SERIES 200 - Bombardier Inc. · PDF fileinterior arrangement 4 ... airstair door & demo of...

D

First Issued: AUG 31/95

CRASH--FIRE--RESCUEINFORMATION

SERIES 200PSM 1--82--14

BOMBARDIER INC.BOMBARDIER REGIONAL AIRCRAFT DIVISION

CUSTOMER SUPPORT123 GARRATT BLVD., DOWNSVIEW, ONTARIO

CANADA M3K 1Y5

CopyrightE 1994 by de Havilland Inc.All rights reserved. No part of this work may be reproduced or copied

in any form or by any means without written permissionof de Havilland Inc.

The information, technical data and designs disclosed in this document (the ”information”) areeither the exclusive property of de Havilland Inc. or are subject to proprietary rights of others.The Information is not to be used for design or manufacture or disclosed to others without theexpress prior written consent of de Havilland Inc. The holder of this document, by its retentionand use, agrees to hold the information in confidence. These restrictions do not apply to per-sons having proprietary rights in the Information, to the extent of those rights.

April 10, 1992

DCRASH---FIRE---RESCUE INFORMATION

SERIES 200 AUG 31/95Page 1

MODEL 202 LIST OF EFFECTIVE PAGES

LIST OF EFFECTIVE PAGES

Insert this page and latest revised page(s). Destroy superseded pages. Listed below are all current pages of themanual and their dates of issue.

PAGE DATE

Title Page August 31, 1995A August 31, 1995Log of Revisions August 31, 1995Table of Contents August 31, 19951 August 31, 19952 August 31, 19953 August 31, 19954 August 31, 19955 August 31, 19956 August 31, 19957 August 31, 19958 August 31, 19959 August 31, 199510 August 31, 199511 August 31, 199512 August 31, 199513 August 31, 199514 August 31, 199515 August 31, 199516 August 31, 199517 August 31, 199518 August 31, 199519 August 31, 199520 August 31, 199521 August 31, 199522 August 31, 199523 August 31, 199524 August 31, 1995



MODEL 202 LIST OF EFFECTIVE PAGES

THIS PAGE INTENTIONALLY LEFT BLANK



MODEL 202 LOG OF REVISIONS

LOG OF REVISIONSInsertion of all Revisions must be recorded in the Log of Revisions below.

Rev.No.

DateInserted

InsertedBy

Rev.No.

DateInserted

InsertedBy


SERIES 200AUG 31/95Page 2

MODEL 202LOG OF REVISIONS




MODEL 202 TABLE OF CONTENTS

TABLE OF CONTENTS

PAGE

GENERAL ARRANGEMENT 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FAMILIARIZATION AND LOCATION GUIDE 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .EXTERIOR WALK---AROUND 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .INTERIOR ARRANGEMENT 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CABIN CROSS---SECTION 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FLIGHT COMPARTMENT (VIEW FORWARD) 6. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FLIGHT COMPARTMENT (VIEW AFT) 7. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .EXITS AND SERVICE DOORS 8. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .AIRCRAFT DOORS AND GROUND SERVICE PANELS 9. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .EVACUATION ROUTES 10. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PASSENGER AND CREW ESCAPE SYSTEMS 11. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .BAGGAGE DOOR OPERATION 12. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FLIGHT COMPARTMENT EMERGENCY HATCH 13, 14. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENGINE DANGER AREAS 15. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CUT---THROUGH AREAS 16. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FUSELAGE SAFETY EQUIPMENT LOCATIONS 17. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CREW OXYGEN LOCATIONS 18. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PASSENGER OXYGEN CYLINDER (OPTIONAL) 19. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .PASSENGER OXYGEN AUTOMATICPRESENTATION SYSTEM (OPTIONAL) 20. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FIRE CONTROL RECOMMENDATIONS 21. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FLAMMABLE MATERIAL LOCATIONS 22. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENGINE FIRE ACCESS LOCATIONS 23. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENGINE FIRE EXTINGUISHER AND BATTERY POWER SWITCH LOCATION 24. . . . . . . . . .



