Ata 25

A319/A320/A321TECHNICAL TRAINING MANUAL

MECHANICS / ELECTRICS & AVIONICS COURSE

25 EQUIPMENT/FURNISHINGS

This document must be used for training purpose 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 Industrie.

GENERAL** System Presentation (1) 1.......................

COCKPIT** Cockpit Seats Presentation (1) 9................** Cockpit Emergency Equipment (1) 17.............** Cockpit Seats Description/Operation (3) 21.....Sliding Windows Desc/Operation (3) 27.............Cockpit Escape Rope D/O (3) 31.....................** Components (3) 35................................

PASSENGER COMPARTMENT** Cabin Presentation (1) (A320) 41................** Cabin Presentation (1) (A319) 45................** Cabin Presentation (1) (A321) 49................** Cabin EQPT & Furnishings Presentation (1) 53...Typical Galley Presentation (1) 57.................Typical Lavatory Presentation (1) 63...............Typical Galley Installation D/O (3) 69............Typical Lavatory Installation D/O (3) 77..........Passenger and Attendant Seats (3) 85...............** Cabin Panel Removal/Installation (3) 101.......** Cabin Equipment & Furnishings CMPNTS (3) 113...

EMERGENCY EQUIPMENT** Escape Facility Presentation(1)(A320/319) 125..** Escape Facility Presentation (1) (A321) 131....** Miscellaneous Emergency EQPT Present. (1) 137..** Pax Door ESC SLD/Desc/Depl (3) 143.............** Pax Door ESC SLD/Disctn (3) 147.................** Pax Door ESC SLD/INSTL (3) 151..................** Pax Door ESC SLD/Raft Desc/Depl (3) 155........** Pax Door ESC SLD/Raft Disctn (3) 159...........** Pax Door ESC SLD/Raft INSTL (3) 163............** Offwing ESC SLD Deploy. (3) 167.................** Offwing ESC SLD Removal (3) 171.................

** Offwing ESC SLD CYL R/I (3) 175.................** Offwing ESC SLD INSTL (3) 179...................** EMER Exit ESC SLD/Desc/Deploy (3) (A321) 183...** EMER Exit ESC SDL/Disctn (3) (A321) 187........** Pax Door ESC SLD/Raft Inflat. CYL CHK(3) 191...** Offwing ESC SLD Inflation CYL CHK(3) 195.......** Offwing ESC SLD Release Mechanism Desc.(3) 203.** Components (3) 213...............................

CARGO COMPARTMENTS** Cargo Compartment Presentation (1) 221.........** Cargo Compartment Interior (1) 225.............** Cargo Compartment Capabilities (1) (A320) 235..** Cargo Compartment Capabilities (1) (A319) 243..** Cargo Compartment Capabilities (1) (A321) 251..** Cargo Loading System Presentation (1) 259......** Cargo Loading Operation (3) 271.................** Cargo Bulk Loading (3) 275......................** Draining System D/O (3) 283.....................** Cargo Loading Components (3) 287................

_A319/A320/A321 TECHNICAL TRAINING MANUAL25 EQUIPMENT/FURNISHINGSMECHANICS / ELECTRICS & AVIONICS COURSE

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25 - EQUIPMENT/FURNISHINGS

25-00-00 SYSTEM PRESENTATION

CONTENTS:GeneralCockpitPassenger CompartmentCargo CompartmentEmergency EquipmentAvionics Compartment

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SYSTEM PRESENTATION

GENERAL

The equipment and furnishings which are installed inthe aircraft provide comfort and safety to passengersand crew.The equipment and furnishings are located in differentcompartments :

- The cockpit,- The passenger compartment,- The cargo compartments.

COCKPIT

Various furnishings and equipment are fitted in thecockpit for the comfort, convenience and safety of theoccupants.The cockpit is also equipped with adjustable seats fortwo crew members and folding seats for the thirdoccupant and, if it the option is installed, for thefourth occupant.

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SYSTEM PRESENTATION

PASSENGER COMPARTMENT

The passenger compartment is divided into utility areasand seating areas.The equipment and furnishings which are installed in:The seating areas :

- First-class and/or economy-class passengerseats and cabin attendant seats,

- Linings and furnishings that cover thecompartment structure,

- Overhead stowage compartment,- Passenger service/information units,

The utility areas :- Cabin attendant seats,- Passenger Service Units (PSUs),- Ancillary equipment,- Galleys,- Lavatories.

CARGO COMPARTMENT

In the lower deck of the aircraft, there are two lowerholds: the FWD cargo compartment and, the AFT/Bulkcargo compartments.




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SYSTEM PRESENTATION

EMERGENCY EQUIPMENT

Emergency equipment is kept in different locations inthe cockpit and in the cabin.Emergency equipment is composed of :

- Fire protection and emergency oxygen equipment,- Cockpit and cabin escape facilities,- Floatation and survival equipment,- Evacuation signalling equipment,- Rapid decompression system.

AVIONICS COMPARTMENT

The avionics compartment is located in the underfloorbelow the cockpit.For maintenance it can be accessed through four outsideaccess doors and an access panel in the passengercompartment.




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25-11-00 COCKPIT SEAT PRESENTATION

CONTENTS:GeneralCaptain And First Officer SeatsThird Occupant SeatFourth Occupant Seat

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COCKPIT SEAT PRESENTATION

GENERAL

The cockpit is basically equipped with three seats :- a Captain seat,- a First Officer seat,- a Third Occupant seat located against the rightAFT panel.

If the option is installed, a folding seat for theFourth Occupant is located in the cockpit left AFTsection.

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CAPTAIN AND FIRST OFFICER SEATS

The Captain and First Officer seats are symmetricaland their operation is identical.They are not interchangeable.The Captain and First Officer seats are secured to thecockpit floor.




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THIRD OCCUPANT SEAT

The Third Occupant seat is a folding seat attached tothe right rear panel in the cockpit.No longitudinal adjustment is provided.It can slide along the lateral axis.

FOURTH OCCUPANT SEAT

The Fourth Occupant seat is a folding seat locatedagainst the left rear partition in the cockpit.The fourth occupant seat is optionally installed.This seat is not adjustable.




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25-60-00 COCKPIT EMERGENCY EQUIPMENT

CONTENTS:Escape RopeFire ExtinguisherSmoke HoodFire Protective GlovesCrash AxeLife VestMedical KitOxygen Masks Flash Light

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COCKPIT EMERGENCY EQUIPMENT

ESCAPE ROPE

Two items.

FIRE EXTINGUISHER

One item.

SMOKE HOOD

One item.

FIRE PROTECTIVE GLOVES

One item.

CRASH AXE

One item.

LIFE VEST

Four items.

MEDICAL KIT

One item

OXYGEN MASKS

Four items.

FLASH LIGHT

Two items.

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25-11-00 COCKPIT SEATSDESCRIPTION/OPERATION

CONTENT:Pilot SeatsThird Occupant SeatFourth Occupant Seat

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COCKPIT SEATS DESCRIPTION/OPERATION

PILOT SEATS

Seat movements can be electrically or manuallyadjusted.

VERTICAL TRAVELTo adjust the seat upwards or downwards, pull thecontrol handle marked "V"to unlock the seat.Manual control :

- Take your weight off the seat and adjust theseat to the required position.

- Release the handle to lock the seat.- To adjust the seat downwards the procedure issimilar, your weight is sufficient to move theseat downwards.

- The down movement of the seat is slowed downby means of a gas cylinder.

Electrical control :- For vertical electrical control, place thecontrol switch in the UP or DOWN position untilthe seat reaches the required position.

HORIZONTAL TRAVELTo move the seat forwards or backwards pull the controlhandle marked "H"to unlock the seat.Manual control :

- When the desired position is reached, releasethe handle to lock the seat.

Electrical control :- For horizontal electrical control, place thecontrol switch in the FORWARD or REAR positionuntil the seat reaches the required position.

NOTE: Horizontal travel indicators give thelongitudinal position of the seat.

BACKRESTPull the control handle marked "R" to adjust thebackrest position.The system is controlled via two cables.A gas cylinder acts as a return spring for the backwardsmovement of the backrest.

LUMBAR RESTTwo coaxial knobs enable vertical and horizontal lumbarrest adjustment.Rotation of the triangular knob ensures depthadjustment of the lumbar rest.Rotation of the second serrated knob ensures verticalmovement of the lumbar rest.

INBOARD ARMRESTThe inboard armrest can be raised vertically and stowedbehind the backrest.The inboard armrest is located on the pedestal sideHeight adjustment is made using a knob located on thefront.

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PILOT SEATS

SIDESTICK ARMRESTThe sidestick armrest comprises the fixed arm, thecarrier arm and the sidestick table.The fixed arm is attached to the seat pan.It supports the carrier arm and sidestick tableassembly.Sidestick table height adjustment is controlled by aknob located on the armrest.Armrest table tilt angle is controlled by a knoblocated on the front of the armrest.A position indicator fitted on top of the table showsthe table tilt.A wheel avoids interference between the armrest andthe lateral console when the seat is moved forwardswith the table fully inclined.

SAFETY HARNESSThe shoulder harness is fitted on an inertia reel whichcan be locked by a control lever, located behind thebackrest.

THIRD OCCUPANT SEAT

Seat movements are manually adjusted.A manual control enables the seat to be moved from itsstowage.A second control serves to unlock the headrest.The headrest can be folded down so that the circuitbreaker panel can be opened while the seat is in itsstowed position.A compartment closed by VELCRO tapes and containing alife vest is provided in the lower part of the seat.The safety harness includes straps and an inertia reelcontrolled by a handle located on the left of the seat,which serves to lock or unlock the inertia reel.


The fourth occupant seat is a non- adjustable foldingseat.The seat cushion is folded down into place and returnsto its stowed position by pressing it upwards andagainst the partition.The lower section of the seat is provided with acompartment containing a life vest and closed by VELCROtapes.The safety harness includes straps and an inertia reel,locking control located in the coat storagecompartment.The fourth occupant seat is optionally installed.

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25-61-00 COCKPIT SLIDING WINDOWSDESCRIPTION/OPERATION

CONTENTS:Windows

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COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION

WINDOWS

One side window is provided on each side of the cockpitbeside the seats.The cockpit sliding windows can only be operated fromthe inside.To open a window, push down the red indicator on topof the opening handle.Prior to closing, unlock the window by pulling thelocking pin.

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25-61-00 COCKPIT ESCAPE ROPEDESCRIPTION/OPERATION

CONTENTS:Ropes

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COCKPIT ESCAPE ROPE DESCRIPTION/OPERATION

ROPES

Two ropes enable cockpit crew evacuation through thesliding windows.Two escape ropes are provided in stowage boxes locatedover the sliding windows.Pull the cover off the stowage box, grasp the handleand throw it out.Each rope can be used through either sliding windowin any normal or abnormal aircraft configuration.

