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Effective Pages 1 * Nov 05/2014

Contents 1 * Nov 05/2014

Chapter 00 1 * Nov 05/20142 * Nov 05/20143 * Nov 05/20144 * Nov 05/20145 * Nov 05/20146 * Nov 05/20147 * Nov 05/20148 * Nov 05/20149 * Nov 05/2014

10 * Nov 05/201411 * Nov 05/201412 * Nov 05/201413 * Nov 05/201414 * Nov 05/201415 * Nov 05/201416 * Nov 05/201417 * Nov 05/201418 * Nov 05/201419 * Nov 05/201420 * Nov 05/201421 * Nov 05/201422 * Nov 05/201423 * Nov 05/201424 * Nov 05/201425 * Nov 05/201426 * Nov 05/201427 * Nov 05/201428 * Nov 05/201429 * Nov 05/201430 * Nov 05/201431 * Nov 05/201432 * Nov 05/201433 * Nov 05/201434 * Nov 05/201435 * Nov 05/201436 * Nov 05/201437 * Nov 05/201438 * Nov 05/201439 * Nov 05/201440 * Nov 05/2014

41 * Nov 05/201442 * Nov 05/201443 * Nov 05/201444 * Nov 05/201445 * Nov 05/201446 * Nov 05/201447 * Nov 05/201448 * Nov 05/2014


LIST OF EFFECTIVE PAGES

Chapter Page Date Chapter Page Date

Model 400

Page 1

Nov 05/2014

The asterisk (*) indicates pages revised, added or deleted by current revision.

EFFECTIVEPAGES


THIS PAGE INTENTIONALLY LEFT BLANK

CHAPTER 00 Chapter title

Aircraft Dimensions 1Familiarization and Location Guide 3Exterior Walk−Around 4Typical Interior Configurations 5Passenger − Compartment Cross Section 9Typical Flight Compartment Arrangement (LookingForward)

10

Typical Flight Compartment Arrangement (Looking Aft) 11Aircraft Doors and Ground Service Panels 12Evacuation Routes 13Passenger and Crew Escape Systems 15Forward Passenger Door−Ditching Dam Operation 20Forward Baggage Door Operation/Forward Type IEmergency Exit Door

22

Forward RH Type I Emergency Exit Door−Ditching DamOperation

24

Aft Baggage Door Operation 26Flight Compartment Escape Hatch 28Fortified Flight Compartment Door Operation 30Propeller/Engine Exhaust Danger Areas 32Cut−Through Areas 34Flammable Material Locations (Excluding PassengerCabin)

35

Flammable/Hazardous Material Locations in PassengerCabin

36

Fire Control Recommendations 40Crew Oxygen System 42Engine Fire Access Locations 43Fire Extinguishing Systems Locations 44Fire Extinguishing Systems Operation 46Battery Power Switch Locations 48


TABLE OF CONTENTS

Title Page

Model 400

Page 1

Nov 05/2014CONTENTS



CHAPTER 00

CHAPTER TITLE



93ft 3in.(28.42m)

43.31in.(1.10m)

28ft 10in.(8.80m)

13ft 6in.(4.11m)

107ft 9in.(32.83m)

27ft 4in.(8.34m)

45.94in.(1.17m)

101ft 10in.(31.04m)

60.83in.(1.55m)

10ft 9in.(3.28m)

GROUNDREFERENCE LINE

60.85in.(1.55m)

48.98in.(1.24m)

12ft 4in.(3.76m)

*

* * * *

*

NOTE36ft 10in.(11.22m)

8ft 2in.(2.48m)

30ft 5in.(9.27m)

DIHEDRAL 2.5 o38.67in.(98.22cm)

12ft 10in.(3.92m)

25ft 8in.(7.81m)

**

*

Dimensions with respect to groundreference line are approximate andwill vary with aircraft configurationand loading conditions.

36.00in.(91.44cm)

45ft 9in.(13.94m)

cg35

65a0

1.dg

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014

*


AIRCRAFT DIMENSIONS (INCL EXTRA CAPACITY CONFIGURATION) (Sheet 1 of 2)

Figure 00 − 1Model 400

Page 1

Nov 05/2014

AFT PASSENGER DOOR24.00 in. (60.96 cm) W65.00 in. (165.10 cm) H

TYPE I EXIT ANDSERVICE DOOR

24.00 in. (60.96 cm) W54.00 in. (137.16 cm) H

FLIGHT COMPARTMENTESCAPE HATCH

18.50 in. (46.99 cm) L20.60 in. (52.32 cm) W

FORWARD PASSENGER DOOR30.00 in. (76.20 cm) W65.00 in. (165.10 cm) H

EMERGENCY EXIT DOOR

UPPER (TYPE II) ANDLOWER (TYPE III) FORWARDEMERGENCY EXIT DOORS

20.20 in. (51.31 cm) W56.00 in. (142.24 cm) H

24.00 in. (60.96 cm) W54.00 in. (137.16 cm) H

BAGGAGE DOOR51.00 in. (129.54 cm) W59.00 in. (149.86 cm) H

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20/2

014

FORWARD TYPE IFORWARD BAGGAGE DOOR/

Type II/III emergency exit door is de−activated for the extra capacity configuration.NOTES

