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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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(145)
