Pilot’s Manual

PM-132A VII-1

TABLE OF CONTENTS

Cockpit Description .................................................................................. 7-1General Arrangement — Cockpit (Figure 7-1) .................................. 7-3Crew Seats............................................................................................... 7-5Cockpit Seat (Figure 7-2)....................................................................... 7-7

Cabin Description...................................................................................... 7-9Passenger Seats .................................................................................... 7-10Passenger Seat (Figure 7-3)................................................................. 7-10

Emergency Equipment ........................................................................... 7-12Smoke Goggles..................................................................................... 7-12Hand Held Fire Extinguishers ........................................................... 7-12First Aid Kit and Crash Axe (If Installed) ........................................ 7-12Protective Breathing Equipment (If Installed)................................. 7-12

Normal Operation .......................................................................... 7-13Donning the PBE......................................................................... 7-13Removing the PBE ...................................................................... 7-16

Disposal............................................................................................ 7-16Abnormal Condition of Operation............................................... 7-16

Failure of the Starter Candle ..................................................... 7-17Inadequate Oronasal Mask Seal ............................................... 7-17

Loss of Infiltration Seal .................................................................. 7-17Flotation Equipment............................................................................ 7-17

Miscellaneous Equipment ...................................................................... 7-18Crew Compartment............................................................................. 7-18

Flashlights .................................................................................... 7-18Approach Plate Holder .............................................................. 7-18Lighted Approach Plate Holders.............................................. 7-18Sunvisors...................................................................................... 7-18Forward Pocket Doors ............................................................... 7-18

Passenger Compartment..................................................................... 7-19Cabinets, Drawers and Tables....................................................... 7-19

Forward Left Cabinet ................................................................. 7-19Jump Seat ..................................................................................... 7-19

Forward Left Cabinet (Figure 7-4)..................................................... 7-20Forward Right Storage Closet/Avionics Cabinet ...................... 7-21

Forward Right Closet/Avionics Cabinet (Figure 7-5) .................... 7-21Galley Cabinet ................................................................................. 7-22

Galley Cabinet (Figure 7-6)................................................................. 7-23

SECTION VIIINTERIOR EQUIPMENT

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VII-2 PM-132A

TABLE OF CONTENTS (Cont)

Sidewall Storage Boxes.................................................................. 7-24Aft Pyramid Cabinets (Optional) ................................................. 7-25

Aft Pyramid Cabinets (Figure 7-7).................................................... 7-25Tables................................................................................................ 7-25

Table Installations (Typical) (Figure 7-8) .......................................... 7-26Cabin Management System ............................................................... 7-27

Description ...................................................................................... 7-27Cabin Management System Components/Locations

(Figure 7-9)........................................................................................ 7-27Galley Switch Panel ................................................................... 7-27Cockpit Switch Panel................................................................. 7-27Entry Switch Panel..................................................................... 7-27Lavatory Switch Panel............................................................... 7-28Lighting Control Unit (LCU).................................................... 7-28Passenger Interface Unit (PIU)................................................. 7-28Master Control Unit (MCU) ..................................................... 7-28

Operation......................................................................................... 7-28Cabin Management System Equipment/ Circuit Breaker Locations

(Typical) (Figure 7-10) ..................................................................... 7-29Flight Phone ................................................................................ 7-30Digital Airborne Telephone (Optional)................................... 7-30AC Electrical Outlets (Optional) .............................................. 7-30Window Shades.......................................................................... 7-30Gasper Outlets ............................................................................ 7-30Aft Cabin Stowage Compartment ........................................... 7-31Lavatory/Vanity......................................................................... 7-31

Lavatory/Vanity (Typical) (Figure 7-11) .......................................... 7-32Toilet............................................................................................. 7-33

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PM-132A 7-1

COCKPIT DESCRIPTIONThe cockpit (Figure 7-1) is configured in a standard side-by-side seatingarrangement with a center pedestal mounted between the seats. Theinstrument panel is installed with an 18° forward cant which providesan ergonomic view of the panel by either crew member. The throttlequadrant is located between the center pedestal and the instrumentpanel. The instrument panel, center pedestal and throttle quadrant areeasily accessible by both pilots.

The dual primary flight controls consist of a textured surface controlwheel mounted to a control column and an adjustable set of rudderpedals. The control wheel and column operate with the normal push-pull (pitch) and left/right rotation (roll) input commands. The controlwheels have a trim switch, microphone switch and a Control WheelMaster Switch (MSW) installed on the outboard side of the wheel. Achecklist line advance switch, a transponder switch and a Touch Con-trol Steering (TCS) switch are installed on the inboard side of the con-trol wheels. The pilot’s control wheel is equipped with an aileron (roll)disconnect lever. Each control column is equipped with an approachplate holder that will secure an entire approach plate booklet. Anilluminated approach plate holder is available as an option. The leftand right rudder pedals provide yaw control during flight and areelectrically adjustable fore/aft for different sized pilots. The rudderpedals also control nose wheel steering and braking while the wheelsare on the ground.

Secondary flight controls and thrust levers are mounted on the throttlequadrant at the forward side of the pedestal. The elevator disconnecthandle, emergency gear freefall lever, flap control lever, emergency/parking brake handle and spoiler control handle are all located in thethrottle quadrant. The system test control switch, pitch trim biasswitch, radio control hot bus switch, rudder boost switch and clearancedelivery radio are located at the forward end of the quadrant. Switchesfor the enhanced ground proximity warning system are installed aft ofthe clearance delivery radio. The Multi-Function Display (MFD) joy-stick is located in the quadrant, aft of the thrust levers.

