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UF94200
EFFECTIVITY Page 174
ALL
25 - EQUIPMENT/FURNISHINGS
25-62-00 OFFWING ESCAPE SLIDE CYLINDER
REMOVAL/INSTALLATION
CONTENTS:
Removal
Installation
Test
TMUESFL01 LEVEL 3
EFFECTIVITY 25-62-00 Page 1
Mar 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 175
ALL
OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION
REMOVAL
WARNING
Make sure that the lockpin assembly is correctly
installed in the valve assembly head of the inflation
cylinder to prevent an accidental extension of the
escape slide.
The cylinder is pressurized with gas to 3000 psi
(207 bar).
The removal/installation procedures of the left and
right cylinders are almost identical.
ACCESS
Open the AFT cargo door.
Put the access platform in position.
Remove the access panels.
Open the circuit breakers.
Install the lockpin on the cylinder valve assembly.
NOTE: The lockpin is stowed in the stowage pocket.
CABLE ASSEMBLIES
Loosen the knurled sleeve nut and remove the two
collets.
Move the two cable assemblies apart.
ELECTRICAL CONNECTOR
Disconnect and put blanking caps on the electrical
connectors.
FLEXIBLE HOSE ASSEMBLY
Disconnect the flexible hose assembly from the bulkhead
union.
Put blanking plugs on the disconnected line ends.
CYLINDER REMOVAL
Remove and keep the bolt that supports the flexible
hose assembly.
Loosen the attach clamp screws.
Remove the inflation cylinder.
INSTALLATION
CYLINDER INSTALLATION
Make sure that the lockpin assembly is correctly
installed in the valve assembly head of the inflation
cylinder to prevent an accidental extension of the
escape slide.
Install the cylinder assembly in the support bracket.
Tighten the attach clamp screws when in position.
FLEXIBLE HOSE ASSEMBLIES
Put the flexible hose assembly in position and tighten
the bolt by hand.
Remove the blanking caps and connect the flexible hose
to the bulkhead union.
Tighten the bolt.
ELECTRICAL CONNECTOR
Remove the blanking caps and install the electrical
connector.
TMUESFL01-T01 LEVEL 3
EFFECTIVITY 25-62-00 Page 2
Mar 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 176
ALL
TMUESFL01-P01 LEVEL 3
OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION
EFFECTIVITY 25-62-00 Page 3
Mar 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 177
ALL
OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION
TEST
ADJUSTMENT
After test tool installation and setting the cursor
to zero, (adjusting the flexible assembly nuts if
necessary) set the emergency exit hatch in armed
position and remove it.
Remove the cap and connect the RELEASE TEST TOOL and
CABLE ESCAPE SLIDE adapter to the flexible control
assembly.
Set the cursor to zero.
Put the forward emergency exit-hatch in the armed
position and remove the hatch.
Make sure that the test tool cursor has moved to show
a minimum indication of 50 mm (1.9685 in.).
Adjust conduit, adjust nuts on the flexible control
assembly.
Make an adjustment of the conduit length.
Set the cursor on the test tool to zero.
CABLE ASSEMBLIES
Connect the two cable assemblies.
Install the two collets and tighten the knurled sleeve
nut.
FUNCTIONAL CHECK
Lift the door lever up to check that the resistance
and the play between the flexible control and release
cable assembly are satisfactory.
LOCKPIN ASSEMBLY
Remove the lockpin from the cylinder and put it in the
stowage pocket.
CLOSE UP
Install the access panels.
Remove the platform.
Close the cargo doors.
TMUESFL01-T01 LEVEL 3
EFFECTIVITY 25-62-00 Page 4
Mar 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 178
ALL
25 - EQUIPMENT/FURNISHINGS
25-62-00 OFFWING ESCAPE SLIDE INSTALLATION
CONTENTS:
Offwing Escape Slide Installation
TMUESFD01 LEVEL 3
EFFECTIVITY 25-62-00 Page 1
Jul 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS
UF94200
EFFECTIVITY Page 179
ALL
　
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