the
 channel B of the FADEC 1(2).
 10. On the MCDU, push the line key
 adjacent to the RETURN
 indication until the CFDS menu
 page comes into view.
 11. Stop the MCDU.
 **ON A/C ALL
 5. Close-up________
 Subtask 78-31-00-864-050
 A. Depressurize Hydraulic System:
 FOR 1000EM1

 Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-864-001).
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 E E FOR 1000EM2 Depressurize the auxiliary Yellow hydraulic system (Ref. TASK 29-24-00-864-001).

 Subtask 78-31-00-860-052
 B. Put the aircraft back to its initial configuration.
 (1) On the overhead maintenance panel 50VU:
 (a) push the FADEC GND PWR 1 (2) pushbutton switch. On the pushbutton switch, the ON legend goes off.

 (b) push the HYD/LEAK MESUREMENT VALVES/B/G/Y pushbutton switch . On the pushbutton switch the OFF legend goes off

 (2) Do the EIS stop procedure: (Ref. TASK 31-60-00-860-002) Subtask 78-31-00-862-050
 C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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 1. Reason for the Job

__________________
 Self Explanatory

 2. Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific low frequency generator No specific soft nose pliers
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied from the External Power
　
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