SECTION VIIINTERIOR EQUIPMENT

Pilot’s Manual

7-2 PM-132A

The instrument panel consists of three major horizontal tiers ofinstruments and controls. Within each tier, the controls for each systemare grouped together on a separate panel and/or display. Theglareshield panels (upper tier) provide controls for operating the flightdirector/autopilot and for managing information displayed on thePrimary Flight Displays (PFDs), Multi-Function Display (MFD) andEngine Indicating and Crew Alerting System (EICAS) display. Themain instrument panel (middle tier) provides visual displays and con-trols for communication/navigation, engine management and elec-tronic flight instrument systems management. The subpanel (lowertier) provides control for several aircraft systems and for control of thelights and landing gear.

The upper tier (glareshield panel) is located immediately below theglareshield. It consists of the integrated flight guidance controller andthe pilot’s and copilot’s Electronic Flight Instrument System (EFIS)control panels. The glareshield panels also contain the pilot’s andcopilot’s display unit reversion panels and master warning/cautionannunciator/reset switch.

The main instrument panel, in the middle tier area, is identified by four8 x 7 inch high resolution color Cathode Ray Tube (CRT) displays. Dis-play Units (DUs) on the pilot’s side include both a Primary FlightDisplay (PFD) and an Engine Indicating/Crew Alerting System (EI-CAS). DUs on the copilot’s side include a multi-function display (MFD)and a second PFD. The standby instruments (Airspeed, AttitudeIndicator and Altimeter) are located between the EICAS and copilot’sMFD. The Crew Warning Panel (CWP) and Radio Management Unit(RMU) displays are located below the standby instruments andbetween the EICAS and copilot’s MFD. The angle-of-attack indicators(if installed), digital chronometers and audio control panels for both thepilot’s and copilot’s side are located near the outboard ends of the maininstrument panel.

The pilot’s subpanel contains the reversion control panel, electricalcontrol panel and the Attitude Heading Reference System (AHRS)control for AHRS 1. It also contains the pilot’s side crew lighting paneland rudder pedal adjustment switch. The copilot’s subpanel containsthe cabin pressurization and oxygen control panel, the environmentalcontrol panel and cockpit voice recorder control panel. It also containsthe AHRS control for AHRS 2, the crew lighting panel and the rudderpedal adjustment switch. The anti-ice panel, aircraft light control paneland landing gear/hydraulic panel are all installed near the center of thesubpanel (center switch subpanel), directly above the forward side ofthe throttle quadrant.

Pilot’s Manual

PM-132A 7-3/7-4 (Blank)

F40-070000-001-01

1. Pedestal2. Throttle Quadrant3. Air Outlet (ankle)4. Fire Extinguisher (mounted on crew chair)5. Smoke Goggle Storage6. Pilot's Circuit Breaker Panel7. Air Outlet (armrest level)8. Pilot's Mic/Phone Jack Panel9. Map Light

10. Pilot's and Copilot's Subpanels11. Pilot's Control Column & Wheel12. Glareshield Panels13. Cockpit Speakers14. Pilot's Primary Flight Display (PFD) (DU-1)15. Engine Indicating and Crew Alerting

16. Dome Light17. Sunvisor18. Overhead Air Outlet19. Eye Reference Locator20. Assist Handle21. Magnetic Compass22. Crew Warning Panel23. Multi-Function Display (MFD) (DU-3)24. Copilot's Primary Flight Display (PFD) (DU-4)25. Copilot's Control Column & Wheel26. Instrument Panel27. Copilot's Mic/Phone Jack Panel28. Cabin Lighting Control29. Copilot's Circuit Breaking Panel30. Access for hanging plumb bob

1

23

45

6

7

8

910

11

12

1314

15

16

17

18

19

20

2122 23

24

25

26

27

28

29

30

System (EICAS) (DU-2)

7

1816

13

9

7

5

3

4

GENERAL ARRANGEMENT — COCKPITFigure 7-1

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PM-132A 7-5

The pedestal is typically equipped with a single Flight ManagementSystem (FMS), a trim control panel, a weather radar control panel, anEmergency Locator Transmitter (ELT) switch, and an engine/fuel con-trol panel. Optional equipment in the pedestal may include a second(dual) FMS, a high frequency communication control head, a SELCALcontrol panel, and a 12-vdc cigarette lighter.

An inflatable harness type oxygen mask with an integral microphone isstored on the outboard side of each crew seat. Smoke goggles are storedin the left and right lower sidewall storage compartments. Hand-heldfire extinguishers are installed on the crew seats directly behind thepilot’s and copilot’s legs. Life vests are stowed inside plastic holderswhich are mounted to cabinets located directly behind each crew seat.

A magnetic compass is installed on the windshield center post near thetop of the windshield. The headliner houses a dome light, air outlets,an assist handle and an access for a plumb bob location for leveling theaircraft. The sunvisors are also attached to the headliner. No switches,instruments or placards are located overhead. Circuit breaker panelsare located on the pilot and copilot upper sidewall panels. A flexiblemap light is attached to the upper sidewall above the circuit breakerpanel on each side. Cabin and spot light control switches are locatedadjacent to the copilot’s circuit breaker panel. Flashlights are installedon the cabinet behind each crew seat. Air outlets are installed in thecockpit sidewall panels and lower forward cockpit side panels. Storagecompartments are built into the lower sidewall panels for charts andJeppesen manuals. Drink holders are attached to the forward side of thestorage compartments. Additional manual storage is provided in theleft storage cabinet located behind the pilot’s seat.

