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REFERENCE DESIGNATION
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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-84-62-991-002 Fig. 402
**ON A/C 301-399,
27-84-62-991-002-A Fig. 402A
**ON A/C ALL
27-84-62-991-004 Fig. 406
3. Job Set-up
__________
Subtask 27-84-62-941-056
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice(s) is in the cockpit to tell persons not to operate the slat controls.
(3)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
Subtask 27-84-62-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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PANEL DESIGNATION IDENT. LOCATION
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49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 Subtask 27-84-62-860-052
C. Aircraft Maintenance Configuration
(1)
Make sure that the adjustable access platform is below the applicable zone 510 or 610.
(2)
Make sure that the applicable slats have been removed:
-
for track 5 and 6 side-rollers (Ref. TASK 27-84-64-000-001)
-
for track 7 and 8 side-rollers (Ref. TASK 27-84-65-000-001)
-
for track 9 and 10 side-rollers (Ref. TASK 27-84-66-000-001)
-
for track 11 and 12 side-rollers (Ref. TASK 27-84-67-000-001).
(3)
Make sure that the applicable actuators have been removed:
-
for tracks 5, 6, 8, 10 and 12 (Ref. TASK 27-84-49-000-001)
-
for tracks 7, 9 and 11 (Ref. TASK 27-84-49-000-002).
(4)
Make sure that the applicable side rollers have been removed (Ref. TASK 27-84-61-000-002).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 402/TASK 27-84-62-991-002)
**ON A/C 301-399,
(Ref. Fig. 402A/TASK 27-84-62-991-002-A)
**ON A/C ALL
(Ref. Fig. 406/TASK 27-84-62-991-004)
Subtask 27-84-62-420-057
A. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Set the Track Datum use the GAUGE-SLAT TRACK SETTING (98D27804021000) as follows:
Slat Track 5 thru 12 - Zero Datum Tool
Figure 406/TASK 27-84-62-991-004
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NOTE : This procedure is only necessary where all the side rollers
____
are removed.
(a)
Install the applicable setting track (35).
(b)
Install and lock the two clamp assemblies (36) at the locations of the non-datum side-rollers.
(c)
Turn the thumb screws (37) equally until they stop.
(d)
Install the gage assembly (40) with the washers (22) and the bolts (21) at the location of the aft datum side-roller.
(e)
Turn the torque screw (38) on the gage assembly (40) until it stops. Lock it in position with the thumb screw (39).
(5) To calculate the thickness of the datum side-roller shims (23): NOTE : This procedure is only necessary where all the side rollers
____
are removed.
(a) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵8(89)
