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CRASH−FIRE−RESCUE MANUAL
E
Technical Publications B Manual Change Request
TO: MCR FOCAL, TECHNICAL PUBLICATIONS Name of Airline: BOMBARDIER AEROSPACE 123 GARRATT BLVD. Bombardier Reference #: TORONTO, ONTARIO, CANADA, M3K 1Y5 MAIL STOP: N42−25 FAX: (416) 375−4538 Date: E−MAIL ADDRESS: [email protected] ALL fields marked with an asterisk * are required Contact Information *Name: *Corporation Name: *Dept Name/Code:
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CRASH−FIRE−RESCUE MANUAL
Initial Issue 1 2 3 CRASH−FIRE−RESCUE MANUAL
CRASH−FIRE−RESCUE MANUAL
CRASH−FIRE−RESCUE MANUAL
CRASH−FIRE−RESCUE MANUAL
CRASH−FIRE−RESCUE MANUAL LIST OF EFFECTIVE PAGES
Chapter Page Date Chapter Page Date 41 * Nov 05/2014 Effective Pages 1 * Nov 05/2014 42 * Nov 05/2014 43 * Nov 05/2014 Contents 1 * Nov 05/2014 44 * Nov 05/2014 45 * Nov 05/2014 Chapter 00 1 * Nov 05/2014 46 * Nov 05/2014 2 * Nov 05/2014 47 * Nov 05/2014 3 * Nov 05/2014 48 * Nov 05/2014 4 * Nov 05/2014 5 * Nov 05/2014 6 * Nov 05/2014 7 * Nov 05/2014 8 * Nov 05/2014 9 * Nov 05/2014 10 * Nov 05/2014 11 * Nov 05/2014 12 * Nov 05/2014 13 * Nov 05/2014 14 * Nov 05/2014 15 * Nov 05/2014 16 * Nov 05/2014 17 * Nov 05/2014 18 * Nov 05/2014 19 * Nov 05/2014 20 * Nov 05/2014 21 * Nov 05/2014 22 * Nov 05/2014 23 * Nov 05/2014 24 * Nov 05/2014 25 * Nov 05/2014 26 * Nov 05/2014 27 * Nov 05/2014 28 * Nov 05/2014 29 * Nov 05/2014 30 * Nov 05/2014 31 * Nov 05/2014 32 * Nov 05/2014 33 * Nov 05/2014 34 * Nov 05/2014 35 * Nov 05/2014 36 * Nov 05/2014 37 * Nov 05/2014 38 * Nov 05/2014 39 * Nov 05/2014 40 * Nov 05/2014
The asterisk (*) indicates pages revised, added or deleted by current revision.
Model 400
EFFECTIVE Page 1 PAGES Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK CRASH−FIRE−RESCUE MANUAL TABLE OF CONTENTS Title Page CHAPTER 00 Chapter title Aircraft Dimensions 1 Familiarization and Location Guide 3 Exterior Walk−Around 4 Typical Interior Configurations 5 Passenger − Compartment Cross Section 9 Typical Flight Compartment Arrangement (Looking 10 Forward) Typical Flight Compartment Arrangement (Looking Aft) 11 Aircraft Doors and Ground Service Panels 12 Evacuation Routes 13 Passenger and Crew Escape Systems 15 Forward Passenger Door−Ditching Dam Operation 20 Forward Baggage Door Operation/Forward Type I 22 Emergency Exit Door Forward RH Type I Emergency Exit Door−Ditching Dam 24 Operation Aft Baggage Door Operation 26 Flight Compartment Escape Hatch 28 Fortified Flight Compartment Door Operation 30 Propeller/Engine Exhaust Danger Areas 32 Cut−Through Areas 34 Flammable Material Locations (Excluding Passenger 35 Cabin) Flammable/Hazardous Material Locations in Passenger 36 Cabin Fire Control Recommendations 40 Crew Oxygen System 42 Engine Fire Access Locations 43 Fire Extinguishing Systems Locations 44 Fire Extinguishing Systems Operation 46 Battery Power Switch Locations 48
Model 400
