Subtask 27-54-62-820-076
J. Check and Adjustment of the Outboard Flap Rigged Position
NOTE : Before you do the rigging procedure, make sure that:
____
-
the aircraft weight is on the landing gear or on jacks
-
the No 1 and the No 2 engines are installed or not installed
-
the fuel load is symmetrical or the wing tanks are empty
-
the flaps are fully retracted (Ref. TASK 27-50-00-866-012).
(1)
Install the sharks fin flap rigging tools and do a check of the outboard flap rigged position (Ref. TASK 27-51-00-820-003).
(2)
If the flap rigged position is not correct, adjust as necessary until the flap is in the specified limits (Ref. TASK 27-51-00-820-008), (Ref. TASK 27-54-62-000-001) and (Ref. TASK 27-54-62-400-001).
**ON A/C 051-052,
Subtask 27-54-62-820-076-A
J. Check and Adjustment of the Outboard Flap Rigged Position
NOTE : Before you do the rigging procedure, make sure that:
____
-
the aircraft weight is on the landing gear or on jacks
-
the No 1 and the No 2 engines are installed or not installed
-
the fuel load is symmetrical or the wing tanks are empty
-
the flaps are fully retracted (Ref. TASK 27-50-00-866-012).
(1)
Install the sharks fin flap rigging tools and do a check of the outboard flap rigged position (Ref. TASK 27-51-00-820-003).
(2)
If the flap rigged position is not correct, adjust as necessary until the flap is in the specified limits (Ref. TASK 27-51-00-820-008), (Ref. TASK 27-54-62-000-001) and (Ref. TASK 27-54-62-400-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-62Page 424 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-001,
Subtask 27-54-62-420-098
K. Complete the Connection of the Flap Drive Arms to the Rotary Actuator Drive-Levers
(1)
Remove the SLAVE PIN and install the bolts (55).
(2)
Install the washers (56) and the nuts (57).
(3)
TORQUE the nuts (57) to between 7.6 and 8.5 m.daN (56.04 and 62.68 lbf.ft).
(4) Safety the nuts (57) with the new cotter pins (58). R **ON A/C 002-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-62-420-098-A
K. Complete the Connection of the Flap Drive Arms to the Rotary Actuator Drive-Levers
(1) TORQUE the nuts (57) to between 7.6 and 8.5 m.daN (56.04 and 62.68 lbf.ft).
(2) Safety the nuts (57) with the new cotter pins (58). R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-62-420-084
L. Safety the Flap to the Flap Carriage Connections
(Ref. Fig. 403/TASK 27-54-62-991-010)
(1)
Make sure that the failsafe hook nuts (144) are hand tight only.
(2)
Remove the nuts (136).
(3)
Make sure that the spherical bearings, the splined bushes (142) and the locking plates (141) are engaged correctly.
(4)
Install the new crushable spacers (138) and the nuts (136).
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(5)
TORQUE the nuts (136) to between 15 and 20 m.daN (110.61 and 147.49 lbf.ft).
(6)
Safety the nuts (136) with the new cotter pins (137).
(7) Install the washers (140) and the nuts (139). Subtask 27-54-62-420-081
M. Safety the Forward Eccentrics
(Ref. Fig. 407/TASK 27-54-62-991-003-A)
(1)
If the forward eccentrics have been adjusted, do the steps that follow:
(a)
Install the serrated plate (152) on the eccentric bolt (156) at track 3.
(b)
Install the bolt (151), the washer (153) and the nut (154).
(c)
Tighten the nut (154) and safety with a new cotter pin (155).
(d)
Install the serrated plate (159) on the eccentric bolt (160) at track 4.
(e)
Install the bolt (157) and the washer (158).
(2)
Make sure that the outboard flap trailing edge is still in the correct rigged position (Ref. TASK 27-51-00-820-003).
Subtask 27-54-62-916-054
N. Application of Special Materials
(Ref. Fig. 407/TASK 27-54-62-991-003-A)
(1) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: 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(64)