MODEL 202TABLE OF CONTENTS




MODEL 202

GENERAL ARRANGEMENT

85 FT 0 IN.(25.89m)

CLEARANCE (STATIC)

13 FT 0 IN. DIA.(3.96m)

26 FT 0 IN.(7.93m)

11 FT 11 IN. *(3.63m)

25 FT 10.4 IN.(7.88m)

3 FT 1 IN.*(937mm)

8 ft 4 in.(2.54m)

4 FT 11 IN.(1.49m)

6 FT 8 IN.(2.03m)

4 FT 3 IN.(1.3m)

24 FT 7 IN.*(7.49m)

73 FT 0.1 IN.(22.26 m)

AB C B

26 FT 1 IN.(7.95m)

*BASIC WEIGHT = 21,400 lb. (9,707 kg.)MAX. TAKE---OFF WEIGHT = 36,300 lb. (16,466 kg.)SEATING CAPACITY = UP TO 37 PAX.

AND 4 CREW

DIMENSIONS TO GROUND LINE INDICATED* ARE APPROXIMATE ONLY AND VARYDEPENDING ON LOADING CONDITIONSAND AIRCRAFT CONFIGURATION.

*BASIC WEIGHT WILL VARY DUE TOCONFIGURATION AND MODIFICATIONNO FUEL, NO PAX OR CREW.

NOTE:

A=125.00 IN (3.18m)B=43.00IN (1.09m)C=63.00IN (1.6m)

WHEELS RETRACTED

APPROX 2 FT (.61m)LOWER IN WHEELSRETRACTED SITUATION.

WHEELS EXTENDED



MODEL 202

FAMILIARIZATION AND LOCATION GUIDE

FLIGHT COMPARTMENT

FORWARD CABIN

AFT CABIN

BAGGAGECOMPARTMENT

FLIGHT COMPARTMENT

A. FIRE EXTINGUISHERB. FIRE AXE LOCATIONC. PORTABLE OXYGEN BOTTLE

FORWARD CABIN

A. OXYGEN BOTTLESB. GALLEY LOCATIONC. EMERGENCY DOOR---TYPE IID. FIRST AID KIT

AFT CABINA. EMERGENCY DOORS---TYPE IIIB. FIRE EXTINGUISHER BOTTLES

BAGGAGE COMPARTMENT

A. ACCESS TO BAGGAGE COMPARTMENTB. SMOKE DETECTOR

*

*

*

*



MODEL 202

EXTERIOR WALK--AROUND

2

34

5

1

67

8

9

10

11

EXTERIOR WALK---AROUND

1. AIRSTAIR DOOR & DEMO OF EXTERNAL OPENINGSEQUENCE.

2. NOSE BAY ACCESS DOORS---BATTERY LOCATION& MAIN ELECTRICAL CONTACTOR BOX.

3. OXYGEN BOTTLE.4. NOSE GEAR WHEEL WELL, NOSE GEAR HYDRAULIC &RESERVOIR.

5. TYPE II EMERGENCY DOOR --- EXTERNAL OPENINGSEQUENCE.

7. TYPE III EMERGENCY DOOR --- EXTERNAL OPENINGSEQUENCE.

8. REAR COMPARTMENT ACCESS DOOR --- OPENINGSEQUENCE & FLIGHT DATA RECORDER & COCKPITRECORDER LOCATION.

9. BAGGAGE COMPARTMENT DOOR --- OPENINGSEQUENCE.

10. TYPE III EMERGENCY DOOR --- EXTERNAL OPENINGSEQUENCE.

11. NO1. NACELLE, MAIN LANDING GEAR & HYDRAULICRESERVOIR.



MODEL 202

INTERIOR ARRANGEMENT

MOVEABLEBULKHEAD

BAGGAGE DOOR50 in. W x 60 in. H(1.27 m x 1.52 m)

GALLEYLAVATORY

PASSENGER DOOR &CREW ENTRY

30 in. W x 65 in. H(0.762 m x 1.65 m)

FLIGHTATTENDANT’S

SEAT

WARDROBE

dod0570000_002.dg,pt,06/02/95

PASSSENGER CABIN LENGTH30 ft. 1 in. (9.16 m)

OBSERVER’SSEAT BAGGAGE

DOOR

BAGGAGE COMPARTMENT3

OVERHEAD BINS

300 cu ft ( 8.49 m )

107 in.( 2718 mm )

37 PASSENGERS



MODEL 202

CABIN CROSS--SECTION

* DIMENSIONS ARE APPROXIMATEAND MAY VARY DEPENDING ONAIRCRAFT CONFIGURATION ANDLOADING CONDITIONS.