Forward type I emergency exit door is installed only on aircraft with extra capacity configuration.2

2


AIRCRAFT DIMENSIONS (INCL EXTRA CAPACITY CONFIGURATION) (Sheet 2 of 2)


Page 2

Mar 18/2005


Model 400

Page 3

Nov 05/2014

brb9

4a01

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4

1

2

34

56

7

8 9

10

11

1213

14

8

EXTERIOR WALK AROUND SEQUENCE (FOR CREW TRAINING PURPOSES)

1. Airstair door location and demo of external opening sequence.2. Nose fuselage access door − batteries and contactor box locations.3. Crew oxygen bottle.4. Nose landing gear location and description, auxiliary hydraulic reservoir

and hydraulic lines location and description.5. Forward baggage door location and demo of external opening sequence,

fire bottle location /forward type I emergency exit location and demo of

6. Type II/III emergency exit door location and demo of external opening sequence.7. No. 2 nacelle − main landing gear location and description, hydraulic reservoir

and hydraulic lines location and description, fire bottle locations.8. Fuel tanks location and description.9. Service door location and demo of external opening sequence.

10. Aft equipment bay access door−opening sequence, flight data recorder andcockpit voice recorder locations.

11. Auxiliary power unit (APU) bay access door − APU location and description.12. Aft baggage door location and demo of external opening sequence,

fire bottle locations.13. Aft passenger door location and demos of external opening sequence, optional folding

14. No. 1 nacelle − main landing gear location and description, hydraulic reservoirand hydraulic lines location and description, fire bottle locations.

stairs (if equipped).

Forward type I emergency exit door is installedonly on aircraft with extra capacity configuration.

Type II/III forward emergency exit door isde−activated for the extra capacity configuration.

NOTES

external opening sequence.


EXTERIOR WALK−AROUND


Page 4

Nov 05/2014

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TYPICAL SERIES 400 INTERIOR CONFIGURATIONS (Sheet 1 of 4)


Page 5

Nov 05/2014

7

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Page 6

Nov 05/2014

PA

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.(1

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30.0

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. H(6

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.65

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Page 7

Nov 05/2014

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. (18

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Page 8

Nov 05/2014

br72

1a01

.dg,

gv,

12/

04/0

2

106.0 in.(2.69 m)

77.0 in.(1.95 m)

56.5 in.(1.44 m)

24.3 in.(0.62 m)

12.4 in.(0.32 m)

15.8 in.(0.40 m)

20.0 in(0.51 m)

25.9 in.(0.66 m)

99.0 in.(2.51 m)

80.0 in.(2.03 m)

108.8 in.(2.76 m)

GROUND REFERENCE LINE

OVERHEAD STOWAGE BINS(CAPACITY IS 1.67 Ft (0.047 m )/PAX.)2 3

NOTE

71.8 in.(1.82 m)

1

111.37 in (28.9 cm)

AT DOOR CENTER LINE

101.1 in.(2.56 m)

This dimension is approximate and will vary with aircraft configuration and loading conditions.

15.74 in. (14.6 cm)AT FWD EDGE OF DOOR6.21 in. (15.8 cm) AT AFT EDGE OF DOOR

GROUND REFERENCE LINE


PASSENGER COMPARTMENT CROSS SECTION


Page 9

Nov 05/2014

1. Overhead speakers.2. Stowage pockets.3. Map tables.4. Gaspers.5. Sun visors.6. Hand holds.7. Compass calibration card.8. Eye level indicator.9. Standby compass.

10. Caution/Warning lights panel.

11. Overhead panel.12. Nosewheel steering hand control.13. Center console (aft).14. Center console (fwd).15. Side console (pilot & copilot).16. Utility lights.17. Glareshield panel.18. Copilot’s instrument panel.19. Engine instrument panel.20. Pilot’s instrument panel.

LEGEND

986161

5

4

15

12

3

2

20 19 13 14 18

17

10 116

161

75

4

15

3

2

br25

1a01

.dg,

pt,

05/0

5/00


TYPICAL FLIGHT COMPARTMENT ARRANGEMENT (LOOKING FORWARD)


Page 10

Nov 05/2014

1. Right DC circuit breaker panel.2. Circuit breaker panel lights.3. Oxygen masks ( Pilot’s and Copilot’s).4. Observers headset stowage.5. Dome lights.6. Mirror.7. Viewer.8. Avionics bay air vent.9. Headset jacks.

10. Observer’s seat backrest.11. Weight and balance papers.12. C of A and C of R holders.

14. Landing gear emergency extensionhandpump handle.

15. Avionics circuit breaker panel.16. Left DC circuit breaker panel.17. Variable frequency AC circuit breaker

panel.

