3. Job Set-up__________
 (Ref. Fig. 401/TASK 27-84-67-991-001)
 Subtask 27-84-67-941-050
 A. Safety Precautions
 (1) Put the safety barriers in position. 
R  (2) Fully retract the slats (Ref. TASK 27-80-00-866-005). 
R  (3) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) 
R  on the flap/slat control lever on panel 114VU. 
R  (4) Put a warning notice in position to tell persons not to operate the
 slat controls.
 Subtask 27-84-67-860-054 
R  B. Aircraft Maintenance Configuration 
R  (1) Energize the ground service network 
R  (Ref. TASK 24-42-00-861-001). 
R  (2) On the MCDU: 
R  (a) Get access to the SYSTEM REPORT/TEST F/CTL page (Ref. TASK 31-32-
R  00-860-006). 
R  -------------------------------------------------------------------------------
R  ACTION  RESULT 
R  -------------------------------------------------------------------------------

R  1. On MCDU:  On the MCDU: 
R  - push the line key for <SFCC1  - the MCDU shows the SFCC1 menu page 1. 
R 
R  2. Push the NEXT PAGE button  - the MCDU shows the SFCC1 menu page 2. 
R 
R  3. Push the line key (2L) SYSTEM  - the MCDU shows the slat SYSTEM DATA 
R  DATA SLT>  submenu. 
R

 Slat-to-Slat Interface - Location Figure 401/TASK 27-84-67-991-001
 1EFF : 1 1R 1CES  ALL  1 11 1 27-84-67 Page 404 Aug 01/03

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
4.
 Push 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 or push (in) the line key PRINT > to get a print out of the screen.

 (3)
 De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 (4)
 Remove the safety collar from the circuit breakers 9CV and 11CV.

 Subtask 27-84-67-010-050
 C. Get Access
 (1)
 Put the adjustable access platform below the zone 510(610):

 (2)
 Remove the applicable access panel (Ref. TASK 57-41-37-000-006):

 -
for the left wing, remove 522NB

 -
for the right wing, remove 622NB.

 (3)
 Remove the applicable torque shaft (Ref. TASK 27-84-45-000-004):

 -
for the left wing remove FIN 6010CM

 -
for the right wing remove FIN 6060CM.

 (4)
 Install the ADAPTOR-DRIVE, SLAT (AND FLAP) and a pneumatic wrench on the bevel gearbox:

 -
for the left wing, use FIN 6010CM

 -
for the right wing, use FIN 6060CM.
 This will let you operate the slats manually.

 (5)
 Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-000-003).

 (6)
 Manually extend the slats to the fully extended position.

 (7)
 Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. TASK 27-50-00-400-003).

 (8)
 Remove the slat closing plate (Ref. TASK 27-84-69-000-001).

 1EFF : ALL 1 27-84-67Page 405 1 1 May 01/04R 1 1 1CES 1

 Subtask 27-84-67-865-050
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/WTB/SLT/SYS2 11CV P19 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU FLIGHT CONTROLS/WTB/SLT/SYS1 9CV S06
 Subtask 27-84-67-480-051
 E. Installation of the Support Equipment
 (1) Install the SLING-SLATS (Ref. TASK 27-80-00-400-001).
 4. Procedure
_________
 (Ref. Fig. 401/TASK 27-84-67-991-001)
 **ON A/C 001-049, 051-061, 101-105, 201-203,

 (Ref. Fig. 402/TASK 27-84-67-991-002) R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 402A/TASK 27-84-67-991-002-A)
　
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