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时间:2011-03-24 08:31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

 -the green line between the ESS TR and the DC ESS busbar is not shown.
 During the CSM/G test (when the CSM/G is running), push the TR RESET pushbutton switch (15PU) on the panel 103VU to reset the essential TR.
On the overhead panel 21VU:
-make sure that the safety guard isback in place.
 On the lower ECAM display unit:
 -the Blue electrical hydraulic pump stops and the generator is disconnected from its network automatically,
 -all indications are cancelled,
 -the ELEC page goes off.
 (a)
 Push the left rudder pedal (on one of the two rudder pedal pairs) and then the right rudder pedal forward to operate the rudder. Put the rudder back to the neutral position. Do this procedure two times.

 (b)
 Pull and push the side stick controller to operate the elevators. Put the side stick controller to the neutral position. Do this procedure two times.


 (6)
 Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).

 (7)
 Wait approximately 5 minutes before you continue, to let the system become stable.


 1EFF : ALL 1 29-00-00Page 250 1 1 May 01/04R 1 1 1CES 1


 (8)
 Do a check of the fluid level in the Blue reservoir. Add fluid as necessary (Ref. TASK 12-12-29-611-002) or (Ref. TASK 12-12-29-611-001).

 (9)
 Do the procedure steps (1) thru (8) again, two more times.


 (10)
 Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).

 (11)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (12)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (13)
 Do the subsequent steps to make sure that there is no air in the hydraulic system:

 (a)
 Do a check of the fluid level of the Blue reservoir.

 (b)
 If it is necessary to add fluid:

 (c)
 Make sure that the air pressure in the reservoir of the Blue hydraulic system is not less than 50 psi (3.4473 bar). If necessary, pressurize the reservoir (Ref. TASK 29-14-00-614-002).

 (d)
 Read the gage of the Blue reservoir and make a note of the fluid level.

 (e)
 Depressurize the reservoir of the Blue hydraulic system. (Ref. TASK 29-14-00-614-001).

 (f)
 After 5 minutes read the gage again and make a note of the level.

 (g)
 Compare both levels.

 (h)
 If the difference between both levels is more than 1 liter, do the bleeding procedure again until the result is satisfactory.

 


 1_ Depressurize the reservoir (Ref. TASK 29-14-00-614-001)
 2_ Keep the reservoir depressurization valve (2087GM) open and
 fill the reservoir (Ref. TASK 12-12-29-611-002) or (Ref. TASK
 12-12-29-611-001).

 1EFF : ALL 1 29-00-00Page 251 1 1 May 01/04R 1 1 1CES 1

 

R **ON A/C 001-049, 051-061, 101-105, 201-203,
 Subtask 29-00-00-720-051-A
 B. Do the Ram Air Turbine System Bleeding Procedure (Ref. TASK 29-00-00-870-010).
 **ON A/C ALL
 5. Close-up
________
 Subtask 29-00-00-860-074

 A. Put the aircraft back to the serviceable condition.
 (1)
 Make sure that the level of hydraulic fluid in the reservoir of the Blue hydraulic system is correct. Add fluid as necessary (Ref. TASK 12-12-29-611-001) or (Ref. TASK 12-12-29-611-002).

 (2)
 Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).

 

 

R **ON A/C 001-049, 051-061, 101-105, 201-203,
 TASK 29-00-00-870-010
 Ram Air Turbine System Bleeding Procedure
 NOTE : In accordance with the AOT 29A1112/12, if the required ground equipment
____ is not available, you must do the bleeding procedure of the ram-air turbine within 20 flight hours or 3 days after the maintenance action, whichever occurs first.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 682003008 1 CONTROL UNIT - RAT
 98D29207550001 1 PROTECTION EQUIPMENT - RAT

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 
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