LEGEND

1

17

9

2

3

45

6 7 8 53

2

9

15

16

13 14 11 10

3

13. Observer’s smoke goggles.

18. Crew PBE.

18

br25

2a01

.dg,

pt,

12/1

1/98


TYPICAL FLIGHT COMPARTMENT ARRANGEMENT (LOOKING AFT)


Page 11

Nov 05/2014

SERVICE DOOR

AFTPASSENGER DOOR

AFTBAGGAGE DOOR

AFTEQUIPMENT BAYACCESS DOOR

APU CLAMSHELLACCESS DOOR

FORWARDPASSENGER DOOR


TYPE II/IIIEMERGENCYEXIT DOOR

FORWARD BAGGAGE DOOR/FORWARD TYPE I

EMERGENCY EXIT DOOR

cg35

66a0

1.dg

, cs,

aug

20/2

014

Type II/III emergency exit door is de−activated for the extra capacity configuration.NOTES

Forward type I emergency exit door is installed only on aircraft with extra capacity configuration.2

2


AIRCRAFT DOORS AND GROUND SERVICE PANELS (INCL EXTRA CAPACITYCONFIGURATION)


Page 12

Nov 05/2014

brb9

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16/2

014

FORWARD PASSENGERAIRSTAIR DOOR

TYPE IEMERGENCY EXIT/

AFT PASSENGER DOOR


TYPE II/IIIEMERGENCY EXIT


STANDARD CONFIGURATION

WITH DITCHING DAM

SERVICE DOOR


EVACUATION ROUTES (Sheet 1 of 2)


Page 13

Nov 05/2014

TYPE II/IIIEMERGENCY EXIT


SERVICE DOOR


FORWARD PASSENGERAIRSTAIR DOOR


AFT PASSENGER DOOR

FORWARD TYPE IEMERGENCY EXIT DOOR

WITH DITCHING DAM

NOTE

Type II/III emergency exit door is de−activatedfor the extra capacity configuration br

b92a

02.d

g, c

s/km

w, s

ep15

/201

4

EXTRA CAPACITY CONFIGURATION


EVACUATION ROUTES (Sheet 2 of 2)


Page 14

Nov 05/2014

Passenger and Crew Escape Systems

A. General

1. There are five emergency exits on the aircraft.

a. A flight compartment emergency escape hatch for the flight crew. This is installed inthe flight compartment roof. The hatch is operated by an internal handle.

b. The forward passenger door is an airstair type door. This is installed on the forwardleft side of the fuselage. The forward passenger door is operated by internal orexternal handles.

c. The forward Type I emergency exit door which is a translating type door. This isinstalled on the forward right side of the fuselage for the extra capacityconfiguration. It consists of an upper and a lower door. The lower door can be keptclosed by a internal locking handle in the event of a ditching procedure. Thisemergency exit can be operated by internal or external handles.

NOTE: The forward Type I emergency door is installed in lieu of forward baggagedoor for the extra capacity configuration.

d. A type II/III emergency exit door is installed on the forward right side of the fuselage.It consists of an upper and a lower door. The lower door can be kept closed in theevent of a ditching procedure. This emergency exit can be operated by internal orexternal handles.

NOTE: The type II/III emergency exit is de−activated for the extra capacityconfiguration.

e. The aft passenger door which is a translating type door is installed on the aft leftside of the fuselage. This can be operated by internal or external handles.

f. The aft service door which is also a translating type door is installed on the aft rightside of the fuselage. This can be operated by internal or external handles.

B. Forward Passenger Door Operation

1. Stay on the left side of the door.2. Push in the flap at the top of the door operating handle. Pull the door operating handle

down quickly and fully.

NOTE: This will unlock the door and move it up a small distance and out.3. Hold the door and lower it to the open position.

NOTE: You can use the door lowering assist to help you to do this.4. Push down on the struts of the handrail to lock the door in the open position.

C. Aft Passenger Door Operation

NOTE: The door will come out 16 inch (40 cm) before it swings to the left. Make sure theladder or platform is placed more than this distance.


Model 400

Page 15

Nov 05/2014

1. Push in the flaps at the top of the handle with your fingers.2. Pull the door operating handle out.

NOTE: This will unlock the handle and open the vent door3. Turn the door operating handle 90° counterclockwise.

NOTE: This will unlock the door and move it up and out a small distance.4. Use the handle to pull and move the door fully to the left to engage the gust lock.

NOTE: This will lock the door in the open position.

NOTE: Optional folding stairs may be installed. The stairs slide forward from theirenclosure (located in the aft baggage bulkhead, just inboard of the aft passengerdoor threshold) and are unfolded and extended by hand. The folding stairs areintended for use in normal ramp operations only.

D. Forward Type I Emergency Exit Door Operation

NOTE: The forward Type I emergency exit door is installed in lieu of forward baggage dooron aircraft with the extra capacity configuration.

NOTE: The Forward Type I Emergency Exit Door consists of an upper and a lower door.The lower door is kept closed by a internal locking handle in the event of a ditchingprocedure.

NOTE: The door will come out 16 inch (40 cm) before it swings to the right. Make sure theladder or platform is placed more than this distance.


