**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
27-54-49-991-005 Fig. 403
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
27-54-49-991-005-A Fig. 403A
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-54-49-991-002 Fig. 404
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-54-49-991-002-A Fig. 404A **ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
(Ref. Fig. 403/TASK 27-54-49-991-005) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 403A/TASK 27-54-49-991-005-A)
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 404/TASK 27-54-49-991-002) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 404A/TASK 27-54-49-991-002-A)
**ON A/C ALL
Subtask 27-54-49-941-061
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notice(s) in position to tell persons not to operate the flight controls.
Subtask 27-54-49-860-051
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) Extend the flaps fully (Ref. TASK 27-50-00-866-008).
Flap Track 2 Actuator
Figure 404/TASK 27-54-49-991-002
R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-54-49Page 456 1 1 May 01/05 1 1 1CES 1
Flap Track 2 Actuator Figure 404A/TASK 27-54-49-991-002-A
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-54-49Page 457 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1
(2)
Make sure the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever in the cockpit.
(3)
Extend the No. 1 spoiler (Ref. TASK 27-60-00-866-002).
(4)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
Subtask 27-54-49-865-055
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-54-49-010-055
D. Get Access
(1)
Put the access platform in position below the applicable access panel.
(2)
Remove the applicable access panels:
-
FOR 6211CM remove 193AB, 193BB 573AB, 573BB, 573CB, 575CB
-
FOR 6261CM remove 194AB, 194BB 673AB, 673BB, 673CB, 675CB.
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 404/TASK 27-54-49-991-002) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 404A/TASK 27-54-49-991-002-A)
**ON A/C ALL
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 27-54-49-480-051
A. Installation of Support Equipment
(1) Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on the torque shafts (1) and (6) (Ref. TASK 27-50-00-400-003).
Subtask 27-54-49-740-060
B. Do a Check of the Position Pick-Off Units (PPUs) on the Centralized Fault Display System (CFDS)
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Get access to the SYSTEM REPORT/TEST (F/CTL) page on the Multipurpose Control Display Unit (MCDU) (Ref. TASK 31-32-00-860-006).
(3)
Do a check of the flap PPU angles (deg) at the slat/flap control lever position FULL on the MCDU as follows:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU: On the MCDU:
-push (in) the line key < SFCC - the MCDU shows the SFCC 1 menu.
1.
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5(111)
