(2)
Open the access doors 325ER, 325EL, 325DR, 325DL.
(Ref. Fig. 506/TASK 27-21-00-991-006)
Subtask 27-21-00-480-051
B. Installation of the tool.
(1) Install the PROTRACTOR-CONTROL SURFACE DEFLECTION (98A27308005000) (or RIGMASTER SYSTEM (TR60)) on the rudder and on the vertical surface opposite the center servocontrol.
1EFF : ALL 1 27-21-00Page 530 1 1 Aug 01/04R 1 1 1CES 1
Position of the Servocontrol Figure 506/TASK 27-21-00-991-006
1EFF : 1 1R 1CES ALL 1 11 1 27-21-00 Page 531 Aug 01/04
Subtask 27-21-00-860-063
C. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(3)
Do the IR alignment procedure for the ADIRU 3 (Ref. TASK 34-10-00-860-004).
(4)
On the overhead panel 23VU, make sure that:
-the FLT CTL/FAC1, FLT CTL ELAC1, and FLT CTL/SEC1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off.
(5)
On the overhead panel 24VU, make sure that:
-the FLT CTL/FAC2, FLT CTL ELAC2, FLT CTL/SEC2 and FLT CTL/SEC3 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off.
(6)
Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).
(7)
On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows O.
(8)
On the center pedestal, on the ECAM control panel, push the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
Subtask 27-21-00-865-052
D. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
1EFF : ALL 1 27-21-00Page 532 1 1 Aug 01/04R 1 1 1CES 1
Subtask 27-21-00-865-055
E. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01
4. Procedure
_________
(Ref. Fig. 506/TASK 27-21-00-991-006)
R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 27-21-00-720-050
A. Do this test :
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. In the CAPT or F/O seat: - push the right pedal until it touches the mechanical stop (the adjustable stop). The rudder moves smoothly to the right.On the lower ECAM display unit, on theF/CTL page:- the RUD/G, B, Y symbols are green, - the pointer of the RUD indicator moves smoothly to the right mark, - the protractor that measures the rudder travel shows 25. plus or minus 1..
2. Slowly release the right pedal. The rudder moves to the neutral position. On the lower ECAM display unit, on the F/CTL page: - the RUD/G, B, Y symbols are green, - the pointer of the RUD indicator moves to the neutral position, - the protractor that measures the rudder travel shows 0.. The maximum
no-return value is 15'.
NOTE : The no-return value is the sum____
of the two no-return values of
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3.
Push the left pedal until it touches the mechanical stop.
4.
Slowly release the left pedal.
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1(145)
