(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever (Ref. TASK 27-00-00-480-002).
(4)
Make sure that the access platform is in position:
-
for the left wing, below zone 580
-
for the right wing, below zone 680.
Subtask 27-51-44-865-074
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 501/TASK 27-51-44-991-005)
**ON A/C 301-399,
(Ref. Fig. 501A/TASK 27-51-44-991-005-A)
**ON A/C ALL
Subtask 27-51-44-820-053
A. Adjustment of the Interconnecting Strut
(1)
Install the PIN-SETTING (98D27504031000) in the inspection/rigging hole of the interconnecting strut (1).
(2)
If necessary, adjust the actuating rod of the interconnecting strut
(1)
so that you can install the PIN-SETTING as follows:
(a)
If necessary, remove and discard the lockwire from the locknut (1).
(b)
Loosen the locknut (1) sufficiently to let you turn the nut (2).
(c)
Adjust the nut (2) until you can install the PIN-SETTING. Make sure that you can see the threads of the rod-end (3) through the check hole. If you cannot see the threads of the rod-end (3) through the check hole, check the flap rigging (Ref. TASK 27-51-00-820-003).
Adjustment of the Interconnecting Strut
Figure 501/TASK 27-51-44-991-005
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 504 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Adjustment of the Interconnecting Strut
R Figure 501A/TASK 27-51-44-991-005-A
R 1EFF : 301-399, 1 27-51-44 Page 505
1 1 May 01/04
1 1
1CES 1
(d) Torque the locknut (1) to between 5.1 and 5.9 m.daN (37.61 and
43.51 lbf.ft).
(3) Remove the PIN-SETTING from the hole in the interconnecting strut (1).
Subtask 27-51-44-865-075
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-51-44-710-056
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: On the MCDU:
1.
Push (in) the line key < SFCC 1. - the MCDU shows the SFCC 1 page.
2.
Push (in) the line key SYSTEM - the MCDU shows the SFCC 1 SYSTEM
STATUS FLP >. STATUS 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
1EFF : ALL 1 27-51-44Page 506 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3.
Push (in) the line key <RETURN.
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
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