25 EQUIPMENT_FURNISHINGS

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SINGLE AISLE 
 TECHNICAL TRAINING MANUAL 
 MAINTENANCE COURSE - T1 (V2500-A5/ME) 
 EQUIPMENT/FURNISHINGS 
This document must be used for training purposes only
Under no circumstances should this document be used as a reference
It will not be updated.
All rights reserved
No part of this manual may be reproduced in any form,
by photostat, microfilm, retrieval system, or any other means,
without the prior written permission of AIRBUS S.A.S.
EQUIPMENT/FURNISHINGS
GENERAL
Equipment Furnishings Level 2 (2) . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
COCKPIT
Cockpit Emergency Equipment Presentation (1) . . . . . . . . . . . . . . . . 30
Cockpit Seats Description/Operation (3) . . . . . . . . . . . . . . . . . . . . . . 32
Sliding Windows Description/Operation (3) . . . . . . . . . . . . . . . . . . . 36
Cockpit Escape Rope D/O (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38
PASSENGER COMPARTMENT
Typical Galley Installation D/O (3) . . . . . . . . . . . . . . . . . . . . . . . . . . 40
Typical Lavatory Installation D/O (3) . . . . . . . . . . . . . . . . . . . . . . . . 48
Passenger and Attendant Seats D/O (3) . . . . . . . . . . . . . . . . . . . . . . . 54
Cabin Panel Removal and Installation (3) . . . . . . . . . . . . . . . . . . . . . 70
EMERGENCY EQUIPMENT
Pax Door Escape Slide Deployment/Description (3) . . . . . . . . . . . . . 92
Pax Door Escape Slide Disconnection (3) . . . . . . . . . . . . . . . . . . . . . 94
Pax Door Escape Slide Installation (3) . . . . . . . . . . . . . . . . . . . . . . . . 96
Pax Door ESC SLD/Raft Deployment/Desc.(3)(option) . . . . . . . . . 100
Pax Door ESC SLD/Raft Disconnection (3) (option) . . . . . . . . . . . 102
Pax Door ESC SLD/Raft Installation (3) (option) . . . . . . . . . . . . . . 104
Offwing Escape Slide Deployment/Description (3) . . . . . . . . . . . . . 108
Offwing Escape Slide Removal (3) . . . . . . . . . . . . . . . . . . . . . . . . . 110
Offwing Escape Slide Cylinder Removal & INSTL(3) . . . . . . . . . . 114
Offwing Escape Slide Installation (3) . . . . . . . . . . . . . . . . . . . . . . . 132
EMER Exit ESC SLD Deployment/Descr. (3) (A321) . . . . . . . . . . 136
EMER Exit ESC SLD Disconnection (3) (A321) . . . . . . . . . . . . . . 140
Pax Door ESC SLD/Raft Inflation CYL CHK(3)(option . . . . . . . . . 142
Offwing ESC SLD Inflation Cylinder Check (3) . . . . . . . . . . . . . . . 144
Offwing ESC SLD Release Mechanism Description(3) . . . . . . . . . 156
CARGO COMPARTMENTS
Cargo Loading Operation (3) (option) . . . . . . . . . . . . . . . . . . . . . . . 164
Cargo Bulk Loading D/O (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 180
Draining System D/O (3) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 186
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TABLE OF CONTENTS May 11, 2006
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
SYSTEM OVERVIEW
The equipment and furnishings are located in different compartments:
- the cockpit,
- the passenger compartment,
- the cargo compartment.
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SYSTEM OVERVIEW
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
SYSTEM OVERVIEW (continued)
CABIN PANEL LAYOUT
The cabin interior is equipped with removable panels. The lining
design allows cabin customization. The lower side wall panels are
mounted between the cabin floor and the upper side wall panels. They
are equipped with rapid decompression doors. The upper side wall
panels are mounted on the side of the cabin. They include the window
contour. Inner window panels and sun visors are installed on to the
window frame. The cover light panels cover the space between the
upper side wall panels and the overhead stowage compartments.
The cover light panels are removable to replace cabin lights.
The overhead stowage compartments are installed above the cabin
seat rows. They extend from the first seat row to the last seat row on
the left and right hand side of the cabin. The overhead stowage
compartments are of different sizes and are arranged to suit the cabin
layout.
Removable ceiling panels are mounted in the cabin. They are installed
over the full length of the cabin and the utility areas.
The passenger service information units comprise the Passenger
Service Units (PSUs) and Passenger Information Units (PIUs).
They are installed in the service channel, above the seat rows. The
PSUs and PIUs have different lengths depending on the aircraft
furnishing configuration. These units are:
- information panel,
- attendant call panel,
- emergency oxygen mask and generator container,
- reading light panel,
- individual air outlet panel.
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SYSTEM OVERVIEW - CABIN PANEL LAYOUT
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
SYSTEM OVERVIEW (continued)
PASSENGER DOOR ESCAPE SLIDE
The forward and aft cabin doors are equipped with either a single lane
escape slide (as shown on the picture) or a slide raft.
The inflation and deployment is automatically initiated when the cabin
door is opened in the armed mode. if the escape slide does not inflate
automatically, the red manual inflation handle located on the right
hand side of the gird bar must be pulled.
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SYSTEM OVERVIEW - PASSENGER DOOR ESCAPE SLIDE
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
SYSTEM OVERVIEW (continued)
EMERGENCY EXIT ESCAPE SLIDE
The A318, A319 and A320 emergency exits are equipped with a dual
lane escape slide, which will deploy automatically by the opening of
a left hand or right hand overwing exit. If the automatic inflation fails,
a red handle located in each exit frame, when pulled, activates the
manual inflation. The emergency exit escape slide containers are
located in the wing root fairing and the inflation reservoirs are in the
aft cargo compartment. The inflation reservoirs are accessible from
the aft cargo compartment.
The emergency exit escape slides are located in a container underneath
each door in the fuselage.
The inflation reservoirs are installed above each door in the overhead
stowage compartment.
The escape slide is of single lane type.
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SYSTEM OVERVIEW - EMERGENCY EXIT ESCAPE SLIDE
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SYSTEM OVERVIEW - EMERGENCY EXITESCAPE SLIDE
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
SYSTEM OVERVIEW (continued)
CARGO COMPARTMENTS AND CARGO LOADING
The lower deck is divided into three cargo compartments:
- the forward cargo compartment,
- the aft cargo compartment,
- the bulk cargo compartment.
