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时间:2010-06-06 21:52来源:蓝天飞行翻译 作者:admin
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UF94200
EFFECTIVITY Page 102
ALL
TMUESCB01-P01 LEVEL 3
CABIN PANEL REMOVAL/INSTALLATION - CEILING PANELS
EFFECTIVITY 25-20-00 Page 3
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 103
ALL
CABIN PANEL REMOVAL/INSTALLATION
OVERHEAD STOWAGE COMPARTMENTS
Before removing the overhead stowage compartment :
- the ceiling panels and the cove light panels
adjacent to the stowage compartment,
- the emergency oxygen container,
- the Passenger Service Information Unit,
must be removed.
On the stowage compartment lower side, remove the bolts
and washers on support plates "F" and junction plates
"D".
Disconnect the turnbuckles at support plates "F" and
attachment point "G".
Support the stowage compartment.
Inside the compartment, remove the pin at upper
attachment points "A" and "H",
Remove the overhead stowage compartment.
TMUESCB01-T02 LEVEL 3
EFFECTIVITY 25-20-00 Page 4
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 104
ALL
TMUESCB01-T02 LEVEL 3
CABIN PANEL REMOVAL/INSTALLATION - OVERHEAD STOWAGE COMPARTMENTS
EFFECTIVITY 25-20-00 Page 5
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 105
ALL
CABIN PANEL REMOVAL/INSTALLATION
PSIUs
To remove the Passenger Service Information Unit, apply
the following the procedure:
Open and safety the corresponding circuit breakers,
Remove the mounting seal each side of the PSIU,
Push the PSIU up to release the hinges from the mounting
rail,
Disconnect the electrical connectors,
Remove the PSIU.
NOTE : For installation use the tool pulley assembly
to insert the rubber seal properly.
TMUESCB01-T03 LEVEL 3
EFFECTIVITY 25-20-00 Page 6
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 106
ALL
TMUESCB01-P03 LEVEL 3
CABIN PANEL REMOVAL/INSTALLATION - PSIUs
EFFECTIVITY 25-20-00 Page 7
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 107
ALL
CABIN PANEL REMOVAL/INSTALLATION
COVE LIGHT PANELS
To remove the cove light panel, apply the following
procedure :
- Remove the seal from the rail at the junction
with the overhead stowage compartment,
- Move the panel to disconnect it from the rail,
- Remove the bonding strap,
- Lift the panel, and pull it out.
TMUESCB01-T04 LEVEL 3
EFFECTIVITY 25-20-00 Page 8
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 108
ALL
CABIN PANEL REMOVAL/INSTALLATION - COVE LIGHT PANELS
TMUESCB01-P04 LEVEL 3
EFFECTIVITY 25-20-00 Page 9
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 109
ALL
CABIN PANEL REMOVAL/INSTALLATION
UPPER SIDEWALL PANELS
To remove the upper sidewall panel apply the following
procedure :
- First, remove the passenger seats in the area
of the upper sidewall panel which is to be
removed,
- Remove the decor cover and the inner pane from
the window,
- Remove the 2 screws fitted on each window,
- Pull out the lining strips,
- Lift the panel to release it from the mounting
brackets and remove it.
LOWER SIDEWALL PANELS
To remove the lower sidewall panel, apply the following
procedure :
- Use a punch to release the center pins of the
quick release pins,
- Pull the lower edge of the panel away from the
compartment wall,
- Pull the panel down and remove the fasteners
from the attachment fittings,
- Remove the panel.
TMUESCB01-T05 LEVEL 3
EFFECTIVITY 25-20-00 Page 10
Jul 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 110
ALL
CABIN PANEL REMOVAL/INSTALLATION - UPPER AND LOWER SIDEWALL PANELS
TMUESCB01-P05 LEVEL 3
EFFECTIVITY 25-20-00 Page 11
 
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