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25-11-00 COCKPIT COMPONENTS

CONTENTS:Captain and First Officer SeatsPilot Seat HarnessSidestick ArmrestThird Occupant SeatFourth Occupant Seat

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COCKPIT COMPONENTS

CAPTAIN AND FIRST OFFICER SEATS

IDENTIFICATIONFIN: 3MS(CAPTAIN), 4MS(F/O)

LOCATIONZONE: 211, 212

COMPONENT DESCRITIONAll the manual controls must be operative for eachpilot.Electrical controls are optionally installed and maybe inoperative.

PILOT SEAT HARNESS



COMPONENT DESCRITIONThe aircraft may not leave an airport where repair orreplacements can be made.

SIDESTICK ARMREST



COMPONENT DESCRITIONThe manual controls may be inoperative provided settingis suitable for proper operation.

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THIRD OCCUPANT SEAT

IDENTIFICATIONFIN: 14MM

LOCATIONZONE: 212


IDENTIFICATIONFIN: 13MM

LOCATIONZONE: 211The fourth occupant seat is optionally installed.

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25-20-00 CABIN PRESENTATION

CONTENTS:GeneralClass LayoutPassenger SeatsCabin Attendant SeatsGalleysLavatoriesCurtains And Partitions

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CABIN PRESENTATION

GENERAL

The passenger compartment can be equipped in differentconfigurations.

CLASS LAYOUT

Three typical cabin configurations are :- Basic all economy,- Typical mixed class,- High density.

Basic all economy cabin configuration accomodates onlytourist class with six seats abreast.Typical mixed class cabin configuration accomodatesfirst class with four seats abreast, tourist classwith six seats abreast.High density cabin configuration accomodates onlytourist class with six seats abreast.

PASSENGER SEATS

The passenger seats are mounted on standard trackswhich allow quick removal for cabin configurationchange.

CABIN ATTENDANT SEATS

Cabin attendant seats are attached to partitions orlavatory walls.Depending on the cabin configuration, the number andlocation of cabin attendant seats can vary.The three main types of cabin attendant seats are wallmounted single, wall mounted double bench and wallmounted swivel; all are folding seats.

GALLEYS

The number and location of the galleys vary with thecabin configuration and the aircrft utilization.

LAVATORIES

The number and location of the lavatories change withthe cabin configuration.

CURTAINS AND PARTITIONS

Classes and zones are divided by floor mountedpartitions and ceiling mounted curtains.

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CABIN PRESENTATION

GENERAL


CLASS LAYOUT

Three typical cabin configurations are :- Basic all economy,- Typical mixed class,- High density.

Basic all economy cabin configuration accomodates onlytourist class with six seats abreast.Typical mixed class cabin configuration accomodatesfirst class with four seats abreast, tourist classwith six seats abreast.High density cabin configuration accomodates onlytourist class with six seats abreast.

PASSENGER SEATS



Cabin attendant seats are attached to partitions orlavatory walls.Depending on the cabin configuration, the number andlocation of cabin attendant seats can vary.The three main types of cabin attendant seats are wallmounted single, wall mounted double bench and wallmounted swivel; all are folding seats.

GALLEYS


LAVATORIES







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CABIN PRESENTATION

GENERAL


CLASS LAYOUT

Three typical cabin configurations are :- Standard specification,- Optional mixed class,- High density.

Standard specification cabin configurationaccomodates only tourist class with six seats abreast.Optional mixed class cabin configuration accomodatesfirst class with four seats abreast, tourist classwith six seats abreast.High density cabin configuration accomodates onlytourist class with six seats abreast.

PASSENGER SEATS



Depending on the cabin configuration, the number andlocation of cabin attendant seats can vary.There are three main types of cabin attendant seatsand all are folding seats.Free standing seats are attached to the cabin floorstructure.

Swivel seats are attached to the cabin floor structure.Wall mounted single seats are attached to the partitionor to the lavatory wall.

GALLEYS


LAVATORIES







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CABIN PRESENTATION



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25-20-00 CABIN EQUIPMENT AND FURNISHINGSPRESENTATION

CONTENTS:General Lower Sidewall PanelsUpper Sidewall PanelsCove Light PanelsOverhead Stowage CompartmentCeiling PanelsPSU/PIUSelf Examination

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CABIN EQUIPMENT AND FURNISHINGS PRESENTATION

GENERAL

The cabin interior is equipped with removable panels.The modular lining design allows cabin customizationwithin flexibility areas.

LOWER SIDEWALL PANELS

The lower sidewall panels are mounted between the cabinfloor and the sidewall panels.They are equipped with rapid decompression doors.

UPPER SIDEWALL PANELS

The upper sidewall panels are mounted on the side ofthe cabin.They include the window contourInner window panels and sunvisors are fitted to thewindow frames.

COVE LIGHT PANELS

The cove light panels covers the space between theupper sidewall panels and the overhead stowagecompartments.The cove light panels are removable to allow cabinlight replacement.

OVERHEAD STOWAGE COMPARTMENT

The overhead stowage compartments are intalled abovethe cabin seat rows.

They extend from the first seat row to the last seatrow on the left and right side of the cabin.The overhead stowage compartments are of differentsizes and are arranged to suit the cabin layout.

CEILING PANELS

Removable ceiling panels are mounted in the cabin.They are installed over the full lenght of the cabinand the utility areas.

PSU/PIU

The Passenger Service Information Units comprise thePassenger Service Units and Passenger InformationUnits.They are installed in the service channel, above theset rows.The PSU’s and PIU’s have different lenghts to agreeto aircraft furnishing configuration.These units are:

- information panel,- attendant call panel,- emergency oxygen mask and generator container,- reading light panel,- individual air outlet-panel.

NOTE: On the attendant call panel and the reading lightpanel the bulb cover is removable. This enablesthe bulbs to be replaced without removing thePSIU’s.

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SELF EXAMINATION

Which cabin panels are removable ?A - Lower sidewall panels only.B - All the panels.C - Upper sidewall panels only.

Where are passenger oxygen masks stored ?A - In the Passenger Service Unit.B - In the seat arm rest.C - In the overheat stowage compartment.

Where are the cabin depressurization doors mounted? A - On the upper sidewall panels.B - On the ceiling panels.C - On the lower sidewall panels.

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25-30-00 TYPICAL GALLEY PRESENTATION

CONTENTS:GeneralDry GalleysWet GalleysGalleys Cooling

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TYPICAL GALLEY PRESENTATION

GENERAL

The galleys are buyer furnished equipment. They arenormally installed in the Forward and Aft sectionsof the cabin.They are attached at the top to the aircraft structureand at the bottom to the strengthened points in thecabin floor structure. The position and the number ofgalleys change with the cabin configuration.

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DRY GALLEYS

The dry galleys are not connected to the aircraftsystems such as ventilation or potable water.Dry galleys are mainly used to store the trolleys andto keep foods and drinks.

WET GALLEYS

The wet galleys are connected to :- the water and waste system,- the air extraction system,- the main air cabin ventilation system,- the electrical power system.

GALLEYS COOLING

At most galley locations, chilled air systems are usedto cool the meal trolleys.The freon cooling system requires special servicing.

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25-40-00 TYPICAL LAVATORY PRESENTATION

CONTENTS:GeneralLavatory

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TYPICAL LAVATORY PRESENTATION

GENERAL

Lavatories are normally installed at the forward andaft sections of the cabin.They are assembled as modular units and they areattached at the top of the aircraft structure and atthe bottom to hard points in the cabin floor structure.The position and the number of lavatories change withthe cabin configuration.

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LAVATORY

All lavatories have the same equipment.They are connected to the electrical power system, airconditioning system and water/waste system.In case of emergency all lavatories can be unlockedfrom the outside.

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25-30-00 TYPICAL GALLEY INSTALLATION D/O

CONTENTS:

GeneralLower AttachmentUpper AttachmentInterfacesSafety Precautions

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TYPICAL GALLEY INSTALLATION D/O

GENERAL

Installation of any galley includes the adaptationsof the surrounding furnishings and the installationof dummy metal windows behind lateral galleys wherenecessary.Galley equipment may contain:

- ovens, - water heaters,- hot jugs, - hot cups, - coffee makers, - waste trolleys, - containers.

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LOWER ATTACHMENT

Galleys are mounted to the floor on existing seat railswherever possible. Remaining attachment points consistof hard points which are fixed on additionallongitudinal beams.These additional longitudinal beams are only mountedat selected galley locations on structural provisionsexisting in the uncustomized aircraft.Seat rail attachments provide inch by inch flexibilityand hard points provide 2 inches by 2 inchesflexibility.




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UPPER ATTACHMENT

Upper attachments consist of a bracket and twoadjustable tie rods. The final attachment is thenachieved from the galley by means of tie rods whichare part of the galley.The upper attachment points, the fittings for the tierods, are mounted on the frames on the selected galleylocations on the aircraft structure.The final attachment of the galley to the fitting isachieved with a tie rod.




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INTERFACES

A wet galley unit has several interfaces:- The typical water and waste connections whichgo through the aircraft floor panel.

- The hoses for the typical individual andexhaust air interface which are located on topof the galley. An exhaust air system must beinstalled on galleys with ovens.

- Galleys with electrical equipment which areconnected to the nearest terminal board forthe power supply. The connectors are found inthe ceiling.The wiring should contain sufficient freelength to allow removal and installation ofthe galley unit or galley equipment.

SAFETY PRECAUTIONS

These are the safety precautions for the installationof a galley unit.

REMOVAL: - Open, safety and tag corresponding circuitbreakers.

- Empty galley compartments.- Remove galley catering equipment.- Remove linings in galley area where necessary.- Drain the aircraft water system.

INSTALLATION: - Open, safety and tag corresponding circuitbreakers.

- Installation of removed linings in galley area.- Operational test of coffee maker, water heaterand oven.

WARNINGS: - USE SOLVENTS AND SEALANTS ONLY WITH GOODSUPPLY OF AIR.- OBEY THE MANUFACTURER’S INSTRUCTIONS.- PUT ON PROTECTIVE CLOTHING.- GET NOTHING IN YOUR MOUTH AND DON’T SMOKE.- DON’T BREATHE THE VAPORS.- GET MEDICAL HELP IF THE SKIN OR EYES BECOMEIRRITATED.

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25-40-00 TYPICAL LAVATORY INSTALLATION D/O

CONTENTS:AttachmentInterfacesSafety PrecautionsDoor Operation

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TYPICAL LAVATORY INSTALLATION D/O

ATTACHMENT

Each lavatory, made of composite material, is acompletely assembled housing with an integratedfloor.Each lavatory is equipped with several accessories.

LOWERLower attachments are obtained by means of fourhard points or four seat rail attachments.

UPPER (LATERAL)Lateral lavatories have one attachment at the top andone attachment at the rear side.Depending on the location of the lavatory, one or twoupper attachments are used.

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INTERFACES

A lavatory unit has several interfaces:- Typical individual and exhaust air interface.- Typical water and waste interface.- Plug which supplies power for the differentelectrical systems which are installed in thelavatory.

SAFETY PRECAUTIONS

These are the safety precautions for the installationof a lavatory unit.

