6215CM(6265CM)/6219CM(6269CM)/6223CM (6273CM)/6225CM(6275CM)/6229CM(6279CM)/6231CM(6281CM) 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance
**ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-45-991-001 Fig. 401
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
27-54-45-991-001-A Fig. 401A
**ON A/C ALL
27-54-45-991-004 Fig. 405
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 401/TASK 27-54-45-991-001)
R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-54-45-991-001-A) **ON A/C ALL
Subtask 27-54-45-941-087
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flap/slat controls.
Subtask 27-54-45-860-073
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(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 on panel 114VU.
(3)
Make sure that the access platform is in the applicable position.
(4)
Make sure that the applicable access panels are removed:
-
for 6224CM, panel 575CB
-
for 6274CM, panel 675CB
-
for 6230CM, panel 575EB
-
for 6280CM, panel 675EB.
(5)
Make sure that the applicable spoiler is in the 'M' (Maintenance) position (Ref. TASK 27-60-00-866-002).
(6)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
(7)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the removed component.
1EFF : ALL 1 27-54-45Page A438 1 1 Aug 01/02R 1 1 1CES 1
Subtask 27-54-45-865-091
C. 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/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure
_________ (Ref. Fig. 405/TASK 27-54-45-991-004) 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.
Subtask 27-54-45-420-073
A. Preparation for Installation
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(1)
Clean the component interface and/or the adjacent area with a 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)
Do one of the steps that follow:
CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.
_______
GREASE AND ASSEMBLY PASTE DO NOT MIX.
(a)
Apply a thin layer of COMMON GREASE (Material No. 04-022) to the torque shaft splines.
- or
(b)
Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.
1EFF : ALL 1 27-54-45Page A439 1 1 Aug 01/02R 1 1 1CES 1
Subtask 27-54-45-420-060
B. Installation of the Torque Shafts 6224CM(6274CM)/6230CM(6280CM)
(1)
Install the torque shaft (83).
(2)
Install the applicable steady bearing (82) (Ref. TASK 27-54-44-400-002):
-
FOR 6224CM
install the steady bearing 6225CM
-
FOR 6230CM
install the steady bearing 6229CM
-
FOR 6274CM
install the steady bearing 6275CM
-
FOR 6280CM
install the steady bearing 6279CM.
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(55)
