(2)
Pressurize the Blue hydraulic system
(Ref. TASK 29-10-00-863-003).
NOTE : The Blue and/or the Green hydraulic system(s) operate(s) the
____ slat system. If necessary, use the alternative hydraulic system.
1EFF : ALL 1 27-80-00Page 223 1 1 Nov 01/01R 1 1 1CES 1
NOTE : If you use the Blue Hydraulic System, an ECAM S/CTL SLAT SYS 2
____ FAULT message will show. This message can be ignored.
NOTE : If you use the Green Hydraulic System, an ECAM S/CTL SLAT SYS
____ 1 FAULT message will show. This message can be ignored.
4. Procedure
_________
**ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,
(Ref. Fig. 202/TASK 27-80-00-991-002) R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
(Ref. Fig. 202A/TASK 27-80-00-991-002-A)
**ON A/C ALL
Subtask 27-80-00-866-056
A. Reset of the Torque Limiters of the Slat System on the Ground
(1) Release the load from the torque limiter(s) and allow the indicators to be closed, as follows:
(a) Put the slat/flap control lever to the last position that had been set, before the torque limiter(s) operated.
(2) Remove the safety collar from the circuit breakers 9CV and 11CV. Subtask 27-80-00-865-063
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
Torque Limiters - Detail and Location
Figure 202/TASK 27-80-00-991-002
R 1EFF : 001-049, 051-061, 101-105, 151-152, 1 27-80-00Page 225 1201-204, 1May 01/05 1 1 1CES 1 Torque Limiters - Detail and Location Figure 202A/TASK 27-80-00-991-002-A
R 1EFF : 062-099, 106-149, 153-199, 205-299, 1 27-80-00Page 226 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 27-80-00-866-057
C. Complete the Reset of the Torque Limiters
(1) Push each applicable indicator (1) down so that it aligns with the torque limiter, in the usual system condition.
Subtask 27-80-00-710-051
D. Operational Test
(1) Do the operational test of the slat system (Ref. TASK 27-84-00-710-001).
5. Close-up
________ Subtask 27-80-00-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable access panel(s) removed to gain access to the torque limiter(s):
for the slat No.1 Torque Limiters:
521CB, 521EB
621CB, 621EB
for the slat No.2 Torque Limiters:
522AB, 522CB
622AB, 622CB
for the slat No.3 Torque Limiters:
522FB, 522HB, 522JB, 522KB
622FB, 622HB, 622JB, 622KB
for the slat No.4 Torque Limiters:
522NB, 522QB
622NB, 622QB
for the slat No.5 Torque Limiters:
522SB, 522UB
622SB, 622UB.
1EFF : ALL 1 27-80-00Page 227 1 1 Nov 01/01R 1 1 1CES 1
Subtask 27-80-00-865-064
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
Subtask 27-80-00-860-057
C. Aircraft Maintenance Configuration
(1)
Install the safety collars on the circuit breakers 9CV and 11CV.
(2) 中國航空網 m.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7(42)