NOTE: This will unlock the handle and open the vent door.3. Turn the door operating handle 90° clockwise.

NOTE: This will unlock the door and move it up and out a small distance.4. Use the handle to pull and move the door fully to the right to engage the gust lock.


E. Type II/III Emergency Exit Door Operation

NOTE: The Type II/III emergency exit door is de−activated on aircraft with the extra capacityconfiguration.

NOTE: The weight of the door is 29 lb (13.15 kg)

1. Operate the pushbutton on the handle to release it.2. Turn the handle counterclockwise to the open marking.

NOTE: This will unlock the door and move it in.


Model 400

Page 16

Nov 05/2014

3. Push the door in.

NOTE: With the ditching dam handle in the LAND position, the lower door will fall open.With the ditching dam handle in the SEA position, the lower door will stay closed.

F. Service Door Operation







Model 400

Page 17

Nov 05/2014

brb9

0a01

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, sep

11/2

014

A B

EXTERIOR OF FORWARD PASSENGER DOOR

EXTERIOR OF AFT PASSENGER DOOR

HANDLE IN OPENPOSITION(TYPICAL)

PULL HANDLEAND TURNTO OPEN


DOORLOWERING

ASSISTPUSH

WARNINGKEEP CLEAR

OF DOORPULL HANDLE

OUT AND DOWNTO OPEN

SUPPORT DOORWHILE LOWERING

VENT DOOR


PASSENGER AND CREW ESCAPE SYSTEMS (Sheet 1 of 2)


Page 18

Nov 05/2014

HANDLE INOPEN POSITION



EXTERIOR OF TYPE II / III EMERGENCY EXIT DOOR

EXTERIOR OF AFT

PUSH TORELEASE

TURN HANDLE DOWNAND PUSH HATCH IN

brb9

0a02

.dg,

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kmw

, oct

01/2

014

FLIGHTCOMPARTMENTESCAPE HATCH

CREW EMERGENCYDESCENT ROPE

(TYPICAL BOTH SIDES)



EXTERNAL OPERATINGHANDLE

(CLOSED POSITION)

VENT DOOR


Type II/III emergency exit door is de−activated

NOTES

1

for the extra capacity configuration.1

EXTERIOR OF FORWARD BAGGAGE DOOR/FORWARD TYPE I EMERGENCY EXIT DOOR

VENT DOOR

SERVICE DOOR

PUSH TO LOCK

PUSH TO LOCK

3. The forward baggage door has a separate interiorlockable door which can prevent exterior access.


PASSENGER AND CREW ESCAPE SYSTEMS (Sheet 2 of 2)


Page 19

Nov 05/2014

Forward Passenger Door−Ditching Dam Operation

A. Deploy the ditching dam as follows:

1. Pull the ditching dam down by its handle until it is at chest level.2. Put your hand on the top surface of the ditching dam and push it down to the floor.

NOTE: With the ditching dam correctly deployed, it will be inclined slightly outboard.3. Open the forward passenger door for evacuation.


Model 400

Page 20

Nov 05/2014

A

brl1

0a01

.dg,

sw

, 23/

07/9

9

LEGEND

1

2

1. Flight attendant seat.2. Handle.

EXIT

2

NOTEPull down to deployditching dam.


FORWARD PASSENGER DOOR − DITCHING DAM OPERATION


Page 21

Nov 05/2014

Forward Baggage Door Operation/Forward Type I Emergency Exit Door

A. Forward Baggage Door Operation

NOTE: The forward baggage compartment is removed and forward Type I emergency exitdoor is installed in lieu of forward baggage door for the extra capacity configuration.

NOTE: Do not attempt to enter the passenger cabin from the forward baggage compartment(i.e. through the interior compartment door). Access may be restricted by optionalgalley stowage equipment and/or baggage and there is no handle on the baggage−compartment side of the door.







Model 400

Page 22

Nov 05/2014

br84

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.dg,

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/km

w, o

ct01

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4

A

A



VIEW LOOKING INBOARD ON R/H SIDE


(CLOSED POSITION)

VENT DOOR


(OPEN POSITION)

AIRCRAFTCENTERLINE

VIEW LOOKING DOWN ON R/H SIDEFORWARD BAGGAGE DOOR/ FORWARD TYPE I

EXTERIOR OF FORWARD BAGGAGE DOOR/FORWARD TYPE I EMERGENCY EXIT DOOR


2. The forward baggage door has a separate interior

NOTES

1

1

EMERGENCY EXIT DOOR (OPEN POSITION)

PUSH TO LOCK

lockable door which can prevent exterior access.


FORWARD BAGGAGE DOOR/ FORWARD TYPE I EMERGENCY EXIT DOOR OPERATION


Page 23

Nov 05/2014

Forward RH Type I Emergency Exit Door−Ditching Dam Operation

A. Deploy the ditching dam as follows:

1. Turn the ditching dam handle clockwise from the horizontal position.

NOTE: This will extend the lock pins to engage the ditching dam to the surroundstructure and disengage from the emergency exit door.

