(2)
Do the interface and power-up test of the CIDS. (Ref. TASK 23-73-00-740-010)
5. Close-up
________ Subtask 33-27-41-862-050
A. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002)
Subtask 33-27-41-410-050
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the warning notice(s).
(3)
Close the access door 121AL.
(4)
Remove the access platform(s).
R 1EFF : 106-149, 301-399, 401-499, 1 33-27-41Page 412 1 1 Aug 01/05 1 1 1CES 1
CARGO AND SERVICE COMPARTMENTS - DESCRIPTION AND OPERATION
__________________________________________________________
1. General
_______
The cargo and service compartment lighting-system provides illumination to
the service area, forward and aft cargo compartment, avionics compartment
and wheel wells. A maintenance outlet is installed in the air conditioning
duct and accessory compartment.
2. System Description
__________________
A. Service Area Lighting
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-224,
(Ref. Fig. 001) R **ON A/C 106-149, 225-299, 301-399, 401-499,
(Ref. Fig. 001A)
**ON A/C ALL
The service area lighting comprises the lighting installation of the equipment compartment in Section 19 and the APU compartment. Electrical outlets are provided for portable maintenance lights in Section 19. The lights and outlets are supplied with 28VDC.
B. Air Conditioning Duct and Accessory Compartment
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-224,
(Ref. Fig. 001) R **ON A/C 106-149, 225-299, 301-399, 401-499,
(Ref. Fig. 001A)
**ON A/C ALL
A single outlet is installed for a portable maintenance light. The outlet is supplied with 28VDC.
Service Compartment Lights
Figure 001
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 33-30-00Page 2 1201-224, 1May 01/05 1 1 1CES 1
Service Compartment Lights
Figure 001A
R 1EFF : 106-149, 225-299, 301-399, 401-499, 1 33-30-00Page 3 1 1 Aug 01/05 1 1 1CES 1
C. Forward and Aft Cargo-Compartment Lighting
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 002)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 002A)
**ON A/C 301-399,
(Ref. Fig. 002B)
**ON A/C ALL
The fluorescent lamps illuminate the cargo compartment. They are installed in the ceiling. A loading light is installed in each compartment. Electrical outlets are provided for portable maintenance lights. The fluorescent lamps are supplied with 115VAC, the electrical outlets and loading lights are supplied with 28VDC.
D. Avionics Compartment Lighting (Ref. Fig. 003) The system comprises a number of lights and electrical maintenance outlets. The lights are supplied with 28VDC. A number of outlets are supplied with 28VDC and the remainder with 115VAC. The lights may come on automatically when an equipment bay door is opened. You can also switch them on with the control switch in the cockpit.
E. Wheel Well Lighting
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
(Ref. Fig. 004)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
R Post SB 92-1032 For A/C 001-049,051-099,101-105,151-199,201-220,
R (Ref. Fig. 004A)
Cargo Compartment Lights
Figure 002
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 33-30-00Page 5 1 1 May 01/05 1 1 1CES 1
Cargo Compartment Lights
Figure 002A
R 1EFF : 151-199, 401-499, 1 33-30-00Page 6 1 1 Aug 01/05 1 1 1CES 1
Cargo Compartment Lights
Figure 002B
R 1EFF : 301-399, 1 33-30-00 Page 7
1 1 Feb 01/05
1 1
1CES 1
Avionics Compartment Lights Figure 003
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Wheel Well Lights
Figure 004
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 33-30-00Page 9 1201-220, 1May 01/05 1 1 1CES 1R Wheel Well Lights R Figure 004A
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 33-30-00Page 10 1201-220, 1Aug 01/05 1 1 1CES 1
R **ON A/C ALL
The system comprises the lighting installation of the wheel wells and the hydraulic compartment. Electrical outlets are provided in the wheel wells for maintenance purposes. A switch in the left-hand wheel well controls the lights.
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