-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking plugs No specific circuit breaker(s) safety clip(s) No specific plastic bag No specific safety barriers No specific warning notice No specific access platform 1.82 m (5 ft. 12 in.) No specific access platform 3.65 m (11 ft. 12 in.)
 1EFF : ALL 1 57-51-15Page 401 1 1 Aug 01/05R 1 1 1CES 1

 B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  27-50-00-866-008 27-54-45-000-003 29-00-00-864-001 32-12-00-010-001 32-43-31-000-001 32-43-32-000-001 53-35-11-000-001  Extension of the Flaps on the GroundRemoval of the Torque Shaft 6206CM(6256CM)Put the Related Hydraulic System in the Depressurized Configuration before Maintenance ActionOpen the Main Gear Doors for AccessRemoval of the Alternate-Brake Servovalve Manifold 2614GM(2615GM) Removal of the Alternate-Brake Manifold 2853GM(2852GM)Removal of the Wing-to-Fuselage Fairings 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 57-51-15-991-002  Fig. 401 
R  **ON A/C 401-499, 
R  57-51-15-991-002-A  Fig. 401A 
R  **ON A/C ALL
 3. Job Set-up__________
 Subtask 57-51-15-941-052
 A. Safety Precautions
 (1) Put the warning notice in the cockpit to tell persons not to operate the flaps or the slats.
 (2) Put the safety barriers in position.

 Subtask 57-51-15-010-051
 B. Get Access 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)
 Fully extend the flaps (Ref. TASK 27-50-00-866-008).

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

 (3)
 Open the MLG doors (Ref. TASK 32-12-00-010-001).

 (4)
 Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.

 (5)
 Put the access platform in position below zone 570(670).

 (6)
 Put the access platform in position to get access to the top surface of the wing in zone 570(670).

 (7)
 Remove the upper wing/fuselage fillet fairing(s) 191ET(192ET) (Ref. TASK 53-35-11-000-001) to get access to the three shroud box/fuselage attachments.

 Subtask 57-51-15-865-053
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
 4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 (Ref. Fig. 401/TASK 57-51-15-991-002)

 Shroud Box - Location and Detail Figure 401/TASK 57-51-15-991-002- 14 (SHEET 1)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-15Page 404 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1

 Shroud Box - Location and Detail Figure 401/TASK 57-51-15-991-002- 24 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-15Page 405 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1

 Shroud Box - Location and Detail Figure 401/TASK 57-51-15-991-002- 34 (SHEET 3)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-15Page 406 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1

 Shroud Box - Location and Detail Figure 401/TASK 57-51-15-991-002- 44 (SHEET 4)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-51-15Page 407 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1R **ON A/C 401-499,

R (Ref. Fig. 401A/TASK 57-51-15-991-002-A)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
　
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