On the A320 and A321 the forward and aft cargo compartments can
be optionally equipped with a semi-automatic cargo loading system.
Basically they have tie-down/attachment points for the nets and straps
to keep the bulk cargo in place.
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SYSTEM OVERVIEW - CARGO COMPARTMENTS AND CARGO LOADING
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
DAILY CHECKS
The passenger cabin is checked for general condition and cleanliness.
Galleys and lavatories are checked for general condition, cleanliness and
evidence of water leakage. The passenger cabin emergency equipment
is checked for presence, proper stowage and condition.
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DAILY CHECKS
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
MEL/DEACTIVATION
One or more Escape Slide/Slide Raft Cabin Passenger Door may be
inoperative provided the associated door is considered inoperative or one
or more may be removed provided the associated door is considered
inoperative. One or both Overwing Emergency Exit escape slide may be
inoperative provided associated emergency exit is considered inoperative
or one or both may be removed provided the associated emergency exit
is considered inoperative.
NOTE: Note: When an overwing escape slide is inoperative, both
emergency exits on the same side are considered inoperative.
SLIDE BOTTLE PRESS INDICATION ON THE PTP
(CLASSIC CIDS)
The Slide Bottle Pressure Indication of the Passenger Door (If
Installed) on the Programming and Test Panel (PTP) may be
inoperative. The Slide Bottle Pressure Indication of the Emergency
Exit on the PTP may be inoperative provided associated slide bottle
pressure is checked before the first flight of each day or may be
inoperative provided both emergency exits on the same side are
considered inoperative.
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MEL/DEACTIVATION - SLIDE BOTTLE PRESS INDICATION ON THE PTP (CLASSIC CIDS)
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
MEL/DEACTIVATION (continued)
SLIDE BOTTLE PRESS INDICATION ON THE FAP
(ENHANCED CIDS)
The Slide Bottle Pressure Indication of the Passenger Door (If
Installed) on the Flight Attendant Panel (FAP) may be inoperative.
The Slide Bottle Pressure Indication of the Emergency Exit on the
FAP may be inoperative provided the associated slide bottle pressure
is checked before the first flight of each day or may be inoperative
provided both emergency exits on the same side are considered
inoperative.
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MEL/DEACTIVATION - SLIDE BOTTLE PRESS INDICATION ON THE FAP (ENHANCED CIDS)
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
MEL/DEACTIVATION (continued)
CARGO COMPARTMENT
A Decompression Panel in the Cargo Compartment May be damaged
or missing provided the affected cargo compartment is empty or does
not contain inflammable or combustible materials. A Cargo
Compartment Sidewall and Ceiling Lining Panel May be damaged
provided the affected cargo compartment is empty or does not contain
inflammable or combustible materials. A Cargo Compartment Sidewall
and Ceiling Lining Panel May be missing provided affected cargo
compartment is empty.
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MEL/DEACTIVATION - CARGO COMPARTMENT
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
MAINTENANCE TIPS
PAX DOOR SLIDE R/I AND SAFETY PRECAUTIONS
Four cabin PAX door are installed, one or both may be inoperative
or removed provided the associated emergency exit is considered
inoperative.
NOTE: Note: When an over wing escape slide is inoperative, both
emergency exits on the same side are considered inoperative.
To remove the PAX doors escape slide you have to perform several
precautions on:
- the door damper and emergency operation cylinder,
- the escape-slide.
To disarm the percussion mechanism of the door damper and
emergency operation cylinder you have to:
- install the RIGGING PIN,
- remove and discard the lockwire from the knurled screw,
- loosen the knurled screw,
- pull back the striker lever to disarm it,
- tighten the knurled screw.
To safety the inflation reservoir of the escape-slide you have to:
- install the safety/lock pin assembly in the valve/regulator assembly
of the inflation reservoir,
NOTE: The safety/lock pin assembly is kept in a stowage pocket
on the soft-cover of the pack-assembly.
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MAINTENANCE TIPS - PAX DOOR SLIDE R/I AND SAFETY PRECAUTIONS
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
MAINTENANCE TIPS (continued)
OVER WING SLIDE R/I AND SAFETY PRECAUTIONS
Two over wing emergency exits are installed, one or both may be
inoperative or removed provided the associated emergency exit is
considered inoperative.
NOTE: Note: When an over wing escape slide is inoperative, both
emergency exits on thesame side are considered inoperative.
If the gage shows an incorrect indication, you must replace the
inflation reservoir.
Safety the applicable inflation reservoir:
- remove the safety/lock pin assembly from the pocket,
- install the safety/lock pin assembly in the valve/regulator assembly.
WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS
CORRECTLY INSTALLED IN THE REGULATOR
VALVE ASSEMBLY OF THE INFLATION
RESERVOIR.
THIS PREVENTS ACCIDENTAL:
- DISCHARGE OF THE INFLATION RESERVOIR
- DEPLOYMENT OF THE ESCAPE-SLIDE WHICH
CAN CAUSE INJURY AND/OR DAMAGE.
PUT THE SAFETY DEVICES AND THE WARNING
NOTICES IN POSITION BEFORE YOU START A
TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED
DOORS
- COMPONENTS THAT MOVE.
MAKE SURE THAT YOU INSTALL THE PRESSURE
SEAL CAPS ON THE DISCONNECTED LINE ENDS.
THE ESCAPE-SLIDE CAN DEPLOY IF THE
AIRCRAFT IS PRESSURIZED AND THE PRESSURE
SEAL CAPS ARE NOT INSTALLED. UNWANTED
DEPLOYMENT OF THE ESCAPE-SLIDE CAN
CAUSE INJURY AND/OR DAMAGE.
Safety precautions in the cockpit:
- set the flap/slat control lever to the 0 position,
- install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER
(98D27803000000) on the flap/slat control lever when you work on
or near the flaps,
- put a WARNING NOTICE in position on the flap/slat control lever
to tell persons not to operate the flaps.
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MAINTENANCE TIPS - OVER WING SLIDE R/I AND SAFETY PRECAUTIONS
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
'A' CHECK ITEMS
PRESS GAGE INDICATION CHECK (IF NOT
CONNECTED TO CIDS)
The PAX door escape slide and its inflation reservoir are located in
a container at the bottom of the door. The inflation reservoir is part
of the slide pack assembly. The inflation reservoir pressure can be
checked through a pressure gage. Moreover, in relation with the
Maintenance Planning Document (MPD), the door escape slide/raft
pressure indication check must be performed every check A.
