Transducer Unit 49CE1, 49CE2
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-10-00-864-003 Depressurize the Blue Hydraulic System
55-13-11-000-001 Removal of the THS Trailing Edge Access Panels
55-16-48-000-001 Removal of the Elevator Support Struts
27-34-41-991-004 Fig. 401
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
27-34-41-991-001 Fig. 402
**ON A/C 051-051,
27-34-41-991-001-A Fig. 402A
**ON A/C ALL
27-34-41-991-003-A Fig. 403
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-34-41-991-004)
Subtask 27-34-41-860-051
A. Aircraft Maintenance Configuration
(1) Make sure that the elevators and the trimmable horizontal stabilizer are set to a neutral position.
R R Hoist Points Plugs Figure 401/TASK 27-34-41-991-004
1EFF : 1 1 1CES ALL 1 111 27-34-41 Page 403 May 01/98
Subtask 27-34-41-860-050
B. Depressurize Hydraulic Systems
(1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-864-003).
Subtask 27-34-41-865-050
R C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 27-34-41-481-050
R D. Install Locking Pins.
(1) Put the PIN-SIDE STICK LOCKING in the CAPT and F/O side stick controllers.
Subtask 27-34-41-941-050
E. Safety Precautions
(1)
Put the warning notices in the flight compartment to tell persons not to operate the flight controls.
(2)
Put the warning notices in position to tell persons not to operate the hydraulic systems.
(3)
Put the access platform in position at zone 334 for theleft hand elevator and/or zone 344 for the right hand elevator.
Subtask 27-34-41-010-050
F. Access
(1) Open the THS lower trailing edge access panels of the horizontal stabilizer. 334BB, 344BB, 334DB, 344DB, 334FB, 344FB, 334GB, 344GB, 334HB, 344HB (Ref. TASK 55-13-11-000-001).
Subtask 27-34-41-020-052
G. Hoisting Lugs
(1) Remove the hoist point plugs (10).
(2) Install the hoisting lugs NSA9006-12B.
Subtask 27-34-41-480-050
H. Attach Support Equipment
(1)
Put the crane into position.
(2)
Attach the SLING-ELEVATOR to the hoisting points and to the crane.
(3)
Operate the crane and slowly tighten the sling cables. Adjust the turnbuckles as necessary to get an equal tension on all cables.
4. Procedure
_________ R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 402/TASK 27-34-41-991-001)
**ON A/C 051-051,
(Ref. Fig. 402A/TASK 27-34-41-991-001-A)
**ON A/C ALL
(Ref. Fig. 403/TASK 27-34-41-991-003-A)
Elevator-Removal/Installation.
Figure 402/TASK 27-34-41-991-001
R 1EFF : 001-049, 052-099, 101-149, 151-199, 1 27-34-41Page 406 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R Elevator-Removal/Installation.
R Figure 402A/TASK 27-34-41-991-001-A
R 1EFF : 051-051, 1 27-34-41 Page 407
1 1 May 01/05
1 1
1CES 1
Elevator-Removal/Installation Figure 403/TASK 27-34-41-991-003-A
1EFF : 1 1R 1CES ALL 1 11 1 27-34-41 Page 408 May 01/05
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-34-41-020-053
A. Removal of the Elevator
(1)
Disconnect the bonding straps (elevator side).
(a) Remove the nuts (18), the washers (20) and the bolts (21) and disconnect the bonding straps (19). 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3(49)
