曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 Subtask 27-80-00-865-055
 D. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
 4. Procedure_________
 Subtask 27-80-00-866-052 
R  A. Extension of the Slats on the Ground
 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. 
R R R R  CAUTION : IF THE THRUST REVERSER COWLS ARE OPEN, MAKE SURE THAT THE HALF_______ DOORS OF THE THRUST REVERSER ARE RETRACTED BEFORE YOU EXTEND THE SLATS. IF THE DOORS ARE EXTENDED, YOU CAN CAUSE DAMAGE TO THE SLATS AND HALF DOORS WHEN THE SLATS EXTEND.
 (1) Set the slat/flap control lever to position 1, 2 or FULL.
 (2) Make sure that on the ECAM upper DU the slat position bar moves to the correct position.

 

 (3) Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the slat/flap control lever (Ref. TASK 27-00-00-480-002). ________
5. Close-Up
 Subtask 27-80-00-860-053
 A. Aircraft Maintenance Configuration
 (1)
 Depressurize the Blue hydraulic system
 (Ref. TASK 29-10-00-864-003).

 (2)
 On the ECAM control panel, set the control/brightness controls to OFF.

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

 Subtask 27-80-00-942-057
 B. Removal of Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the safety barriers.

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 1EFF : ALL 1 27-80-00Page 204 1 1 Aug 01/05R 1 1 1CES 1

 TASK 27-80-00-866-007
 Manual Extension of the Slats
 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 GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

R
 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) No specific pneumatic right-angle wrench No specific safety barriers No specific warning notice No specific access platform 1.8 m (5 ft. 11 in.) 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP) 98D27804011000 1 BAR-TURNING

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001)
 27-80-00-866-005 Retracting the Slats on the Ground
 27-80-00-866-008 Manual Retraction of the Slats

R 27-84-45-000-005 Removal of the Torque Shaft 6012CM(6062CM) 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page 27-80-00-991-004 Fig. 201
 3. Job Set-up
__________
 Subtask 27-80-00-941-059
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice in position on the panel 114VU to tell persons not to operate the flap/slat controls.

 Subtask 27-80-00-860-060
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the slats are fully retracted (Ref. TASK 27-80-00-866-005).

 (2)
 Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER on the flap/slat control lever on panel 114VU.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(36)