A correct indication is shown when:
- the gage needle is in the green band,
- or to the right of the green band.
An incorrect indication is shown when the gage needle is to the left
of the green cursor.
NOTE: Note: the cursor is sensitive to temperature changes and
moves independently of the gage needle. It reacts to
temperature changes faster than the gas expansion in the
inflation reservoir
If the gage shows an incorrect indication wait for temperature
conditions to become stable, then examine the gage again. If the gage
continues to show an incorrect indication, you must replace the slide
pack assembly.
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'A' CHECK ITEMS - PRESS GAGE INDICATION CHECK (IF NOT CONNECTED TO CIDS)
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EQUIPMENT FURNISHINGS LEVEL 2 (2)
'A' CHECK ITEMS (continued)
CARGO COMPARTMENT VISUAL INSPECTION
In relation with the MPD, the visual inspection of cargo compartment
decompression and lining panels must be performed every 500 Flight
Hours (FH).
Examine each decompression panel for cracks and other damage.
NOTE: If a decompression panel is damaged, do a repair or replace
the panel.
Make sure that each decompression panel has a seal installed: missing
seals are not permitted. Make sure that seals are in the correct
condition. Make sure that each decompression panel is in the correct
position.
Examine each lining panel for cracks and other damage, as well as
their correct attachment.
NOTE: If a lining panel is damaged, do a repair or replace the panel.
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'A' CHECK ITEMS - CARGO COMPARTMENT VISUAL INSPECTION
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COCKPIT EMERGENCY EQUIPMENT PRESENTATION (1)
EMERGENCY EQUIPMENT
The emergency equipment is:
- two escape ropes,
- one fire extinguisher,
- two smoke hoods,
- one pair of fire protective gloves,
- one crash axe,
- four life vests,
- one medical kit,
- four oxygen masks,
- two flash lights,
- one portable oxygen bottle.
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EMERGENCY EQUIPMENT
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COCKPIT SEATS DESCRIPTION/OPERATION (3)
PILOT SEATS
Seat movements can be electrically or manually adjusted.
VERTICAL TRAVEL
To adjust the seat upwards or downwards, pull the control handle
marked "V" to unlock the seat. For manual control:
- take your weight off the seat and adjust the seat to the required
position,
- release the handle to lock the seat,
- to adjust the seat downwards the procedure is similar, your weight
is sufficient to move the seat downwards,
- the down movement of the seat is slowed down by means of a gas
cylinder.
For electrical control, place the control switch in the UP or DOWN
position until the seat reaches the required position.
HORIZONTAL TRAVEL
To move the seat forwards or backwards pull the control handle
marked "H" to unlock the seat. For manual control:
- when the desired position is reached, release the handle to lock the
seat.
For electrical control, place the control switch in the FWD or REAR
position until the seat reaches the required position.
NOTE: Horizontal travel indicators give the longitudinal position
of the seat.
BACKREST
Pull the control handle marked "R" to adjust the backrest position.
The system is controlled via two cables. A gas cylinder acts as a return
spring for the backwards movement of the backrest.
LUMBAR REST
Two coaxial knobs enable vertical and horizontal lumbar rest
adjustment. Rotation of the triangular knob is used for the depth
adjustment of the lumbar rest. Rotation of the second serrated knob
is used for the vertical movement of the lumbar rest.
INBOARD ARMREST
The inboard armrest can be raised vertically and stowed behind the
backrest. The inboard armrest is on the pedestal side. Tilt angle
adjustment is made using a knob installed on the front.
SIDE STICK ARMREST
The side stick armrest comprises the fixed arm, the carrier arm and
the side stick table. The fixed arm is attached to the seat pan. It
supports the carrier arm and side stick table assembly. Side stick table
height adjustment is controlled by a knob installed on the armrest.
The side stick table tilt angle is controlled by a knob installed on the
front of the armrest. A position indicator installed on top of the table
shows the table tilt. A wheel avoids interference between the armrest
and the lateral console when the seat is moved forwards with the table
fully inclined.
SAFETY HARNESS
Theshoulder harness is put on an inertia reel which can be locked by
a control lever installed behind the backrest.
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PILOT SEATS - VERTICAL TRAVEL ... SAFETY HARNESS
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COCKPIT SEATS DESCRIPTION/OPERATION (3)
THIRD OCCUPANT SEAT
Seat movements are manually adjusted. A manual control moves the seat
from its stowage. A second control is applied to unlock the headrest. The
headrest can be folded down so that the C/B panel can be opened while
the seat is in its stowed position. A compartment closed by velcro tapes
and containing a life vest is installed in the lower part of the seat. The
safety harness includes straps and an inertia reel controlled by a handle
installed on the left hand side of the seat, which is used to lock or unlock
the inertia reel.
FOURTH OCCUPANT SEAT
The fourth occupant seat is a non-adjustable folding seat. The seat cushion
is folded down into place and returns to its stowed position by pressing
it upwards and against the partition. The lower section of the seat has a
compartment containing a life vest and is closed by velcro tapes. The
safety harness includes straps and an inertia reel. The fourth occupant
seat is optionally installed.
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THIRD OCCUPANT SEAT & FOURTH OCCUPANT SEAT
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SLIDING WINDOWS DESCRIPTION/OPERATION (3)
WINDOWS
One side window is installed on each side of the cockpit beside the seats.
The cockpit sliding windows can only be operated from the inside. To
open a window, push down the red indicator on top of the opening handle.
Prior to closing, unlock the window by pulling the locking pin.
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WINDOWS
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COCKPIT ESCAPE ROPE D/O (3)
ROPES
Two escape ropes are used for cockpit crew evacuation through the sliding
windows. They are installed in stowage boxes set over the sliding
windows. Pull the cover off the stowage box, grasp the rope and throw
it out. Each rope can be used through either sliding window in any normal
or abnormal A/C configuration.
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ROPES
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TYPICAL GALLEY INSTALLATION D/O (3)
GENERAL
Installation of any galley includes the adaptation of the surrounding
furnishings and the installation of dummy metal windows behind lateral
galleys where necessary. Galley equipment may contain:
- ovens,
- water heaters,
- hot jugs,
- hot cups,
- coffee makers,
- trolleys,
- waste trolleys,
- containers.
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GENERAL
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TYPICAL GALLEY INSTALLATION D/O (3)
LOWER ATTACHMENT
Galleys are mounted to the floor structure on existing seat rails or hard
points which are fixed on additional longitudinal beams. These additional
longitudinal beams are only mounted at selected galley locations on
structural provisions existing in the uncustomized A/C. Seat rail
attachments provide inch-by-inch flexibility and hard points provide 2
inches by 2 inches flexibility.
