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 27-50-00-400-003 Installation of the Lock-Torque Shaft - Flaps and
 Slats (98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
 F/CTL Page
 27-54-49-400-003 Installation of the Flap Track 3 Actuator
 6221CM(6271CM) (for corrective action)

 **ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
 27-54-49-991-005 Fig. 403

R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
 27-54-49-991-005-A Fig. 403A
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 27-54-49-991-003 Fig. 405
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 27-54-49-991-003-A Fig. 405A
 FOR FIN 6221CM
 27-54-45-000-007 Removal of the Torque Shafts

 6214CM(6264CM)/6220CM(6270CM)
 27-54-45-000-010 Removal of the Torque Shaft 6222CM(6272CM)
 FOR FIN 6271CM
 27-54-45-000-007 Removal of the Torque Shafts

 6214CM(6264CM)/6220CM(6270CM)
 27-54-45-000-010 Removal of the Torque Shaft 6222CM(6272CM)

 **ON A/C ALL
 3. Job Set-up
__________
 **ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,

 (Ref. Fig. 403/TASK 27-54-49-991-005) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
 (Ref. Fig. 403A/TASK 27-54-49-991-005-A)
 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 405/TASK 27-54-49-991-003) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 405A/TASK 27-54-49-991-003-A)
 **ON A/C ALL

 Subtask 27-54-49-941-063
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put the warning notice(s) in position to tell persons not to operate the flight controls.

 Subtask 27-54-49-860-052
 B. Aircraft Maintenance Configuration 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.
 (1) Extend the flaps fully (Ref. TASK 27-50-00-866-008).

 Flap Track 3 Actuator
 Figure 405/TASK 27-54-49-991-003

R 1EFF : 001-049, 051-061, 101-105, 201-203, 1 27-54-49Page 481 1 1 May 01/05 1 1 1CES 1

 Flap Track 3 Actuator Figure 405A/TASK 27-54-49-991-003-A
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-54-49Page 482 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

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

 (3)
 Extend the No. 2 and the No. 3 spoilers (Ref. TASK 27-60-00-866-002).

 (4)
 Put a COLLAR-SAFETY, SPOILER (98D27604000000) on the piston rod of each servo-control.

 Subtask 27-54-49-865-056
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 Subtask 27-54-49-010-056
 D. Get Access
 (1)
 Put the access platform in position below the applicable access panel.

 (2)
 Remove the applicable access panels:

 -
FOR 6221CM
 remove 573BB, 575AB, 575BB, 575CB, 575DB

 -
FOR 6271CM
 remove 673BB, 675AB, 675BB, 675CB, 675DB.

 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 405/TASK 27-54-49-991-003) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 405A/TASK 27-54-49-991-003-A)

 **ON A/C ALL

 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
 EDGE:

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
　
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