2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 001-003, 051-054,
21-61-00-991-006 Fig. 801
**ON A/C ALL
3. Job Set-up
__________
Subtask 21-61-00-860-054
A. Aircraft Maintenance Configuration
(1) Make sure that you can get access to the components for which repair or replacement is necessary.
4. Procedure
_________ Subtask 21-61-00-350-051
A. Replacement of a Shouldered Bushing - Ram Air Inlet
(1) Use an applicable method and remove the shouldered bushing (4) from the lever (12).
(a) Use an applicable method and install the shouldered bushing (4) in the lever (12).
NOTE : Make sure that you do not distort or damage the lever when
____
you do this.
(b) The procedure is the same for the shouldered bushing (5). Subtask 21-61-00-350-052
B. Replacement of a Bushing or Spacer - Ram Air Inlet
(1) Use an applicable method and remove the bushing (3) or the spacer (6) from the bracket (15) or the lever (12).
(a) Use an applicable method and install the bushing (3) or the spacer (6) in the bracket (15) or the lever (12).
NOTE : Make sure that:
____
-you do not distort or damage the bracket or the lever when you do this.
-the ends of the bushing (3) are flush with the sides of the bracket (15).
-you have the 1.0 mm (0.0393 in.) dimension 'A' at one end of the spacer (6).
1EFF : ALL 1 21-61-00Page 802 1 1 May 01/98R 1 1 1CES 1
R **ON A/C 001-003, 051-054,
Subtask 21-61-00-350-053
C. Replacement of a Shouldered Bushing - Ram Air Outlet
(Ref. Fig. 801/TASK 21-61-00-991-006)
(1) Use an applicable method and remove the shouldered bushing (3) from the lever (5).
(a) Use an applicable method and install the shouldered bushing (3) in the lever (5).
NOTE : Make sure that you do not distort or damage the lever when
____
you do this.
(b) The procedure is the same for the shouldered bushing (4).
R 1EFF : 001-003, 051-054, 1 21-61-00Page 803 1 1 May 01/05 1 1 1CES 1
Attachment and Linkage Components - Ram Air Outlet
Figure 801/TASK 21-61-00-991-006
R 1EFF : 001-003, 051-054, 1 21-61-00Page 804 1 1 May 01/05 1 1 1CES 1
TASK 21-61-00-300-002 Ram Air Outlet-Flap Guide Plates - Replacement of Sheared or Loose Rivets NOTE : You can only do the repair if the diameter of the holes for the
____ replacement rivets is not more than 4.1mm (0.1614 in.)
1.
Reason for the Job
__________________
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)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-61-52-000-002 Removal of the Ram-Air Outlet Flap 21-61-52-400-002 Installation of the Ram-Air Outlet Flap 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure 53-35-13-400-002 Installation of the Quick-Release Access Panels on the Belly Fairing Structure 21-61-00-991-007 Fig. 802
3. Job Set-up
__________ Subtask 21-61-00-861-058
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
R 1EFF : 001-003, 051-054, 1 21-61-00Page 805 1 1 May 01/05 1 1 1CES 1 Subtask 21-61-00-865-067
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9HH
122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21 122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC 4HH Y19 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
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 AIR CONDITIONING 空调 5(14)