2. Open the forward Type I emergency exit door for the evacuation.


Model 400

Page 24

Nov 05/2014

1. Ditching dam.2. Type I emergency exit door.3. Ditching dam handle.

LEGEND

VIEW LOOKING OUTBOARD

3

1

2

brbs

45a0

1.dg

, km

w, s

ep16

/201

4

4. Label, ditching dam operation.

4


FORWARD TYPE I EMERGENCY EXIT DOOR − DITCHING DAM OPERATION


Page 25

Nov 05/2014

Aft Baggage Door Operation

A. Aft Baggage Door Operation

1. Push the pushbutton on the door operating handle to release the handle from therecess.

2. Turn the handle 90° counterclockwise.

NOTE: This will unlock the door and move it in.3. Lift the door up a sufficient distance that you can get access to the telescopic strut.

Remove the telescopic strut from the stowed position.

NOTE: Make sure you do this before you open the door fully or it will be too high to closeeasily.

4. Continue to lift the door until it is fully open.5. Attach the telescopic strut to the receptacle on the lower left side of the door opening.

This will give more support to the door.


Model 400

Page 26

Nov 05/2014

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011

A

A

EXTERIOR OF AFT BAGGAGE COMPARTMENT DOOR


HANDLE IN OPENPOSITION

SIDE VIEW OF DOOR IN OPEN POSITION

Z−100.032FLOOR LEVEL

HANDLEPOSITION

TELESCOPIC STAY ASSY

DOOR BALANCED WITH

(CLOSED POSITION)


AFT BAGGAGE COMPARTMENT DOOR − LOCATION AND OPERATION


Page 27

Nov 05/2014

Flight Compartment Escape Hatch

NOTE: In an emergency, you can try to get access by cutting through the outer skin to move theoperating handle from the outside. Then push the hatch down.

WARNING:HOLD THE ESCAPE HATCH DURING THE PROCEDURE. IF YOU DO NOTDO THIS, THE ESCAPE HATCH CAN FALL AND CAUSE INJURIES TOPERSONS AND DAMAGE TO THE EQUIPMENT.

A. Open the flight compartment escape hatch as follows:

1. Turn the handle 72 degrees counterclockwise. The escape hatch opens approximately 1in. at the front.

2. Pull the door down with 40 lb of force to release the rollers from the lock mechanism.


Model 400

Page 28

Nov 05/2014

PULL HANDLE DOWNTO REMOVE HATCH

VENT CLOSED

PULL HANDLE DOWN

TO REMOVE HATCH

VENT

CLOSED

PULL HANDLE DOWNTO REMOVE HATCH

VENT CLOSED

1

2

3

ROTATE HANDLE TOVENT POSITION

PULL DOWNON HANDLE

REMOVE HATCH

br20

1a01

.dg,

pt,

21/0

8/97

A

A

REAR SUPPORTFITTINGS

REAR SUPPORTBRACKET

FLIGHT COMPARTMENTEMERGENCY EXIT HATCH

TORQUE SHAFTASSEMBLY

ARM

ARM/SPRINGDETENT

MECHANISM

OPERATINGHANDLE

OPERATING HANDLE OPERATING HANDLE


FLIGHT COMPARTMENT ESCAPE HATCH


Page 29

Nov 05/2014

Fortified Flight Compartment Door Operation

A. Opening Flight Compartment Door from Flight Compartment Side

1. Pull slide latch to the right and push flight compartment door open.2. If engaged, rotate deadbolt handle 90 degrees clockwise to the unlatched position (two

red dots on dead bolt plate behind knob will become visible).

B. Opening Flight Compartment Door from Cabin Side

1. Emergency Access

In an emergency, use a pry bar. Work the pry bar into the door jam at the slide latchand deadbolt location until the door frame distorts sufficiently to allow the flightcompartment door to open.

2. Optional Entry

NOTE: U.S. registered aircraft do not have Remote Access System.

Press the Remote Access System Flight Attendant Access Switchlight on thewardrobe maintenance panel. A white light will illuminate on the switch. The flightcompartment door will automatically open after a timed delay of 40 seconds if there isno response by the flight crew. An amber light will illuminate on the Flight AttendantAccess Switchlight indicating that the flight compartment door is unlatched.ORThe Remote Access System can be disabled by removing electrical power from theaircraft (i.e. disconnect batteries and ground power). Door latch solenoid will de−energize and door will open.

NOTE: The Fortified Flight Compartment Door will not open if the deadbolt lock isengaged.

NOTE: The key access feature for the deadbolt lock will be disabled if both arms ofthe rotary knob on the flight compartment side are set to the latched position .


Model 400

Page 30

Nov 05/2014

CDPL595

PINS MUST BE FULLY ENGAGED AT ALL TIMES

FOR GROUND U

SE UNLY

DEADBOLT POSITIONS

UNLOCKED

KEY OPERABLE

LOCKED

LOCKED

KEY INOPERABLE

CDPL600

HUNTINGTON BEACH,CA

SERIAL NO.

GROSS W

T. LBS

GROSS W

T. KGS

MFG.DATEPART NO.