NOTE:

dod0510000_003.dg,pb,03/01/94

106.00 in. DIA(2692 mm)

26.3 in.(668 mm)

17.3 in.(439 mm)

17.3 in.(439 mm)

20.3 in.(516 mm)

15.8 in.(401 mm)

80 in.(2032 mm)

76.5 in.(1943 mm)

57.4 in.(1458 mm)

24 in.(610 mm)

12.4 in.(315 mm)



MODEL 202

FLIGHT COMPARTMENT (VIEW FORWARD)

PILOT’S FLIGHTINSTRUMENT PANEL

FORWARD CENTERCONSOLE

CONTROLQUADRANT

AFT CENTERCONSOLE

ENGINEINSTRUMENTPANEL

MAPTABLE

CO---PILOT’S SIDECONSOLE PANEL

CO---PILOT’S FLIGHTINSTRUMENT PANEL

AIR VENT(GASPER)

GLARESHIELDPANEL ANDSHROUD

SUN VISORCOMPASS CORRECTION CARDASSIST HANDLE

UTILITY LIGHTDOME LIGHT

CAUTION LIGHTS PANEL

OVERHEAD CONSOLE

EMERGENCY ESCAPEROPE PANEL

CEILINGPANEL

PILOT’S SIDECONSOLE PANEL

NOSE WHEELSTEERING

SIDEWALLPANEL

CHARTHOLDER



MODEL 202

FLIGHT COMPARTMENT (VIEW AFT)

EMERGENCY LANDINGGEAR EXTENSIONHANDPUMP HANDLE

PORTABLEOXYGENBOTTLE

RIGHT DCCIRCUITBREAKERPANEL

VARIABLEFREQUENCYAC CIRCUITBREAKERPANEL

CO---PILOT’SOXYGENMASK

HEADSETSTOWAGE

MIRROR PASSENGERCABINVIEWER

OBSERVER’S OXYGEN MASK

PILOT’S OXYGEN MASK

FLASH LIGHTSAVIONICSCIRCUITBREAKERPANEL

LEFT DC

BREAKERPANEL

FIRE AXE

FIREEXTINGUISHER

WEIGHT ANDBALANCEMANUALSTOWAGE

DOOR OPENS INTOPAX COMPARTMENT

CIRCUIT



MODEL 202

EXITSGENERALThere are five emergency exits located on the aircraft. A Flight Compartment Emergency Escape Hatch, avail-able to the flight crew, is located in the Flight Compartment roof and is operated by an internal handle. AnAirstair door, located on the forward left side of the fuselage, is operated by internal or external handles. TheAirstair door incorporates an inflatable seal fed from the 18 psi deicing system. A Type II emergency exit door islocated on the right side of the fuselage, opposite the airstair door. Two Type III emergency exit doors are lo-cated one on each side of the fuselage, just forward of the wing. The Type II and Type III emergency exit doorseach incorporate a window and may be opened by either internal or external handles located below the win-dow. The Type II and Type III emergency exit doors incorporate a compression seal around the outside of thedoor to contain aircraft pressurization when the doors are closed.

TYPE II AND TYPE III EMERGENCY EXIT DOOR OPERATIONThe external handle, located below the window, is flush with the door skin and incorporates a push---button forquick---release, enabling the handle to be rotated. Rotating the handle actuates the locking pin and vent dishby a system of pulleys, a cable and a shaft quadrant. A cable guard is installed over the shaft quadrant.To remove either the Type II or Type III emergency exit door using the external handle, push the quick--- releasebutton to release the handle. Turn the handle counterclockwise to open the vent and retract the locking pin.Push the door inward.

AIRSTAIR DOOR OPERATIONThe Airstair door is opened externally by operation of the door handle lever located on the left side of the fuse-lage just forward of the door. Initial movement of the handle trips the door seal pressurizing valve to release theseal pressure allowing cabin pressure to deplete. Continued movement of the handle moves the door upwardand inward to clear the ten pressure pads from theirmating stops so that the doormay bemanually pulled open.Door lowering is assisted by a door counter---balance system.

