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时间:2011-03-26 00:04来源:蓝天飞行翻译 作者:admin
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 **ON A/C ALL
 A. Entrance Lighting 
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-399, 401-499,
 (Ref. Fig. 003) 
R  **ON A/C 106-149, 
R  (Ref. Fig. 003A) 
R  **ON A/C ALL
 The entrance lighting consists of fluorescent lamps with ballast units installed in the ceiling panels at the forward and aft entrances. Two fluorescent lamps are installed in the LH and RH ceiling panels at each entrance. The operation is identical to the cabin lighting.
 (1) The entrance lighting at entrance 1 LH is automatically dimmed to DIM 2 level (10 %) whenever the cockpit door is opened with the engines running.

 

 (2) The CIDS directors 101RH and 102RH receive one signal from the engine oil-pressure system and another signal from the cockpit door microswitch. The directors 101RH and 102RH transmit their output signal to the DEU which controls the entrance 1 LH fluorescent lamp with ballast unit. The DEU provides a DIM 2 signal and the light dims to 10 % intensity.


 Attendant Panels - Component Location
 Figure 006
 1EFF :  211-299,  1  33-21-00 Page 46 
1  1  Aug 01/05
 1  1
 1CES  1

 

 Attendant Panels - Component Location
 Figure 006A
 1EFF :  301-399,  1  33-21-00 Page 47 
1  1  Aug 01/05
 1  1
 1CES  1

 

 Ceiling & Window Lighting Strips
 Figure 007
 1EFF :  211-299,  1  33-21-00 Page 48 
1  1  Aug 01/05
 1  1
 1CES  1

 

 Ceiling & Window Lighting Strips
 Figure 007A
 1EFF :  301-399,  1  33-21-00 Page 49 
1  1  Aug 01/05
 1  1
 1CES  1

 

 GENERAL ILLUMINATION - ADJUSTMENT/TEST
______________________________________ TASK 33-21-00-710-001 Operational Test of the General Illumination WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.

 1.
 Reason for the Job

__________________
 To make sure that the cabin general lighting operates correctly.


 2.
 Job Set-up Information


______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  21-31-34-000-001 Removal of the Cabin Pressure Controller (11HL,12HL) 23-73-00-861-001 Energize the Cabin Intercommunication Data System (CIDS) 23-73-00-862-001 De-energize the Cabin Intercommunication Data System (CIDS) 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
 3. Job Set-up
__________
 Subtask 33-21-00-861-050

 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).


 Subtask 33-21-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
 49VU COM/CIDS/DEU A ESS/LINE 2 155RH 49VU COM/CIDS/DEU A ESS/LINE 1 154RH **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-399, G05G04
 49VU COM/CIDS/DEU B/ESS **ON A/C 001-049, 051-099, 101-105, 201-299, 153RH  G03
 49VU COM/CIDS/DIR 1 AND 2/ESS **ON A/C ALL 150RH  G02
R  49VU ENGINE/2/FADEC A/AND EIU 2 49VU ENGINE/1/FADEC A/AND EIU 1 **ON A/C 106-149, 151-199, 301-399, 401-499, 2KS2 2KS1  A05A04 
49VU COM DIR ESS/1 **ON A/C 001-049, 051-061, 101-105, 201-203, 150RH  G01
 121VU COM NAV/CIDS/FWD ATTND/PNL **ON A/C 001-049, 051-099, 101-105, 201-299, 170RH  M14
 121VU COM NAV/CIDS/DEU A NORM/R AFT 121VU COM NAV/CIDS/DEU A NORM/L AFT 121VU COM NAV/CIDS/DEU A NORM/R MID 121VU COM NAV/CIDS/DEU A NORM/L MID  168RH 167RH 166RH 165RH  M13M12M11M10

 

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
121VU COM NAV/CIDS/DEU A NORM/R FWD 121VU COM NAV/CIDS/DEU A NORM/L FWD 121VU COM NAV/CIDS/DEU B/NORM  164RH 163RH 162RH  M09M08M07
 
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