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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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_______ GEAR.
 CAUTION : DO NOT USE THE APU BLEED AIR TO SUPPLY THE WING ANTI-ICE SYSTEM
_______ DURING THE GROUND TEST. THE APU BLEED-AIR SYSTEM DOES NOT SUPPLY SUFFICIENT PRESSURE FOR THE GROUND TEST PROCEDURE.
 CAUTION : DO NOT USE ENGINE POWER WHEN YOU DO A LEAK TEST OF THE WING ANTI-ICE
_______ DUCTS. HOT AIR FROM THE ENGINE CAN CAUSE INJURY.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform, adjustable 4.0 m (13 ft. 1 in.)
 1EFF : ALL 1 30-11-00Page 508 1 1 Nov 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 -------------------------------------------------------------------------------
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 27-80-00-866-004 Extending the Slats on the Ground 27-80-00-866-005 Retracting the Slats on the Ground 32-00-00-481-001 Installation of the Safety Devices on the Landing
 Gears 30-11-42-000-001 Removal of the Anti-Ice Duct (for corrective action) 30-11-42-400-001 Installation of the Anti-Ice Duct (for corrective
 action)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 30-11-00-991-006  Fig. 502
 **ON A/C 301-399,
 30-11-00-991-006-A  Fig. 502A **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. 502/TASK 30-11-00-991-006)
 **ON A/C 301-399,

 (Ref. Fig. 502A/TASK 30-11-00-991-006-A)
 **ON A/C ALL

 Subtask 30-11-00-941-068
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 Put a warning notice in the cockpit to tell persons not to operate the flight controls.


 Subtask 30-11-00-860-051
 B. Aircraft Maintenance Configuration
 (1)
 Fully extend the slats (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the slat/flap control lever.

 


 Wing Anti-Ice Control Valve - Location and Detail
 Figure 502/TASK 30-11-00-991-006

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 30-11-00Page 511 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1


 Wing Anti-Ice Control Valve - Location and Detail Figure 502A/TASK 30-11-00-991-006-A
R 1EFF : 301-399, 1 30-11-00Page 512 1 1 May 01/05 1 1 1CES 1 Subtask 30-11-00-010-063


 C. Get Access
 (1)
 Put an access platform, adjustable in position at the applicable zone 520(620).

 (2)
 Remove the applicable leading edge access panels:


 -522AB, 522CB, 622AB, 622CB.
 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 30-11-00-860-053
 A. Preparation for Test
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).


 (2)
 Open the wing anti-ice control valve:

 (a)
 Move the indicator (2) to the OPEN position.

 (b)
 Remove and discard the lockwire from the screw (1).

 (c)
 Remove the screw (1) and install it in the end of the indicator

 (2) to lock it in the OPEN position.
 
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