SERVICE DOORSBAGGAGE DOOR OPERATIONTheBaggagedoor is located on the left side of the rear fuselage. Thedoor is opened and closedmanually usingan external handle which normally is flush with the door skin. A quick---release button is located in the center ofthe handle.To open the Baggage door, release the handle from the stowed position by pushing the quick---release button.Rotate the handle 180 degrees counterclockwise to unlock the door and initiate an inward and upward move-ment. Stow the handle by pressing it back into its recess in the door and, while supporting the door, manuallyraise to the fully open position. Secure the door in the open position by engaging the door support strut.

NOTE

Cabin compartment emergency entry from the baggage compartment is not normally possible.



MODEL 202

AIRCRAFT DOORS AND GROUND SERVICE PANELS

TYPE III MID CABIN EMERGENCYEXIT DOORS.(20.2 x 35.6 IN.) (513 x 904 mm)

REAR FUSELAGE ACCESSDOOR ( TO AIRCONDITIONING UNIT ANDA.P.U. ONLY).

BAGGAGE COMPARTMENTDOOR(50.0 x 60.0 IN.) (1270 x1524mm)

TYPE II FORWARDCABIN EMERGENCYEXIT DOOR.(20.2 x 55.3 IN.)(513 x 1403 mm)

FLIGHT COMPARTMENTEMERGENCY HATCH(18.5 x 20.6 IN.)(470 x 523 mm)

NOSE COMPARTMENT DOORS(DC CONTACTOR BOX.BATTERY & CREW OXYGEN)

AIRSTAIR DOOR(30.0 x 66 IN.)(762 x 1676 mm)



MODEL 202

EVACUATION ROUTES

TYPE III MID CABINEMERGENCY EXIT

TYPE II FORWARDCABIN EMERGENCYEXIT

FLIGHT COMPARTMENTEMERGENCY HATCH

AIRSTAIR DOOR TYPE III MID CABINEMERGENCY EXIT



MODEL 202

PASSENGER AND CREW ESCAPE SYSTEMS

WARNINGKEEP CLEAROF DOOR

PULL HANDLEOUT AND DOWNTO OPEN

SUPPORT DOORWHILE LOWERING

PUSH

OPEN

POSITION

TURN HANDLE DOWNAND PUSH HATCH IN

ROOF ESCAPE HATCH(SEE PAGE 13FOR DETAILS)

CREW EMERGENCY

DESCENT DEVICETYPICAL BOTHSIDES.



MODEL 202

BAGGAGE DOOR OPERATION

WARNING

LIFT DOOR TO OPENHANDLE TO BE FLUSH BEFORE LIFTING

WHEN RAISING OR LOWERING KEEP CLEAR OFDOOR PATH



MODEL 202

FLIGHT COMPARTMENT EMERGENCY ESCAPE HATCH

DESCRIPTION

The Flight Compartment escape hatch, located in the Flight Compartment roof, is completely detachable foremergency exit or can be partially opened for ventilation when the aircraft is on the ground. The hatch ismounted at the rear on two support fittings and at the front by two locking and release fittings. An operatinghandle, located in the center of the hatch, is retained in an open or closed position by an overcenter spring. Thehandle operates a transversely---mounted torque shaft assembly with arms attached at each end. Rollers at theend of each arm engage detented locking release fittings installed in the Flight Compartment roof structure.A seal is installed around the edge of the hatch to contain the aircraft pressurization when the hatch is closed.

OPERATION

To open the Flight Compartment escape hatch, rotate the handle 72 degrees counterclockwise. A mechanicallinkage connected to the handle rotates the torque tube and the rollers move forward in the fittings where theyare supported by the spring--- loaded detents. Controlled by the geometry of the torque tube and the rollers, thehatch pivots about the rear support fittings and opens approximately one inch at the front. Opening the hatchpermits depressurization and provides a modest amount of ventilation to the Flight Compartment.A downward pull on the handle of approximately 40 pounds releases the rollers against the action of the forwardlocking and release detent springs. The hatch may then be completely removed.



MODEL 202

FLIGHT COMPARTMENT EMERGENCY ESCAPE HATCH

NOTE:

IN AN EMERGENCY IT MAY BE POSSIBLEBY CUTTING THROUGH THE OUTER SKINTO GAIN ACCESS TO REPOSITION THEOPERATING HANDLE FROM OUTSIDE ANDTHEN FORCE THE HATCH DOWNWARDS.

