Subtask 52-41-23-020-050
A. Removal of the Maintenance Door 314AR
(1)
Remove the nut (10), the bolt (6), the washer (9) and disconnect the bonding jumper (7) from the bonding angle (8).
(2)
Hold the maintenance door (5) and remove the screws (1) and the washers (2).
(3)
Remove the retainer (3), the seal (4) and the maintenance door (5) from the fuselage hinge (11).
1EFF : ALL 1 52-41-23Page 402 1 1 Aug 01/05 1 1 1CES 1
Maintenance Door 314AR
Figure 401/TASK 52-41-23-991-001
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 52-41-23Page 403 1201-210, 1May 01/05 1 1 1CES 1
Maintenance Door 314AR
Figure 401A/TASK 52-41-23-991-001-A
R 1EFF : 106-149, 159-199, 211-299, 301-399, 1 52-41-23Page 404 1401-499, 1Aug 01/05 1 1 1CES 1 TASK 52-41-23-400-001
Installation of the Maintenance Door 314AR
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific warning notice
No specific access platform 3.7 m (12 ft. 2 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
51-75-13-916-001 Repair to a layer of Moisture-Removing Oil
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
52-41-23-991-001 Fig. 401 R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
52-41-23-991-001-A Fig. 401A
1EFF : ALL 1 52-41-23Page 405 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
3. Job Set-up
__________
Subtask 52-41-23-860-051
A. Aircraft Maintenance Configuration
(1)
Make sure that the warning notice is in the flight compartment to tell persons not to start the APU.
(2)
Make sure that the access platform is in position below the maintenance door 314AR.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
(Ref. Fig. 401/TASK 52-41-23-991-001) R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
(Ref. Fig. 401A/TASK 52-41-23-991-001-A)
**ON A/C ALL
Subtask 52-41-23-420-052
A. Installation of the Maintenance Door 314AR
(1)
Put the maintenance door (5), the seal (4) and the retainer (3) on the fuselage hinge (11) and install the washers (3) and the screws (2).
(2)
Put the bonding strap (7) on the bonding angle (8) and attach it with the screw (9), the washer (8) and the nut (6) (Ref. TASK 20-28-00-912-004).
1EFF : ALL 1 52-41-23Page 406 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 52-41-23Page 407 1 1 Feb 01/02 1 1 1CES 1 DOOR - BLUE HYDRAULIC SYSTEM ACCESS - REMOVAL/INSTALLATION
Subtask 52-41-23-910-050
B. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Protect the inner surface of the maintenance door (5) (Ref. TASK 51-75-13-916-001).
(3) Remove the warning notice(s).
5. Close-up________
Subtask 52-41-23-410-050
R A. Close Access
R R (1) Move the maintenance door 314AR in its closed position and attach it with the quick-release fasteners.
(2) Remove the access platform(s).
__________________________________________________________
TASK 52-41-24-000-001
Removal of the Access Door of the Blue Hydraulic System (197FB)
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.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
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 DOORS 舱门6(166)