CDPL628−3

CDPL628−3

1

2

1

2

3

3PRY HEREWITH

CROWBAR

1. Fortified door.2. Slide latch (operable

from flight compartmentonly).

3. Deadbolt lock.

LEGEND

bray

38a0

1.dg

, gw

, 01/

03/0

5


FORTIFIED FLIGHT COMPARTMENT DOOR DETAIL


Page 31

Nov 05/2014

Personnel danger areaswhen engines are operating(areas shown are approximate).

108 ft. 35 m

30

20

10

0

50

0

HOT ENGINEEXHAUST GASESVENTEDREAR WARDS

APU EXHAUST(NOT ON ALL AIRCRAFT)

0

0 10

50

20

93 ft.

28.4 m

100LEGEND

brg3

5a01

.dg,

pt,

09/0

2/00


PROPELLER / ENGINE EXHAUST DANGER AREAS (Sheet 1 of 2)


Page 32

Nov 05/2014

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17/2

011

−100

R(ft) 0

100

50 ft/sec 40 ft/sec 30 ft/sec 25 ft/sec 20 ft/sec

100 200 300X(ft)

SLIPSTREAM VELOCITY CONTOURS (~18% TORQUE) (STATIONARY ON GROUND)

SLIPSTREAM VELOCITY CONTOURS (~43% TORQUE) (STATIONARY ON GROUND)

−200

−100

R(ft)

0

100

500400300200100 X(ft)

80 ft/sec

90 ft/sec60 ft/sec

70 ft/sec40 ft/sec

50 ft/sec 30 ft/sec 20 ft/sec


PROPELLER / ENGINE EXHAUST DANGER AREAS (Sheet 2 of 2)


Page 33

Nov 05/2014

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3/03

/01

RECOMMENDEDCUT−THROUGH

AREA DIMENSIONS45.0 x 20.0 in. (1143 x 508 mm)

PASSENGERCOMPARTMENT

WINDOWS

SIDE WINDOW(NON−OPENING) The third window fwd of the aft passenger doors

"Cut−through" areas require portable metal cuttingequipment. It is recommended that major effortto gain access be directed to doors and hatchesdue to the type of structure and possible injuryto personnel within.

WINDSHIELD

INTERIOR CONSTRUCTION −STRINGERSRUN ABOVE AND BELOW WINDOWS−SKIN THICKNESS .006 in. (1.50 mm)

are the recommended first choice cut−throughareas. (Although any window is suitable in extremecircumstances).

2. Cut−through areas shown in red on Rescue Chart may appear as other colours on the aircraft.

NOTES


CUT−THROUGH AREAS


Page 34

Nov 05/2014

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0a01

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jp/p

t, 05

/06/

00

ITEM NAME ITEM LOCATION

1

2

3

4

5

6

7

8

9

1

2

3

4

5

6

7

89

4

Main Battery and Auxiliary Battery

Crew Oxygen Cylinder

Crew PBE

Fuel Tank

No. 1 Hydraulic Reservoir


Cockpit Voice Recorder and FlightData Recorder

Standby Battery


Nose lower compartment−left side

Nose lower compartment−right side

Flight compartment, behind co−pilot’s seat

Integral

Left nacelle

Right nacelle

Aft fuselage

Aft fuselage

Aft fuselage

113AL

112AR

413CR

423CR

311AB

311AB

311AB

ITEM No. ACCESS PANEL/DOOR

NOTES 39.8 Cu Ft A.T.

Based on specific gravity of 0.816(single tank − divide by 2)

US Gal.1785

Imp. Gal.1486

L6756

LB12138

Kg5506

ReservoirNo. 1 SystemNo. 2 SystemNo. 3 SystemAux. System (Nose)

US Qt. Imp. Qt. L8.3

12.52.6

1.06

6.910.42.2

1.27

7.911.82.5

1.20

TOTAL FUEL CAPACITY

HYDRAULIC FLUID CAPACITY

NOTEStandby battery in nosewith APU installed.


FLAMMABLE MATERIAL LOCATIONS (EXCLUDING PASSENGER CABIN)


Page 35

Nov 05/2014

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LEGEND

Fire extinguisher.

Oxygen bottle.o2

o2

PBE Crew ProtectiveBreathing Equipment.

PBE

PBEx 4

x 2 x 2

o2

−In doghouse

−2 in doghouse −1 on top of doghouse −1 on fwd. side of doghouse



FLAMMABLE/HAZARDOUS MATERIAL LOCATIONS IN PASSENGER CABIN (Sheet 1 of 4)


Page 36

Nov 05/2014

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014


LEGEND

Fire extinguisher.

Oxygen bottle.o2

o2


PBE

PBE

o2

PBE

X 3

−On aft baggage bulkhead

−In drawer behind seats, opens aft




Page 37

Nov 05/2014

bru1

6a03

.dg,

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/cs,

aug

25/2

014

LEGEND

Fire Extinguisher.