FLIGHT COMPARTMENTEMERGENCY HATCH18.5” X 20.6” (470 X 523 mm)

EMERGENCYESCAPE ROPE

REAR SUPPORT FITTINGS

10 x 8 IN. (254 x 203 mm)

SEAL

ROLLERSPRING

DETENT

TORQUE SHAFT ASSEMBLYARM

ROLLERSPRING

OVERCENTER SPRING

OPERATING HANDLE



MODEL 202

ENGINE DANGER AREAS

0 3.05 6.10 9.14 12.19 15.2 18.3 21.3 24.4

0 10 20 30 40 50 60 70 80

0

10

20

30

40

50

60

70

0

3.05

6.10

9.14

12.19

15.2

18.3

21.3

FEET METRES

METRES

FEET

HOT EXHAUST

GASES VENTEDREARWARDS.

PERSONNEL DANGER AREAS(WHEN ENGINES ARE OPERATING)

*NOT ALL AIRCRAFT

APU EXHAUST*



MODEL 202

CUT--THROUGH AREAS

NOTE:

“CUT---THROUGH” AREAS REQUIRE PORTABLEMETAL---CUTTING EQUIPMENT. IT IS RECOMMENDEDTHAT MAJOR EFFORT TO GAIN ACCESS BEDIRECTED TO HATCHES AND DOORS DUE TO THETYPE OF STRUCTURE AND POSSIBLE INJURY TOPERSONNEL WITHIN.

INTERIOR CONSTRUCTION

---STRINGERS RUN ABOVE & BELOW WINDOWS---SKIN THICKNESS .060 IN. (1.50mm).

CUT---THROUGH AREASTYPICAL BOTH SIDES

SIDE WINDOW(NON---OPENING)

WINDSHIELD

PASSENGER COMPARTMENTWINDOWS.

TYPICAL CUT---THROUGH

AREA DIMENSIONS(42.0 x 20.0 IN.) (1067 x 508 mm)

THE THIRD WINDOW AFTOF AIRSTAIR DOOR IS RECOMMENDEDFOR FIRST CHOICE CUT---THROUGH(ALTHOUGH ANY WINDOW IS SUITABLE).



MODEL 202

FUSELAGE SAFETY EQUIPMENT LOCATIONS

*NOTE: MAY VARY WITH AIRLINE & CONFIGURATION

DOORBAGGAGE

FIREEXTINGUISHER

FLIGHTATTENDANT’SSEAT

LIFE JACKETAND FLASHLIGHT

EMERGENCY EQUIPMENTAND SUPPLIES STOWAGECOMPARTMENT

GALLEY

VIEW LOOKING FORWARD

VIEW LOOKING OUTBOARDLEFT SIDE

GALLEY

OXYGENMASK BAG

DETAIL ‘A’ AND ‘C’

CYLINDER

STRAP

FIRE EXTINGUISHER

DETAIL ‘B’

DETAIL ‘A’

OXYGENCYLINDER

TAPE

HOLDER

SEAT BELTEXTENDERS



MODEL 202

CREW OXYGEN LOCATIONS

RED:GREEN:YELLOW:BLUE RADIAL:

0 --- 250 psi (DANGER LEVEL250 --- 1800 psi (USEABLE RANGE)1800 --- 2500 psi (OVERPRESSURE)1300 psi (MINIMUM DISPATCH)

RANGE MARKS

OXYGEN INDICATOR

CO---PILOT’S OXYGEN MASK

OBSERVER’S HEADSET

OBSERVER’S HEADSET CONN’NAND MICROPHONE SWITCH

OBSERVER’S OXYGEN MASK

PILOT’S OXYGEN MASK

FULL FACESMOKEMASK

PILOT’S OXYGENSUPPLY OUTLET

CREW PORTABLEOXYGEN CYLINDER

FORWARD PRESSURE BULKHEAD

PRESSURE INDICATOR

CREW ---OXYGEN CYLINDER(39.4 CU FT./ 1.1m3)

OVERBOARDDISCHARGEINDICATOR

COPILOT’S OXYGENSUPPLY OUTLET



MODEL 202

PASSENGER OXYGEN CYLINDER (OPTIONAL)

PRESSUREGAUGE

PASSENGEROXYGENCYLINDER

BLOW OUT DISC(EXTERNALLY VISIBLE)

PRESSUREREGULATOR

PRESSUREGAUGE

CHARGINGVALVE

BAGGAGE COMPARTMENT



MODEL 202

FLOWCONTROLSELECTOR

PRESSUREGAUGE

PASSENGER OXYGEN AUTOMATIC PRESENTATION SYSTEM (OPTIONAL)



MODEL 202

FIRE CONTROL RECOMMENDATIONS

FIRE AREA EXTINGUISHER TYPE NOTES

PREFERRED ALTERNATIVE AVOID

ENGINE FIRES HALON 1211 FOAM CO2 CAN DAMAGEENGINE.