CREW SEATS

The crew seats (Figure 7-2) are comprised of three basic structures: theseat base, the seat bottom and the seat back. The seat base is attached toand travels on the seat tracks. The seat bottom is located above the seatbase and provides controls for forward/aft movement, seat heightadjustment and seat back reclining adjustment. The seat back containsthe lumbar adjustment control, adjustable armrests and an adjustableheadrest.

The crew seats are constructed of lightweight alloys covered with foampadding and sheepskin and are equipped with a five-point restraintsystem. The lap belts and negative-G strap are mounted to the seatbottom. The rotary buckle is attached to the outboard lap belt. The man-ual lock/unlock handle for the shoulder harness belts is located on theinboard side of the seat back frame.

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7-6 PM-132A

Seat height adjustment is accomplished by pulling up on the verticaladjustment control lever located under the forward edge of the seatbottom near the outboard side of the seat. When the lever is pulled, themechanism is unlocked and the seat will move downward under theoccupant’s weight. To raise the seat, remove occupant weight from theseat while pulling up on the lever. Gas cylinders will cause the seat toautomatically raise up. Release the lever at the desired height to lockthe seat into place.

Forward and aft adjustment of the seat is accomplished by pulling upon the fore/aft adjustment control lever located under the forwardedge of the seat bottom near the inboard side of the seat. The seat canbe moved by holding the control lever up, and at the same time, slidingthe seat forward or aft on the seat tracks. When the desired position isobtained, the control lever can be released to lock the seat to the seattrack.

The headrest may be adjusted for both angle and height. The headrestcan be tilted forward to an angle of up to 60° by tilting it by hand. Theheadrest can also be raised up to 2 inches by lifting the headrest. Theheadrest can be lowered by pushing it down to the desired height.

The back cushion/lumbar support is controlled by turning the fore/aftlumbar adjustment control handwheel located on the inboard side ofthe seat back frame. Turning the handwheel counterclockwise (asviewed looking outboard) extends the lumbar support forward.Turning the handwheel clockwise will retract the lumbar support.

The armrests are individually stowable and adjustable. Each armresthas an adjusting wheel on the underside of the armrest. To deploy thearmrest, slide the armrest out from the seat back and rotate it down intoposition. To raise and lower the armrest position, turn the adjustingwheel on the underside of the armrest. The armrests will adjust 15 to26°. To stow the armrests for entry and exit, lift the armrest until it isparallel with the seat back and push it in toward the seat spine.

The seat back recline angle is adjustable. The recline adjustment controllever is located on the outboard side of the crew seat bottom. Pull up onthe recline control lever to release the seat back lock and lean the seat tothe desired angle. The seat back can be reclined 25°. The seat back willlock in the selected position when the control lever is released.

Pilot’s Manual

PM-132A 7-7

SHOULDER

HEADRESTOXYGEN

OXYGEN

LINE

ARMREST

SEAT

SEAT

RECLINE

ADJUSTMENT

VERTICAL

ADJUSTMENT

FIRE EXTINGUISHER

FORE/AFT

ADJUSTMENT

NEGATIVE-G STRAP

LAP STRAPS

SEAT

ARMREST

ADJUSTING

LUMBAR

ADJUSTMENT

SHOULDER STRAP RESTRAINT

LOCK/UNLOCK HANDLESEAT BACK FRAME

STRAPS

POCKET

MASK

BOTTOM

CONTROL

BASE

CONTROL

CONTROL

WHEEL

HANDWHEEL

BACK

NOTE:Pilot's seat shown.

Copilot's seat is similar with

controls on the opposite side.

COCKPIT SEATFigure 7-2

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7-8 PM-132A

A flexible oxygen hose is routed between the oxygen outlets on the leftand right cabin sidewalls and the lower outboard side of each crew seatbottom. This hose provides oxygen for the oxygen mask installationadjacent to each headrest. The crew mask microphone wiring is routedwith the oxygen hose through the crew seat.

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PM-132A 7-9

CABIN DESCRIPTIONThe aircraft cabin is divided into three areas: the entryway galley, thepassenger seating area and the lavatory/aft cabin stowagecompartment. The entryway galley is located at the forward end of thecabin. The passenger seating area is located in the center of the cabin.The lavatory/aft cabin stowage compartment is located at the aft endof the cabin.

The entryway galley area begins at the cabin entry door area andextends forward to the cockpit. The entryway galley area is comprisedof the left forward storage cabinet, the right forward storage closet andthe right galley cabinet. The typical galley is equipped with a coffeewarmer, a trash container, an ice chest and food/beverage storage andpreparation equipment.

The passenger seating compartment is located aft of the cabin doorentryway and extends aft to the lavatory. The typical passengercompartment has six individual passenger seats in a two-abreastconfiguration, with one seat on each side of a main center aisle.Individual reading lights, air outlets, and passenger oxygen masks arelocated in the overhead convenience panels and center headlinerpanels above the seats. Drinkholders, pull-out tables and lighting andentertainment control panels are built into the cabin sidewall adjacentto the seats. Optional 110-vac/60-Hz (230-vac/50-Hz) outlets may beavailable throughout the cabin (Refer to AC ELECTRICAL OUTLETSthis section).

The lavatory is located on the aft side of a partition at the aft end of thepassenger compartment, adjacent to the aft cabin stowagecompartment. The partition features sliding doors between thelavatory and passenger compartment. The lavatory consists of a toiletand vanity cabinet. The toilet is located on the forward right side of thelavatory. The vanity is located aft of the toilet. Optional equipment inthe lavatory are a vanity mirror and a vanity which includes a warmwater wash basin.