Page 1 CONTENTS Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK CHAPTER 00
CHAPTER TITLE CRASH−FIRE−RESCUE MANUAL
THIS PAGE INTENTIONALLY LEFT BLANK CRASH−FIRE−RESCUE MANUAL 93ft 3in. (28.42m) 30ft 5in. (9.27m) 13ft 6in. (4.11m)
25ft 8in.* (7.81m) 12ft 10in.* (3.92m) 38.67in.* o (98.22cm) DIHEDRAL 2.5
43.31in. (1.10m) 28ft 10in. (8.80m)
36.00in. (91.44cm)
36ft 10in. NOTE (11.22m) * Dimensions with respect to ground reference line are approximate and will vary with aircraft configuration and loading conditions. 8ft 2in. (2.48m) 12ft 4in. (3.76m)
45ft 9in. (13.94m) 10ft 9in.* (3.28m) 27ft 4in.* (8.34m)
45.94in.* 48.98in.* GROUND 60.85in.**60.83in. (1.17m) (1.24m) REFERENCE LINE (1.55m) (1.55m) 101ft 10in. (31.04m) 107ft 9in. g3565a01.dg, cs, aug20/2014
(32.83m) c AIRCRAFT DIMENSIONS (INCL EXTRA CAPACITY CONFIGURATION) (Sheet 1 of 2)
Figure 00 − 1 Model 400
Page 1 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
FORWARD BAGGAGE DOOR/ FLIGHT COMPARTMENT FORWARD TYPE I ESCAPE HATCH EMERGENCY EXIT DOOR 2 18.50 in. (46.99 cm) L 24.00 in. (60.96 cm) W 20.60 in. (52.32 cm) W 54.00 in. (137.16 cm) H
FORWARD PASSENGER DOOR UPPER (TYPE II) AND 30.00 in. (76.20 cm) W LOWER (TYPE III) FORWARD 65.00 in. (165.10 cm) H EMERGENCY EXIT DOORS 20.20 in. (51.31 cm) W 56.00 in. (142.24 cm) H
AFT PASSENGER DOOR 24.00 in. (60.96 cm) W 65.00 in. (165.10 cm) H TYPE I EXIT AND SERVICE DOOR 24.00 in. (60.96 cm) W BAGGAGE DOOR 54.00 in. (137.16 cm) H 51.00 in. (129.54 cm) W 59.00 in. (149.86 cm) H
NOTES Type II/III emergency exit door is de−activated for the extra capacity configuration.
2 Forward type I emergency exit door is installed only on aircraft with extra capacity configuration. cg3565a02.dg, cs, aug20/2014 AIRCRAFT DIMENSIONS (INCL EXTRA CAPACITY CONFIGURATION) (Sheet 2 of 2)
Figure 00 − 1 Model 400
Page 2 Mar 18/2005 CRASH−FIRE−RESCUE MANUAL
Model 400
Page 3 Nov 05/2014 3 Model 400 4 2 5 14. No.1nacelle−mainlandinggearlocationanddescription, hydraulicreservoir 13. Aftpassengerdoorlocationanddemosofexternal openingsequence,optionalfolding 12. Aftbaggagedoorlocationanddemoofexternalopening sequence, 11. Auxiliarypowerunit(APU)bayaccessdoor−APU locationanddescription. 10. Aftequipmentbayaccessdoor−openingsequence, flightdatarecorderand 6 1. Airstairdoorlocationanddemoofexternalopeningsequence. EXTERIOR WALKAROUNDSEQUENCE(FORCREWTRAININGPURPOSES) 7. No.2nacelle−mainlandinggearlocationanddescription,hydraulicreservoir 8. Fueltankslocationanddescription. 6. TypeII/IIIemergencyexitdoorlocationanddemoofexternalopeningsequence. 2. Nosefuselageaccessdoor−batteriesandcontactorboxlocations. 9. Servicedoorlocationanddemoofexternalopening sequence. 5. Forwardbaggagedoorlocationanddemoofexternalopeningsequence, 4. Noselandinggearlocationanddescription,auxiliaryhydraulicreservoir 3. Crewoxygenbottle. 