• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-03-21 13:47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

 5. Close-up
________ Subtask 27-26-00-860-053
 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)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001)

 

 

 Subtask 27-26-00-410-054
 B. Close Access
 (1)
 Close the access doors 325BL (325BR).

 (2)
 Remove the access platform(s).

 


 YAW DAMPER ACTUATION - ADJUSTMENT/TEST
______________________________________ TASK 27-26-00-710-001 Operational Test of the Yaw Damper Actuation
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-63-00-710-001 Operational Test of the Yaw Damper Function
 3. Job Set-up
__________ Subtask 27-26-00-860-058
 A. Not applicable
 4. Procedure
_________ Subtask 27-26-00-710-050
 A. Do the operational test of the yaw damper actuation (Ref. TASK 22-63-00-710-001).


 TASK 27-26-00-820-001 Adjustment of the Yaw Damper Actuation WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A 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 access platform 1.60 m (5 ft. 3 in.)
 No specific access platform 5.87 m (19 ft. 3 in.)
 98D27207516000 2 RIGGING PIN SET

R 98D27207548000 1 PIN - RIGGING R 98D27207549000 1 PIN - RIGGING
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific  Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)


 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
 -------------------------------------------------------------------------------
7 cotter pin 27-21-47 01 -210 R 7 cotter pin 27-21-47 01A-210
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
22-63-00-710-001 Operational Test of the Yaw Damper Function 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
 27-26-00-991-001 Fig. 501

 3. Job Set-up
__________
 Subtask 27-26-00-861-051
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
 Subtask 27-26-00-010-056
 B. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Open the access door 822.

 (3)
 On the battery power center 105VU:
 
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2(160)