(1)
Make sure that the ground service network is energized
(Ref. TASK 24-41-00-861-002)
(2)
Clean the component interface and/or the adjacent area.
(3)
Do an inspection of the component interface and/or the adjacent area.
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25-23-48Page 404
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
4. Procedure
_________
(Ref. Fig. 401/TASK 25-23-48-991-001)
Subtask 25-23-48-420-051
A. Installation of the Cove Light Panel (3)
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Engage the brackets (6) of the cove light panel (3) in the fitting (5).
(3)
Connect the bonding strap (8) to the cable socket (7).
(4)
Align the flange (2) with the rail (1).
(5) Engage the flange (2) on the rail (1). R
R (6) Make sure that the dimension 'X' is 10 +2 -2 mm (0.3937 +0.0787 -0.0787 in.).
R (7) Install the seal (4) if removed into the rail (1). Use PULLEY ASSEMBLY - SEALING CORD (98A25207503000).
5. Close-up
________
Subtask 25-23-48-862-050
A. De-energize the ground service network
(Ref. TASK 24-42-00-862-001)
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25-23-48Page 405
OVERHEAD STOWAGE COMPARTMENTS - DESCRIPTION AND OPERATION
_________________________________________________________
1.
General
_______ The overhead stowage compartments (OHSC) are installed above the left and right seat rows according to the cabin layout of the aircraft.
2.
Component Location
__________________
(Ref. Fig. 001, 002)
3.
Component Description
_____________________ (Ref. Fig. 001, 002) The overhead stowage compartments (OHSC) have a box structure and are of different lengths:
-spacer,
-1-frame pitch,
-2-frame pitch,
-3-frame pitch and
-4-frame pitch.
Each OHSC has: R - one or more doors with a handle/latch assembly for each door,
-a handgrip along its length,
-hinge mechanisms that attach the door to the OHSC,
-a gas filled damper strut on each hinge mechanism (spacer OHSC only on one
hinge) for a controlled door operation,
-upper attachment brackets,
-lower attachment brackets.
-mounting rails for the installation of the passenger service/information
unit (PSUI) and the emergency oxygen container (Ref. 25-25-11),
Brackets connect the OHSC to each other.
Brackets and turnbuckles attach the OHSC to the fuselage structure.
Cabin temperature control sensors are installed between the OHSC according
to the cabin layout. (Ref. 21-63-17).
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25-24-00Page 1
Overhead Stowage Compartments - Component Location
Figure 001
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Feb 01/98
CES
Overhead Stowage Compartment
Figure 002
EFF : ALL 25-24-00 Page 3
Feb 01/98
CES
OVERHEAD STOWAGE COMPARTMENTS - ADJUSTMENT/TEST
_______________________________________________
TASK 25-24-00-710-001
Adjustment of the Overhead Stowage-Compartment Doors
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power
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