-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
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
29-10-00-864-003 Depressurize the Blue Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
29-24-00-864-001 Depressurize the Yellow Hydraulic System
31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
F/CTL Page
71-00-00-710-003 Engine Automatic Start
71-00-00-710-004 Engine Manual Start
71-00-00-710-027 Engine Shutdown
71-00-00-710-028 Engine Shutdown
3. Job Set-up__________
Subtask 27-51-00-941-069
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notices in postion to tell persons that the flap and slat systems are in operation.
Subtask 27-51-00-860-066
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Make sure that the aircraft batteries are fully charged (Ref. TASK 24-38-00-710-001).
(3)
Get access to the SYSTEM REPORT/TEST (F/CTL) page on the MCDU (Ref. TASK 31-32-00-860-006).
(4)
Do the automatic integrity test of the two SFCC's which includes Slat and Flap BITE tests of the two computers (Ref. TASK 27-51-00-750-001).
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(5) Make sure that the Wing Tip Brakes (WTBs) are not set (Ref. TASK 27-50-00-869-006).
Subtask 27-51-00-865-086
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-51-00-865-087
D. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/FLP/SYS2 12CV P20 122VU FLIGHT CONTROLS/WTB/FLP/SYS1 10CV S07
Subtask 27-51-00-860-067-A
E. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1)
Start both engines by the Engine Automatic-Start Procedure (Ref. TASK 71-00-00-710-003) or the Engine Manual-Start Procedure (Ref. TASK 71-00-00-710-004).
(2)
Pressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-863-001), (Ref. TASK 29-10-00-863-002) and (Ref. TASK 29-10-00-863-003).
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4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-00-710-068
A. Operational Test of the Wing Tip Brake and the Pressure-Off Brake WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
NOTE : Use the Multipurpose Control Display Unit (MCDU) 3 on panel 1VU
____ for the test. If the MCDU 3 is defective, use the MCDU 2 on panel 11VU.
NOTE : When you do this test the flap surfaces will move automatically.
____
NOTE : Make sure that the CFDS is not in the SFCC menu mode before you
____ start the test. The test will not operate, if a BITE test was completed before. Subsequently Corrupted RAM - Return On Line - or Pin Prog Fault will be displayed. 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4(45)