R/I SAFETY PRECAUTIONS :* Make sure that corresponding circuit breakers areopen, safetied and tagged.* Drain the potable water system and the toiletsystem.* Do not service the potable water system.* Do not service the toilet system.

WARNINGS : * AS SOLVENTS, SEALANTS AND OTHER SPECIALMATERIAL ARE USED, BE SURE THAT SUFFICIENT AIR IS SUPPLIED.* PUT NOTHING IN YOUR MOUTH.* DON’T SMOKE.* IF NECESSARY, PUT ON PROTECTIVE CLOTHING.* GET MEDICAL HELP IF YOUR SKIN OR EYESBECOME IRRITATED.* OBEY THE MANUFACTURER’S INSTRUCTIONS.




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DOOR OPERATION

During normal door operation, when the indicator readsVACANT, the door can be opened from the outside byrotating the latch.To open the door from the inside, the locking devicehas to be pushed to unlock the door and then the knobhas to be rotated.In case of emergency, the door can be unlocked fromoutside without using a special tool.Lift the lavatory cover-plate and push the unlockingpin.Then rotate the latch to open the door.




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25-21-00 PASSENGER AND ATTENDANT SEATS

CONTENTS:Pax SeatPax Seat DescriptionPax Seat AttachementCabin Attendant SeatCabin Attendant Seat DescriptionCabin Attendant Seat AttachmentSelf Examination

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PASSENGER AND ATTENDANT SEATS

PAX SEAT

Passenger seats are designed for the comfort and safetyof the passengers.They are located in the cabin, from the cockpitpartition to the aft pressure bulkhead.

PAX SEAT DESCRIPTION

The passenger seat consists of a framework assemblywith:

- an upholstered seatpan,- an upholstered backrest assembly,- a folding table,- seat belts,- an upholstered armrest and,- a pocket.

FRAMEWORKThe seat framework holds the seatpan, backrest, armrestand table.A luggage bar is fitted to the front framework legs.Holders for life vests are found below each seatpan.The seat electronic box which serves the passengerservice units is installed between the front and rearlegs.

SEATPANThe upholstered seatpan is installed on the seatframework.It is not foldable or adjustable.

BACKRESTThe upholstered backrest assembly of each seat canbe hydraulically reclined backwards until it hits anadjustable mechanical stop.The backrest can be mechanically folded forward.

TABLEA folding table is installed in the rear of eachbackrest.When not in use, it is kept in a recess in the backrestby means of a latch.Two hinged arms hold the table when it is folded down.In-armrest tables are installed in the seats, locatedjust behind partitions, galleys or lavatories.

SEAT BELTEach seat is equipped with a seat belt.It is attached to the seat framework and has a buckleto lock and to adjust the seat belt length.

ARMRESTEach 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 button for the backrest and anashtray are installed in the armrest.

POCKETA pocket is installed on the back of each seat backrest.A safety instruction card and an air-sickness bag arekept in this pocket.

TMUESPS02-T01 LEVEL 3



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PASSENGER AND ATTENDANT SEATS - PAX SEAT

TMUESPS02-P01 LEVEL 3



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PAX SEAT ATTACHMENT

A quick release fitting in each rear leg and a retainerin each front leg attach the seat unit to the seattracks.By placing the quick release device in the up position,the seat can be moved on the tracks or removedcompletely.




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PASSENGER AND ATTENDANT SEATS - PAX SEAT ATTACHMENT



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CABIN ATTENDANT SEAT

Cabin attendant seats are installed in the forward andaft utility areas or in the passenger seating area.The different types of cabin attendant seats are freestanding, swivel and wall mounted attendant seats.




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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT



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CABIN ATTENDANT SEAT DESCRIPTION

Cabin Attendant seats consist of:- an aluminium framework,- a backrest with cushion,- a seatpan with cushion,- a headrest with cushion,- a stowage container and,- seat belts.

FRAMEWORKThe seat frame of the cabin attendant seat is assembledout of two aluminium side frames and a backrestframework.

HEADRESTThe headrest cushion is upholstered with foam and seatfabric.The headrest is attached to the seat frame.

BACKRESTThe backrest cushion is upholstered with foam and seatfabric.

SEATPANThe seatpan is made of an aluminium pan.The seatpan cushion is upholstered with foam and seatfabric.Hinges attach the seatpan to the seat frame.The seatpan is spring loaded to retrct when not inuse.

SAFETY HARNESSEach cabin attendant seat has a seat belt and a shoulderharness with a center buckle.The shoulder harness is pulled-in automatically oninertia reels when not in use.

STOWAGE CONTAINERA stowage container with a latch door is located belowthe seatpan.




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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT DESCRIPTIONTMUESPS02-P04 LEVEL 3



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CABIN ATTENDANT SEAT ATTACHMENT

Cabin attendant seats are attached to walls or to thecabin floor.

WALL MOUNTEDThe three sections of the cabin attendant seat areattached with six bolts to:

- partitions,- lavatories walls.




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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - WALL MOUNTED




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FREE STANDINGFree standing cabin attendant seats can be mounted onseat rails with inch by inch flexibility.Free standing cabin attendant seats can also beattached to the cabin floor structure by hardpoints.




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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - FREE STANDING




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SWIVELSwivel attendant seats are attached to the cabin floorstructure by hardpoints.




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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - SWIVEL




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SELF EXAMINATION

How are passenger seats attached ?A - With retainers in the front legs and

with quick release fittings in the rearlegs.

B - With retainers in the front legs as wellas in the rear legs.

C - With quick release fittings in the frontlegs as well as in the rear legs.

TMUESPS02 LEVEL 3



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25-20-00 CABIN PANEL REMOVAL/INSTALLATION

CONTENT:Ceiling PanelsOverhead Stowage CompartmentsPassenger Service Information Unit (PSIUs)Cove Light PanelsUpper Sidewall PanelsLower Sidewall Panels

TMUESCB01 LEVEL 3



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CABIN PANEL REMOVAL/INSTALLATION

CEILING PANELS

To remove the ceiling panel, apply the followingprocedure :

- Disconnect the two electrical connectorsthrough access doors located in thecorresponding overhead stowage compartment.

- Unlock the two quick release fasteners at theleft side of the ceiling panel.

- Push the left side of the ceiling panel upward.- Move the ceiling panel to the left and out ofthe spring fasteners.

- Lower the right side and slide the ceilingpanel out, making sure the right side is clearfrom the overhead stowage compartments.

- Remove the ceiling panel.

TMUESCB01-T01 LEVEL 3



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TMUESCB01-P01 LEVEL 3

CABIN PANEL REMOVAL/INSTALLATION - CEILING PANELS



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OVERHEAD STOWAGE COMPARTMENTS

Before removing the overhead stowage compartment :- the ceiling panels and the cove light panelsadjacent to the stowage compartment,

- the emergency oxygen container,- the Passenger Service Information Unit,

must be removed.

On the stowage compartment lower side, remove the boltsand washers on support plates "F" and junction plates"D".Disconnect the turnbuckles at support plates "F" andattachment point "G".Support the stowage compartment.Inside the compartment, remove the pin at upperattachment points "A" and "H",Remove the overhead stowage compartment.




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CABIN PANEL REMOVAL/INSTALLATION - OVERHEAD STOWAGE COMPARTMENTS



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PSIUs

To remove the Passenger Service Information Unit, applythe 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 mountingrail,Disconnect the electrical connectors,Remove the PSIU.NOTE : For installation use the tool pulley assembly

to insert the rubber seal properly.




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TMUESCB01-P03 LEVEL 3

CABIN PANEL REMOVAL/INSTALLATION - PSIUs



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COVE LIGHT PANELS

To remove the cove light panel, apply the followingprocedure :

- Remove the seal from the rail at the junctionwith the overhead stowage compartment,

- Move the panel to disconnect it from the rail,- Remove the bonding strap,- Lift the panel, and pull it out.




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CABIN PANEL REMOVAL/INSTALLATION - COVE LIGHT PANELSTMUESCB01-P04 LEVEL 3



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To remove the upper sidewall panel apply the followingprocedure :

- First, remove the passenger seats in the areaof the upper sidewall panel which is to beremoved,

- Remove the decor cover and the inner pane fromthe window,

- Remove the 2 screws fitted on each window,- Pull out the lining strips,- Lift the panel to release it from the mountingbrackets and remove it.


To remove the lower sidewall panel, apply the followingprocedure :

- Use a punch to release the center pins of thequick release pins,

- Pull the lower edge of the panel away from thecompartment wall,

- Pull the panel down and remove the fastenersfrom the attachment fittings,

- Remove the panel.




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CABIN PANEL REMOVAL/INSTALLATION - UPPER AND LOWER SIDEWALL PANELSTMUESCB01-P05 LEVEL 3



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TMUESCB01 LEVEL 3



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25-20-00 CABIN EQUIPMENT AND FURNISHINGCOMPONENTS

CONTENTS:Ceiling PanelsOverhead Stowage CompartmentsPassenger Service Information Units (PSIUs)Cove Light PanelsUpper Sidewall PanelsLower Sidewall PanelsCabin Attendant SeatsPassenger seats

TMUESCE01 LEVEL 3



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CABIN EQUIPMENT AND FURNISHING COMPONENTS

CEILING PANELS

IDENTIFICATIONFIN: TBD

LOCATIONZONE: 230, 250, 220, 260

OVERHEAD STOWAGE COMPARTMENTS


LOCATIONZONE: 200

TMUESCE01-T01 LEVEL 3



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CABIN EQUIPMENT AND FURNISHING COMPONENTS - CEILING PANELS - OVERHEAD STOWAGE COMPARTMENTSTMUESCE01-P01 LEVEL 3



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PASSENGER SERVICE INFORMATION UNITS (PSIUs)


LOCATIONZONE: 200

COVE LIGHT PANELS


LOCATIONZONE: 200




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TMUESCE01-P02 LEVEL 3

CABIN EQUIPMENT AND FURNISHING COMPONENTS - PASSENGER SERVICE INFORMATION UNITS (PSIUs) -COVE LIGHT PANELS



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LOCATIONZONE: 200



LOCATIONZONE: 200




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CABIN EQUIPMENT AND FURNISHING COMPONENTS - UPPER SIDEWALL PANELS - LOWER SIDEWALL PANELSTMUESCE01-P03 LEVEL 3



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LOCATIONZONE: 220, 240, 260




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CABIN EQUIPMENT AND FURNISHING COMPONENTS - CABIN ATTENDANT SEATSTMUESCE01-P04 LEVEL 3



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PASSENGER SEATS


LOCATIONZONE: 200




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CABIN EQUIPMENT AND FURNISHING COMPONENTS - PASSENGER SEATSTMUESCE01-P05 LEVEL 3



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TMUESCE01 LEVEL 3



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25-60-00 ESCAPE FACILITY PRESENTATION

CONTENTS:GeneralCockpitPassenger Door SlideEmergency Exit SlideSlide InstallationSelf Examination

TMUESEP05 LEVEL 1



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ESCAPE FACILITY PRESENTATION

GENERAL

Escape facilities are provided for passenger and crewevacuation.They are located in the cockpit and in the cabin.