Access to the aft cabin stowage compartment is accomplished throughthe lavatory at the center aisle. The aft stowage compartment isequipped with a decorative coat rod and a baggage restraining net.

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7-10 PM-132A

PASSENGER SEATS

The passenger seats have a standard lap and shoulder restraint builtinto each seat (Figure 7-3). An articulating inboard armrest and leathercovering are standard equipment. An optional outboard armrest is alsoavailable.

SHOULDER STRAP

LAP BELTRESTRAINTS

SWIVEL/TRACKING

RECLINE CONTROL

ADJUSTABLE HEADREST

SMOKE HOOD STORAGE

STORAGEDRAWER

SEAT TRACKRELEASELEVER(Optional)

OUTBOARD ARMREST(Optional)

FLOTATION

SEAT CUSHION

CONTROL

DEVICE/

(Optional)

RECLININGSEATBACK

PASSENGER SEATFigure 7-3

Pilot’s Manual

PM-132A 7-11

The individual passenger seats are designed to be swiveled 360°. Theseats are equipped with lateral tracking on the seat base which allowsthem to be located as far outboard as possible for takeoff and landing,thus maintaining maximum aisle clearance. After takeoff, the seats canbe positioned inboard for increased comfort. The passenger seats canalso be adjusted forward and aft on the seat base while the seat baseremains stationary. These adjustments are accomplished by pulling upon the swivel control lever located at the end of the armrest. The swivelcontrol lever is the larger of the two levers on the armrest.

Pulling up partially on the swivel/tracking control lever will releasethe seat to swivel, pulling the lever all the way up will allow the seat tobe moved (in three directions) from side-to-side, forward/aft and in aswiveling motion. Releasing the swivel control lever will cause the seatlocking mechanism to automatically lock the seat in the selected posi-tion. The two furthest aft passenger seats (those against the aft lavatorypartitions) do not have tracking capabilities.

The recline control lever is located at the end of the armrest, adjacent tothe swivel control lever. The recline control lever is the smaller of thetwo levers on the end of the armrest. The seat will recline up to an 85°angle when the recline control lever is pulled up and the occupantapplies weight against the seat back. The seat recline mechanism willlock in place when the recline control lever is released. To place the seatin an upright position, remove occupant weight from the seat backwhile pulling up on the recline lever. The mechanism willautomatically raise the seat back into an upright position.

The passenger seat has an adjustable headrest installed in the seat back.The passenger headrest can be adjusted up and down by pulling it upor pushing it down with both hands. A smoke hood is stored in apocket located on the forward side of each seat bottom. The seat cush-ion may also be used as a personal flotation device. The seat base hasproximity lights installed on the inboard side of the base.

Optional equipment may be installed on the passenger seats. Anarticulating outboard armrest is available that can be articulated forheight. This armrest is standard equipment on the aft right passengerseat, which is situated adjacent to the right aft emergency exit. Anunderseat storage drawer may be incorporated into the forward end ofthe passenger seat. A seat track release mechanism is available whichallows the entire passenger seat and seat base to be moved forward oraft along the seat tracks.

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7-12 PM-132A

EMERGENCY EQUIPMENT

SMOKE GOGGLES

Smoke goggles are provided for each crew member and are stowed inthe lower sidewall storage compartment. The goggles are donned ifsmoke or fumes are present in the aircraft.

HAND-HELD FIRE EXTINGUISHERS

Two hand-held fire extinguishers are mounted on the front of each crewseat. Each cockpit fire extinguisher contains 1.25 pounds of Halon 1211.

An additional hand-held fire extinguisher is mounted in the lavatory.The cabin fire extinguisher contains 2.5 pounds of Halon 1211.

The extinguishers incorporate a pressure gauge which indicates thestate of propellant charge. If properly charged, the indicator needle willbe within the green segment. When an extinguisher has been manuallydischarged, the indicator will be in the red area. This provides the crewwith visual indication that the bottle has been partially or totallydischarged. The extinguishers are rechargeable.

FIRST AID KIT AND CRASH AXE (IF INSTALLED)

The first aid kit and crash axe are located in the forward right storagecloset.

PROTECTIVE BREATHING EQUIPMENT (IF INSTALLED)

Protective Breathing Equipment (PBE) is available for a crew memberto use in fighting cabin fires. The PBE is designed to protect the user’seyes and respiratory system from the harmful atmosphere which maybe generated by a cabin fire. The PBE is a hood with a visor which isplaced over the head and seals around the neck. An oxygen generatingcanister provides breathing oxygen for the user. The PBE is vacuumsealed in a bag and stored in a box accessible to the crew. The PBE is athrow-away unit that must be replaced whenever the vacuum seal isbroken. It is imperative that the vacuum seal be maintained since theoxygen-generating chemicals react with moisture.

Duration of oxygen production is nominally 15 minutes dependingupon the work rate and size of the user. Useful life of a sealed PBE is 10years from the date of manufacture.

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PM-132A 7-13

NORMAL OPERATION

Donning the PBE:

There are two available carriers for the PBE. A portable container storedin a cabinet behind the cockpit or a mounted container (normally mount-ed to the aft side of the pedestal).

1. Remove mask from container. a. To open the portable con-

tainer, lift the single latchon the cover and lift.Remove sealed bag fromthe container.

b. On the mounted container,grasp the red access handleon the protective containerfirmly and pull forcibly todisengage the cover. Whenthe cover is removed fromthe container, immediatelydrop it. (The vacuumsealed bag does not need tobe removed from the con-tainer to open.) The pack-aged unit may be removedfrom the stowage containerprior to opening and car-ried to a remote locationfor use.

