-
FLP LH PROX SNSR 1 MISADJUSTMENT and FLP LH PROX SNSR 2 OR WIRING TO LGCIU 2
-
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.
-
the MCDU shows the SFCC 1 page.
-
the MCDU shows the SYSTEM REPORT/TEST PAGE.
-
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
1EFF : ALL 1 27-51-44Page 419 1 1 May 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-FLP RH PROX SNSR 2 OR WIRING TO LGCIU 2.
Subtask 27-51-44-865-062
F. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-44-420-051
G. Installation of the Interconnecting Strut
(1)
Make sure that the bolt (15), the washer (14) and the nut (13) are installed. Tighten the nut (13).
(2)
TORQUE the nut (13) 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 flange of the
____ bush and the strut attachment bracket. This is satisfactory.
(3)
Install the new cotter-pin (12).
(4)
If you loosened the locknut (17), TORQUE it to between 5.1 and 5.9 m.daN (37.61 and 43.51 lbf.ft).
(5)
Safety the locknut (17) with MISCELLANEOUS (Material No. 19-010).
(6)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolt (2), the nut (6), the washer (5) and the cotter pin (7)
-
the bolt (15), the nut (13), the washer (14) and the cotter pin (12).
R **ON A/C 301-399,
R Subtask 27-51-44-420-051-A
R G. Installation of the Interconnecting Strut
R (1) Make sure that the bolt (19), the washer (18) and the nut (16) are
R installed. Tighten the nut (16).
R (2) TORQUE the nut (16) to between 1.1 and 1.7 m.daN (97.34 and 150.44
R lbf.in).
R NOTE : It is possible to have a clearance between the flange of the____
R bush and the strut attachment bracket. This is satisfactory.
R (3) Install the new cotter-pin (17).
R (4) If you loosened the locknut (21), TORQUE it to between 5.1 and 5.9
R m.daN (37.61 and 43.51 lbf.ft).
R (5) Safety the locknut (21) with MISCELLANEOUS (Material No. 19-010).
R (6) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
R - the bolt (11), the nut (3),the washer (4) and the cotter pin (2)
R - the bolt (19), the nut (16), the washer (18) and the cotter pin
R (17)
R - the bolts (5), the washers (6) and the nuts (10).
R **ON A/C ALL
Subtask 27-51-44-865-052
H. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
6CV, 8CV.
Subtask 27-51-44-710-050-A
J. Test
(1) Remove the LOCKING TOOL - FLAP/SLAT CONTROL LEVER from the flap/slat
control lever on panel 114VU.
(2) Do an operational test of the flap system (Ref. TASK 27-54-00-710-
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱4(110)
