A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(94)

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

No specific access platform 1.6 m (5 ft. 3 in.)
 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 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 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 1EFF : ALL 1 27-94-00Page 510 1 1 May 01/04R 1 1 1CES 1

 3. Job Set-up
__________

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-94-00-860-055
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the aircraft hydraulic systems are depressurized (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).

 (3)
 On the FLT CTL panel 23VU:

 -make sure that the FLT CTL/SEC 1 and FLT CTL/ELAC 1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off)
 -release the FLT CTL/SEC 1 pushbutton switch (on this pushbutton switch the OFF legend comes on).

 (4)
 On the FLT CTL panel 24VU:

 -make sure that the FLT CTL/SEC 2, FLT CTL/SEC 3 and FLT CTL/ELAC 2 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off)
 -release the FLT CTL/SEC 3 pushbutton switch (on this pushbutton switch the OFF legend comes on).

 (5)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (6)
 On the center pedestal, on the ECAM control panel, push the F/CTL key (on the lower ECAM DU, the F/CTL page comes into view).

 (7)
 On the panel 114VU, make sure that the flap and slat control lever is not in position FULL.

 (8)
 Read the status of the monitored circuit breakers (installed on the battery power center 105VU), directly on the upper ECAM DU. If the warning C/B TRIPPED R ELEC BAY is shown, get access to 105VU panel:

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

 (b)
 Open the access door 822.

 

 

 (c) On the battery power center 105VU, loosen the two screws and
 remove the protective cover. 
R  **ON A/C 301-399, 
R  Subtask 27-94-00-860-055-A 
R  A. Aircraft Maintenance Configuration 
R  (1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-
R  002). 
R  (2) Make sure that the aircraft hydraulic systems are depressurized 
R  (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 
R  29-10-00-864-003). 
R  (3) On the FLT CTL panel 23VU: 
R  - make sure that the FLT CTL/SEC 1 and FLT CTL/ELAC 1 pushbutton 
R  switches are pushed (on these pushbutton switches, the FAULT and 
R  OFF legends are off) 
R  - release the FLT CTL/SEC 1 pushbutton switch (on this pushbutton 
R  switch the OFF legend comes on). 
R  (4) On the FLT CTL panel 24VU: 
R  - make sure that the FLT CTL/SEC 2, FLT CTL/SEC 3 and FLT CTL/ELAC 2 
R  pushbutton switches are pushed (on these pushbutton switches, the 
R  FAULT and OFF legends are off) 
R  - release the FLT CTL/SEC 3 pushbutton switch (on this pushbutton 
R  switch the OFF legend comes on). 
R  (5) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) 
R  (Ref. TASK 31-60-00-860-001). 
R  (6) On the center pedestal, on the ECAM control panel, push the F/CTL key 
R  (on the lower ECAM DU, the F/CTL page comes into view). 
R  (7) On the panel 114VU, make sure that the flap and slat control lever is 
R  not in position 3 or FULL. 
R  (8) Read the status of the monitored circuit breakers (installed on the 
　
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9(94)