Oxygen bottle.o2

o2


PBE

PBE

x 3

x 2 x 2

o2

x 2

o2

−2 in drawer behind seats,opens aft

−1 on fwd. side of enclosure

−In doghouse

−1 on top of doghouse −1 on fwd. side of doghouse





Page 38

Nov 05/2014

bru1

6a04

.dg,

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aug

25/2

014

o2

LEGEND

Fire extinguisher.

Oxygen bottle.

x 2

x 3o2

x 2o2

o2

EXTRA CAPACITY CONFIGURATION




Page 39

Nov 05/2014

Fire Control Recommendations

A. Fire Area Extinguisher Type NotesPreferred Alternative Avoid

AircraftStructural Fire

Foam Halon 1211* Dry chemicalpowder/Carbon dioxide

may be used ascomplimentary agents in

conjunction with foamEngine Fire Halon 1211* Dry chemical

powder(corrosive)

Foam Avoid foam unless adjacentstructures are at risk

Carbon dioxide(can damage

engine)Fuel Fire 1. Dry chemical

powder forleaking fuel

2. Water fog orfoam on ground

spill areaWheel Fire Dry chemical

powder or waterfog (intermittent

application)

Halon 1211* Carbon Dioxide−wheel breakage

is possible

1. Wheels are equippedwith fusible plugs which will

blow between 342°F to360°F (172°C to 182°C)

Approach landing gear fromforward or aft. Stand

upwind of fire to avoid’Skydrol’ fumes

Electrical Fire Halon 1211* Dry chemicalpowder/Carbon

dioxide

Water

HydraulicService Bay

Fire

Halon 1211* Dry chemicalpowder/Carbon

dioxide

Water

Galley Fire Halon 1211* Dry chemicalpowder

Water

FlightCompartment/

Cabin Fire

Halon 1211* Dry chemicalpowder

Water Water can be used in flightcompartment/cabin if

electrical/flammable liquidsnot involved (eg.

upholstery)Cargo

CompartmentFire

Halon 1211* Dry chemicalpowder/Carbon

dioxide

Water


Model 400

Page 40

Nov 05/2014

* Use of Halon 1211 may be restricted by local authority.CRASH−FIRE−RESCUE MANUAL

Model 400

Page 41

Nov 05/2014

A

B

C

CREW OXYGENCYLINDER ASSEMBLY

COPILOT’SOXYGENSUPPLYOUTLET

PILOT’SOXYGENSUPPLYOUTLET

1

2

3

4

LEGEND

OXYGENSUPPLY PRESSURE

MADE IN USA

0500

10001500

2000

PSIUSE NOOIL

OXYGEN CYLINDERPRESSURE GAUGE

1. Oxygen cylinder.2. Low pressure oxygen supply line.3. High pressure capillary line.4. High pressure relief line.5. Oxygen cylinder pressure gauge.6. Clamps.7. Overboard discharge indicator.8. Low pressure relief valve.9. Pressure reducer assembly.

10. Fill check valve.11. Flight compartment oxygen pressure gauge.

A

C

VIEW ON ARROW

6

11

8

910

5

7

4

2

3

B

1

TO FLIGHTCOMPARTMENT

OXYGENPRESSURE GAUGE

DISCHARGEINDICATOR

TOOVERBOARD

brd5

1a01

, gv,

04/

11/9

8


CREW OXYGEN SYSTEM


Page 42

Nov 05/2014

INTAKE TOGROUND LEVEL7.60 FT. (2.32 m)

EXHAUST TOGROUND LEVEL10.96 FT. (3.34 m)

1. Approximately 3 ft. lower in wheels−up situation.

2. There are no externally accessible fire access panels.

NOTES

brd4

9a01

, gv,

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11/9

8


ENGINE FIRE ACCESS LOCATIONS


Page 43

Nov 05/2014

brb9

5a01

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rm, 0

2/10

/98

A

A

B

C

OUTBD

ENGINE FIREEXTINGUISHER BOTTLES

VIEW LOOKING INBOARDON LH SIDE


FIRE EXTINGUISHING SYSTEMS LOCATIONS (Sheet 1 of 2)


Page 44

Nov 05/2014

brb9

5a02

.dg,

rm, 0

2/10

/98

CARGO BAYFIRE EXTINGUISHER BOTTLES

APU FIRE EXTINGUISHERBOTTLE

B

C

INBD

INBD


FIRE EXTINGUISHING SYSTEMS LOCATIONS (Sheet 2 of 2)


Page 45

Nov 05/2014

A

AENGINE FIRE

1. POWER levers − FLT IDLE.2. Condition levers − FUEL OFF.3. PULL FUEL/HYD OFF handle (affected engine) − Pull. Check FUEL VALVE CLOSED and

HYD VALVE CLOSED advisory lights illuminate.4. TANK 1 AUX PUMP and TANK 2 AUX PUMP switches − OFF.5. EXTG switch (affected engine) − FWD BTL.

Wait up to 30 seconds, if fire persists:

6. EXTG switch − AFT BTL.7. BATTERY MASTER switch − OFF.8. DC CONTROL EXT PWR and AC CONTROL EXT PWR switches − OFF.9. PARK/EMERG BRAKE lever − PARK.

