680.
(2)
Remove the lower kink seals of the two wings (Ref. TASK 27-54-61-000-002).
Subtask 27-51-00-020-051
E. Disconnect the Interconnecting Strut
(1) Make a mark on the interconnecting strut (1) for normal position of R the actuating rod (holes in the eye-end and bracket are aligned).
(2)
Hold the flap interconnecting struts (1).
(3)
Remove and discard the cotter pins (2).
(4) Remove the nuts (3), the washer (4) and the bolts (5).
Subtask 27-51-00-865-058
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-51-00-865-061
G. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
4. Procedure
_________ Subtask 27-51-00-710-056
A. Operational Test of the Flap Interconnecting Strut and the
Flap-Attachment Failure-Detection Sensors
NOTE : Use one of the Multipurpose Control and Display Units (MCDU) for
____
the test.
(1) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. At the LH flaps: - push in the actuating rod of the flap interconnecting strut until it comes in contact with At the LH flap interconnecting strut:- the sensors give a 'target far'signal to the SFCC.
the stop.
R R R In the cockpit: - a single chime sounds
R - an amber MASTER CAUT light comes on.
R R R On the upper ECAM DU: - the F/CTL FLAPS LOCKED message comes on
- the ALIGNMENT FAULT message comes on.
R R R 2. On Panel 130VU (131VU): - push (in) the MASTER CAUT pushbutton switch (P/BSW). On Panel 130VU (131VU): - the amber MASTER CAUT light goes out.
3. On the MCDU: On the MCDU:
- push the line key < SFCC 1. - the SFCC 1 menu shows.
NOTE : Alternatively you can use the SFCC 2 menu but do not change SFCC
____
menu's during the test procedure.
4. Push the line key SYSTEM STATUS - SFCC 1 SYSTEM STATUS FLAP CHECK LH
FLP >. DRIVE INTEGRITY shows.
5. Push the line key < RETURN
frequently until the SYSTEM
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
REPORT/TEST - F/CTL menu is shown.
6. At the LH flaps: - move the actuating rod into the normal position.
7. Open the circuit breakers 6CV and 8CV.
8. Close the circuit breakers 6CV and 8CV.
R R R
9. Push the line key F/CTL >.
10. Push the line key < SFCC 1.
The SFCC 1 and SFCC 2 are de-energized.
The failure conditions are reset.
On the upper ECAM DU:
-
the F/CTL FLAPS LOCKED message goes out
-
the ALIGNMENT FAULT message goes out.
-
the SYSTEM REPORT/TEST - F/CTL menu shows.
-
the SFCC 1 menu shows.
NOTE : Alternatively you can use the SFCC 2 menu but do not change SFCC
____
menu's during the test procedure.
11. Push the line key SYSTEM STATUS FLP >.
12. Push the line key < RETURN frequently until the SYSTEM REPORT/TEST - F/CTL menu is shown.
13. At the LH flaps: - pull out the actuating rod of the flap interconnecting strut until it comes in contact with the stop.
R R R
R R R
-the MCDU shows SFCC 1 SYSTEM STATUSFLAP NO FAULTS.
At the LH flap interconnecting strut:
-the sensors give a 'target far'signal to the SFCC.
In the cockpit:
-a single chime sounds
-an amber MASTER CAUT light comes on.
On the upper ECAM DU:
-
the F/CTL FLAPS LOCKED message comes on
-
the ALIGNMENT FAULT message comes on.
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
R R R 14. On Panel 130VU (131VU): - push (in) the MASTER CAUT P/BSW. On Panel 130VU (131VU): - the amber MASTER CAUT light goes out.
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