1. Reason for the Job
__________________
 Self Explanatory
 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(s)
 No specific adjustable access platform 3.6 m (11 ft. 10 in.)
 98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 98D27804006000 2 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3)

 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 27-80-00-866-005 27-84-45-000-005 27-84-45-000-006 27-84-45-000-007 27-84-48-400-001 31-32-00-860-006  Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Retracting the Slats on the GroundRemoval of the Torque Shaft 6012CM(6062CM)Removal of the Torque Shafts 6014CM(6064CM)/6028CM(6078CM)/6036CM(6086CM)/ 6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)/6044CM(6 094CM)Removal of the Torque Shafts 6016CM(6066CM)/6020CM(6070CM)/6026CM(6076CM)/ 6030CM(6080CM)Installation of the Type A Actuators 6013CM(6063CM)/6015CM(6065CM)Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page

 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,
 27-84-48-991-001 Fig. 401 R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
 27-84-48-991-001-A Fig. 401A
 **ON A/C ALL

 3. Job Set-up
__________
 **ON A/C 001-049, 051-061, 101-105, 151-152, 201-204,

 (Ref. Fig. 401/TASK 27-84-48-991-001)

 Type A Actuators - Slat Power Transmission
 Figure 401/TASK 27-84-48-991-001

R 1EFF : 001-049, 051-061, 101-105, 151-152, 1 27-84-48Page 403 1201-204, 1May 01/05 1 1 1CES 1R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,

 (Ref. Fig. 401A/TASK 27-84-48-991-001-A)
 **ON A/C ALL

 Subtask 27-84-48-941-051
 A. Safety Precautions
 (1)
 Put the safety barriers in position.

 (2)
 Put a warning notice(s) in the cockpit to tell persons not to operate the slat controls.

 Subtask 27-84-48-860-051
 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)
 Retract the slats fully (Ref. TASK 27-80-00-866-005).

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever on panel 114VU.

 Subtask 27-84-48-740-050
 C. Do a Check of the Position Pick-Off Units (PPUs) on the Centralized Fault Display System (CFDS)
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Get access to the SYSTEM REPORT/TEST (F/CTL) page on the Multipurpose Control Display Unit (MCDU) (Ref. TASK 31-32-00-860-006).

 Type A Actuators - Slat Power Transmission
 Figure 401A/TASK 27-84-48-991-001-A

R 1EFF : 062-099, 106-149, 153-199, 205-299, 1 27-84-48Page 405 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (3) Do a check of the slat PPU angles (deg) at the slat/flap control lever position 0 on the MCDU as follows:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the MCDU:  On the MCDU:

 -push (in) the line key < SFCC - the MCDU shows the SFCC 1 menu page
 1.  1.

 2.
 Push (in) the NEXT PAGE button. - the MCDU shows the SFCC 1 menu page

 2.
 3.
 Push (in) the line key (2L)  - the MCDU shows the SLAT SYSTEM DATA SYSTEM DATA SLT>. submenu.

 4.
 Push (in) the line key (1L) <PPU. - the MCDU shows the PPU DATA page(s).

 5.
 Write down the APPU and the FPPU
 angles (deg) shown on the display
　
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