2. To remove the PBE from thevacuum sealed bag, locate thered I.D. tag and pull sharply totear open the vacuum sealedbag. Reach into the openedvacuum-sealed bag and firmlygrasp the PBE. Pull the PBEstraight out of the bag. Ifnecessary hold the bag with theopposite hand.

STEP 1

Portable Container

MountedContainer

STEP 2

A25 1064

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7-14 PM-132A

3. Place both hands inside theneckseal opening with palmsfacing each other and PBEvisor facing downward withthe oxygen generating canis-ter resting on the tip of thehands.

4. With the top of the head bentforward, guide the PBE neck-seal over the top of the headand down over the face usingthe hands to shield the faceand glasses from the oronasalmask cone.

5. With both hands, grasp theadjustment straps at thelower corners of the visor andpull outward sharply to actu-ate the starter candle. Within1 to 5 seconds, a rushingnoise of oxygen entering thehood will be heard and infla-tion will be evident.

.

Human hair ishighly flammable. Hair that protrudes through theneckseal could ignite if brought into direct contactwith flame.

6. With the straps still in handand head bent forward, pullbackward to secure the oro-nasal mask cone high on thenose for a tight seal.

STEP 3

STEP 4

STEP 5

WARNING

A25-1031STEP 6

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PM-132A 7-15

7. If wearing glasses, adjusttheir position to rest on thetip of the oronasal mask coneby moving the sides of theframe through the hood fab-ric. Do not attempt to adjustthrough the neckseal as thiswill result in infiltration ofthe surrounding atmosphereinto the interior of the hood.

8. When the neckseal is posi-tioned at the neck and theoxygen generating canister isresting on the nape of theneck, remove the hands,checking to see that clothingis not trapped in the seal andhair does not protrudebetween the seal and theneck. Pull the protective neckshield down to cover the col-lar and upper shoulder area.

Following actuation, the hood will inflate over a 15- to 20-secondperiod. After this period, the starter candle will cease flowing and theonly sound will be a slight rustling of the fabric on each inhalation andexhalation. Dependent upon breathing rate, there will be a slightexhalation resistance as the exhaled breath is forced through theoxygen generating canister. Inhalation resistance will be almostunrecognizable since inhalation is directly from the interior of the hoodthrough a diaphragm type check valve located at the base of theoronasal mask. The visor should remain clear of fogging or misting.Heat is produced by both the chemical air regeneration process andtransfer of body heat during the rebreathing cycle. Heat build-upwithin the hood is normal and is dependent upon the amount of workperformed. There should be no irritating or strong unusual odorswithin the hood. Operational duration is variable dependent upon theamount of work performed by the user.

STEP 7

STEP 8

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7-16 PM-132A

If the PBE is worn to exhaustion of the chemical regeneration system,this will be evidenced by a gradual reduction in the expended volumeof the hood until the point that the hood is collapsed tightly around thehead at the end of a full inhalation. Additionally, there will be a rapidbuildup of heat and moisture in the hood as the canister loses itseffectiveness. At this point, the wearer should immediately retire to asafe breathing area clear of flame and toxic fumes and remove thedevice.

Removing the PBE

1. Go to a safe area away from immediate contact with fire or openflame and/or toxic fumes.

2. With both hands, reach for the two lower corners of the visorarea and push forward on the metal tabs of the adjustment strapbuckles to release the strap tension.

3. Place both hands under the neckseal in the forward area andpull up, guiding the oronasal cone and neckseal over the face/glasses until the PBE is clear of the head.

4. Place the expended PBE in a safe place to cool away from fire orexposure to water.

Disposal

The expended PBE still contains unreacted oxidizing material andstrong alkali materials. At the completion of flight, it must be turnedover to maintenance for authorized disposal.

ABNORMAL CONDITION OF OPERATION

This device produces oxygen which will vigorouslyaccelerate combustion. Do not intentionally exposethe device to direct flame contact, or remove in theimmediate presence of fire or flame. Due to oxygensaturation of the hair, do not smoke or becomeexposed to fire or flame immediately after removing.

Users should be trained to recognize abnormal conditions which couldsignify malfunction or failure of the equipment to properly operate asfollows:

CAUTION

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PM-132A 7-17

Failure of the Starter CandleIf the starter candle fails to actuate when the adjustment strap is pulled,an additional sharp pull on the strap may be sufficient to dislodge thelanyard pin and actuate the device. If the device still fails to actuate, thehood will continue to function, although the initial purge capability islost. Sticking the fingers into the neckseal to allow a large lunginhalation may be required to enable sufficient breathing volume untilthe chemical regeneration system begins producing a surplus ofoxygen.

Inadequate Oronasal Mask SealAbsence of a tight seal of the oronasal cone to the face may result inexcess leakage of the exhaled breath into the hood, short circuiting theoxygen-generating canister. This condition may result in a build-up ofCO2 within the rebreathing volume in the hood. Excessive CO2 isnormally indicated by breathing distress such as rapid and laboredbreathing accompanied by a general feeling of insufficient ability to getone’s breath, although there is no restriction to breathing. Presence ofmoisture or fogging on the visor and the sensation of air escaping fromthe mask, particularly around the nose and eyes, are indications of alack of proper fit. Adjustment of the mask straps and mask position tominimize leakage should rapidly alleviate the problem. If theperception of breathing distress persists, the user should quickly go toa safe area and remove the PBE and don alternate breathing equipmentif required.