COCKPIT

In case of emergency evacuation, there are twopossibilities for the flight crew to evacuate thecockpit.The simplest emergency evacuation procedure for theflight crew is to go through the cockpit door and usethe passenger door slide.If necessary a secondary means enables the flight crewto evacuate the cockpit by opening the sliding windowsand using the escape ropes stowed in the ceiling.

PASSENGER DOOR SLIDE

Single lane escape slides are installed on eachpassenger door.They provide quick evacuation for the passengers andthe crew in an emergency evacuation and operateautomatically if the door is opened in ARMED mode.

EMERGENCY EXIT SLIDE

The two emergency exits of each side are equipped witha dual lane offwing escape slide.The four emergency exits provide quick evacuation forthe passengers. The dual lane escape slide operatesautomatically if one door of each side is opened inARMED mode.

TMUESEP05-T01 LEVEL 1



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TMUESEP05-P01 LEVEL 1




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SLIDE INSTALLATION

Escape slides are installed at all the aircraft exits.The passenger door escape slide and its inflationreservoir are located in a container at the bottom ofthe door.The emergency exit escape slide is located in acontainer above the wing in each wing-to-fuselagefairing, and the inflation reservoirs are installedin the AFT cargo compartment, behind the sidewallpanels.




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SELF EXAMINATION

Where is the inflation reservoir of the escapeslide of emergency exit located ?

A - In a container at the bottom of the door.B - In the overhead stowage compartment over

the door.C - In the cargo compartment.

TMUESEP05 LEVEL 1



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25-60-00 ESCAPE FACILITY PRESENTATION

CONTENTS:GeneralCockpitPassenger Door SlideEmergency Exit SlideSlide InstallationSelf Examination

TMUESEP04 LEVEL 1



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GENERAL

Escape facilities are provided for passenger and crewevacuation.They are located in the cockpit and in the cabin.

COCKPIT

In case of emergency evacuation, there are twopossibilities for the flight crew to evacuate thecockpit.The simplest emergency evacuation procedure for theflight crew is to go through the cockpit door and usethe passenger door slide.If necessary a secondary means enables the flight crewto evacuate the cockpit by opening the sliding windowsand using the escape ropes stowed in the ceiling.

PASSENGER DOOR SLIDE

Single lane escape slides are installed on eachpassenger door.They provide quick evacuation for the passengers andthe crew in an emergency evacuation and operateautomatically if the door is opened in ARMED mode.

EMERGENCY EXIT SLIDE

The four emergency exits are equipped with a singlelane escape slide.The four emergency exits provide quick evacuation forthe passengers. The single lane escape slides operatesautomatically if the door is opened in ARMED mode.




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SLIDE INSTALLATION

Escape slides are installed at all the aircraft exits.The passenger door escape slide and its inflationreservoir are located in a container at the botton ofthe door.The emergency exit escape slide is located in acontainer under the door and the inflation reservoiris over the door in the overhead stowage compartment.




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SELF EXAMINATION

Where is the inflation reservoir of the escapeslide of emergency exit located ?

A - In a container at the botton of the door.B - In the overhead stowage compartment over

the door.C - In the cargo compartment.

TMUESEP04 LEVEL 1



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25-60-00 MISCELLANEOUS EMERGENCYEQUIPMENT PRESENTATION

CONTENTS:GeneralFire ExtinguisherOxygen KitSmoke HoodCrash AxeFirst Aid KitMegaphoneEmergency Radio BeaconFlash LightLife Vest Manual Release ToolSelf Examination

TMUESEE03 LEVEL 1



UC64200


MISCELLANEOUS EMERGENCY EQUIPMENT PRESENTATION

GENERAL

The emergency equipment is kept in different locationsin the cockpit and the cabin.Emergency equipment is composed of :

- Fire extinguisher,- Oxygen kit,- Smoke hood,- Crash axe,- First aid kit,- Megaphone,- Emergency radio beacon,- Flash light,- Life vest,- Manual release tool.

NOTE: The exact quantity and location of these itemsdepend on individual airline configuration andcabin layout.

FIRE EXTINGUISHER

The portable fire extinguishers are used to extinguishany fire in the cockpit and cabin.They are fitted under the attendant seats in thepassenger compartment and in the cockpit next to thethird occupant seat

OXYGEN KIT

The portable oxygen equipment is installed in thepassenger cabin to supply oxygen to the passengers inan emergency.

SMOKE HOOD

The flight crew emergency breathing hood systemprovides protection to the eyes and respiratory systemfor crew members.Smoke masks are also supplied for the cabin attendantsto fight a fire or, against the emission of smoke andnoxious gases.

CRASH AXE

The crash axe is used to cut through light structures,panels and windows to get access or exit in anemergency.The insulated handle is resistant to high voltages.

FIRST AID KIT

First aid kits are kept near forward and aft attendantstations, in overhead stowage compartments.

MEGAPHONE

A megaphone is stowed in the left forward and aftattendant stations.

TMUESEE03-T01 LEVEL 1



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TMUESEE03-P01 LEVEL 1




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EMERGENCY RADIO BEACON

An emergency radio beacon is stowed in the left aftattendant station.

FLASH LIGHT

Hand held flash lights are installed as movable lightsources.They are used if bad light conditions occur during anon-board emergency.

LIFE VEST

One passenger life vest is stowed under each passengerseat.Life vest components include :

- a CO2 gas inflation system,- an oral inflation tube,- a lamp for survivor location in poor visibilityor night conditions,

- a water activited cell (battery) to supply thelamp,

- a whistle to attract attention

MANUAL RELEASE TOOL

Manual release tools, used to open the passenger oxygenmask doors, are available at each cabin attendantstation.

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SELF EXAMINATION

Smoke hoods are supplied for the cabin attendantsto:

A - supply oxygen for passengers.B - fight a fire or against emission of

smoke or noxious gases.C - breathe oxygen.

TMUESEE03 LEVEL 1



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25-62-00 PASSENGER DOOR ESCAPE SLIDEDESCRIPTION/DEPLOYMENT

CONTENTS:Passenger Door Escape Slide Description/Deployment

TMUESFB03 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

Passenger Door Escape Slide Description/Deployment

A slide deployment can be initiated when ever the dooris opened in the emergency configurationWhen the slide is armed it can be checked on a redindicator, located on the button of the slidedecorative cover.As soon as the door handle is lifted the door opensand the escape slide is ejected from its container andthe inflation system is activated.The deployment and inflation sequence is automaticallyinitiated when the cabin door is opened.The slide deploys into its final usable position within3 seconds.The escape slide is connected to the cabin floor by agirt extension which is attached to the girt bar atthe door sill.Should the escape slide not inflate automatically ared manual inflation handle must be pulled. This handleis located on the girt extension.Let’s have a look at the inflation system.The system is automatically activated as soon as theslide is ejected from its container.The valve regulator assembly incorporates a directreading, temperature compensated pressure gage, whichindicates the gas charge in the inflation reservoir,relative to ambient temperature.The gas stored within the inflation reservoir isdischarged into the inflatable through flexible hosesand an aspirator.Ambient air is drawn in, through the flaps of theaspirator by the partial vacuum, created by the highvelocity in the venturi.

Then the flaps close and the remaining gas charge topsthe inflatable up to its operating pressure.Inflation is therefore rapid and reservoir size ismaintained at minimum.Restraint devices are used to control the deploymentsequence.The primary restraint mechanism is a precision fusefrangible link, which separates at a predeterminedforce value.In case of pressure loss, no fail handles, located onboth side of the runway end, allow the inflation tobe used as a hand-held evacuation chute.In the event of a ditching, grasp lines are fittedaround the outside of the inflatable to facilitate theuse of slide as a flotation device.The slide is equipped with a lighting system.The lights located along the side tubes and across therunway, are supplied from the aircraft emergency powersupply units.The lights are automatically supplied with power whenthe slide is deployed.The escape slide can be disconnected from the aircraftfloor whenever necessary.For the disconnection the following steps must betaken.Lift the flap of the girt extension to gain access tothe white disconnect handle.Pull the handle.The girt extension incorporates a quick releasefeature, a daisy chain, which permits rapid detachmentof the inflatable from the aircraft.

TMUESFB03-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENTTMUESFB03-P01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

Once detached from the floor the inflatable drops fromthe aircraft but remains attached to the girt bar bymeans of a string, which must be cut by using the knifelocated next to it, on the girt extension.The inflatable is then completely disconnected fromthe aircraft.

TMUESFB03-T01 LEVEL 3



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25-62-00 PASSENGER DOOR ESCAPE SLIDEDISCONNECTION

CONTENTS:Passenger Door Escape Slide Disconnection

TMUESFG02 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE DISCONNECTION

Passenger Door Escape Slide Disconnection

Disconnect the electrical line.Tie the retaining cord to the slide handle.Disconnect the slide attaching device by removing thesafety pin.Undo the lacing system.Remove the girt bar by unlocking the door thresholdsupports.Using the retaining cord, take the escape slide away.

TMUESFG02-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE DISCONNECTIONTMUESFG02-P01 LEVEL 3



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TMUESFG02 LEVEL 3



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25-62-00 PASSENGER DOOR ESCAPE SLIDEINSTALLATION

CONTENTS:Passenger Door Escape Slide Installation

TMUESFA03 LEVEL 3



UC64200


PASSENGER DOOR ESCAPE SLIDE INSTALLATION

PASSENGER DOOR ESCAPE SLIDE INSTALLATION

Check that door emergency opening percussion systembehind the door support arm, is in the disarmedposition.First, connect the electrical line... place it on theright-hand side or left-hand side according to thedoor.Fit the girt bar into the mooring line and slide itinto 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 electrical connector.Screw the container in 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 iscorrect.Lift the door and check that the slide mechanism isproperly attached to the door.Remove the safety pin from the slide percussion system.Fit the slide cover.

TMUESFA03-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE INSTALLATIONTMUESFA03-P01 LEVEL 3



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TMUESFA03 LEVEL 3



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25 - EQUIPMENT/FURNISHING

25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFTDESCRIPTION / DEPLOYMENT

CONTENTS:DescriptionNormal OperationManual Operation

TMUESRB01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT DESCRIPTION / DEPLOYMENT

NOTE : In this module the PASSENGER DOOR SLIDEDESCRIPTION / DEPLOYMENT is described on theA320 but the principle is the same for the A319and the A321.

DESCRIPTION

The forward and rear cabin doors of the A320 areequipped with slide rafts.The inflation and deployment sequence is automaticallyinitiated when the door is opened in armedconfiguration.The slide raft is ejected out of its container, andremains folded by restraint devices which break atdetermined pressure points to allow correctdeployment.The slide raft is stowed in a container connected tothe cabin door.

NORMAL OPERATION

As soon as the door handle is lifted, the door ispneumatically pushed open and the slide raft, fixedwith a girt bar to the cabin floor, is pulled out ofthe container, drops down and inflates automatically.As the inflatable falls down, the inflation system isactivated.The gas stored in the inflation cylinder is dischargedthrough flexible hoses to the aspirators.The aspirator flaps open and ambient air is drawn inunder partial vaccum, created by the high velocity inthe venturi.Then the flaps close and the remaining gas, tops upthe inflatable to its operational pressure.

