R (3) Make sure that a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. TASK 27-50-00-400-003): - on the torque shaft, inboard of of the applicable component - on the torque shaft, outboard of the applicable component.
(4) Make sure that the adjustable access platform is in position below the applicable access panel.
(5) Make sure that the applicable access panels have been removed:
- FOR 6014CM
R panels 521CB, 521EB
- FOR 6028CM
R panels 522AB, 522CB
- FOR 6036CM
R panels 522LB, 522NB
- FOR 6038CM
R panels 522NB, 522QB
- FOR 6040CM
R panels 522QB, 522SB
- FOR 6042CM
R panel 522SB
- FOR 6044CM
R panels 522UB
- FOR 6064CM
R panels 621CB, 621EB
- FOR 6078CM
R panels 622AB, 622CB
- FOR 6086CM
R panels 622LB, 622NB
- FOR 6088CM
R panels 622NB, 622QB
- FOR 6090CM
R panels 622QB, 622SB
- FOR 6092CM
R panel 622SB
- FOR 6094CM
R panel 622UB.
Subtask 27-84-45-865-072
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure_________
R (Ref. Fig. 402/TASK 27-84-45-991-002)
R
Subtask 27-84-45-420-074
R A. Preparation for Installation
R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______
R GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1) Clean the component interfaces and/or the adjacent areas with a
R MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS
R (Material No. 11-026).
(2) Do an inspection of the component interface and/or the adjacent area.
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
R (4) Do one of the steps that follow:
R CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT._______
R GREASE AND ASSEMBLY PASTE DO NOT MIX.
R (a) Apply a thin layer of COMMON GREASE (Material No. 04-022) to the
R torque shaft splines.
R
R - or
R (b) Apply a thin layer of COMMON GREASE (Material No. 04-018) to the
R torque shaft splines.
R
Subtask 27-84-45-420-075
B. Installation of the Torque Shafts
R (1) Put the retaining ring (6) in position over the shaft (3).
(2) Install the universal joint (5) and attach it with the pin (7) and
the retaining ring (6).
(3) Install the universal joint (1).
(4) Install the shaft (3) and attach it with the bolts (4) and the nuts (2).
(5) TORQUE the nuts (2) to between 1.02 and 1.24 m.daN (90.26 and 109.73 lbf.in).
(6) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to: - the nuts (2) - the bolts (4) - the flanges of the universal joints (1) and (5) - the flanges of the shaft (3).
R (7) Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (Ref. TASK 27-50-00-400-003): - from torque shaft, inboard of the applicable component - from the torque shaft, outboard of the applicable component.
Subtask 27-84-45-210-064
R C. Dimensional/Visual Checks (Ref. Fig. 402/TASK 27-84-45-991-002)
R R R R R R (1) Make sure that: - you cannot see the spline engagement groove at the movable joint - the dimension A is a minimum of 6.5 mm (0.2559 in.) at the movable joint.
Subtask 27-84-45-865-073
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 27-84-45-710-054
E. Test
CAUTION : MAKE SURE THE POWER TRANSMISSION SYSTEM IS COMPLETE BEFORE YOU_______ DO A PREPARATION FOR TEST OR A TEST.
R R (1) Do an operational test of the slat power-transmission system (Ref. TASK 27-84-00-710-001). Make sure that the rotation of the torque shafts does not cause damage.
5. Close-up
________
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7(141)
