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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