-
THE FLIGHT CONTROL SURFACES
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THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1. Reason for the Job
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Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific 1 ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE No specific 1 WARNING NOTICE
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
55-33-13-010-002 Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-410-002 Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-00-991-001 Fig. 601
3. Job Set-up__________
Subtask 55-33-00-865-050
A. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 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 AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 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
Subtask 55-33-00-860-050
B. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(2)
Put a WARNING NOTICE in the cockpit to tell persons not to operate the flight controls.
(3)
Put an ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE in position at the vertical stabilizer trailing edge.
4. Procedure
_________
(Ref. Fig. 601/TASK 55-33-00-991-001)
Subtask 55-33-00-210-050
A. Do an inspection of the vertical stabilizer trailing edge access-panels for missing fasteners
R R (1) Make sure that the studs (4) and the washers (5) are installed and in the correct condition.
(2) If necessary, open/remove the trailing edge access-panels (Ref. TASK 55-33-13-010-002):
(a) Make sure that the receptacles (1) are installed and in the correct condition.
(b) Replace/install the receptacles (1) as necessary.
R R (c) Make sure that the washers (3) and the snap-rings (2) are installed at the studs (4) and in the correct condition.
R R (d) If necessary replace/install the washers (3) and/or the snap-rings (2).
(3) Replace the missing fasteners within 100 flight hours.
R R (a) Make sure that the new studs (4) have a washer (5) and (3) and a snap-ring (2).
NOTE : You can temporarily replace a missing fastener by a____ fastener from another panel. Make sure that the replacement fastener has the same size and the same length as the missing one. Obey the criteria in the subsequent table when you remove a fastener from any other panel.
R Vertical Stabilizer Trailing Edge Access-Panels Figure 601/TASK 55-33-00-991-001- 12 (SHEET 1)
1EFF : 1 1 1CES ALL 1 111 55-33-00 Page 604 Aug 01/03
R Vertical Stabilizer Trailing Edge Access-Panels Figure 601/TASK 55-33-00-991-001- 22 (SHEET 2)
1EFF : 1 1 1CES ALL 1 111 55-33-00 Page 605 Aug 01/03
|-------------|----------------------------------|----------------------------| | Panel | Vertical Stabilizer Missing | Maximum Quantity of | | Designation | Fasteners Description | Missing Fasteners | | | (Refer to the No. 1 zones on the | per Panel | | | figure) | | |-------------|----------------------------------|----------------------------| | 325EL | One missing fastener permitted. | Seven missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325ER | One missing fastener permitted. | Seven missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325DL | One missing fastener permitted. | Five missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325DR | One missing fastener permitted. | Six missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325CL | One missing fastener permitted. | Four missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325CR | One missing fastener permitted. | Four missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325BL | One missing fastener permitted. | Four missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| | 325BR | One missing fastener permitted. | Four missing fasteners | | | | permitted. | |-------------|----------------------------------|----------------------------| 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 STABILIZERS 安定面(87)