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LOWER ATTACHMENT
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TYPICAL GALLEY INSTALLATION D/O (3)
UPPER ATTACHMENT
Upper attachments consist of a bracket and two adjustable tie rods. The
final attachment is then achieved from the galley by means of tie rods
which are part of the galley. The upper attachment points and the fittings
for the tie rods are mounted on the fuselage frames of the A/C structure
at the selected galley locations. The final attachment of the galley to the
fitting is achieved with a tie rod.
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UPPER ATTACHMENT
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TYPICAL GALLEY INSTALLATION D/O (3)
INTERFACES
A wet galley unit has several interfaces:
- the typical potable water and waste water connections which are located
on the bottom of the galley,
- the hoses for the typical individual and exhaust air interface which are
located on top of the galley. An exhaust air system must be installed on
galleys with ovens,
- galleys with electrical equipment are connected to the nearest terminal
board for the power supply. The connectors are found in the ceiling.
The wiring should contain sufficient free length to allow removal and
installation of the galley unit or galley equipment.
SAFETY PRECAUTIONS
WARNING: S:
USE SOLVENTS AND SEALANTS ONLY WITH A
GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURER'S INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
GET NOTHING IN YOUR MOUTH AND DO NOT
SMOKE.
DO NOT BREATHE THE VAPORS.
GET MEDICAL HELP IF THE SKIN OR EYES BECOME
IRRITATED.
REMOVAL
- Open, safety and tag corresponding C/Bs,
- empty galley compartments,
- remove galley catering equipment,
- remove linings in the galley area where necessary,
- drain the A/C water system.
INSTALLATION
Open, safety and tag corresponding C/Bs,
- install the removed linings in the galley area,
- do an operational test of the coffee maker, water heater and oven.
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TYPICAL LAVATORY INSTALLATION D/O (3)
ATTACHMENT
Each lavatory, made of composite material, is a completely assembled
housing with an integrated floor. Each lavatory is equipped with several
accessories.
LOWER
Lower attachments are obtained by means of four hard points or four
seat rail attachments.
UPPER (LATERAL)
Lateral lavatories have one attachment at the top and one attachment
at the rear side. Depending on the location and the equipment of the
lavatory, one or two upper attachments are used.
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ATTACHMENT - LOWER & UPPER (LATERAL)
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TYPICAL LAVATORY INSTALLATION D/O (3)
INTERFACES
A lavatory unit has several interfaces:
- typical individual and exhaust air interface,
- typical potable water and waste water interface,
- typical vacuum exhaust,
- plug which supplies power for the different electrical systems which
are installed in the lavatory.
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INTERFACES
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TYPICAL LAVATORY INSTALLATION D/O (3)
REMOVAL/INSTALLATION SAFETY PRECAUTIONS
These are the safety precautions for the installation of a lavatory unit.
WARNING: S:
- AS SOLVENTS, SEALANTS AND OTHER SPECIAL
MATERIAL ARE USED, BE SURE THAT SUFFICIENT
AIR IS SUPPLIED,
- PUT NOTHING IN YOUR MOUTH,
- DO NOT SMOKE,
- IF NECESSARY, PUT ON PROTECTIVE CLOTHING,
- GET MEDICAL HELP IF YOUR SKIN OR EYES
BECOME IRRITATED,
- OBEY THE MANUFACTURER'S INSTRUCTIONS.
- make sure that corresponding C/Bs are open, safetied and tagged,
- drain the potable water system and the toilet system,
- do not service the potable water system,
- do not service the toilet system.
DOOR OPERATION
During normal door operation, when the indicator reads VACANT, the
door can be opened from the outside by rotating the latch. To open the
door from the inside, the locking device has to be pushed to unlock the
door and then the knob has to be rotated. In case of emergency, the door
can be unlocked from outside without using a special tool. Lift the
lavatory cover-plate and push the unlocking pin. Then rotate the latch to
open the door.
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REMOVAL/INSTALLATION SAFETY PRECAUTIONS & DOOR OPERATION
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PASSENGER AND ATTENDANT SEATS D/O (3)
PAX SEAT
Passenger seats are designed for the comfort and safety of the passengers.
They are located in the cabin, from the cockpit partition to the aft pressure
bulkhead.
PAX SEAT DESCRIPTION
The passenger seat consists of a framework assembly with:
- an upholstered seat pan,
- an upholstered backrest assembly,
- a folding table,
- seat belts,
- an upholstered armrest,
- a pocket.
FRAMEWORK
The seat framework holds the seatpan, backrest, armrest and table. A
luggage bar is fitted to the front framework legs. Holders for life vests
are found below each seatpan. The Seat Electronic Box (SEB), which
serves the Passenger Service Units (PSUs) is installed between the
front and rear legs.
SEATPAN
The upholstered seatpan is installed on the seat framework. It is not
foldable or adjustable.
BACKREST
The upholstered backrest assembly of each seat can be hydraulically
reclined backwards until it hits an adjustable mechanical stop. The
backrest can be mechanically folded FWD.
TABLE
A folding table is installed in the rear of each backrest. When not in
use, it is kept in a recess in the backrest by means of a latch. Two
hinged arms hold the table when it is folded down. In-armrest tables
are installed in the seats, located just behind partitions, galleys or
lavatories.
SEAT BELT
Each seat is equipped with a seat belt. It is attached to the seat
framework and has a buckle to lock and to adjust the seat belt length.
ARMREST
Each seat has armrests. The outer armrests of a seat unit are not
foldable. The armrests between the seats can be folded up. The
reclining control P/B for the backrest and an ashtray are installed in
the armrest.
POCKET
A pocket is installed on the back of each seat backrest. A safety
instruction card and an air-sickness bag are kept in this pocket.
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PAX SEAT & PAX SEAT DESCRIPTION
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PASSENGER AND ATTENDANT SEATS D/O (3)
PORTABLE ELECTRONIC DEVICE
The in-seat power supply system supplies the electrical outlets of the
passenger seats for the connection of Portable Electronic Devices (PEDs)
or music players. The master control unit controls the supply of the In-Seat
Power Supply (ISPSU) in 115V AC/400Hz. The ISPSU converts the
electrical power into 110V AC/60Hz and provides the Outlet Unit (OU).