Loss of Infiltration SealThe smoke and toxic fumes generated by the combustion of mostaircraft cabin interior materials has many strong irritants. Thecontinued presence of strong irritation odors inside the hood resultingin eye and respiratory tract discomfort is a good indicator of the lack ofan effective infiltration seal. Verify that the seal is in contact with theskin or the neck and does not have clothing or jewelry trapped in theseal, or hair protruding between the seal and the neck. If the conditionpersists, or there is evidence of a tear in the neckseal, the user should goquickly to a safe area and don alternate breathing equipment ifrequired.

FLOTATION EQUIPMENT

Life vests are stowed in plastic compartments located behind the pilot’sand copilot’s seats and also in a compartment at the front of each pas-senger seat. A life vest is also stowed in the lavatory adjacent to the toi-let seat (on toilet seats with seat belts). The life vests are inflated bypulling the red CO2 release tabs. Each passenger seat cushion has beendesigned to also be used as a personal flotation device.

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7-18 PM-132A

MISCELLANEOUS EQUIPMENT

CREW COMPARTMENT

FLASHLIGHTS

Two flashlights are installed in the crew compartment. The flashlightsare located behind each crew member’s seat. The pilot’s flashlight issecured to a bracket mounted to the forward side of the forward leftstorage cabinet. The copilot’s flashlight is secured to a bracket mountedto the forward side of the forward right storage cabinet.

Rechargeable flashlights are available as optional equipment. Therechargeable flashlights are mounted in a location similar to thestandard flashlights. The rechargeable flashlights are waterproof,flotable and flame retardant.

APPROACH PLATE HOLDER

A spring-loaded chart holder is installed on each control wheel. Theholders are large enough to hold an entire approach plate.

LIGHTED APPROACH PLATE HOLDERS

Optional illuminated chart holders are available for each control wheel.The chart holders provide illumination of the approach plates.

SUNVISORS

Two sunvisors are located at the upper edge of the windshield, one oneach side. Each sunvisor is hinged so it can be folded down and willslide along its track as desired.

FORWARD POCKET DOORS

Optional solid sliding doors may be installed which separate thecockpit from the entryway galley and passenger compartment.

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PM-132A 7-19

PASSENGER COMPARTMENT

CABINETS, DRAWERS and TABLES

Standard and optional cabinets, drawers and tables may be built intothe passenger compartment. The following descriptions and figuresshow the most common accessories:

Forward Left Cabinet

The forward left cabinet (Figure 7-4) is located immediately aft of thepilot’s seat, on the forward side of the cabin entry door. The left cabinethas a hinged door and storage space built into the aisle side. Anentryway railing is installed on the aft side of the cabinet adjacent to theentrance steps. A cabin entryway lighting control panel (entryway con-trol unit) is installed on the aft side of the cabinet above the railing. Theentryway control unit contains switches for the pilot’s overhead domelight, entry spotlight, cabin overhead lights, spotlights and lavatoryoverhead lights. An optional video monitor may be installed above theentryway switch panel.

Jump Seat

An optional jump seat may be installed on the aft side of the forwardleft cabinet. The jump seat unfolds down from the cabinet with the oc-cupant situated in a side-facing position for access to the right forwardgalley. The jump seat cannot be occupied during takeoff or landing. Itmust be folded up against the aft side of the forward left cabinet forboth takeoff and landing.

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FORWARD LEFT CABINETFigure 7-4

VIDEO

MONITOR

ENTRYWAY

CONTROL

UNIT

ENTRYWAY

RAILING

JUMP

SEAT FORWARD

LEFT

CABINET

DOOR

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Forward Right Storage Closet/Avionics Cabinet

The forward right storage closet/avionics cabinet is located in theforward right side of the cabin, aft of the copilot’s seat. The closet isequipped with a door which is hinged at the forward side and shelveslocated in the main compartment. The avionics cabinet racks are locat-ed behind a panel and are not accessible by door.

FORWARD RIGHT CLOSET/AVIONICS CABINETFigure 7-5

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Galley Cabinet

The galley cabinet (Figure 7-6) is located on the forward right side ofthe cabin next to and aft of the forward right storage closet/avionicscabinet. The galley cabinet consists of three customized insert modulesinside the cabinet; the upper module, the middle module and the bot-tom module. Each module is configured according to the customer’s re-quests, so galley cabinet assemblies will vary.

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NOTE: Galley cabinets will vary in both equipment installation and arrangement.

GALLEY CABINETFigure 7-6

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The following equipment and features are standard and will beinstalled in the galley cabinet:

The following equipment is optional and may be installed in the galleyor closet:

Sidewall Storage Boxes

Headphones, as well as other small items, may be stored in theoutboard sidewall storage boxes located along the cabin armrests.

Water/Coffee Warmer

Soft Drink/Juice Can & Ice Storage

Trash Compartment

Warming Oven Microwave Oven Wine Storage

Catering Tray Crystal China

CD Player(closet)

DVD Player(closet)

Multi-DVD Player(closet)

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Aft Pyramid Cabinets (Optional)

Optional aft pyramid cabinets (Figure 7-7) may be located behind theaft seats on both the right and left sides of the cabin. The pyramid cab-inets can be opened by lifting and pulling latches near the top of eachdrawer panel. The pyramid cabinets may be configured for can storage,magazine and/or miscellaneous storage.

