Subtask 27-96-00-010-053
B. Get Access
(1)
Put the access platform in position at the access door 822.
(2)
Open the access door 822.
(3)
On the battery power center 105VU:
-loosen the two screws and remove the protective cover.
Subtask 27-96-00-865-086
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU COM/AUDIO/FLT/INTPH 9RN G08 49VU COM/AUDIO/ACP/CAPT 4RN G06 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU EIS/F/O/LOUD/SPKR 4WW P08 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 27-96-00-860-054
D. Aircraft Maintenance Configuration
(1)
Do the reset of the EFCS computers.
(a) On the panel 23VU:
-release the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches, the OFF legend comes on).
(b) On the panel 24VU:
-release the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches, the OFF legend comes on).
(2)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(3)
On the center pedestal, on the ECAM control panel, push the F/CTL pushbutton switch (on the lower ECAM display unit, the F/CTL page comes into view).
(4)
Pressurize the aircraft hydraulic systems (Ref. TASK 29-24-00-863-001), (Ref. TASK 29-23-00-863-001), (Ref. TASK 29-10-00-863-003).
(5)
On the panel 23VU:
-push the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches the OFF and FAULT legends go off).
(6)
On the panel 24VU:
-push the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches the OFF and FAULT legends go off).
NOTE : You can release one or several EFCS computers (ELAC 1, ELAC 2,
____ SEC 1, SEC 2, SEC 3) before the start of this test procedure (this configuration is shown in the applicable trouble-shooting procedure).
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4. Procedure
_________ Subtask 27-96-00-710-076
A. Operational Test of the EFCS
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the CAPT (F/O) lateral console: On the F/CTL page, on the lower ECAM
Give the orders below one after the display unit:
other and keep the side stick in - the symbols for the elevators and/or
each position during 3 seconds: the ailerons and/or the spoilers move
- full nose up according to the system configuration
- release the handle computer engaged, in relation to the
- full nose down side stick orders.
- release the handle
- full right turn
- release the handle
- full left turn
- release the handle.
5. Close-up________
Subtask 27-96-00-860-055
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-24-00-864-001), (Ref. TASK 29-23-00-864-001), (Ref. TASK 29-10-00-864-003).
(2)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(3)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002)
Subtask 27-96-00-410-054 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱9(158)
