3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-54-48-991-001)
Subtask 27-54-48-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever.
(3)
Make sure that the spoiler No. 1 is in the 'M' (Maintenance) position (Ref. TASK 27-60-00-866-002).
(4)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
(5)
Make sure that the warning sign is on panel 114VU, to tell persons not to operate the flap/slat controls.
(6)
Make sure that the access platform is in the applicable position.
R (7) Make sure that the access panels are removed (Ref. TASK 57-51-37-000-R 002) (Ref. TASK 57-51-37-000-004):
-
for the left wing, panels 573CB, 575AB
-
for the right wing, panels 673CB, 675AB.
Subtask 27-54-48-865-052
B. 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/WTB/FLP/SYS2 12CV P20 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
4. Procedure
_________
(Ref. Fig. 401/TASK 27-54-48-991-001)
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
NOTE : The gearbox is a unit filled with grease and is not a hermetically
____ sealed unit. It is normal for this grease to have some oil separation. The external surfaces of the gearbox may be moist with this separated oil as it is not a sealed unit. However, any separated oil in the unit that touches the grease will be changed back during operation. The oil separation will decrease during in-service operation until the lubricant is in a condition that is stable. This is normal and will not cause damage to the unit.
Subtask 27-54-48-210-050
A. Preparation for Installation
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1)
Clean the parts:
(a)
Remove all the used sealant from the bevel gearbox/structure interface with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(b)
Clean the splined connection with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Apply a layer of SEALANTS (Material No. 09-018) to:
-
the bevel gearbox/structure interface (but not on the area around the bonding points)
-
the shanks of the bolts (4) (but not the bonding bolt).
(4)
Do one of the steps that follow:
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
1EFF : ALL 1 27-54-48Page 409 1 1 Aug 01/02R 1 1 1CES 1
(a)
Apply a thin layer of COMMON GREASE (Material No. 04-022) to the splined connections.
- or
(b)
Apply a thin layer of COMMON GREASE (Material No. 04-018) to the splined connections.
Subtask 27-54-48-420-052
B. Installation of the Bevel Gearbox 6217CM(6267CM)
(1)
Put the bevel gearbox (2) in position on to the drive shaft (5) and the trailing edge rib.
(2)
Install the washers (3) and the bolts (4) in to the bevel gearbox (2).
(3)
Electrically bond the applicable bolt (4) (Ref. TASK 20-28-00-912-004).
(4)
TORQUE the bolts (4) to between 0.7 and 0.8 m.daN (61.94 and 70.79 lbf.in).
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱5(95)