Should the automatic inflation system fail, the slideraft must be inflated manually.

MANUAL OPERATION

For that, the red manual inflation handle located onthe right hand side of the girt extension must bepulled.A lighting system is fitted on both sides and on therunway end of the inflatable. The power supply forthis lighting system is provided by the cabin emergencypower supply units.Two assist handles are located on both sides at thelower end of the inflatable, to allow assisting peopleto hold on.In case of a ditching, prior to door opening thesurvival kit must be connected to the slide raft. Thesurvival kit is stored in the nearest overhead bin.Place the survival kit on the floor, forward of thedoor, detach the lanyard from the girt bar.Pull the lanyard and the hook, to snap on front of thesurvival kit.Then open the door.The slide raft drops out of the container and deploys.

TMUESRB01-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT DESCRIPTION / DEPLOYMENTTMUESRB01-P01 LEVEL 3



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TMUESRB01 LEVEL 3



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25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFTDISCONNECTION.

CONTENTS:PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

TMUESRG01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

Disconnect the pack-assembly electrical supply.The quick-disconnect connector is installed below thecable routing velcro.Open the girt flap.Open the lanyard velcro and remove the survival kitattach-loop from the telescopic end fitting of thegirt bar.Open the blue and the green velcros and separate thesurvival kit lanyard and the girt bar release-strap.Remove the girt bar release-strap from the girt barrelease-lever.Pull the mooring line from the girt pocket and supportthe escape slide raft with the mooring line.Pull the release handle, release the mooring lineslowly and let the girt lace-up joint and the girtassembly release from the girt bar.Carefully lower the escape slide raft to the ground.Make sure that you do not damage the reservoir whenyou lower the slide raft to the ground.Hold the girt bar and push in the girt bar release-leverby hand.Remove the girt bar from the floor attach fittings.Remove the mooring line loop-end from the girt bar andkeep the girt bar with the aircraft.Lift the empty pack assembly soft-cover clear of thepassenger/crew door and close the door.Remove the pack assembly decorative-cover and keep itwith the aircraft.Loosen the link nut and remove and retain the attachlink and the pull-handle from the stud assembly.Remove the stud assemblies, with the allen key, fromthe door attach anchor nuts.

Move the packboard inboard on its supports and holdit.Disconnect the pack assembly connector from theelectrical connector installed on the passenger/crewdoor.Remove the packboard from the passenger crew doorsupports.Service the door damper and emergency operationcylinder.

TMUESRG01-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.TMUESRG01-P01 LEVEL 3



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TMUESRG01 LEVEL 3



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25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFTINSTALLATION.

CONTENTS :PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.

TMUESRA01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.


Make sure that the operation striker lever of the doordamper and emergency operation cylinder is in theDISARMED position.Make sure that the passenger/crew door on which youwill install the pack assembly is closed and locked.Make sure that the emergency control handle is in theDISARMED position and that the safety pin is installed.Make sure that the lockpin assembly is installed inthe operating head of the slide raft inflationreservoir.Check the pack electrical supply-cable, and make surethat the cable is installed for the left door or theright door as required.Make sure that the short girt flap is on the top ofthe 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 awayfrom the slide raft pack, and that the telescopic endis in the forward position in relation to the aircraft.Install the mooring line loop on the girt bar rearend.Pull the cord loops attached to the long girt flap upthrough the grommets in the short girt flap.Put the loops through each other from each end of thegirt towards the center.Put the parachute pin through the small cord loop andremove and discard the temporary tie.Safety the parachute pin in position with nylon threadwith a breaking strain.

Put the girt bar release strap through the girt barrelease lever and position the release strap along theslide raft girt.Attach the survival kit lanyard to the release strapwith the same color velcros and position the lanyardalong the slide raft girt.Fold the long girt flap over the girt bar and attachit to the short girt flap velcro attach strips.Lift the slide raft pack assembly onto thepassenger/crew door supports.Carefully move the packboard assembly inboard at anangle onto its supports and hold it.Connect the pack assembly connector on the electricalconnector on the passenger/crew door.Move the pack assembly in position and install thestud assemblies in the door attach anchor nuts.Carefully tighten the two stud assemblies with theallen key, until there is no play between the door andpackboard assembly.Connect the two pull handles to the stud assemblieswith the attach links.Remove the safety pin from the emergency control handleand set the handle to the ARMED position.Hold the passenger/crew door to prevent it movingoutboard and set the door control handle to the OPENposition.Install the girt bar into the floor attach fittings.Slowly move the door control handle to CLOSED position,and move the emergency control handle to the DISARMEDposition.Set the door control handle to the OPEN position.

TMUESRA01-T01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.TMUESRA01-P01 LEVEL 3



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PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.(Cont‘d)

Make sure that the control shaft levers and thetelescopic forks on the door have engaged correctlywith the girt bar.Set the door control handle to the CLOSED position,and set the emergency control handle to the ARMEDposition.Hold the passenger/crew door to prevent it movingoutboard and set the door control handle to the OPENposition.Make sure that the girt bar has engaged correctly withthe floor attach fittings.Set the door control handle to the CLOSED position.Set the emergency control handle to the DISARMEDposition and install the safety pin.Remove the lockpin assembly from the operating headof the slide raft inflation reservoir and put thelockpin assembly in the stowage pocket installed onthe pack assembly soft-cover.Put the pack assembly decorative-cover in position.Connect the cover attach straps.Check the indication of the decorative cover bracketand girt-bar visual indicator.Make sure that the operation striker lever of the doordamper and emergency operation cylinder is in the ARMEDposition.

TMUESRA01-T02 LEVEL 3



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25-62-00 OFFWING ESCAPE SLIDE DEPLOYMENT

CONTENTS:Offwing Escape Slide Deployment

TMUESFC01 LEVEL 3



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OFFWING ESCAPE SLIDE DEPLOYMENT

NOTE : In this module the OFFWING ESCAPE SLIDEDEPLOYMENT is described on the A320 but theprinciple is the same for the A319.

The offwing escape slide is packed in a containerassembly, which in turn is mounted into the centrefuselage belly fairing.Two type "3" exits are located over each wing and arealways in armed configuration.Two emergency lights underneath the wing exits lightthe escape way leading to the escape slide which ispointed out with red fluorescent arrows.The opening of one wing exit will initiate thedeployment sequence.The escape slide is ejected out of its, container anddeploys 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 theinflation sequence.The gas stored in the cylinder is discharged to theinflatable slide through flexible hoses and anaspirator.The aspirator flaps open and ambient air is drawn intothe slide.The slide remains folded by restraint devices, whichbreak at a predetermined force, to permit correctdeployment.Two black arrows located on the ramp section indicatethe direction of the escape route.A lighting system is provided on the slide.The lights are located on the ramps along the sidetubes and across the runway end.

A red manual inflation handle, located in each exitframe, must be pulled to manually activate theinflation and deployment sequence, in case of automaticrelease failure.If the slide is deployed but not inflated, it stillcan be used as a hand-held escape chute.On the ramp section top, a hook is located and thishook must be connected to an attachment fitting on thewing.Two red NO FAIL HANDLES are located on both sides ofthe escape slide on the runway end.Four able bodied men must hold the deflated slideextended, by means of the no fail handles, to allowthe passengers on the wing to descend.

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TMUESFC01-P01 LEVEL 3

OFFWING ESCAPE SLIDE DEPLOYMENT



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25-62-00 OFFWING ESCAPE SLIDE REMOVAL

CONTENTS:Offwing Escape Slide Removal

TMUESFE01 LEVEL 3



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OFFWING ESCAPE SLIDE REMOVAL

NOTE : In this module the OFFWING ESCAPE SLIDE REMOVALis described on the A320 but the principle isthe same for the A319.

Push in the flapper valves of the aspirator and releasethe pressure from the offwing escape slide.Disconnect the inflation hose from the stowagecompartment union.Disconnect the electrical connectors at the emergencylighting supply cable.Undo the strap press-studs, to separate the containerpanel from the escape slide.To release the TOP girt bar assembly, support the slideand open the girt flap.Remove the girt release handle, and pull it.Undo the laces.Follow the same procedure to release the LOWER andFORWARD 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 sealstrips.Loosen the attach panel studs.Move the top of the stowage compartment outboard atan angle and hold it.Disconnect the inflation hose from the fuselage union.Disconnect the emergency lighting electricalconnector, and remove the escape slide stowagecompartment from the aircraft.The inflation reservoir has to be replaced.

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OFFWING ESCAPE SLIDE REMOVAL



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25-62-00 OFFWING ESCAPE SLIDE CYLINDERREMOVAL/INSTALLATION

CONTENTS:RemovalInstallationTest

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OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION

REMOVAL

WARNINGMake sure that the lockpin assembly is correctlyinstalled in the valve assembly head of the inflationcylinder to prevent an accidental extension of theescape slide.The cylinder is pressurized with gas to 3000 psi(207 bar).The removal/installation procedures of the left andright cylinders are almost identical.

ACCESSOpen 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 ASSEMBLIESLoosen the knurled sleeve nut and remove the twocollets.Move the two cable assemblies apart.

ELECTRICAL CONNECTORDisconnect and put blanking caps on the electricalconnectors.

FLEXIBLE HOSE ASSEMBLYDisconnect the flexible hose assembly from the bulkheadunion.Put blanking plugs on the disconnected line ends.

CYLINDER REMOVALRemove and keep the bolt that supports the flexiblehose assembly.Loosen the attach clamp screws.Remove the inflation cylinder.

INSTALLATION

CYLINDER INSTALLATIONMake sure that the lockpin assembly is correctlyinstalled in the valve assembly head of the inflationcylinder to prevent an accidental extension of theescape slide.Install the cylinder assembly in the support bracket.Tighten the attach clamp screws when in position.

FLEXIBLE HOSE ASSEMBLIESPut the flexible hose assembly in position and tightenthe bolt by hand.Remove the blanking caps and connect the flexible hoseto the bulkhead union.Tighten the bolt.

ELECTRICAL CONNECTORRemove the blanking caps and install the electricalconnector.

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TEST

ADJUSTMENTAfter test tool installation and setting the cursorto zero, (adjusting the flexible assembly nuts ifnecessary) set the emergency exit hatch in armedposition and remove it.Remove the cap and connect the RELEASE TEST TOOL andCABLE ESCAPE SLIDE adapter to the flexible controlassembly.Set the cursor to zero.Put the forward emergency exit-hatch in the armedposition and remove the hatch.Make sure that the test tool cursor has moved to showa minimum indication of 50 mm (1.9685 in.).Adjust conduit, adjust nuts on the flexible controlassembly.Make an adjustment of the conduit length.Set the cursor on the test tool to zero.

CABLE ASSEMBLIESConnect the two cable assemblies.Install the two collets and tighten the knurled sleevenut.