AFT PYRAMID CABINETSFigure 7-7

Tables

Two pull-out bi-fold executive tables are located (one) on each side ofthe cabin and are stored inside the sidewall between the facing seats.The executive tables are 20 inches (50.8 centimeters) wide with foldingleaves and a solid work surface. The table is extended for use by pullingit up from the cabin sidewall and then unfolding the leaves until theylock in place. The tables (Figure 7-8) can be stowed by folding the leavestogether, raising them up until parallel with the cabin sidewall, andthen sliding them down into the compartment inside the cabinsidewall.

An optional left side slimline table may be installed in the cabin side-wall adjacent to the aft forward-facing seat. The left side table unfoldsand stows in the same manner as the larger tables. An optional rightside table is stowed aft of the left side divider and plugs into thereceptacles in the escape hatch armrest. Both tables are approximately10 inches (25.4 centimeters) wide.

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TABLE INSTALLATIONS (TYPICAL)Figure 7-8

EXECUTIVE TABLE SLIMLINE TABLE

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CABIN MANAGEMENT SYSTEM

DESCRIPTION

An Audio International cabin management system has been installedin the aircraft to manage various cabin systems and components. Thesesystems and components include cabin lights, lavatory lights, cabin au-dio and video entertainment systems (if installed), cabin temperature,galley equipment, and water system (if installed). The cabin manage-ment system uses discrete signal lines or a two-wire, bidirectional databus for communication between components.

This Audio International cabin management system consists of aswitch control unit, a cockpit switch panel, an entry switch panel, a gal-ley switch panel, a lavatory switch panel, eight Lighting Control Unit(LCU) switch panels, a Passenger Interface Unit (PIU) and a MasterControl Unit (MCU) switch panel. The following table lists the cabinmanagement system components and locations.

CABIN MANAGEMENT SYSTEM COMPONENTS/LOCATIONSFigure 7-9

Galley Switch PanelThe galley switch panel controls the hot liquid container, second hotliquid container (if installed), and galley drain system (if installed).

Cockpit Switch PanelThe cockpit switch panel controls the cabin lights, entry light, and read-ing/table lights. This unit can also disable all cabin switch panels.

Entry Switch PanelThe entry switch panel controls the cabin wash lights, lavatory washlights, cockpit lights, entry light, reading/table lights, and the optionalexterior lighting system (if installed).

Component LocationCockpit switch panel Copilot’s sidewall panelEntry switch panel Forward left cabinet aft face

Galley switch panel Forward right cabinet headerLavatory switch panel Lavatory cabinet backsplashLighting Control Unit (LCU) (6) Cabin side ledge (5) and PSU (1)

Master Control Unit (MCU) VIP seat side ledgePassenger Interface Unit (PIU) Behind side ledge

Switch control unit Forward left cabinetPAX CTRLS circuit breaker Copilot’s circuit breaker panel

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Lavatory Switch PanelThe lavatory switch panel controls the toilet flush, lavatory wash andspot lights. This unit includes an ordinance sign. This switch panel alsocontrols the optional water pump and sink drain system (if installed).

Lighting Control Unit (LCU)The LCU allows the passengers to control the reading and table lights.

Passenger Interface Unit (PIU)The PIU provides the communication interface for the aft right PSUmounted LCU.

Master Control Unit (MCU)The MCU communicates with the other units and allows the occupantof the VIP seat to control the cabin wash lights, cabin temperature, andother cabin functions.

OPERATION

The Audio International cabin management system utilizes a bidirec-tional data bus and discrete outputs to control switching functions. Ac-tuation of a discrete push button control switch sends a signal directlyto the device being controlled. Actuation of a push button controlswitch on the data bus sends a data word to the bidirectional data bus.Each data word is addressed to a particular device. The addressed de-vice decodes the data word, activates the appropriate control or func-tion, and sends a feedback response to the control switch to change theLED display (if applicable).

Consult the manufacturer’s documentation for complete programmingand operating instructions.

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CABIN MANAGEMENT SYSTEM EQUIPMENT AND CIRCUIT BREAKER LOCATION (TYPICAL)

Figure 7-10

Equipment Location Control Circuit Breaker/s

Cabin Audio Amplifier Aft LavatorySPKRS (Pilot's CB Panel) CABIN PA (Pilot's CB Panel)

Master Control Unit (MCU) LH or RH Side LedgePAX CTRLS (Copilot's CB Panel)

Power Switching Module Forward LH CabinetPAX CTRLS (Copilot's CB Panel)

Passenger Control Units (PCU)

LH/RH Side LedgePAX CTRLS (Copilot's CB Panel)

A/V Distribution UnitForward RH Cabin Side-wall

AUDIO (Copilot's CB Panel)

IR Receiver Forward LH CabinetPAX CTRLS (Copilot's CB Panel)

CD Changer, Control Head Forward RH Cabinet AUDIO (Copilot's CB Panel)

CD Changer, Remote Unit Forward RH Cabinet AUDIO (Copilot's CB Panel)

Single CD Player (SCD) Forward RH Cabinet AUDIO (Copilot's CB Panel)

Cassette Tape Player (CTP) Forward RH Cabinet AUDIO (Copilot's CB Panel)

Digital Video Disc Player (DVD)

Forward RH Cabinet AUDIO (Copilot's CB Panel)

Dual Digital Video Disc Player (Dual DVD)

Forward RH Cabinet AUDIO (Copilot's CB Panel)

Video Cassette Player (VCP) Forward RH Cabinet AUDIO (Copilot's CB Panel)

10.4" MonitorForward LH Cabinet and/or Aft Bulkhead

VIDEO (Copilot's CB Panel)

Lavatory Switch Panel Lavatory BacksplashPAX CTRLS (Copilot's CB Panel)

