-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
55-13-11-400-001 Installation of the THS Trailing Edge Access Panels 55-15-11-400-001 Installation of the Apron 333AT/333AB/343AT/343AB
**ON A/C 001-003, 051-054,
53-56-11-991-001 Fig. 401 R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
53-56-11-991-001-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-56-11-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft is in the same configuration as for the removal task.
(2)
Make sure that the warning notice is in position to tell persons not to move the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______ BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
EFF : ALL
53-56-11Page 415
Subtask 53-56-11-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
**ON A/C 001-003, 051-054,
(Ref. Fig. 401/TASK 53-56-11-991-001)
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 53-56-11-991-001-A)
EFF : ALL
53-56-11Page 416
**ON A/C ALL
Subtask 53-56-11-914-050
A. Preparation for Installation:
(1)
Remove the sealant from the links with a nonmetallic scraper.
(2)
Clean the links, component interface and the adjacent area with CLEANING AGENTS (Material No. 11-003).
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE
_______
SPECIAL MATERIAL.
THIS MATERIAL IS DANGEROUS.
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(3)
Examine the links, componenents, component interface and adjacent area for good condition.
(4)
Apply COMMON GREASE (Material No. 04-004) to the new O-rings (31) and put them in position in the sleeve (18).
(5)
Apply COMMON GREASE (Material No. 04-004) to the bushes (4), the sleeves (6), the Y-bolt (17), the sleeve (18), the bushes (20), the washers (21) and the bolt (24).
R **ON A/C 001-003, 051-054,
Subtask 53-56-11-420-050
B. Installation:
(1)
Install the bolts (8) in the link (19).
(2)
Put the links (19) and (23) in position.
EFF : ALL
53-56-11Page 417
(3)
Apply SEALANTS (Material No. 09-013) to the contact surfaces of the spacer (13) and the washers (10).
(4)
Install one of the washers (10) on the bolt (24) and push the bolt
(24) through the link (19), spacer (13) and the link (23). 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身3(134)
