-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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 3.5 m (11 ft. 6 in.)
98D27504030001 2 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
98D27804007000 2 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12)
1EFF : ALL 1 27-84-49Page 419 1 1 Nov 01/01R 1 1 1CES 1
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)
27-80-00-866-005 Retracting the Slats on the Ground
27-84-45-000-006 Removal of the Torque Shafts
6014CM(6064CM)/6028CM(6078CM)/6036CM(6086CM)/ 6038CM(6088CM)/6040CM(6090CM)/6042CM(6092CM)/6044CM(6 094CM)
27-84-45-000-011 Removal of the Torque Shaft 6032CM(6082CM)
27-84-45-000-012 Removal of the Torque Shaft 6034CM(6084CM)
27-84-48-400-001 Installation of the Type A Actuators
6013CM(6063CM)/6015CM(6065CM) 31-32-00-860-006 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,
27-84-49-991-001 Fig. 401
R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
27-84-49-991-001-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 27-84-49-991-001)R **ON A/C 062-099, 106-149, 153-199, 205-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 27-84-49-991-001-A)
**ON A/C ALL
Subtask 27-84-49-941-053
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 27-84-49-860-051
B. Aircraft Maintenance Configuration
(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 slat/flap control lever on panel 114VU.
Subtask 27-84-49-740-053
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).
(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:
-push (in) the line key < SFCC
1.
2.
Push (in) the NEXT PAGE button.
3.
Push (in) the line key (2L) SYSTEM DATA SLT>.
4.
Push (in) the line key (1L) <PPU.
5.
Write down the APPU and the FPPU angles (deg) shown on the display or push (in) the line key PRINT > to get a print-out of the screen.
NOTE : These angles, shown at
____ removal, will be used as a datum. They will let you compare the APPU and the FPPU angles after the installation of the actuator (Ref. TASK 27-84-48-400-001).
6.
Push the line key < RETURN frequently until the CFDS menu page is shown.
7.
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
On the MCDU:
-
the MCDU shows the SFCC 1 menu page
1.
-
the MCDU shows the SFCC 1 menu page
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