(b)
If necessary, remove and discard the lockwire from the locknut (10).
(c)
Loosen the locknut (10) sufficiently to let you turn the nut (12).
(d)
Adjust the nut (12) until you can install the PIN-SETTING. Make sure that you can see the threads of the rod-end (9) through the check hole. If you cannot see the threads of the rod-end (9) through the check hole, check the flap rigging (Ref. TASK 27-51-00-820-003).
(e)
Tighten the locknut (10).
(f)
Install the washer (13) and the nut (15).
(g)
Torque the nut (15) to between 1.1 and 1.7 m.daN (97.34 and
150.44 lbf.in).
NOTE : It is possible to have a clearance between the bush and
____
the strut attachment bracket.
(h)
Install a new cotter pin (14).
(i)
If you loosened the locknut (10), TORQUE it to between 5.1 and
5.9 m.daN (37.61 and 43.51 lbf.ft).
(j) Safety the locknut (10) with MISCELLANEOUS (Material No. 19-010).
(3)
Remove the PIN-SETTING from the inspection/setting hole in the interconnecting strut.
(4)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the head of the bolt (16)
-
the nut (15)
-
the washer (13)
-
the cotter pin (14).
(5)
Do an operational test of the flap interconnecting strut and the flap-attachment failure-detection sensors (Ref. TASK 27-51-00-710-002).
Subtask 27-51-44-865-077
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-51-44-710-059
C. Test
(1)
Get access to the flight controls (F/CTL) page of the MCDU (Ref. TASK 31-32-00-860-006)
(2)
Do this test of the flap interconnecting strut and the
flap-attachment failure-detection sensors:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
On the MCDU:
1. Push (in) the line key < SFCC 1.
1. Push (in) the line key SYSTEM STATUS FLP >.
On the MCDU:
-
the MCDU shows the SFCC 1 page.
-
the MCDU shows the SFCC 1 SYSTEMSTATUS FLAP page. These subsequent messages must not occur:
-
FLP 1 NO SFCC 2 DATA CHECK WIRING & SFCC 2
-
FLP 1 FAULTY FLP 2 DATA CHECK SFCC 1 OR 2
-NO LGCIU 1 DATA CHECK WIRING TO FLP 1
-FLP LH PROX SNSR 1 MISADJUSTMENT and FLP LH PROX SNSR 2 OR WIRING TO LGCIU 2
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
4.
Push (in) the line key <RETURN.
5.
Push (in) the line key < SFCC
2.
6. Push (in) the line key SYSTEM STATUS FLP >.
-
FLP LH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP LH PROX SNSR 2 OR WIRING TO LGCIU 2
-
FLP RH PROX SNSR 1 MISADJUSTMENT and FLP RH PROX SNSR 2 OR WIRING TO LGCIU 2
-
FLP RH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP RH PROX SNSR 2 OR WIRING TO LGCIU
2.
-FLP RH PROX SNSR 2 OR WIRING TO LGCIU
2.
-
the MCDU shows the SFCC 1 page.
-
the MCDU shows the SYSTEM REPORT/TESTPAGE.
-
the MCDU shows the SFCC 2 page.
-
the MCDU shows the SFCC 2 SYSTEMSTATUS FLAP page. These subsequent messages must not occur:
-
FLP 2 NO SFCC 1 DATA CHECK WIRING & SFCC 1
-
FLP 2 FAULTY FLP 1 DATA CHECK SFCC 1 OR 2
-NO LGCIU 2 DATA CHECK WIRING TO FLP 2
-
FLP LH PROX SNSR 2 MISADJUSTMENT and FLP LH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP LH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP LH PROX SNSR 2 OR WIRING TO LGCIU 2
-
FLP RH PROX SNSR 2 MISADJUSTMENT and FLP RH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP RH PROX SNSR 1 OR WIRING TO LGCIU 1
-
FLP RH PROX SNSR 2 OR WIRING TO LGCIU
2.
Subtask 27-51-44-860-067
D. Aircraft Maintenance Configuration
(1)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
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本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱4(122)