The OU and the indication light are located in the passenger seat armrest.
OPERATION
The passenger PED Power P/BSW on the cockpit overhead panel
enables or disables the portable electronic device power. The power
supply for the portable electronic device has to be deactivated during
critical flight phases. There is no electric power supply to the PED
power outlets during take-off and landing.
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PORTABLE ELECTRONIC DEVICE - OPERATION
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PASSENGER AND ATTENDANT SEATS D/O (3)
PAX SEAT ATTACHMENT
A quick release fitting in each rear leg and a retainer in each front leg
attach the seat unit to the seat tracks. By placing the quick release device
in the UP position, the seat can be moved on the tracks or removed
completely.
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PAX SEAT ATTACHMENT
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PASSENGER AND ATTENDANT SEATS D/O (3)
CABIN ATTENDANT SEAT
Cabin attendant seats are installed in the FWD and aft utility areas or in
the passenger seating area. The different types of cabin attendant seats
are free standing, swivel and wall-mounted attendant seats.
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CABIN ATTENDANT SEAT
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PASSENGER AND ATTENDANT SEATS D/O (3)
CABIN ATTENDANT SEAT DESCRIPTION
Cabin attendant seats consist of:
- an aluminum framework,
- a backrest with cushion,
- a seatpan with cushion,
- a headrest with cushion,
- a stowage container,
- seat belts.
FRAMEWORK
The seat frame of the cabin attendant seat is assembled out of two
aluminum side frames and a backrest framework.
HEADREST
The headrest cushion is upholstered with foam and seat fabric. The
headrest is attached to the seat frame.
BACKREST
The backrest cushion is upholstered with foam and seat fabric.
SEATPAN
The seatpan is made of an aluminum pan. The seatpan cushion is
upholstered with foam and seat fabric. Hinges attach the seatpan to
the seat frame. The seatpan is spring-loaded to retract when not in
use.
SAFETY HARNESS
Each cabin attendant seat has a seat belt and a shoulder harness with
a center buckle. The shoulder harness is pulled in automatically on
inertia reels when not in use.
STOWAGE CONTAINER
A stowage container with a latch door is located below the seatpan.
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CABIN ATTENDANT SEAT DESCRIPTION - FRAMEWORK ... STOWAGE CONTAINER
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PASSENGER AND ATTENDANT SEATS D/O (3)
CABIN ATTENDANT SEAT ATTACHMENT
Cabin attendant seats are attached to walls or to the cabin floor.
WALL-MOUNTED
The three sections of the wall-mounted cabin attendant seat are
attached with six bolts to:
- partitions,
- lavatory walls.
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CABIN ATTENDANT SEAT ATTACHMENT - WALL-MOUNTED
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PASSENGER AND ATTENDANT SEATS D/O (3)
CABIN ATTENDANT SEAT ATTACHMENT (continued)
FREE-STANDING
Free-standing cabin attendant seats can be mounted on seat rails with
inch-by inch-flexibility. Free-standing cabin attendant seats can also
be attached to the cabin floor structure by hardpoints.
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PASSENGER AND ATTENDANT SEATS D/O (3)
CABIN ATTENDANT SEAT ATTACHMENT (continued)
SWIVEL
Swivel attendant seats are always attached to the cabin floor structure
by hardpoints.
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CABIN ATTENDANT SEAT ATTACHMENT - SWIVEL
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE CEILING PANEL
JOB SET-UP
After energizing the ground service network, open, safety and tag the
concerned C/Bs.
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REMOVAL OF THE CEILING PANEL - JOB SET-UP
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE CEILING PANEL (continued)
PROCEDURE 1/2
- open the applicable door on the right and left side of the A/C,
- remove the retaining rings, washer and the pins,
- hold the door and remove the pins from hinges,
- carefully remove the door from the compartment.
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REMOVAL OF THE CEILING PANEL - PROCEDURE 1/2
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE CEILING PANEL (continued)
PROCEDURE 2/2
- open the access doors in the overhead stowage compartment and
disconnected electrical connectors,
- put blanking caps on the disconnect electrical connectors,
- open the two quick-release fasteners at the left,
- push the left side of the ceiling panel up,
- move the ceiling panel to the left and out of the spring fasteners,
- move the ceiling panel at an angle with the right side down,
- make sure the right side of the ceiling panel is clear from the
overhead stowage compartments,
- carefully remove the ceiling panel.
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REMOVAL OF THE CEILING PANEL - PROCEDURE 2/2
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE OVERHEAD STOWAGE
COMPARTMENTS
JOB SET-UP 1/2
After energizing the ground service network, open, safety and tag the
concerned C/Bs.
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REMOVAL OF THE OVERHEAD STOWAGE COMPARTMENTS - JOB SET-UP 1/2
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE OVERHEAD STOWAGE
COMPARTMENTS (continued)
JOB SET UP 2/2
Put a stepladder 1.0 M (3.3 FT) adjacent to the stowage compartment
you will remove.
Make sure that the stowage compartment is empty.
Remove the ceiling panels adjacent to the stowage compartment.
Remove the cove light panels adjacent to the stowage compartment.
Remove the fluorescents tubes.
Remove the emergency oxygen container.
REMOVE THE PASSENGER SERVICE EQUIPEMENT
Remove the Passenger Service/Information Unit (PSIU):
- remove the passenger reading light-panel,
- remove the individual air-outlet panel.
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REMOVAL OF THE OVERHEAD STOWAGE COMPARTMENTS - JOB SET UP 2/2 & REMOVE THE PASSENGER SERVICE EQUIPEMENT
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE OVERHEAD STOWAGE
COMPARTMENTS (continued)
PROCEDURE
Remove lower attachments:
- disengage the panel from the attachment rail, pull it down and remove
it,
- remove the screw, the washer, the nut and disconnect the bonding
strap,
- if necessary remove the clamps and disconnect the hoses,
- remove the nuts, the washers, and the screws,
- remove the lock-pins, the washers and the pins,
- remove the nuts, the washers and the screws.
Remove the upper attachments:
- open the stowage compartment doors for access,
- remove the split-rings, the washers,
- remove the nuts and the washers.
- support the stowage compartment and remove the pins or remove
the screws and the washers,
- remove the stowage compartment,
- loosen the clamp,
- remove the hose from the cabin temperature sensor outlet pipe (where
applicable),
- remove the screws, and remove the screen from between the overhead
stowage compartments.
