Subtask 27-14-00-010-053
 B. Get Access
 (1)
 Put the access platform in position:

 (a)
 at the zone 575 for the left aileron,

 (b)
 at the zone 675 for the right aileron.

 (2)
 Open the access door:

 (a)
 575KB for the left aileron,

 (b)
 675KB for the right aileron.

 (3)
 Put the access platform in position at the access door 822.

 (4)
 Open the access door 822.

 (5)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover.

 Subtask 27-14-00-865-059
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 R
 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-14-00-991-002)
 Subtask 27-14-00-440-050

 A. Reactivation of the Aileron Servo-Control
 (1)
 Remove the tie-wraps.

 (2)
 Remove the blanking caps from the electrical connector (1) and the receptacle (2).

 (3) Connect the connector (1) to the receptacle (2).
 Subtask 27-14-00-865-060

 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 15CE1, 15CE2, 16CE1, 16CE2
 Subtask 27-14-00-710-054
 C. Do the operational test of the ailerons (Ref. TASK 27-14-00-710-001). Subtask 27-14-00-810-050
 D. Do the trouble shooting for the servocontrol you deactivated (Ref. TSM CH27P.B101).

 5. Close-up
________ Subtask 27-14-00-860-060
 A. Put the aircraft back to its initial configuration.
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the warning notice(s).

 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 Subtask 27-14-00-410-053
 B. Close Access
 (1)
 Close the access door:

 (a)
 575KB for the left aileron,

 (b)
 675KB for the right aileron.

 (2)
 Install the protective cover on the battery power center 105VU.

 (3)
 Tighten the two screws.

 (4)
 Close the access door 822.

 (5)
 Remove the access platform(s).

 AILERON AND HYDRAULIC ACTUATION - ADJUSTMENT/TEST
_________________________________________________
 TASK 27-14-00-710-001
 Operational Test of the Aileron and Hydraulic Actuation
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. 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 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
 Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
 Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems
 after Operation of the PTU
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure

 3. Job Set-up
__________
 Subtask 27-14-00-861-051
R A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)
 Subtask 27-14-00-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20

 Subtask 27-14-00-860-062
 C. Aircraft Maintenance Configuration
　
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(77)