-lift up the spring loaded cover,
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25-45-00Page 6
R R Bi-folding Door Figure 003
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CES
Lavatory Single Blade Door - Emergency Opening from the Outside Figure 004
R EFF : 001-049, 051-099, 101-105, 151-199, 25-45-00Page 8 201-217, May 01/05
CES
Lavatory Single Blade Door - Emergency Opening from the Outside Figure 004A
R EFF : 106-149, 218-299, 301-399, 401-499, 25-45-00Page 9 Aug 01/05
CES R Lavatory Bi-folding Door - Emergency Opening from the outside R Figure 005
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25-45-00Page 10
Feb 01/05 CES
-slide the knob to the side until the VACANT indicator is showm,
-push the door open and disengage the latches,
-fold the door to the fully open position CABINET - SERVICE - REMOVAL/INSTALLATION
________________________________________
TASK 25-45-12-000-001
Removal of the Service Cabinet
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific blanking caps
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
21-24-19-000-001 Removal of the Individual Air Outlet 4150 HM 23-73-11-000-001 Removal of the Area Call Panel (ACP) 340RH 23-73-51-000-001 Removal of the Loudspeaker 23-73-62-000-001 Removal of the Return To Seat Sign 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 24-42-00-861-001 Energize the Ground Service Network from the External Power
**ON A/C 001-003, 051-052,
25-45-12-991-001 Fig. 401 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
25-45-12-991-002 Fig. 402
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25-45-12Page 401
**ON A/C ALL
3. Job Set-up
__________
Subtask 25-45-12-861-050
A. Aircraft Maintenance Configuration
(1)
Energize the ground service network
(Ref. TASK 24-42-00-861-001).
(2)
Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
4. Procedure
_________ R **ON A/C 001-003, 051-052,
Subtask 25-45-12-020-050
A. Removal of the Service Cabinet
(Ref. Fig. 401/TASK 25-45-12-991-001)
(1)
Open the service cabinet door (10) and remove the dispenser (14).
(2)
If installed, remove the screws (6), the washers (7), the nut (9) and the lanyard (8).
(3)
Remove the screws (4) and the washers (5) from the upper part (1) of the service cabinet.
(4)
Remove the upper part (1) of the service cabinet and remove these items:
-
the loudspeaker (2) (Ref. TASK 23-73-51-000-001),
-
the individual air outlet (3) (Ref. TASK 21-24-19-000-001).
(5)
Remove the screws (11), the washers (12), the hinge (13) and the service cabinet door (10).
(6)
Remove the screws (19) and the washers (20).
(7)
Disconnect the call button (16) (Ref. TASK 23-73-11-000-001).
(8)
Disconnect the return to seat sign (17) (Ref. TASK 23-73-62-000-001).
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25-45-12Page 402
R Service Cabinet Figure 401/TASK 25-45-12-991-001
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CES
(9) Disconnect the electrical connector (21) from the razor socket (18).
(10) Put blanking caps on the disconnected electrical connectors.
(11) Remove the lower part (15) of the service cabinet. R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 25-45-12-020-050-A
A. Removal of the Service Cabinet
(Ref. Fig. 402/TASK 25-45-12-991-002)
(1)
Open the service cabinet door (10) and remove the dispenser (14).
(2)
Remove the screws (6), the washers (7) and the nuts (9) from the upper and lower door stops (8).
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