(4)
Assemble the decompression panel:
(a)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(b)
Clean the component interface and/or the adjacent area.
(c)
Do an inspection of the component interface and/or the adjacent area.
(d)
Put the latch assemblies (9) in position on the decompression panel (5).
(e)
Put the clamp (8) in position, and install the washers (7) and the screws (6).
(5)
Install the decompression-panel:
(a) Make sure that the decompression-panel (5) is clean and in the correct condition.
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25-68-41Page 430
(b)
Do an inspection of the component interface and/or the adjacent area.
(c)
Put the seal (10) in position on the decompression panel (5).
(d)
Put the decompression-panel (5) in position in the partition (3) and install it.
NOTE : Use a stable force over the full surface of the
____ decompression panel (1) when you push the decompression panel in the related opening of the ceiling panel (6).
(6) Put the protective panel (1) in position on the partition (3) and install the screws (2).
5. Close-up
________
Subtask 25-68-41-410-050
A. Close Access
(1)
Install the panels in the area where you have replaced the decompression panels:
-
in the passenger compartment
(Ref. TASK 25-23-44-400-001).
-
in the FWD cargo compartment at FR24
(Ref. TASK 25-54-11-400-001).
-
in the FWD cargo compartment
(Ref. TASK 25-54-12-400-002).
-
in the AFT cargo compartment
(Ref. TASK 25-55-12-400-002).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
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25-68-41Page 431
Decompression Panels in the Partition at FR24
Figure 406/TASK 25-68-41-991-007- 12 (SHEET 1)
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Aug 01/05
CES
Decompression Panels in the Partition at FR24
Figure 406/TASK 25-68-41-991-007- 22 (SHEET 2)
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Aug 01/05
CES
ACCESSORY COMPARTMENTS - DESCRIPTION AND OPERATION
__________________________________________________
1. General
_______ (Ref. Fig. 001) The accessory compartments are located on the inner or on the outer areas of the pressurized fuselage. The avionics compartments are in the pressurized area below the cockpit (above the nose landing-gear well). They are identified as the FWD, the lateral and the AFT avionics compartments. The compartments have:
-heat and sound insulation,
-maintenance lighting,
-air-cooled racks for the electrical and electronic equipment and their
related units. The nose landing-gear well is below the avionics compartment and stair bay, in the areas of Zones 123/124. The main landing-gear well is between the FWD and AFT cargo compartments, in the areas of Zones 147/148. Equipment compartments are located in the rear of the aircraft, between FR65 and FR80, in the areas of Zones 171/172, 311/312 and 313/314.
2. Component Location
__________________
A. Avionics Compartments
(1) Compartment Locations
(Ref. Fig. 002)
(a)
The FWD avionics compartment is between FR1 and FR9, in the areas of Zones 121/122. Access to the compartment is through the FWD avionics compartment door 811 and through the floor access panels in the cockpit.
(b)
The lateral avionics compartment is between FR9 and FR20, in the areas of Zones 125/126. Access to the lateral avionics compartment is through:
-
the left hand door 812 of the lateral avionics compartment,
-
the right hand door 822 of the lateral avionics compartment,
-
the floor access panels in the cockpit,
-
the floor access panels in the FWD utility area.
(c)
The AFT avionics compartment is between FR20 and FR24A, in the areas of Zones 127/128. Access to the AFT avionics compartment is through:
-
the right hand door 824 of the AFT avionics compartment,
-
the floor access panels in the FWD utility area,
-
the floor access panels in the FWD cabin area.
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