10. Evacuate airplane.

APU FIRE1. Check APU automatically shuts down (APU RUN advisory light out), APU BTL LOW and

FUEL VALVE CLOSED advisory lights illuminate.If APU BTL ARM or APU FIRE advisory lights remain illuminated after 7 seconds:

2. EXTG switch − EXTG.

brd4

8a01

.dg,

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cs, s

ep09

/201

4

BAGGAGE AFT COMPARTMENT FIRE1. Check for illumination of VENT INLT and VENT OTLT and FIRE BOTTLE AFT ARM advisory lights.2. Illuminated SMOKE/EXTG switch − Press. Check FIRE BOTTLE AFT LOW advisory light

illuminates and FIRE BOTTLE AFT ARM advisory light out.

The FIRE BOTTLE FWD LOW advisory light will illuminateapproximately seven minutes after the FIRE BOTTLE AFTLOW advisory light illuminates.

BAGGAGE FWD COMPARTMENT FIRE1. Check for illumination of FIRE BOTTLE FWD ARM advisory light.

advisory lights illuminate and FIRE BOTTLE FWD ARM advisory light out.

NOTE

2. Illuminated SMOKE/EXTG switch − Press. Check FIRE BOTTLE FWD LOW and AFT LOW

BAGGAGEAFT

VENT VENTINLT OTLT

CLOSEDTEST

1

2

FIRE BLTAFT

FWDAFTFWD

ARM LOW

BAGGAGEFWD

SMOKEEXTG

SMOKEEXTG

TEST

ARM LOW

FIRE EXTINGUISHING SYSTEMS OPERATIONS (STANDARD CONFIGURATION)


FIRE EXTINGUISHING SYSTEMS OPERATIONS (Sheet 1 of 2)


Page 46

Nov 05/2014

A

AENGINE FIRE

1. POWER levers − FLT IDLE.2. Condition levers − FUEL OFF.3. PULL FUEL/HYD OFF handle (affected engine) − Pull. Check FUEL VALVE CLOSED and

HYD VALVE CLOSED advisory lights illuminate.4. TANK 1 AUX PUMP and TANK 2 AUX PUMP switches − OFF.5. EXTG switch (affected engine) − FWD BTL.

Wait up to 30 seconds, if fire persists:

6. EXTG switch − AFT BTL.7. BATTERY MASTER switch − OFF.8. DC CONTROL EXT PWR and AC CONTROL EXT PWR switches − OFF.9. PARK/EMERG BRAKE lever − PARK.

10. Evacuate airplane.

APU FIRE1. Check APU automatically shuts down (APU RUN advisory light out), APU BTL LOW and

FUEL VALVE CLOSED advisory lights illuminate.If APU BTL ARM or APU FIRE advisory lights remain illuminated after 7 seconds:

2. EXTG switch − EXTG.

brd4

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09/2

014

BAGGAGE AFT COMPARTMENT FIRE1. Check for illumination of VENT INLT and VENT OTLT and FIRE BOTTLE AFT ARM advisory lights.2. Illuminated SMOKE/EXTG switch − Press. Check FIRE BOTTLE AFT LOW advisory light

illuminates and FIRE BOTTLE AFT ARM advisory light out.

BAGGAGEAFT

VENT VENTINLT OTLT

CLOSEDTEST

1

2

FIRE BLTAFT AFTARM LOW

SMOKEEXTG

ARM LOW

FIRE EXTINGUISHING SYSTEMS OPERATIONS (EXTRA CAPACITY CONFIGURATION)

The FIRE BOTTLE FWD LOW advisory light will illuminateapproximately seven minutes after the FIRE BOTTLE AFTLOW advisory light illuminates.

NOTE


FIRE EXTINGUISHING SYSTEMS OPERATIONS (Sheet 2 of 2)


Page 47

Nov 05/2014

A

A

DC CONTROL

OFF

STBYBATT

AUXBATT

MAINBATT

BATTERYMASTER

OFF

GEN 1 GEN 2 MAIN BUSTIE

BUS FAULTRESET

EXT PWR

OFF OFF OFF

OFF OFF OFF OFF

brd4

7a01

, gv,

05/

11/9

8

A. Set the MAIN BATT switch to the OFF position.B. Set the AUX BATT switch to the OFF position.C. Set the MAIN BUS TIE switch to the OFF position.D. If necessary, set the STBY BATT switch to the OFF position.E. Set the BATTERY MASTER switch to the OFF position.F. Make sure that the AC EXT PWR switch and the DC EXT PWR

switch are both set to the OFF position.


BATTERY POWER SWITCH LOCATIONS


Page 48

Nov 05/2014

Documents

˘ˇ ˘ˆ ˙ ˝ ˛ ˙ ˚˘ ˘˚ ˆ ˜ ! ˘ˇ ˘ˆ · 12. Aft baggage door location and demo of external opening sequence, fire bottle locations. 13. Aft passenger door location and