R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-62-220-054
R. Measurement and Adjustment of the Flap Guide-Roller Assembly
(Ref. Fig. 408/TASK 27-54-62-991-017)
(1) Measure and if necessary, adjust the flap guide-roller assembly.
(a) Measure the dimension D: 1 If the dimension D is more than 3 mm (0.12 in.), replace the
_ flap guide-roller assembly with one of the correct size (Ref. TASK 27-54-63-400-001).
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Center Cruise Roller Alignment
Figure 408/TASK 27-54-62-991-017
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2_ If the dimension D is less than 3 mm (0.12 in.) or there is no
clearance, (and the flap guide roller assembly turns freely),
the clearance is correct.
S. Measure the Spoiler to Outboard Flap Clearance
(1)
Do a check of the clearance between the spoiler 2 trailing edge and the top surface of the outboard flap (Ref. TASK 27-64-00-820-001).
(2)
Do the procedure again for each of the spoilers 3, 4 and 5 (Ref. TASK 27-64-00-820-001).
Subtask 27-54-62-420-079
T. Installation of the Interconnecting Strut
(1)
Install the interconnecting strut (1) (Ref. TASK 27-51-44-400-001). Subtask 27-54-62-420-082
U.
Not applicable. Subtask 27-54-62-916-051
V. Application of Special Materials (Ref. Fig. 402/TASK 27-54-62-991-009, 403/TASK 27-54-62-991-010, 406/TASK 27-54-62-991-013)
(1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-the bolts (55), the washers (56), the nuts (57) and the cotter pins
(58)
-the nut (136), the cotter pin (137), the nut (139), the washer
(140) and the bolt (143)
-the nut (98).
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W. Flap Installation Procedure - Continued
(1)
Manually fully retract the flaps (Ref. TASK 27-50-00-866-012).
(2)
Connect the bonding straps.
(Ref. Fig. 402/TASK 27-54-62-991-009)
(a)
Attach the bonding straps (49) from the flap track carriages to the flap brackets with the washers (50) and the bolts (51) (Ref. TASK 20-28-00-912-004).
(b)
Attach the bonding strap (53) from the outboard flap to the inboard flap bracket with the nut (54) and the bolt (52) (Ref. TASK 20-28-00-912-004).
(3)
Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
(4)
Install the flap kink seals (Ref. TASK 27-54-61-400-006).
Subtask 27-54-62-865-052
X. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
Subtask 27-54-62-710-050
Y. Test
(1)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
(2)
Do an operational test of the spoiler system (Ref. TASK 27-64-00-710-001).
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5. Close-up
________ Subtask 27-54-62-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Lift the flap track No. 3 and No. 4 movable fairings (Ref. TASK 57-55-11-410-002).
(3)
Install the access panels:
(a) For the LH wing,
-
install 573CB (Ref. TASK 57-51-37-400-002)
-
install 575AB, 575BB (Ref. TASK 57-51-37-400-004).
(b) For the RH wing,
-install 673CB (Ref. TASK 57-51-37-400-002)
-install 675AB, 675BB (Ref. TASK 57-51-37-400-004). Subtask 27-54-62-942-050
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵6(66)
