4. Procedure
_________ Subtask 27-94-00-710-050
A. Operational Test of the SEC 3 NOTE : There must be a minimum of 30 seconds between the depressurization
____
of the hydraulic systems and the start of the test.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
NOTE : During steps 1 to 3, no pressurization is permitted.
____In the cockpit:
1. Open the circuit breaker 21CE3.
2. Wait for 10 seconds. 3. Close the circuit breaker 21CE3. NOTE: During the test, no pressurization is permitted.
R R R R R 4. Pressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001). 5. On the CAPT side: - move the side stick to the right until it touches the stop and keep the side stick in this position for 3 seconds.
-you can hear the single chime. On the upper ECAM DU:
-
the F/CTL SEC 3 FAULT indication
comes into view. On the FLT CTL panel 24VU:
-
the FAULT legend of the FLT CTL/SEC 3 pushbutton switch comes on.
On the FLT CTL panel 24VU:
-after 5 seconds, the FAULT legend ofthe FLT CTL/ SEC 3 pushbutton switch goes off.
On the upper ECAM DU:
-approximatively after 20 seconds, the F/CTL SEC 3 FAULT indication goes out of view.
On the lower ECAM DU, on the F/CTL page:
-the triangle for the right spoiler 2 comes into view.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R - release the side stick.
R
R - move the side stick to the left
R until it touches the stop and
R keep the side stick in this
R position for 3 seconds.
R - release the side stick.
R
R 6. On the F/O side:
R - move the side stick to the
R right until it touches the stop
R and keep the side stick in this
R position for 3 seconds.
R - release the side stick.
R
R - move the side stick to the left
R until it touches the stop and
R keep the side stick in this
R position for 3 seconds.
R - release the side stick.
R
R
5. Close-up________
Subtask 27-94-00-860-051
-
the triangle for the right spoiler 2 goes out of view.
-
the triangle for the left spoiler 2 comes into view.
-
the triangle for the left spoiler 2 goes out of view.
On the lower ECAM DU, on the F/CTL page:
-
the triangle for the right spoiler 2 comes into view.
-
the triangle for the right spoiler 2 goes out of view.
-
the triangle for the left spoiler 2 comes into view.
-
the triangle for the left spoiler 2 goes out of view.
A. Put the aircraft back to its initial configuration.
(1)
On the FLT CTL panel 23VU:
-push the FLT CTL/SEC 1 and FLT CTL/ELAC 1 pushbutton switches (on these pushbutton switches, the OFF legends go off).
(2)
On the FLT CTL panel 24VU:
-push the FLT CTL/SEC 2 and FLT CTL/ELAC 2 pushbutton switches (on these pushbutton switches, the OFF legends go off).
(3)
Depressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-
00-864-001) (Ref. TASK 29-24-00-864-001).
(4)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
COMPUTER - SPOILER ELEVATOR (SEC) (1CE1,1CE2,1CE3) - REMOVAL/INSTALLATION_________________________________________________________________________
TASK 27-94-34-000-001
Removal of the SEC (1CE1,1CE2,1CE3)
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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