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时间:2011-03-25 17:55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

 (1) Stop the electric pump of the Yellow Hydraulic system (Ref. TASK 29-24-00-864-001).
 (2) Make sure the Yellow and the Green Hydraulic systems are depressurized.
 (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 32-31-00-865-100
 D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7XE.

 

 E. Flight Configuration Precautions
 (1) Put the aircraft back to the ground configuration (Ref. TASK 32-00-00-860-002).
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 Subtask 32-31-00-942-080
 F. Removal of Equipment
 (1)
 Remove the SAFETY DEVICE - RAT (Ref. TASK 29-22-00-860-002).

 (2)
 Remove the safety barriers.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (4)
 Remove the warning notice(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 Subtask 32-31-00-942-080-A
 F. Removal of Equipment
 (1)
 Remove the SAFETY DEVICE - RAT (Ref. TASK 29-22-00-860-008).

 (2)
 Remove the safety barriers.

 (3)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (4)
 Remove the warning notice(s).

 (5)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.


 1EFF : ALL 1 32-31-00Page 534 1 1 Aug 01/05 1 1 1CES 1


R

R
R

**ON A/C ALL
 TASK 32-31-00-710-005- 01
 Operational Check to Ensure Safety Valve Closes at 260 kts
 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.
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 323100-04
 Operational Check to Ensure Safety Valve Closes at 260 kts using the
 aircraft batteries and electrical ground power.

 NOTE : This task is an alternative procedure to:
____
 - operational check to ensure safety valve closes at 260 kts using the APU to energize the aircraft electrical circuits or
 - operational check to ensure safety valve closes at 260 kts using the GND PWR Contactor (3XG) Override Box.
 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 colored adhesive tape No specific safety barriers No specific Ground Power Cart 36122 1 ADAPTOR-CHARGING,PITOT PROBE 460005835 1 GROUND LOCK SLEEVE 87202126V15 1 GENERATOR - GROUND PRESSURE 98D29207542000 1 SAFETY DEVICE - RAT 98D29208246001 1 SAFETY DEVICE - RAT
 1EFF : ALL 1 32-31-00Page 535 1 1 May 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R  98D34003500000 1 ADAPTER COVER-STATIC PORT 98F32304000000 1 FALSE TARGET
 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 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-22-00-860-001 Installation of the Safety Device of the Ram Air
 Turbine 29-22-00-860-002 Removal of the Safety Device of the Ram Air Turbine 29-22-00-860-007 Installation of the Safety Device of the Ram Air
 Turbine 29-22-00-860-008 Removal of the Safety Device of the Ram Air Turbine 29-23-00-860-001 Disconnection of the Isolation Coupling of the Power
 Transfer Unit (PTU) 29-23-00-860-002 Connection of the Isolation Coupling of the Power Transfer Unit (PTU) 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical Power 32-00-00-860-002 Ground Configuration after Flight Configuration with
 
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