FUNCTIONAL CHECKLift the door lever up to check that the resistanceand the play between the flexible control and releasecable assembly are satisfactory.

LOCKPIN ASSEMBLYRemove the lockpin from the cylinder and put it in thestowage pocket.

CLOSE UPInstall the access panels.Remove the platform.Close the cargo doors.

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25-62-00 OFFWING ESCAPE SLIDE INSTALLATION

CONTENTS: Offwing Escape Slide Installation

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OFFWING ESCAPE SLIDE INSTALLATION

NOTE : In this module the OFFWING ESCAPE SLIDEINSTALLATION is described on the A320 but theprinciple is the same for the A319.

Put the escape slide stowage compartment in position.Move the top of the stowage compartment outboard atan angle and hold it.Connect the inflation hose to the fuselage union.Connect the emergency lighting electrical connector.Put the stowage compartment in position and tightenthe attach panel studs.Put the seal strips and the seal attach plate inposition and install and tighten the screws.

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OFFWING ESCAPE SLIDE INSTALLATION



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25-62-00 EMERGENCY EQUIPMENT/EMERGENCY EXIT ESCAPE SLIDEDESCRIPTION/DEPLOYMENT

CONTENTS:Description/Deployment

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EMERGENCY EQUIPMENT/EMERGENCY EXIT ESCAPE SLIDE

DESCRIPTION/DEPLOYMENT

The escape slide for the type "C" doors, is storedunderneath the door inside the fuselage.

The inflation cylinder is located in the overhead bin,over the door.

The cylinder is in a protection box and can be seenthrough a plexiglass window.

The pressure can be checked on the pressure levelindicator.For correct pressure the needle must be in the greensection.

To initiate the slide deployment, the door must beopened in the armed configuration.

To open the door, uncover the control handle, lift thehandle fully up, and release!

The door opens outwards. The escape slide in themeantime inflates and deploys completely. The escapeslide is ready for use when the door is locked in thefully open position.

Should the door open but the escape slide not inflate,a red handle for manual inflation is located in thedoor upper right hand frame.

The transparent protective cover must be taken off andthe red handle pulled to initiate the manual slideinflation.

The escape slide for the type "C" doors is stowed ina special compartment in the fuselage, underneath thedoor.

The deployment sequence starts as soon as the door isopened in armed configuration.

One aspirator is connected to the inflation cylinderby means of a flexible hose.

During the door opening the inflation cylinderregulator value is actuated, and primary gas issupplied to the aspirator. The aspirator flaps openand outside air is drawn in. The flaps close as soonas the correct pressure is reached.

The slide has a single lane sliding surface with abrake path at the bottom end, which slows down thespeed of the evacuees.

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EMERGENCY EQUIPMENT - EMERGENCY EXIT ESCAPE SLIDE - DESCRIPTION/DEPLOYMENTTMUESES05-P01 LEVEL 3



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EMERGENCY EQUIPMENT/EMERGENCY EXIT ESCAPE SLIDE

A lighting system is fitted along both sides and atthe bottom of the slide.

The lights automatically come on during the slidedeployment. They remain on as long as the emergencypower supply operates.

A reentry strap is fixed on one side of the slide.

A yellow life line is fixed along the outside of theinflation chambers on both sides.

Red no-fail handles are located on both sides forassisting people to hold the slide in case it is usednot inflated as an evacuation chute.

The slide is slightly canted in order to deploy atsafe distance away from the engine.

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25-62-00 EMERGENCY EQUIPMENTEMERGENCY EXIT ESCAPE SLIDEDISCONNECTION

CONTENTS:Disconnection

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EMERGENCY EQUIPMENTEMERGENCY EXIT ESCAPE SLIDE

DISCONNECTION

The disconnect handle and a knife are located on thegirt extension close to the door step.

The knife is on the left hand side in a clearly markedpouch.

A disconnect handle is located under a velcro flapmarked "FOR DITCHING USE".

To release the slide, lift the flap, grasp the whitehandle and pull. Should the slide not drop immediately,push down on the girt extension.

The daisy-chain on the packboard releases, and theslide is free to drop.

The slide remains attached to the aircraft by meansof a mooring line.

This line must be cut by means of the hook knife.

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EMERGENCY EQUIPMENT - EMERGENCY EXIT ESCAPE SLIDE - DISCONNECTIONTMUESED05-P01 LEVEL 3



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25-62-00 PASSENGER DOOR ESCAPE SLIDEINFLATION CYLINDER CHECK

CONTENTS:Pressure GaugeSelf Examination

TMUESFJ01 LEVEL 3

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PASSENGER DOOR ESCAPE SLIDE INFLATION CYLINDER CHECK

PRESSURE GAUGE

A pressure gauge viewing window is located on the coverprotecting the escape slide.It allows the check of the cylinder pressure.The indication must be in the green GO band.

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PASSENGER DOOR ESCAPE SLIDE INFLATION CYLINDER CHECKTMUESFJ01-P01 LEVEL 3



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SELF EXAMINATION

Where must the pressure indication be?A - In the green GO band.B - In the red band.C - At zero.

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25-62-00 OFFWING ESCAPE SLIDE INFLATIONCYLINDER CHECK

CONTENTS:Cylinder Pressure Check (From Cargo Compartment)Cylinder Pressure Check From PTP (Low PressConfiguration)Cylinder Pressure Check From PTP (Press OKConfiguration)Self Examination

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK

CYLINDER PRESSURE CHECK (FROM CARGO COMPARTMENT)

A pressure gauge is installed on the cylinder valveassembly.The pressure gauge indicator arrow must be in the greenGO band.

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK -CYLINDER PRESSURE CHECK (FROM CARGO COMPARTMENT)



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CYLINDER PRESSURE CHECK FROM PTP (LOW PRESSCONFIGURATION)

The SYSTEM STATUS line key must be pressed to checkthe slide pressure.SLIDES PRESS LOW line key is pressed to get theinformation messages.The slides where the pressure is low are displayed onthe screen.




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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK -CYLINDER PRESSURE CHECK FROM PTP (LOW PRESS CONFIGURATION)




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CYLINDER PRESSURE CHECK FROM PTP (PRESS OKCONFIGURATION)

The SYSTEM STATUS line key must be pressed to see theslide pressure.If the pressure is ok, the SLIDES PRESS OK messageappears.




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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK -CYLINDER PRESSURE CHECK FROM PTP (PRESS OK CONFIGURATION)




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SELF EXAMINATION

From where is the inflation cylinder checked?A - From the cargo compartment only.B - From the PTP only.C - From the cargo compartment or from the

PTP.

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25-62-00 OFFWING ESCAPE SLIDE RELEASEMECHANISM DESCRIPTION

CONTENTS:GeneralLatch PinManual Release HandlesRelease Cable Path

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION

GENERAL

The escape slide release mechanism consists of threedifferent portions:

- the latch pin,- the manual release handles,- the release cable path.

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - GENERALTMUDOFR01-P01 LEVEL 1



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LATCH PIN

The latch pin has two positions, the normal "armed"position and a retracted position used for maintenanceoperations.Using a hexagonal socket wrench, the latch pin can bepushed into the normal "armed"position and locked inthis position by rotating it quater of a turn.




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TMUDOFR01-P02 LEVEL 1

OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - LATCH PIN



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MANUAL RELEASE HANDLES

In case of failure the slide can be released manuallywith the manual release handles, via the catch lever.The release lever is operated by the latch pin in armedposition, upon inward removal of the hatch.This movement, via the shaft, rod, spring rod, anddouble lever, pulls the release cable.




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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - MANUAL RELEASE HANDLESTMUDOFR01-P03 LEVEL 1



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RELEASE CABLE PATH

The release cable transmits the double lever movementto the connection point in the aft cargo compartmentwhere it is connected to the escape slide cylinder.




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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - RELEASE CABLE PATHTMUDOFR01-P04 LEVEL 1



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THIS INTENTIONALLY LEFT BLANCK

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25-60-00 EMERGENCY EQUIPMENT COMPONENTS

CONTENTS:Passenger Doors-Escape SlideEmergency Exits-Escape SlideEmergency Exits-Inflation CylindersEscape Ropes

TMUESFZ03 LEVEL 3

EFFECTIVITY 25-60-00 Page 1Apr 30/96


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EMERGENCY EQUIPMENT COMPONENTS

PASSENGER DOORS-ESCAPE SLIDE

IDENTIFICATIONFIN: 7500MM, 7501MM, 7502MM, 7503MM

LOCATIONZONE: 831, 841, 832, 842

EMERGENCY EXITS-ESCAPE SLIDE

IDENTIFICATIONFIN: 7504MM, 7505MM


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TMUESFZ03-P01 LEVEL 3

EMERGENCY EQUIPMENT COMPONENTS-ESCAPE SLIDES



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EMERGENCY EXITS-INFLATION CYLINDERS






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EMERGENCY EQUIPMENT COMPONENTS-INFLATION CYLINDERS



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ESCAPE ROPES






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EMERGENCY EQUIPMENT COMPONENTS-ESCAPE ROPES



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THIS PAGE LEFT INTENTIONALLY LEFT BLANK

TMUESFZ03 LEVEL 3



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25-50-00 CARGO COMPARTMENT PRESENTATION

CONTENTS:GeneralFWD Cargo CompartmentAFT Cargo CompartmentBulk Cargo CompartmentAccess

TMUECLP08 LEVEL 1



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CARGO COMPARTMENT PRESENTATION

GENERAL

The lower deck is divided into three cargocompartments.The different cargo compartments are:

- The FWD cargo,- The AFT cargo,- The Bulk cargo compartment.

The FWD and AFT cargo compartments can be optionallyequipped with a semi-automatic cargo loading system.Basically they have tie-down/attachment points for thenets and straps which keep the bulk cargo in place.

FWD CARGO COMPARTMENT

The FWD cargo compartment is basically equipped to beloaded with bulk and loose baggage.The optional semi-automatic cargo loading systemtransports pallets and containers and is operated froma control panel installed on the cargo door.

AFT CARGO COMPARTMENT

The AFT cargo compartment is basically equipped to beloaded with bulk and loose baggage.The optional semi-automatic cargo loading systemtransports pallets and containers and is operated froma control panel installed on the cargo door.

BULK CARGO COMPARTMENT

The Bulk cargo compartment can only be loaded withbulk and loose baggageA divider net with a screen separates the bulk cargocompartment from the AFT cargo compartment.

ACCESS

Access to the FWD, Aft and Bulk cargo compartments isgained by two outwards opening doors.Access to the bulk cargo compartment can also be gainedby the optional bulk cargo door, if it is installed.The cargo doors are located on the right hand side ofthe fuselage.The FWD and AFT cargo doors are operated upward by twohydraulic actuators with pressure provided by theyellow electric pump (normal operation) or by a handpump (manual operation).

