(1)
Remove the nuts (32), the washers (31) and (30) and the screws (29).
(2)
Remove the pin-locks (20), the washers (19) and the pins (18).
(3)
Remove the nuts (50), the washers (49), (23) and the screws (22).
(4)
Remove the nut (48), the washer (47), the screw (46) and disconnect the bonding strap (6).
(5)
Remove the nut (27), the split-ring (9) and the washers (8) and (28).
(6)
Record the position and the number of the washers (26) and (28) for the installation procedure .
(7)
Support the spacer bin and remove the pin (7), the screw (24), the washers (25), (26), (28) and the spacer bin.
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R R Spacer Bin at FR38/FR39 Figure 404/TASK 25-24-41-991-013
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TASK 25-24-41-400-001
Installation of the Overhead Stowage Compartments
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
21-24-19-400-001 Installation of the Individual Air outlet 4150 HM 23-36-34-400-001 Installation of the System Control Unit (SCU) 23-73-64-400-001 Installation of the Reading Light 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
25-23-41-400-001 Installation of the Ceiling Panels
25-23-48-400-001 Installation of the Cove Light Panels
R 25-24-00-710-002 Adjustment of the Overhead Stowage-Compartment (OHSC) 25-25-11-400-001 Installation of the Filler Panel(s) of the Passenger
Service/Information Unit(s) (PSIU) 33-21-11-400-001 Installation of the Ballast Unit and Lampholder 1LG1 35-21-41-400-001 Installation of the Emergency Oxygen Containers 25-24-41-991-001 Fig. 401 25-24-41-991-005 Fig. 402 25-24-41-991-012 Fig. 403 25-24-41-991-013 Fig. 404
3. Job Set-up
__________
Subtask 25-24-41-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001)
(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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(4)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(5)
Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 25-24-41-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL SERVICE IDENT. LOCATION -------------------------------------------------------------------------------2000VU CABIN LIGHT POWER-WINDOW FWD 300LG H01 2000VU CABIN LIGHT POWER-WINDOW AFT 301LG H03 2000VU CABIN LIGHT POWER-WINDOW AFT 302LG H04 2000VU CABIN LIGHT POWER-WINDOW FWD 303LG H02 2000VU CABIN LIGHT POWER-CEILING AFT 304LG H07 2000VU CABIN LIGHT POWER-CEILING FWD 305LG H05 2000VU CABIN LIGHT POWER-CEILING FWD 306LG H06 2000VU CABIN LIGHT POWER-CEILING AFT 307LG H08
Subtask 25-24-41-210-051
C. Make an inspection of the component interface and/or the adjacent area.
(1) Make sure that the work area is clean and clear of tools and other items.
4. Procedure
_________
Subtask 25-24-41-420-050
A. Installation of the 2,3 and 4-frame stowage compartments.
(Ref. Fig. 401/TASK 25-24-41-991-001)
(1) Install the upper attachments.
(a) Put the stowage compartment in position and install the pins (7) and (10) (Ref. Detail "A" and "B") or/and the screws (24), (36) and the washers (25), (26) and (28) (Ref. Detail "H" and "J").
NOTE : You must install the washers as recorded in the removal
____
procedure.
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(b) Install the washers (8) and the split-rings (9) and/or the washers (25), (26) and the nuts (27).
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