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REMOVAL OF THE OVERHEAD STOWAGE COMPARTMENTS - PROCEDURE
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE PSIU
JOB SET-UP
Energize the ground service network.
PROCEDURE
Remove the section hose from the mounting rail.
Release and remove the filler panel.
Loosen the screws, release and remove the class-divider-bracket
(where applicable).
If installed, and necessary open/remove the Passenger Service
Information Units (PSIUs) as follows:
- remove the loudspeakers,
- remove the NO SMOKING/FASTEN SEAT BELT signs,
- remove the reading lights,
- remove the individual air outlet,
- remove the emergency oxygen containers.
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REMOVAL OF THE PSIU - JOB SET-UP & PROCEDURE
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE COVE LIGHT PANELS
JOB SET-UP
Energize the ground service network.
PROCEDURE
Move the cove light panel inboard and lift the flange off the rail.
Lower the inboard edge of the cove light panel, but not more than 100
mm (3.9370 in.).
Disconnect the bonding strap.
Lift the cove light panel to disengage the bracket from the fitting.
Remove the cove light panel.
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REMOVAL OF THE COVE LIGHT PANELS - JOB SET-UP & PROCEDURE
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE UPPER SIDEWALL PANEL
JOB SET-UP
Energize the ground service network.
Fold down the backrests of the passenger-seats in the area where you
want to remove the sidewall panel.
Open, safety and tag this C/B:
- MEDICAL OUTLET.
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REMOVAL OF THE UPPER SIDEWALL PANEL - JOB SET-UP
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE UPPER SIDEWALL PANEL (continued)
PROCEDURE
Record the location of the sidewall-panel(s) you want to remove.
With a small screw-driver push the clips in the holes of the decor-cover
to release the decor-cover.
Remove the decor-cover and the decor-panel.
Remove the screws and the washers.
Remove the caps and screws.
Pull the lining strips down and out from between the sidewall panel
and the adjacent panels.
Lift the sidewall-panel, release the yo-yo roller from the brackets and
remove it.
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REMOVAL OF THE UPPER SIDEWALL PANEL - PROCEDURE
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CABIN PANEL REMOVAL AND INSTALLATION (3)
REMOVAL OF THE LOWER SIDEWALL PANEL
JOB SET-UP
Energize the ground service network.
If necessary remove the passenger seats in the area of the panels you
will remove.
PROCEDURE
Use a punch to release the center pins of the quick release pins at the
lower edge.
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.
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REMOVAL OF THE LOWER SIDEWALL PANEL - JOB SET-UP & PROCEDURE
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PAX DOOR ESCAPE SLIDE DEPLOYMENT/DESCRIPTION (3)
PASSENGER DOOR ESCAPE SLIDE
DEPLOYMENT/DESCRIPTION
A slide deployment can be initiated whenever the door is opened in the
emergency configuration. When the slide is armed it can be checkedon
a red indicator, located on the button of the slide decorative cover. As
soon as the door handle is lifted the door opens and the escape slide is
ejected from its container and the inflation system is activated. The
deployment and inflation sequence is automatically initiated when the
cabin door is opened. The slide deploys into its final usable position
within 3 seconds. The escape slide is connected to the cabin floor by a
girt extension which is attached to the girt bar at the door sill. Should the
escape slide not inflate automatically a red manual inflation handle must
be pulled. This handle is located on the girt extension. Let's have a look
at the inflation system. The system is automatically activated as soon as
the slide is ejected from its container. The valve regulator assembly
incorporates a direct reading, temperature compensated pressure gage,
which indicates the gas charge in the inflation reservoir, relative to
ambient temperature. The gas stored within the inflation reservoir is
discharged into the inflatable through flexible hoses and an aspirator.
Ambient air is drawn in, through the flaps of the aspirator by the partial
vacuum, created by the high velocity in the venturi. Then the flaps close
and the remaining gas charge tops the inflatable up to its operating
pressure. Inflation is therefore rapid and reservoir size is maintained.
Restraint devices are used to control the deployment sequence. The
primary restraint mechanism is a precision fuse frangible link, which
separates at a predetermined force value. In case of pressure loss, no fail
handles, located on both sides of the runway end, allow the inflatable to
be used as a hand-held evacuation chute. In the event of a ditching, grasp
lines are fitted around the outside of the inflatable to facilitate the use of
the slide as a flotation device. The slide is equipped with a lighting system.
The lights located along the slide tubes and across the runway, are
supplied from the aircraft emergency power supply units. The lights are
automatically supplied with power when the slide is deployed. The escape
slide can be disconnected from the aircraft floor whenever necessary.
For disconnection the following steps must be taken. Lift the flap of the
girt extension to gain access to the white disconnect handle and pull the
handle. The girt extension incorporates a quick release feature, a daisy
chain, which permits rapid detachment of the inflatable from the A/C.
Once detached from the floor the inflatable drops from the A/C but
remains attached to the girt bar by means of a string, which must be cut
by using the knife located next to it, on the girt extension. The inflatable
is then completely disconnected from the A/C.
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PAX DOOR ESCAPE SLIDE DISCONNECTION (3)
PASSENGER DOOR ESCAPE SLIDE DISCONNECTION
Disconnect the electrical line. Tie the retaining cord to the slide handle.
Disconnect the slide-attaching device by removing the safety pin. Undo
the lacing system. Remove the girt bar by unlocking the door threshold
supports. Using the retaining cord, take the escape slide away.
NOTE: Do not forget to reinstall the girt bar back to the door threshold
supports. Close the door in the armed configuration. Set the
emergency control handle to disarmed.
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PAX DOOR ESCAPE SLIDE INSTALLATION (3)
PASSENGER DOOR ESCAPE SLIDE INSTALLATION
Check that the door emergency opening percussion system behind the
door support arm, is in the disarmed position. First, connect the electrical
line. Place it on the RH or LH side according to the door. Fit the girt bar
into the mooring line and slide it into the slide-attaching device. Connect
to the standby percussion system. Connect to the normal percussion
system. Fit the slide assembly into the door slide hooks. Connect to the
electrical connector. Screw the container into place. Arm the slide system.
Lift the door and close the door again. Fit the girt bar into the door
threshold supports. Close the door and check the slide mechanism is
correct. Lift the door and check that the slide mechanism is properly
attached to the door. Remove the safety pin from the slide percussion
system. Fit the slide cover.
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PAX DOOR ESC SLD/RAFT DEPLOYMENT/DESC.(3)(OPTION)
DESCRIPTION
The FWD and rear cabin doors of the A320 are equipped with slide rafts.