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TMUECLP08-P01 LEVEL 1

CARGO COMPARTMENT PRESENTATION



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TMUECLP08 LEVEL 1



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25-50-00 CARGO COMPARTMENT INTERIOR

CONTENTS:GeneralFWD Cargo CompartmentAFT And Bulk Cargo CompartmentCompartment DrainageSelf Examination

TMUECCI01 LEVEL 1



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CARGO COMPARTMENT INTERIOR

GENERAL

The inside of the cargo compartments is fitted withfloor and ceiling panels, sidewall linings andpartition walls.All the linings are sealed to prevent leakage of waterand spilt fluids.Rapid decompression panels are installed in the cutoutsof the ceiling panels and lateral right sidewalllining.

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TMUECCI01-P01 LEVEL 1




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The floor panels, the ceiling panels and the sidewalllinings prevent damage to the aircraft structure.The floor panels are of sandwich construction and havenon slip surfaces.The ceiling panels are of a sandwich construction andare made of flame resistant synthetic material andpermit fast decompression.They are attached to thestructure with quick release fasteners.The sidewall linings are of a sandwich constructionand are made of flame resistant synthetic material.They are attached to the structure with quick releasefasteners.The FWD cargo compartment is fitted with two fixedpartition walls. They are of a sandwitch constructionand are made of flame resistant synthetic material.Theyare attached to the structure with quick releasefasteners.




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AFT AND BULK CARGO COMPARTMENT

The floor panels, the ceiling panels and the sidewalllinings prevent damage to the aircraft structure.The floor panels are of sandwich construction and havenon slip surfaces.The ceiling panels are of a sandwich construction andare made of flame resistant synthetic material andpermit fast decompression. They are attached to thestructure with quick release fasteners.The sidewall linings are of a sandwich constructionand are made of flame resistant synthetic material.They are attached to the structure with quick releasefasteners.They are equipped with access panels to giveaccess to other systems.The AFT cargo compartment is fitted with two fixedpartition walls.The partition walls are of a sandwichconstruction and are made of flame resistant syntheticmaterial.They are attached to the structure with quickrelease fasteners.




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COMPARTMENT DRAINAGE

The FWD and AFT cargo compartments have drainagesystems.




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SELF EXAMINATION

Where are the rapid decompression panels installed?A - in the cutouts of the ceiling panels.B - in the fixed partition walls.C - in the cutouts of the ceiling panels and

lateral right sidewall linings.

TMUECCI01 LEVEL 1



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25-50-00 CARGO COMPARTMENT CAPABILITIES

CONTENTS:GeneralFWD Cargo CompartmentAFT/Bulk Cargo CompartmentSelf Examination

TMUCLSB01 LEVEL 1



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CARGO COMPARTMENT CAPABILITIES

GENERAL

Here are the cargo loading capabilities.The FWD, AFT and bulk cargo compartments are basicallyequipped to be loaded with bulk and loose baggage.If the cargo loading system option is installed, theFWD and AFT cargo compartments can be loaded withcontainers or pallets.

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TMUCLSB01-P01 LEVEL 1

CARGO COMPARTMENT CAPABILITIES - GENERAL



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The FWD cargo compartment can be basically loaded withbulk and loose baggage.If the cargo loading system is installed in the FWDcargo compartment, it is possible to load 3 Unit LoadDevices (ULDs) which can be mixed (containers orpallets).For the bulk loading, the FWD cargo compartment isdivided into 2 zones by a lateral divider net.A longitudinal door net is installed around the doorto keep the cargo door area free.




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CARGO COMPARTMENT CAPABILITIES - FWD CARGO COMPARTMENT



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AFT AND BULK CARGO COMPARTMENTS

The AFT cargo compartment can be basically loaded withbulk and loose baggage.If the cargo loading system is installed in the AFTcargo compartment, it is possible to load 4 Unit LoadDevices (ULDs) which can be mixed (containers orpallets).For the bulk loading, the AFT cargo compartment isdivided into 3 zones by 2 lateral divider nets.A longitudinal door net is installed around the doorto keep the cargo door area free.The bulk cargo compartment can only be loaded withbulk loading.It is separated from the AFT cargo compartment by alateral divider net.If the bulk door option is installed, a door netprevents damage to the bulk door and keeps the cargodoor area free.




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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENTS



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SELF EXAMINATION

How many Unit Load Devices (ULDs) can be loaded inthe FWD cargo compartment, if the Cargo LoadingSystem is installed ?

A - with 0 ULD.B - with 2 ULDs.C - with 3 ULDs.

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CONTENTS:GeneralFWD Cargo CompartmentAFT/Bulk Cargo CompartmentSelf Examination

TMUCLSB07 LEVEL 1



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GENERAL

Here are the cargo loading capabilities.




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The FWD cargo compartment can be loaded withcontainers, pallets or with bulk loading.In the FWD cargo compartment, it is possible to load2 Unit Load Devices (ULDS) which can be mixed(containers or pallets).For the bulk loading, the FWD cargo compartment isdivided into 2 zones by 1 lateral divider net.Lateral and longitudinal door nets are installed aroundthe door to keep the cargo door area free.




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AFT/BULK CARGO COMPARTMENT

The AFT/Bulk cargo compartment can be loaded withcontainers, palets or with bulk loading.In the AFT cargo compartment, it is possible to load2 Unit Load Devices (ULDS) which can be mixed(containers or pallets) and 1 narrower additionalcontainer (option).For the bulk loading, the AFT cargo compartment isdivided into 2 zones by 1 lateral divider net.Lateral and longitudinal door nets are installed aroundthe door to keep the cargo door area free.The bulk cargo conpartment can only be loaded withbulk loading.It is separated from the AFT cargo compartment by alateral divider net.




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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENT



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SELF EXAMINATION

How many Unit Load Devices (ULDS) can be loaded inthe FWD cargo compartment?

A - with 0 ULD.B - with 2 ULDS.C - with 3 ULDS.

TMUCLSB07 LEVEL 1



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CONTENTS:GeneralFWD Cargo CompartmentAFT and Bulk Cargo CompartmentsSelf Examination

TMUCLSB0A LEVEL 1



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GENERAL

Here are the cargo loading capabilities.The FWD, AFT and bulk cargo compartments are basicallyequipped to be loaded with bulk and loose baggage.If the cargo loading system option is installed, theFWD and AFT cargo compartments can be loaded withcontainers or pallets.

TMUCLSB0A-T01 LEVEL 1



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TMUCLSB0A-P01 LEVEL 1




UC64200




The FWD cargo compartment can be basically loaded withbulk and loose baggage.If the cargo loading system is installed in the FWDcargo compartment it is possible to load 5 Unit LoadDevices (ULDS) which can be mixed (containers orpallets).For the bulk loading, the FWD cargo compartment isdivided into 3 zones by 2 lateral divider nets.Lateral and longitudinal door nets are installed aroundthe door to keep the cargo door area free.




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AFT AND BULK CARGO COMPARTMENTS

The AFT cargo compartment can be basically loaded withbulk and loose baggage.If the cargo loading system is installed in the AFTcargo compartment, it is possible to load 5 Unit LoadDevices (ULDS) which can be mixed (containers orpallets).For the bulk loading, the AFT cargo compartment isdivided into 3 zones by 2 lateral divider nets.Lateral and longitudinal door nets are installed aroundthe door to keep the cargo door area free.The bulk cargo compartment can only be loaded withbulk loading.It is separated from the AFT cargo compartment by alateral divider net.A door net prevents damage to the bulk door and keepsthe cargo door area free.




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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENTS



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SELF EXAMINATION

How many Unit Load Devices (ULDS) can be loaded inthe AFT cargo compartment, if the cargo loadingsystem is installed ?

A - with 0 ULDS.B - with 5 ULDS.C - with 6 ULDS.

TMUCLSB0A LEVEL 1



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25-50-00 CARGO LOADING SYSTEM PRESENTATION

CONTENTS:LogicTransport ComponentsGuidance ComponentsLatching ComponentsControl ComponentsSelf Examination

TMUECCL09 LEVEL 1



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CARGO LOADING SYSTEM PRESENTATION

The semi-automatic cargo loading systems in the forwardand after compartments are identical, they have thesame components and operate similarly.

LOGIC

Each forward and aft cargo loading system is controlledfrom a control panel installed on the cargo door.With no electrical power available, it is possible toload or unload the Unit Loading Devices manually.

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CARGO LOADING SYSTEM PRESENTATION - LOGICTMUECCL09-P01 LEVEL 1



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TRANSPORT COMPONENTS

BALL MATSThe ball mats are installed in the door area in theFWD and AFT compartments.The ball mats extend across the full length of the FWDand AFT compartments.They are used to change the direction of the Unit LoadDevices (ULDs) during loading and unloadingoperations.

ROLLER TRACKSThe roller tracks are installed on the centerline ofthe FWD and AFT cargo compartment floors.Each roller track is fitted with rollers which permitULDs to move in the longitudinal direction.

POWER DRIVE UNITS (PDUs)The Power Drive Units are installed in the FWD and AFTcargo compartments for lateral and longitudinalmovements.There is one PDU for lateral movement on each ball matarea, three PDUs for longitudinal movement on theroller track of the FWD cargo compartment, and fourPDUs for longitudinal movement on the roller track ofthe AFT cargo compartment.The PDUs operate with 115 VAC, 400 HZ, and have athermal overload protection.




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CARGO LOADING SYSTEM PRESENTATION - TRANSPORT COMPONENTSTMUECCL09-P02 LEVEL 1



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GUIDANCE COMPONENTS

ENTRANCE GUIDETwo entrance guides are installed on each door sillof the FWD and AFT cargo compartments.The entrance guides fitted with a vertical roller toalign the ULD in the X and Y directions and preventdamage to the door frame.

Y-GUIDEA Y-guide is installed in the FWD cargo compartment.The Y-guide is fitted with three vertical rollers whichprevent friction between the ULD and the guide.




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CARGO LOADING SYSTEM PRESENTATION - GUIDANCE COMPONENTSTMUECCL09-P03 LEVEL 1



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LATCHING COMPONENTS

DOOR SILL LATCHTwo door sill latches are installed on the sills ofeach cargo compartment.Each sill latch has a housing, a manually operatedYZ-latch, an overridable Y-latch a guide-in roller, alimit switch.It prevents the roll out of a ULD, and locks it inposition.

FIXED YZ-LATCHThe fixed YZ-latches are installed on each sidewallframe of the FWD and AFT cargo compartments.The fixed YZ-latches are equipped with a roller exeptthree YZ-latches in front of each cargo door.They hold the ULDs in the Y and Z directions.A vertical roller guides the ULDs in the X direction.

XZ-SINGLE LATCH 32Two XZ-single latch 32 are installed in the rollertrack of the FWD cargo compartment, and three XZ-singlelatch 32 are installed in the roller track of the AFTcargo compartment.They hold the ULDs in the X and Z directions.Each XZ-single latch 32 is fitted with a proximityswitch which energizes a PDU only if the latch islowered.

END STOPTwo end stops are installed in the roller track ofeach cargo compartment.They hold the ULDs in X and Z directions.