1 external openingsequence. cockpit voicerecorderlocations. and hydrauliclineslocationdescription,firebottle locations. and hydrauliclineslocationdescription. and hydrauliclineslocation anddescription,firebottlelocations. stairs (ifequipped). fire bottlelocation/forwardtypeIemergencyexitanddemoof fire bottlelocations. 8 7 CRASH−FIRE−RESCUE MANUAL EXTERIOR WALK−AROUND 14 9 8 Figure 00−2 13 12 10 Forward typeIemergencyexitdoorisinstalled NOTES only onaircraftwithextracapacityconfiguration de−activated fortheextracapacityconfiguration Type II/IIIforwardemergencyexitdooris 11 Nov 05/2014 ae4 Page . . brb94a01.dg, gv/cs, jul31/2014 Model 400
BAGGAGE DOOR TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H
YIA EIS40ITRO OFGRTOS(Sheet1of4) TYPICAL SERIES400INTERIOR CONFIGURATIONS (60.96 cm x 1.37 m) (51.31 cm x 1.42 m) SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H 5 ft. 9 in. (60.96 cm x 1.37 m) (1.75 m) 11.00 ft. (3.35 m) 3 1 6 CRASH−FIRE−RESCUE MANUAL Figure 00−3
4 5 5 2
AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H (1.30 m x 1.50 m) PASSENGER CABIN LENGTH STA X−39.00 61 ft 8 in. (18.80 m) STA X701.00
LEGEND 1. Forward baggage compartment 91.00 ft 3 (2.58 m 3 ). 2. Rear baggage compartment NOTE 33
Nov 05/2014 365.00 ft (10.33 m ). Layout may vary with optional 3. Lavatory.
ae5 Page configurations. 4. Wardrobe. 5. Flight attendant. 6. Galley. brt70a01.dg, pt/kmw, aug08/2008 Model 400
BAGGAGE DOOR 24.00 in. W x 54.00 in. H TYPE II/III EXIT SERVICE DOOR/TYPE I EXIT YIA EIS40ITRO OFGRTOS(Sheet2of4) TYPICAL SERIES400INTERIOR CONFIGURATIONS (60.96 cm x 1.37 m) 20.20 in. W x 56.00 in. H 24.00 in. W x 54.00 in. H 37.80 in. (51.31 cm x 1.42 m) (60.96 cm x 1.37 m) 96.01 cm 6 6 3 6 11.00 ft (3.35 m) CRASH−FIRE−RESCUE MANUAL
Figure 00−3 1 5 2 4 5 7 AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H (1.30 m x 1.50 m) PASSENGER CABIN LENGTH STA X−39.00 61 ft 8 in. (18.80 m) STA X701.00
LEGEND 1. Forward Baggage Compartment 51.00 ft 3 (1.44 m3 ). 2. Rear Baggage Compartment 365.00 ft 3 (10.33 m3 ). NOTE 3. Lavatory. Nov 05/2014 Layout may vary with optional 4. Wardrobe.
ae6 Page configurations. 5. Flight Attendant Seat. 6. Galley. 7. Cart Storage. brt70a02.dg, pt/kmw, aug08/2008 Model 400
BAGGAGE DOOR TYPE II/III EXIT 24.00 in. W x 54.00 in. H 20.20 in. W x 56.00 in. H (60.96 cm x 1.37 m) (51.31 cm x 1.42 m) SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H YIA EIS40ITRO OFGRTOS(Sheet3of4) TYPICAL SERIES400INTERIOR CONFIGURATIONS 5 ft. 9 in. (60.96 cm x 1.37 m) (1.75 m) 11.00 ft. (3.35 m) 3 1 6 7 5 CRASH−FIRE−RESCUE MANUAL Figure 00−3
7 4 5 8 2
AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT BAGGAGE DOOR 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H 51.00 in W x (76.20 cm x 1.65 m) (60.96 cm x 1.65 m) 59.00 in. H (1.30 m x 1.50 m) PASSENGER CABIN LENGTH STA X−39.00 61 ft 8 in. (18.80 m) STA X701.00
LEGEND 1. Forward baggage compartment 91.00 ft 3 (2.58 m 3 ). 2. Rear baggage compartment 354.00 ft 33 (10.0 m ) approx. 3. Lavatory. NOTE
Nov 05/2014 4. Wardrobe. Layout may vary with optional 5. Flight attendant.
