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时间:2011-03-24 08:55来源:蓝天飞行翻译 作者:admin
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 (2) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002). 
R R  (3) Put a placard in position to tell aircraft crew that one or two of the wing anti-ice control valves are deactivated.
 (4) Make an applicable entry in the aircraft technical log.
 Subtask 30-11-00-942-055
 D. Removal of Equipment
 (1) Remove the safety barriers.
 (2) Remove the warning notice(s).

 

 (3)
 Remove the access platform(s).


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


 1EFF : ALL 1 30-11-00Page 409 1 1 May 01/04R 1 1 1CES 1

 TASK 30-11-00-440-001


 Reactivation of the Wing Anti Ice Control Valve 9DL(10DL) from the CLOSED position
 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 MMEL TASK: 30-11-01
 Wing Ice Protection
 Anti-Ice Control Valve

 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 safety barriers No specific warning notice No specific warning notices No specific access platform 3 m (9 ft. 10 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 1EFF : ALL 1 30-11-00Page 410 1 1 May 01/04R 1 1 1CES 1


 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 FOR FIN 9DL
 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 FOR FIN 10DL
 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 C. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
30-11-51-000-001 Removal of the Wing Anti-Ice Control Valve
 30-11-51-400-001 Installation of the Wing Anti-Ice Control Valve
 57-41-37-000-008 Removal of the Access Panel 522WB(622WB)
 57-41-37-400-008 Installation of the Access Panel 522WB(622WB)
 TSM 30 PB 101 (for corrective action)

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 30-11-00-991-004  Fig. 401
 **ON A/C 301-399,
 30-11-00-991-004-A  Fig. 401A **ON A/C ALL


 3. Job Set-up
__________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (Ref. Fig. 401/TASK 30-11-00-991-004)
 **ON A/C 301-399,

 (Ref. Fig. 401A/TASK 30-11-00-991-004-A)
 **ON A/C ALL

 Subtask 30-11-00-941-060
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Before you do work on the Ice Protection system, put warning notices in position to tell persons not to: - operate the pneumatic system - operate the engines - operate the slats - operate the APU switch.

 (3)
 Install a TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.

 (4)
 On panel 191DB, put a warning notice in position to tell persons not to pressurize the bleed air system.

 


 Subtask 30-11-00-865-053
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 49VU ANTI ICE/WING/CTL 2DL C02 49VU ANTI ICE/WING/MONG 1DL C01 121VU APU/APU/CTL 2KD L42 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
 
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