Cockpit Switch Panel Cockpit Sidewall N/A

Galley Switch Panel Forward RH Cabinet N/A

Entry Switch Panel Forward LH CabinetPAX CTRLS (Copilot's CB Panel) CABIN (Pilot's CB Panel)

Lighting Control Units (LCU) LH Side LedgePAX CTRLS (Copilot's CB Panel)L SPOT (Pilot's CB Panel)

Lighting Control Units (LCU) RH Side LedgePAX CTRLS (Copilot's CB Panel)R SPOT (Copilot's CB Panel)

Speaker (Mid-range/tweeter) Convenience Panels N/A

Speaker (Subwoofer) Cabin Floor N/A

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FLIGHT PHONE

Digital Airborne Telephone (Optional)

The optional Magnastar C2000 is a two voice/data system that hasdirect dialing, multiple calls, fax/data modem, uplink calls, interfone,speed dialing and call charging features. Handsets are installed in boththe cockpit and the passenger compartment.

The passenger compartment handset can be located in any of the cabinarmrest storage boxes. The handset in the cockpit is located on the aftend of the center pedestal.

Power for the flight phone is 28-vdc through the 10-amp FLT PHONEcircuit breaker on the pilot’s circuit breaker panel.

AC ELECTRICAL OUTLETS (Optional)

Four optional 110-vac/60-Hz electrical outlets may be installed in thecabin. One of the outlets is located in the galley cabinet. Two of theoutlets are located in the passenger compartment lower sidewall (oneon the right side and one on the left side) between the facing passengerseats. The 110-vac outlets have a 1200-va capacity. The fourth outlet isequipped with a Ground Fault Interrupt (GFI) circuit which, if tripped,may be reset. This outlet is installed across from the lavatory in the cab-in stowage area at the floor. The GFI outlet can be reset by depressingthe TEST/RESET button. The inverters powering these outlets will au-tomatically shut down if the cabin altitude goes above 9500 feet. Powerwill be restored when the cabin altitude descends below 8300 feet.

A 230-vac/50-Hz circuit is available, as an option, for aircraft whichwill be used primarily overseas.

WINDOW SHADES

Each cabin window is equipped with a window shade. The shades areadjustable and can be raised and lowered to any desired level. Theshades are made of pleated translucent material and may allow somelight in.

GASPER OUTLETS

Individual gasper outlets (air outlets) are located in the cabin overheadconvenience panels. The outlets are adjacent to the lights and can beturned to approximately 40° around its center to direct airflow asdesired. Rotate the conical port counterclockwise to open the outlet andclockwise to close.

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AFT CABIN STOWAGE COMPARTMENT

The aft cabin stowage compartment is located on the left side of theaircraft immediately aft of the passenger compartment. The stowagecompartment is equipped with a coat rod for hanging garments and arestraining web. Some interiors are equipped with a fire extinguisherwhich is mounted to the left partition.

LAVATORY/VANITY

The standard lavatory/vanity (Figure 7-11) is equipped with a toilet, avanity counter, a toilet tissue drawer and a trash/storage drawer.Optional equipment for the standard vanity includes a belted toiletwith a life vest, a lighted vanity mirror and a wash basin with warmrunning water plumbed to an overboard heated drain.

The lavatory is separated from the passenger cabin by sliding doorswhich stow inside the left and right sides of the partition. The doors donot lock and are equipped with a magnetic strip which holds themtogether while closed. The toilet is located on the right side of thelavatory compartment. The toilet is flushed by depressing the toiletFLUSH switch, located in the lavatory switch panel on the forward sideof the toilet. The sink is located at the aft end of the lavatory. The waterfaucet is operated by depressing the PUMP switch located on the lava-tory switch panel adjacent to the basin to dispense running water. Wa-ter in the basin is drained by depressing the DRAIN button which isalso on the lavatory switch panel.

If equipped with the optional sink, the lavatory/vanity will have apotable water tank and pump located under the vanity counter. Thepotable water tank (with an internal heater) holds approximately1.5 gallons of 100° F heated water. The pump and tank (with heater)draw electrical power from the 15-amp LAV SINK circuit breaker locat-ed on the pilot’s circuit breaker panel. The lavatory sink is drainedthrough a heated drain mast on the bottom of the aircraft. The heaterprevents ice from forming in the drain mast.

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LAVATORY/VANITY (TYPICAL)Figure 7-11

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Toilet

A flushing toilet is installed on the right side of the lavatorycompartment. The unit features a two compartment design whichisolates the flushing fluid from the waste. The toilet is located on theright side of the lavatory compartment. The toilet is flushed by depress-ing the toilet FLUSH switch, located in the lavatory switch panel on theforward side of the toilet (see Figure 7-11). The length of the flush cycleis controlled automatically. There are two electric pumps installed in-side the unit. The flushing pump circulates the flushing fluid duringthe flush cycle. The macerator/pump is used to pump the waste fromthe toilet during servicing only.

This toilet is equipped with a macerator pump which has the capabilityto process regular toilet paper. It is not necessary to use the specialbiodegradable toilet paper in this toilet.

Servicing of the toilet is accomplished using servicing ports located onthe aircraft exterior. The macerator/pump is used to pump the wastefrom the toilet while fresh flushing fluid is pumped into the toilet fromthe servicing equipment. Refer to Chapter 12 in the maintenancemanual for servicing instructions.

Electrical power to operate the flushing circuit is 28-vdc suppliedthrough the 3-amp TOILET circuit breaker on the copilot’s circuitbreaker panel.