-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 Push the line key adjacent to the EFCS 1(2).

 2.
 Push the line key adjacent to the GROUND SCAN indication.

3.
 Push the line key adjacent to the START GROUND SCAN indication.

 4.
 After two minutes, push the line key adjacent to the GROUND SCAN STOP indication.

 5.
 Push the line key adjacent to the GROUND REPORT indication.

 6.
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

The EFCS1(2) page comes into view.
The EFCS1(2)/GROUND SCAN page comesinto view.
NO FAULTS RECORDED comes into view.The MCDU shows the CFDS menu page.

 5. Close-up
________ Subtask 27-96-00-410-051
 A. Close Access
 (1)
 Install the protective cover on the battery power center 105VU.

 (2)
 Tighten the two screws.

 (3)
 Close the access door 822.

 (4) Remove the access platform(s). Subtask 27-96-00-860-088
 B. Put the aircraft back to its initial configuration.
 (1)
 On the overhead panel 20VU, on the ADIRS CDU.

 -Set the 3 OFF/NAV/ATT selector switches to OFF (Ref. TASK 34-10-00-860-005).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 TASK 27-96-00-710-024
 Operational Test of the Ground Spoiler Extension
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
355M03190000 3 MLG WHEEL TACHYMETER DRIVING TOOL
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply 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 32-48-51-000-002 Removal of the Impeller Assy 32-48-51-000-005 Removal of the Fan Assy (7GS,8GS,9GS,10GS) 32-48-51-400-002 Installation of the Impeller Assy 32-48-51-400-005 Installation of the Fan Assy (7GS,8GS,9GS,10GS) 34-10-00-860-004 IR Alignment Procedure 34-10-00-860-005 ADIRS Stop Procedure

 3. Job Set-up__________
 Subtask 27-96-00-860-092
 A. Aircraft Maintenance Configuration
 (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
 (2) Do the IR alignment procedure (Ref. TASK 34-10-00-860-004).
 (3) On the panel 23VU, make sure that the FLT CTL/SEC1 and FLT CTL/ELAC1 pushbutton switches are pushed.
 (4) On the panel 24VU, make sure that the FLT CTL/SEC2, FLT CTL/SEC3 and FLT CTL/ELAC2 pushbutton switches are pushed.
 (5) Pressurize the three hydraulic systems (Ref. TASK 29-10-00-863-001), (Ref. TASK 29-10-00-863-002) and (Ref. TASK 29-10-00-863-003).
 Subtask 27-96-00-865-092
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
R  49VU L/G/Y BRK/PRESS/IND  61GG  C10 
R  **ON A/C 401-499, 
R  49VU ABCU &/Y BRK/PRESS IND  61GG  C10 
R  **ON A/C ALL 
R R R R R  121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 121VU HYDRAULIC/SOL VALVES/G/Y/PTU  4GG 3GG 1GG 2GG 1801GL  M36 M35 M34 M33 N34
　
中國航空網 www.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9(169)