DRY CHEMICAL ISCORROSIVE.

FUEL FIRE 1. DRY CHEMICALPOWDER FORLEAKING FUEL.2. WATER FOG OR

FOAM ONGROUND SPILL

AREA.

WHEEL FIRE DRY CHEMICALPOWDER

HALON 1211 CO2 --- WHEELBREAKAGE ISPOSSIBLE.

1. WHEELS AREEQUIPPED WITHFUSIBLE PLUGSWHICH WILLBLOW AT 288oF(142oC).

2. APPROACHLANDING GEARFROM FORWARDOR AFT. STANDUPWIND OF FIRETO AVOID ’SKY-DROL’ FUMES.ALL WHEELS AREFORGED ALUMI-

NUM.

ELECTRICAL FIRE HALON 1211 DRY CHEMICALPOWDER/CO2

WATER

HYDRAULIC SER-VICE BAY FIRE

HALON 1211 DRY CHEMICALPOWDER/CO2

WATER

ELECTRICAL/ELECTRONIC

SERVICE BAY FIRE


WATER

GALLEY FIRE HALON 1211 DRY CHEMICALPOWDER

WATER

FLIGHT COMPART-MENT FIRE

HALON 1211 DRY CHEMICALPOWDER

WATER

CABIN COMPART-MENT FIRE

HALON 1211 DRY CHEMICALPOWDER

WATER

CARGO COM-PARTMENT FIRE


WATER



MODEL 202

FLAMMABLE MATERIAL LOCATIONS

TOTAL OIL CAPACITYFOR BOTH ENGINES

IMP GAL. US GAL. LITRES9.24 11.09 42

RESERVOIR IMP QTS US QTS LITRES

NO. 1 SYSTEMNO. 2 SYSTEMNOSE

2.204.311.06

2.685.191.25

2.504.901.20

ALL SYSTEMS USE PHOSPHATE ESTER---BASEDTYPE IV FLUID eg. SKYDROL

HYDRAULIC FLUID

NO.2 SYSTEMHYDR. RESERVOIR

NOSE GEAR WHEEL WELLHYDRAULIC RESERVOIR

NO.1 SYSTEMHYDR. RESERVOIR

NO.1 TANK OVERWINGREFUEL POINT

PRESSURE REFUEL POINT

NO.2 TANK OVERWINGREFUEL POINT

BASED ON JET A---1 S.G. OF 0.816(SINGLE TANK DIVIDE BY 2)

STANDARD FUEL TANKS 5765 2614 705 846 3203EXTENDED RANGE TANKS 10,433 4732 1276 1532 5800

TOTAL FUEL CAPACITY

LB KGIMPGAL

USGAL LITRES



MODEL 202

ENGINE FIRE ACCESS LOCATIONS

NOTE:

* APPROX. 2 FT. LOWER INWHEELS---UP SITUATION.

* THERE ARE NO EXTERNALLYACCESSIBLE ENGINE FIREACCESS PANELS.

INTAKE TOGROUND LEVEL(7.53 FT) (2.30m)

EXHAUST TOGROUND LEVEL(9.58 FT.) (2.92m)



MODEL 202

ENGINE FIRE EXTINGUISHERAND BATTERY POWER SWITCH LOCATIONS

ENGINE FIRE EXTINGUISHER OPERATION

A. ELECTRICAL POWER MUST BE PRESENTB. PULL “PULL FUEL OFF” HANDLE.C. SELECT “EXTG” TOGGLE SWITCH TOEITHER “AFT BTL” OR “FWD BTL”.

REMOVING ELECTRICAL POWER

A. SELECT “BATTERY MASTER” SWITCHTO “OFF”.

B. SELECT “AUX BATT” AND “MAIN BATT”SWITCHES TO ”OFF”.

C. SELECT “EXT PWR” TO “OFF”.

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