The inflation and deployment sequence is automatically initiated when
the door is opened in the armed configuration. The slide raft is ejected
out of its container, and remains folded by restraint devices which break
at a determined pressure point to allow correct deployment. The slide
raft is stowed in a container connected to the cabin door.
NORMAL OPERATION
As soon as the door handle is lifted, the door is pneumatically pushed
open and the slide raft, fixed with a girt bar to the cabin floor, is pulled
out of the container, drops down and inflates automatically. As the
inflatable falls down, the inflation system is activated. The gas stored in
the inflation cylinder is discharged through flexible hoses to the aspirators.
The aspirator flaps open and ambient air is drawn in under partial vacuum,
created by the high velocity in the venturi. Then the flaps close and the
remaining gas, tops up the inflatable to its operational pressure. Should
the automatic inflation system fail, the slide raft must be inflated
manually.
MANUAL OPERATION
For that, the red manual inflation handle located on the RH side of the
girt extension must be pulled. A lighting system is fitted on both sides
and also on the runway end of the inflatable. The power supply for this
lighting system is provided from the cabin emergency power supply units.
Two assist handles are located on both sides at the lower end of the
inflatable, to allow assisting people to hold on. In case of a ditching, prior
to door opening the survival kit must be connected to the slide raft. The
survival kit is stored in thenearest overhead bin. Place the survival kit
on the floor, FWD of the door and detach the lanyard from the girt bar.
Pull the lanyard and the hook, to snap on the front of the survival kit.
Then open the door. The slide raft drops out of the container and deploys.
NOTE: In this module the PASSENGER DOOR SLIDE
DEPLOYMENT/DESCRIPTION is described on the A320 but
the principle is the same for the A318, the A319 and the A321.
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DESCRIPTION ... MANUAL OPERATION
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PAX DOOR ESC SLD/RAFT DISCONNECTION (3) (OPTION)
PASSENGER DOOR ESCAPE SLIDE RAFT
DISCONNECTION
Disconnect the pack-assembly electrical supply. The quick-disconnect
connector is installed below the cable routing velcro. Open the girt flap.
Open the lanyard velcro and remove the survival kit attach-loop from the
telescopic end fitting of the girt bar. Open the blue and the green velcros
and separate the survival kit lanyard and the girt bar release-strap. Remove
the girt bar release-strap from the girt bar release-lever. Pull the mooring
line from the girt pocket and support the escape slide raft with the mooring
line. Pull the release handle, release the mooring line slowly and let the
girt lace-up joint and the girt assembly release from the girt bar. Carefully
lower the escape slide raft to the ground. Make sure that you do not
damage the reservoir when you lower the slide raft to the ground. Hold
the girt bar and push in the girt bar release-lever by hand. Remove the
girt bar from the floor attach fittings. Remove the mooring line loop-end
from the girt bar and keep the girt bar with the A/C. Lift the empty pack
assembly soft-cover clear off the passenger/crew door and close the door.
Remove the pack assembly decorative-cover and keep it with the A/C.
Loosen the link nut and remove and retain the attach link and the
pull-handle from the stud assembly. Remove the stud assemblies, with
the allen key, from the door attach anchor nuts. Move the packboard
inboard on its supports and hold it. Disconnect the pack assembly
connector from the electrical connector installed on the passenger/crew
door. Remove the packboard from the passenger/crew door supports.
Service the door damper and emergency operation cylinder.
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PAX DOOR ESC SLD/RAFT INSTALLATION (3) (OPTION)
PASSENGER DOOR ESCAPE SLIDE RAFT
INSTALLATION
Make sure that the operation striker lever of the door damper and
emergency operation cylinder are in the DISARMED position. Make
sure that the passenger/crew door on which you will install the pack
assembly is closed and locked. Make sure that the emergency control
handle is in the DISARMED position and that the safety pin is installed.
Make sure that the lockpin assembly is installed in the operating head of
the slide raft inflation reservoir. Check the pack electrical supply cable,
and make sure that the cable is installed for the left door or the right door
as required. Make sure that the short girt flap is on the top of the long
girt flap. Attach a temporary tie to the small cord loop. Put the girt bar
in place. Make sure that the girt bar end fittings point away from the slide
raft pack, and that the telescopic end is in the FWD position in relation
to the A/C. Install the mooring line loop on the girt bar rear end. Pull the
cord loops attached to the long girt flap up through the grommets in the
short girt flap. Put the loops through each other from each end of the girt
towards the center. Put the parachute pin through the small cord loop and
remove and discard the temporary tie. Safety the parachute pin in position
with nylon thread with a breaking strain. Put the girt bar release strap
through the girt bar release lever and position the release strap along the
slide raft girt. Attach the survival kit lanyard to the release strap with the
same color velcros and position the lanyard along the slide raft girt. Fold
the long girt flap over the girt bar and attach it to the short girt flap velcro
attach strips. Lift the slide raft pack assembly onto the passenger/crew
door supports. Carefully move the packboard assembly inboard at an
angle onto its supports and hold it. Connect the pack assembly connector
to the electrical connector on the passenger/crew door. Move the pack
assembly in position and install the stud assemblies in the door attach
anchor nuts. Carefully tighten the two stud assemblies with the allen key,
until there is no play between the door and packboard assembly. Connect
the two pull handles to the stud assemblies with the attach links. Remove
the safety pin from the emergency control handle and set the handle to
the ARMED position. Hold the passenger/crew door to prevent it moving
outboard and set the door control handle to the OPEN position. Install
the girt bar into the floor attach fittings. Slowly move the door control
handle to the CLOSED position, and move the emergency control handle
to the DISARMED position. Set the door control handle to the OPEN
position. Make sure that the control shaft levers and the telescopic forks
on the door have engaged correctly with the girt bar. Set the door control
handle to the CLOSED position, and set the emergency control handle
to the ARMED position. Hold the passenger/crew door to prevent it
moving outboard and set the door control handle to the OPEN position.
Make sure that the girt bar has engaged correctly with the floor attach
fittings. Set the door control handle to the CLOSED position. Set the
emergency control handle to the DISARMED position and install the
safety pin. Remove the lockpin assembly from the operating head of the
slide raft inflation reservoir and put the lockpin assembly in the stowage
pocket installed on the pack assembly soft cover. Put the pack assembly
decorative cover in position. Connect the cover attach straps. Check the
indication of the decorative cover bracket and girt-bar visual indicator.
