-
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 the travel of the rudder for a right turn and a left turn.
 3. Push the left pedal until it The rudder moves smoothly to the left.
 touches the mechanical stop.  On the lower ECAM display unit, on the F/CTL page:
 -the RUD/G, B, Y symbols are green,

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
4.
 Slowly release the left pedal.

5.
 On the center pedestal, on the MCDU:

 -Get the SYSTEM REPORT/TEST page (Ref. TASK 31-32-00-860-001).
-
Push the line key adjacent to the NAV indication.

-
Push the line key adjacent to the ADR3 indication.

 -
Push the line key adjacent to the OUTPUT TEST indication.

-
Push the line key adjacent to the INTERFACE TEST indication.

-Follow the initial condition (set AIR DATA selector switch to CAPT 3).
 -
Push the NEXT PAGE KEY.

-
Push the line key adjacent to the START TEST indication.

-
the pointer of the RUD indicator moves smoothly to the left mark.

 -
the protractor that measures the rudder travel shows 30. plus or minus 1..

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'max.

On the MCDU:
-
The SYSTEM REPORT/TEST page comesinto view.

-
The SYSTEM REPORT/TEST NAV page comesinto view.

-
The ADR3 page comes into view.

-
The ADR3 OUTPUT TEST page comes intoview.

-
The ADR3 INTERFACE TEST 1/2 pagecomes into view.

-
The ADR3 INTERFACE TEST 2/2 page comes into view.

-On the Captain's PFD, the speed scalemoves up and stops at 367.7 KTS.
R 1EFF : 151-199, 401-499, 1 27-21-00Page 537 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
NOTE : Ignore the RETARD warning.
____ To stop it, push the FADEC pushbutton switch on the MAINTENANCE panel 50VU.
 -Wait 30 sec. approximately before you move the pedals.
 6. In the CAPT or F/O seat:
 -push the right pedal until it touches the mechanical stop (adjustable stop).
7.
 Slowly release the right pedal.

8.
 Push the left pedal until it touches the mechanical stop.

9.
 Slowly release the left pedal.

10.
 On the center pedestal, on the MCDU:

 -
Push the line key adjacent to the RETURN indication.

 -
Push the MCDU MENU mode key.

The rudder moves smoothly to the right.
The protractor that measures the rudder
travel shows 3.5. plus or minus 0.3..

The rudder moves to the neutral
 position.
 The protractor that measures the rudder
 travel shows 0..
 The maximum no-return value is 15'.

The rudder moves smoothly to the left.
The protractor that measures the rudder
 travel shows 3.5. plus or minus 0.3..

The rudder moves to the neutral
 position.
 The protractor that measures the rudder
 travel shows 0..
 The maximum no-return value is 15'.

On the MCDU:

 -The MCDU MENU page comes into view.
R 1EFF : 151-199, 401-499, 1 27-21-00Page 538 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 5. Close-up
________ Subtask 27-21-00-080-051
 A. Remove the PROTRACTOR-CONTROL SURFACE DEFLECTION (98A27308005000) (or RIGMASTER SYSTEM (TR60)).
 Subtask 27-21-00-942-056
 B. Make sure that the work area is clean and clear of tool(s) and other items.
 Subtask 27-21-00-865-056
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7XE
 Subtask 27-21-00-410-053
 D. Close Access
 (1) Close the access doors 325ER, 325DR, 325EL, 325DL.
 (2) Remove the access platform(s). Subtask 27-21-00-860-064
 E. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱1(147)