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CARGO LOADING SYSTEM PRESENTATION - LATCHING COMPONENTSTMUECCL09-P04 LEVEL 1



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CONTROL COMPONENTS

CONTROL PANELThe control panels are installed on the inner face ofeach cargo door.They are equipped with:

- a power ON/OFF switch,- a joystick,- a door sill latch switch,- a power indicator light.

CONTROL BOXA control box is installed behind the sidewall panelof both the FWD and AFT cargo compartments.Each control box contains three power relays, anelectronic circuit card, terminal junctions and twoelectrical connectors.




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CARGO LOADING SYSTEM PRESENTATION - CONTROL COMPONENTSTMUECCL09-P05 LEVEL 1



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SELF EXAMINATION

How is the PDU energized ?A - by 26 VAC.B - by 28 VAC.C - by 115 VAC.

The cargo loading control box being supplied, whichlatch ensures the energization of the PDUs ?

A - the door sill latch.B - the XZ-single latch 32.C - the fixed YZ latch.

TMUECCL09 LEVEL 1



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25-52-00 CARGO LOADING OPERATIONS

CONTENTS:Cargo LoadingCargo UnloadingManual LoadingManual Unloading

TMUECLO03 LEVEL 3



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CARGO LOADING OPERATIONS

CARGO LOADING

The cargo compartments can be loaded with differenttypes of containers :- full size container.- half size container.- pallet.The FWD cargo compartment of the A320 can receive threecontainers or pallets and the Aft cargo compartmentfour.Let’s have a look to the A320 aft compartment loadingand unloading.Switch on the compartment lights.Lower the two manual sill latches.Lower the XZ-latches.Switch on the power on the control panel.The cargo loading system is ready to be used.The container itself lowers the overridable silllatches.When the container is over the lateral Power DriveUnit, move the joystick to the "IN" position.At the end of the lateral travel, move the joystickto the longitudinal position.The longitudinal Power Drive Units move the container.When the container is in position, lift thecorresponding XZ-latch.It locks the container and de-energizes the PDUunderneath it.Load the other containers by following the sameprocedure.When the last container is loaded, lift up the twomanual sill latches then check that the two overridablesill latches are up.

When the cargo loading is completed, the power can beswitched off.

CARGO UNLOADING

For the cargo unloading, first of all, lower the manualsill latches, then switch the power ON.Lower and hold down the sill latch switch, theoverridable sill latches lower.Move the joystick to the "OUT" position, the firstcontainer moves out.Lower the XZ-latch locking the next container. Theassociated PDU is available.Unload the container using the joystick.Do not forget to lower the overridable sill latchesbefore moving the joystick to "OUT".Unload the other containers using the same procedure.When the cargo compartment is empty, switch off thepower and lift-up the manual sill latches.

TMUECLO03-T01 LEVEL 3



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CARGO LODING OPERATIONSTMUECLO03-P01 LEVEL 3



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MANUAL LOADING

For the manual cargo loading, the compartmentpreparation is the same as that for cargo loading withthe automatic system. The containers are pushed byhand instead of using the PDUs.

MANUAL UNLOADING

For manual unloading, lower the two manual silllatches, then lower the overridable sill latches usingthe override handle. The containers are unloaded byhand instead of using the PDUs.At the end of the manual unloading, do not forget torelease the overridable sill latches by pushing thehandle, then to lift up the manual sill latches.

TMUECLO03-T02 LEVEL 3



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25-50-00 CARGO BULK LOADING

CONTENTS:FWD Cargo Bulk LoadingAFT Cargo Bulk LoadingBulk Cargo Compartment

TMUECLB03 LEVEL 3



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CARGO BULK LOADING

FWD CARGO BULK LOADING

The FWD cargo compartment is provided with itemsenabling occasional bulk loading:

- Tie down points.- Net attachment points.- Load placards.- Markings to show ceiling clearance.- Divider nets/door nets.

TMUECLB03-T01 LEVEL 3



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CARGO BULK LOADING - FWD CARGO BULK LOADINGTMUECLB03-P01 LEVEL 3



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CARGO BULK LOADING

AFT CARGO BULK LOADING

The AFT cargo compartment is provided with itemsenabling occasional bulk loading:

- Tie down points.- Net attachment points.- Load placards.- Markings to show ceiling clearance.- Divider nets/door nets.

A divider net isolates the AFT cargo compartment fromthe bulk cargo compartment.




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CARGO BULK LOADING - AFT CARGO BULK LOADINGTMUECLB03-P02 LEVEL 3



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CARGO BULK LOADING

BULK CARGO COMPARTMENT

The bulk cargo compartment is only provided with itemsenabling bulk loading.Access to the bulk cargo compartment is gained throughthe bulk cargo door, if the option is installed orthrough the AFT cargo door.The items for bulk loading are : - Typical tie down points, - Tie down points, - Typical attachment points, - Typical multiple attachment points, - Door nets.




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CARGO BULK LOADING - BULK CARGO COMPARTMENTTMUECLB03-P04 LEVEL 3



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TMUECLB03 LEVEL 3



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25-53-00 DRAINING SYSTEMDESCRIPTION/OPERATION

CONTENTS:FWD Cargo CompartmentAFT Cargo Compartment

TMUCLSG01 LEVEL 3



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DRAINING SYSTEM DESCRIPTION/OPERATION


Three outlet assemblies and a drain valve ensure thedraining of the FWD cargo compartment.The three outlet assemblies are installed at the Aftend of the compartment in the floor panel.Each consists of a filter, a fitting and a tube downinto the bilge of the fuselage.The drain valve is provided in the fuselage to cleanthe system.

AFT CARGO COMPARTMENT

Three outlet assemblies and a drain valve ensure thedraining of the AFT cargo compartment.The three outlet assemblies are installed at the Aftend of the compartment in the floor panel.Each consists of a filter, a fitting and a tube downinto the bilge of the fuselage.The drain valve is provided in the fuselage to cleanthe system.

TMUCLSG01-T01 LEVEL 3



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DRAINING SYSTEM DESCRIPTION/OPERATIONTMUCLSG01-P01 LEVEL 3



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TMUCLSG01 LEVEL 3



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25-52-00 CARGO LOADING COMPONENTS

CONTENTS:Ball MatsRollersDoor Sill LatchesYZ-LatchesXZ-Single Latches 32Entrance GuidesY-GuidePower Drive UnitsEnd StopsControl PanelsControl Boxes

TMUECLL07 LEVEL 3



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CARGO LOADING COMPONENTS

BALL MATS



COMPONENT DESCRIPTIONThe ball mats are installed across the full width ofthe cargo compartment floor between the entranceguides.They enable the Unit Load Devices (ULDs) to be movedin the longitudinal and lateral directions.

TMUECLL07-T01 LEVEL 3



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TMUECLL07-P01 LEVEL 3

CARGO LOADING COMPONENTS - BALL MATS



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ROLLERS



COMPONENT DESCRIPTIONRoller tracks are installed on the centerline of theFWD and AFT cargo compartment floors, and they areequipped with rollers.They enable ULDs to be moved in the longitudinaldirection.Guide rollers prevent damage to the door sill andlinings.




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CARGO LOADING COMPONENTS - ROLLERSTMUECLL07-P02 LEVEL 3



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DOOR SILL LATCHES

IDENTIFICATIONFIN: 2404VU1, 2404VU2, 2404VU3, 2404VU4


COMPONENT DESCRIPTIONTwo door sill latches are installed on each cargocompartment door sill.Each door sill latch is provided with : - A manually operated YZ-latch. - An overridable Y-latch. - A guide roller. - A limit switch.




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CARGO LOADING COMPONENTS - DOOR SILL LATCHESTMUECLL07-P03 LEVEL 3



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YZ LATCHES


LOCATIONZONE: 131, 132, 150, 153, 154

COMPONENT DESCRIPTIONThe fixed YZ-latches are installed on each frame onthe cargo compartment sidewalls.There are 12 YZ-latches with transport rollers and 3YZ-latches in the FWD and 18 YZ-latches with transportrollers and 3 YZ-latches in the AFT cargo compartments.




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CARGO LOADING COMPONENTS - YZ-LATCHESTMUECLL07-P04 LEVEL 3



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XZ SINGLE LATCHES 32



COMPONENT DESCRIPTIONManually operated XZ single latches 32 are installedin the roller tracks on the centerline of the cargocompartment floor.There are 2 XZ single latches 32 in the FWD and 3 XZsingle latches 32 in the AFT cargo compartments.They can lock one or two ULDs.Proximity switches below are wired in series with thePower Drive Units.The Power Drive Unit can only be powered when thelatches are lowered.




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CARGO LOADING COMPONENTS - XZ-SINGLE LATCHES 32TMUECLL07-P05 LEVEL 3



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ENTRANCE GUIDES

IDENTIFICATIONFIN: Not listed


COMPONENT DESCRIPTIONTwo fixed entrance guides are installed on the doorsills in each cargo compartment.They align the ULDs in the X and Y directions.

Y GUIDE


LOCATIONZONE: 130

COMPONENT DESCRIPTIONA fixed Y guide is installed across the forward endof the ball mats in the FWD cargo compartment.It is equipped with three vertical rollers to alignthe ULDs in the ball mat area.




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CARGO LOADING COMPONENTS - ENTRANCE GUIDES - Y-GUIDETMUECLL07-P06 LEVEL 3



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POWER DRIVE UNITS

IDENTIFICATIONFIN: 14MY, 15MY, 17MY, 19MY, 110MY, 112MY, 114MY, 115MY, 117MY


COMPONENT DESCRIPTIONThere are 3 Power Drive Units (PDUs) installed in theroller track of the FWD cargo compartment and 4 PowerDrive Units (PDUs) installed in the roller track ofthe AFT cargo compartment for longitudinal movement,and one PDU in each entrance area for lateral movement.The PDU is energized with 115 / 200 VAC, 400 Hz.When the PDU operates in the opposite direction thesupply phases are changed and the gears operate in theopposite direction.




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CARGO LOADING COMPONENTS - POWER DRIVE UNITSTMUECLL07-P07 LEVEL 3



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END STOPS



COMPONENT DESCRIPTIONThe end stops are installed on each end of the rollertracks.They lock the Unit Load Devices (ULDs) in the X and Zdirections.




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CARGO LOADING COMPONENTS - END STOPSTMUECLL07-P08 LEVEL 3



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CONTROL PANELS

IDENTIFICATIONFIN: 2020VU1, 2020VU2


COMPONENT DESCRIPTIONThe control panels are located on the forward edge oneach cargo door inner face.They comprise : - A power ON / OFF toggle switch. - A four position joystick ( IN - OUT - FWD - AFT ). - A door sill latch toggle switch. - A power indicator light.

CONTROL BOXES

IDENTIFICATIONFIN: 1MY, 101MY


COMPONENT DESCRIPTIONThe control boxes supply the PDUs with 115/200 VAC.They also supply 28 VDC to : - The door sill latch actuators. - The relays in all the PDUs. - The proximity switches. - The control panels.




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CARGO LOADING COMPONENTS - CONTROL PANELS - CONTROL BOXESTMUECLL07-P09 LEVEL 3



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TMUECLL07 LEVEL 3



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Ata 25

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