Make sure that the operation striker lever of the door damper and
emergency operation cylinder is in the ARMED position.
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OFFWING ESCAPE SLIDE DEPLOYMENT/DESCRIPTION (3)
OFFWING ESCAPE SLIDE DEPLOYMENT
The offwing escape slide is packed in a container assembly, which in
turn is mounted into the center fuselage belly fairing. Two type 3 exits
are located over each wing and are always in armed configuration. Two
emergency lights underneath the wing exit illuminate the escape way
leading to the escape slide which is pointed out with red fluorescent
arrows. The opening of one wing exit will initiate the deployment
sequence. The escape slide inflates automatically and is ejected out of
its containers and deploys in approximately four seconds. The inflation
system consists of an inflation cylinder, which is located in the aft cargo
compartment. Activation of the release mechanism initiates the inflation
sequence. The gas stored in the cylinder is discharged to the inflatable
through flexible hoses and an aspirator. The aspirator flaps open and
ambient air is drawn into the slide. The slide remains folded by restraint
devices, which break at a predetermined force, to permit correct
deployment. Two black arrows located on the ramp section indicate the
direction of the escape route. A lighting system is provided on the slide.
The lights are located on the ramps along the side tubes and across the
runway end. A red manual inflation handle, located in each exit frame,
must be pulled to manually activate the inflation and deployment
sequence, in case of automatic release failure. If the slide is deployed but
not inflated, it can still be used as a hand-held escape chute. On the ramp
section top, a hook is located. This hook must be connected to an
attachment fitting on the wing. Two red NO FAIL HANDLES are located
on both sides of the escape slide on the way end. Four able bodied men
must hold the deflated slide extended, by means of the no fail handles,
to allow the passengers on the wing to descend.
NOTE: In this module the OFFWING ESCAPE SLIDE
DEPLOYMENT is described on the A320 but the principle is
the same for the A318 and A319.
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OFFWING ESCAPE SLIDE REMOVAL (3)
OFFWING ESCAPE SLIDE REMOVAL
Push in the flapper valves of the aspirator and release the pressure from
the offwing escape slide. Disconnect the inflation hose from the stowage
compartment union. Disconnect the electrical connectors at the emergency
lighting supply cable.
WARNING: USE BLANKING CAPS.
Undo the strap press-studs, to separate the container panel from the escape
slide. To release the TOP girt bar assembly, support the slide and open
the girt flap. Remove the girt release handle, and pull it. Undo the laces.
Follow the same procedure to release the lower and FWD girt assemblies.
Carefully lower the offwing escape slide to the ground. Remove and
retain the seal attach plate screws. Remove and retain the seal attach plate
and the seal strips. Loosen the attach panel studs. Move the top of the
stowage compartment outboard at an angle and hold it. Disconnect the
inflation hose from the fuselage union. Disconnect the emergency lighting
electrical connector, and remove the escape slide stowage compartment
from the A/C. The inflation reservoir has to be replaced.
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OFFWING ESCAPE SLIDE CYLINDER REMOVAL & INSTL(3)
REMOVAL
WARNING: BE CAREFUL WITH THE INFLATION RESERVOIR
AND ITS COMPONENTS. THE RESERVOIR IS AN
ALUMINUM BOTTLE WOUND IN KEVLAR FIBERS
BONDED WITH EPOXY RESINS, AND IS
PRESSURIZED WITH GAS. IF YOU CAUSE DAMAGE
TO THE RESERVOIR, THERE IS A RISK OF
EXPLOSION. NO DAMAGE IS PERMITTED.
JOB SET-UP 1/2
Energize the ground service network.
To get access:
- open the aft cargo-compartment door,
- put an access platform in position adjacent to the aft
cargo-compartment exit,
- set the aft CARGO COMPT light switch to ON,
- remove the access panel 151CW or 151SW,
- remove the access panel 152CW or 152SW.
JOB SET-UP 2/2
Open, safety and tag these C/Bs:
- 49VU COM/CIDS/DEU B/ESS 153RH G03,
- 121VU COM NAV/CIDS/DEU B/NORM 162RH,
- 121VU COM NAV/CIDS/DEU B/NORM 162RH.
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REMOVAL - JOB SET-UP 1/2 & JOB SET-UP 2/2
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OFFWING ESCAPE SLIDE CYLINDER REMOVAL & INSTL(3)
REMOVAL (continued)
PROCEDURE 1/4
Safety the inflation reservoir:
WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS
CORRECTLY INSTALLED IN THE REGULATOR
VALVE ASSEMBLY OF THE INFLATION
RESERVOIR.
THIS PREVENTS ACCIDENTAL DISCHARGE OF
THE INFLATION RESERVOIR, DEPLOYMENT OF
THE ESCAPE-SLIDE, WHICH CAN CAUSE INJURY
AND/OR DAMAGE.
- remove the lock pin from the pocket,
- install the lock pin in the regulator valve assembly.
PROCEDURE 2/4
Remove and discard the lock wire from the sleeve nut.
Loosen the sleeve nut fully to get access to the two clips.
Remove and keep the two clips.
Disconnect the wire-control assembly from the flexible control
assembly:
CAUTION: - CAUTION: do not push the end of the wire into the
wire-control assembly. This can cause a kink in the wire.
- carefully pull the end of the wire out of the slot of the flexible control
assembly,
- make sure that you do not push the end of the wire into the
wire-control assembly.
PROCEDURE 3/4
Remove the protection plug from the pocket.
Put the two clips into the sleeve nut and install the protection plug.
Disconnect the electrical connectors:
- 5555VC-A,
- 5556VC-A.
Install the blanking cap on the socket.
Put blanking caps on the disconnected electrical connectors.
Disconnect the hose assembly from the bulkhead connection.
Put blanking plugs on the disconnected line ends.
Safety the bulkhead connection:
WARNING: MAKE SURE THAT YOU INSTALL THE PRESSURE
SEAL CAPS ON THE DISCONNECTED LINE ENDS.
THE ESCAPE-SLIDE CAN DEPLOY IF THE A/C IS
PRESSURIZED AND THE PRESSURE SEAL CAPS
ARE NOT INSTALLED. UNWANTED
DEPLOYMENT OF THE ESCAPE-SLIDE CAN
CAUSE INJURY AND/OR DAMAGE.
- remove the pressure seal cap from the pocket,
- install the pressure seal cap on the bulkhead connection.
PROCEDURE 4/4
Remove the bolt, the washer, the clamp and the spacer.
Remove