3. Job Set-up
__________ (Ref. Fig. 401/TASK 27-84-61-991-001) Subtask 27-84-61-941-055
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put the warning notice in the cockpit to tell persons not to operate the slat controls.
Subtask 27-84-61-860-050
B. Aircraft Maintenance Configuration
(1) Make sure the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is on the flap and slat control lever on panel 114VU.
Subtask 27-84-61-865-060
C. 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 27-84-61-010-052
D. Get Access
(1)
Remove the applicable closing plate(s) (Ref. TASK 27-84-69-000-001).
(2)
Remove the Slat 1 (Ref. TASK 27-84-63-000-001).
(3)
Remove the applicable access panels:
-
for the left wing, remove the panels 521AB, 521BB, 521CB, 521EB
-
for the right wing, remove the panels 621AB, 621BB, 621CB, 621EB.
(4)
For the tracks 2 and 3, remove the applicable actuator (Ref. TASK 27-84-48-000-001).
1EFF : ALL 1 27-84-61Page 402 1 1 Nov 01/03R 1 1 1CES 1
No. 1 Slat - Location and Detail
Figure 401/TASK 27-84-61-991-001
1EFF : ALL 1 27-84-61 Page 403
1 1 Feb 01/98
1 1
1CES 1
4. Procedure_________
(Ref. Fig. 401/TASK 27-84-61-991-001)
Subtask 27-84-61-020-053
R A. Removal of the Slat Tracks 1 thru 4
NOTE : When slat tracks 1 and 4 are made it can be necessary to install____ spacers in the main channel. This is to get the correct tolerance. The number of spacers installed in a track can be between zero and four. If spacers are installed, do not remove them when you remove the track.
R R R R R R R (1) Install the TOOL-BACKSTOP SLAT (TRACKS 1, 2, 3, AND 4) (98D27804014000) (2) through the guide (3) on the applicable track (1): - on the LH wing, install the TOOL-BACKSTOP SLAT (2) on the inboard side of the track - on the RH wing, install the TOOL-BACKSTOP SLAT (2) on the outboard side of the track.
R R (2) Push the TOOL-BACKSTOP SLAT (2) against the rear stop (4) to disengage it from the track stop.
(3) Pull the track (1) from its installed position and remove it.
(4) Remove the TOOL-BACKSTOP SLAT (TRACKS 1, 2, 3, AND 4) (2) from the track (1).
TASK 27-84-61-400-004
Installation of the Slat Tracks 1 thru 4
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
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 safety barriers
No specific spring gage
No specific warning notice
98D27804014000 1 TOOL-BACKSTOP SLAT (TRACKS 1, 2, 3, AND 4)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-024 AIB AIMS 09-06-001
SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1 R SOLVENT GENERAL PURPOSE (Ref. 20-31-00) 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱8(60)
