R Monitor
R Figure 401/TASK 23-72-22-991-002
1EFF : 216-216, 1 23-72-22 Page 404
1 1 Nov 01/04
1 1
1CES 1
Monitor
R Figure 402/TASK 23-72-22-991-001
1EFF : 216-216, 1 23-72-22 Page 405
1 1 Nov 01/04
1 1
1CES 1
**ON A/C 216-216,
TASK 23-72-22-400-001
R Installation of the Cockpit-Door Surveillance-System Monitor (10RA)
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
23-72-00-710-001 24-41-00-861-002 24-41-00-862-002 Operational Test of the Anti-Hijack Camera-Monitoring-SystemEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External Power
R **ON A/C 216-216,
R Post SB 23-1208 For A/C 216-216,
R R 23-72-22-991-002 23-72-22-991-001 Fig. 401 Fig. 402
1EFF : 216-216, 1 23-72-22Page 406 1 1 Nov 01/04 1 1 1CES 1 1EFF : 216-216, 1 23-72-22Page 407 1 1 Nov 01/04 1 1 1CES 1 1EFF : 216-216, 1 23-72-22Page 408 1 1 Nov 01/04 1 1 1CES 1
**ON A/C 216-216,
3. Job Set-up__________
**ON A/C 216-216,
Post SB 23-1208 For A/C 216-216,
Subtask 23-72-22-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the ground service network is energized (Ref. TASK 24-41-00-861-002)
Subtask 23-72-22-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU DOORS/CKPT/VIDEO/SPLY 15RA T16
**ON A/C 216-216,
4. Procedure_________
R
R **ON A/C 216-216,
R Post SB 23-1208 For A/C 216-216,
R Subtask 23-72-22-710-052
R R A. Installation of the Monitor or Hinge Assembly:
R R (1) If you want install the Monitor only: - Do the paragraph B.
R R (2) If you want install the Hinge Assembly: - Do the paragraph C.
R Subtask 23-72-22-420-053
R B. Installation of the Monitor
R (Ref. Fig. 401/TASK 23-72-22-991-002)
R (1) Do a visual inspection of the component interface and/or the adjacent
R area.
R (2) Clean the component interface and/or the adjacent area.
R (3) Remove the blanking caps from the electrical connectors.
R (4) Make sure that the electrical connectors are clean and in the correct
R condition.
R (5) Install the Monitor (1) with the screws (3) to the hinge assembly (2)
R and TORQUE the screws (3) to 0.300 m.daN (26.54 lbf.in).
R Subtask 23-72-22-420-054
R C. Installation of the Hinge Assembly:
R (1) Do a visual inspection of the component interface and/or the adjacent
R area.
R (Ref. Fig. 402/TASK 23-72-22-991-001)
R (2) Clean the component interface and/or the adjacent area.
R (3) Install the Hinge Assembly (1) with the washers (4) and the screws
R (5) to the mounting plate (3).
R (4) Remove the blanking caps from the elevtrical connectors.
R (5) Make sure that the electrical connectors are clean and in the correct
R condition.
R (6) Connect the electrical connector (2).
Subtask 23-72-22-865-052
R D. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
15RA
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 Communications 通訊3(35)
