• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-24 08:37来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 CAUTION : DO NOT START OR DRY MOTOR THE ENGINES WITH A HYDRAULIC GROUND
_______ POWER SUPPLY CONNECTED TO THE AIRCRAFT. IF YOU DO, YOU CAN CAUSE DAMAGE TO THE ENGINE PUMPS.


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
1. Dry-motor the right (No. 2) engine (Ref. TASK 71-00-00-710-001).
2. On the overhead panel 40VU: - press the YELLOW/ENG 2 PUMP P/BSW. 

On the overhead panel 40VU: - press the YELLOW/ENG 2 PUMP P/BSW. 
R R R 

-
the right (No. 2) engine turns andcauses the engine-driven pump of theYellow hydraulic system to turn.

 On the ECAM upper DU:

 -
the speed of the right (No. 2) engine is approximately 20% N2 RPM.

 On the ECAM lower DU:

 -
the pressure in the Yellow hydraulic system is 3000 +100 -100 psi.

On the overhead panel 40VU:

-
the YELLOW/ENG 2 PUMP OFF light comeson.

 On the ECAM lower DU:

 -
the vertical line between the EDP box and the system indication changes from green to amber.

 -
the engine pump symbol of the Yellow hydraulic system changes from green in-line to amber cross-line.

 -
the pressure in the Yellow hydraulic system decreases to 0 psi.

On the overhead panel 40VU:

-
the YELLOW/ENG 2 PUMP OFF light goesoff.

 On the ECAM lower DU:

 -
the pressure in the Yellow hydraulic system increases to 3000 +100 -100 psi.

 -
the vertical line between the EDP box and the system indication changes from amber to green.

-
the engine pump symbol of the Yellow hydraulic system changes from amber cross-line to green in-line.

 


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3. Stop the dry-motoring of the  On the ECAM lower DU: right (No. 2) engine (Ref. TASK - the pressure in the Yellow hydraulic 71-00-00-710-001). system decreases to 0 psi.
 5. Close-up
________
 Subtask 29-13-00-860-053
 A. Put the aircraft back to the serviceable condition.
 (1)
 On the overhead panel 40VU, press and release the PTU/AUTO P/BSW, (the OFF light goes out).

 (2)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).


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


 1EFF : ALL 1 29-13-00Page 504 1 1 Feb 01/04R 1 1 1CES 1


 MANIFOLD - MAIN HP (3011GM) - REMOVAL/INSTALLATION
__________________________________________________
 TASK 29-13-14-000-001
 Removal of the HP Manifold of the Yellow Hydraulic System
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking caps
 No specific blanking plugs
 No specific circuit breaker(s) safety clip(s)
 No specific warning notices
 No specific container 5.0 l (1.3208 USgal)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action
 29-00-00-910-002 Safety Procedures of the Hydraulic System
 29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
 Transfer Unit (PTU)

R **ON A/C 001-049, 051-058, 101-101,
 29-13-14-991-001 Fig. 401 -------------------------------------------------------------------------------


REFERENCE DESIGNATION
 -------------------------------------------------------------------------------

R **ON A/C 059-099, 102-149, 151-199, 201-299, 301-399, 401-499,
 29-13-14-991-001-A Fig. 401A
 **ON A/C ALL
 3. Job Set-up
__________
 
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 HYDRAULIC POWER 液压3(105)