ae7 Page configurations. 6. Beverage cart stowage. 7. Galley.
brt70a03.dg, pt/kmw, aug12/2008 8. Folding stairs (optional). Model 400
FORWARD TYPE I EMERGENCY EXIT DOOR SERVICE DOOR/TYPE I EXIT 24.00 in. W x 54.00 in. H
YIA EIS40ITRO OFGRTOS(Sheet4of4) TYPICAL SERIES400INTERIOR CONFIGURATIONS TYPE II/III EMERGENCY 24.00 in. W x 54.00 in. H (60.96 cm x 1.37 m) EXIT DE−ACTIVATED (60.96 cm x 1.37 m) 11.00 ft (3.35 m) 2 5 CRASH−FIRE−RESCUE MANUAL
3 4 4 1 Figure 00−3 PASSENGER CABIN LENGTH 61 ft 8 in. (18.80 m)
AIRSTAIR/TYPE I EXIT PAX DOOR/TYPE I EXIT 30.00 in. W x 65.00 in. H 24.00 in. W x 65.00 in. H STA STA (76.20 cm x 1.65 m) X−39.00 (60.96 cm x 1.65 m) X701.00
BAGGAGE DOOR 51.00 in. W x 59.00 in. H (1.30 m x 1.50 m)
LEGEND 1. Rear baggage compartment 365.00 ft 3(10.33 m3 ). 2. Lavatory. 3. Wardrobe. Nov 05/2014 NOTE 4. Flight attendant Seat. 5. Galley. ae8 Page Layout may vary with optional configurations.
brt70a04.dg, cs, jul31/2014 (1.95 m) Model 400 77.0 in. GROUND REFERENCELINE 1 GROUND REFERENCELINE (1.44 m) 56.5 in. aircraftconfigurationandloadingconditions. NOTE This dimensionisapproximateandwillvarywith (0.62 m) 24.3 in. (0.32 m) 12.4 in. PASSENGER COMPARTMENT CROSSSECTION (0.40 m) 15.8 in. (0.51 m) 20.0 in CRASH−FIRE−RESCUE MANUAL 106.0 in. (2.51 m) (2.69 m) (0.66 m) (2.03 m) 99.0 in. 25.9 in. 80.0 in. Figure 00−4 (2.76 m) 108.8 in. 101.1 in. (2.56 m) (CAPACITY IS1.67Ft(0.047m)/PAX OVERHEAD STOWAGEBINS (1.82 m) 71.8 in. AT DOORCENTERLINE 6.21 in.(15.8cm) AT AFTEDGEOFDOOR 5.74 in.(14.6cm) AT FWDEDGEOFDOOR 11.37 in(28.9cm) 2 Nov 05/2014 3 1 ae9 Page 1 .) br721a01.dg, gv, 12/04/02 CRASH−FIRE−RESCUE MANUAL
6 8 9 10 16 11 6 1 16 5 1
4 7 5 15 17
12 4 15 3 3
2 2
20 19 13 14 18
LEGEND 1. Overhead speakers. 11. Overhead panel. 2. Stowage pockets. 12. Nosewheel steering hand control. 3. Map tables. 13. Center console (aft). 4. Gaspers. 14. Center console (fwd). 5. Sun visors. 15. Side console (pilot & copilot). 6. Hand holds. 16. Utility lights. 7. Compass calibration card. 17. Glareshield panel. 8. Eye level indicator. 18. Copilot’s instrument panel. 9. Standby compass. 19. Engine instrument panel. 10. Caution/Warning lights panel. 20. Pilot’s instrument panel. r251a01.dg, pt, 05/05/00 b TYPICAL FLIGHT COMPARTMENT ARRANGEMENT (LOOKING FORWARD)
Figure 00 − 5 Model 400
Page 10 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL 3 6 7 8 5 5 4 3 3 2 2
9 9
17 15
1 16
18 13 14 11 10
LEGEND 1. Right DC circuit breaker panel. 10. Observer’s seat backrest. 2. Circuit breaker panel lights. 11. Weight and balance papers. 3. Oxygen masks ( Pilot’s and Copilot’s). 12. C of A and C of R holders. 4. Observers headset stowage. 13. Observer’s smoke goggles. 5. Dome lights. 14. Landing gear emergency extension 6. Mirror. handpump handle. 7. Viewer. 15. Avionics circuit breaker panel. 8. Avionics bay air vent. 16. Left DC circuit breaker panel. 9. Headset jacks. 17. Variable frequency AC circuit breaker panel. 18. Crew PBE. r252a01.dg, pt, 12/11/98 b TYPICAL FLIGHT COMPARTMENT ARRANGEMENT (LOOKING AFT)
Figure 00 − 6 Model 400
Page 11 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
SERVICE DOOR APU CLAMSHELL ACCESS DOOR
AFT EQUIPMENT BAY TYPE II/III ACCESS DOOR EMERGENCY EXIT DOOR AFT BAGGAGE DOOR
AFT PASSENGER DOOR
FORWARD PASSENGER DOOR FLIGHT COMPARTMENT ESCAPE HATCH
FORWARD BAGGAGE DOOR/ FORWARD TYPE I 2 EMERGENCY EXIT DOOR
NOTES Type II/III emergency exit door is de−activated for the extra capacity configuration.
2 Forward type I emergency exit door is installed only on aircraft with extra capacity configuration. cg3566a01.dg, cs, aug20/2014 AIRCRAFT DOORS AND GROUND SERVICE PANELS (INCL EXTRA CAPACITY CONFIGURATION) Figure 00 − 7 Model 400
Page 12 Nov 05/2014 Model 400 FLIGHT COMPARTMENT AFT PASSENGERDOOR EMERGENCY EXIT/ FORWARD PASSENGER ESCAPE HATCH AIRSTAIR DOOR TYPE I VCAINRUE (Sheet1of2) EVACUATION ROUTES STANDARD CONFIGURATION CRASH−FIRE−RESCUE MANUAL Figure 00−8 EMERGENCY EXIT/ WITH DITCHINGDAM EMERGENCY EXIT SERVICE DOOR TYPE II/III TYPE I Nov 05/2014 ae13 Page
brb92a01.dg, gv/kmw, sep16/2014 CRASH−FIRE−RESCUE MANUAL FLIGHT COMPARTMENT ESCAPE HATCH FORWARD TYPE I EMERGENCY EXIT DOOR WITH DITCHING DAM
FORWARD PASSENGER TYPE II/III AIRSTAIR DOOR EMERGENCY EXIT
TYPE I EMERGENCY EXIT/ AFT PASSENGER DOOR TYPE I EMERGENCY EXIT/ SERVICE DOOR
NOTE EXTRA CAPACITY CONFIGURATION Type II/III emergency exit door is de−activated
for the extra capacity configuration brb92a02.dg, cs/kmw, sep15/2014 EVACUATION ROUTES (Sheet 2 of 2)
Figure 00 − 8 Model 400
Page 14 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
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 in the 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 forward left side of the fuselage. The forward passenger door is operated by internal or external handles. c. The forward Type I emergency exit door which is a translating type door. This is installed on the forward right side of the fuselage for the extra capacity configuration. It consists of an upper and a lower door. The lower door can be kept closed by a internal locking handle in the event of a ditching procedure. This emergency exit can be operated by internal or external handles. NOTE: The forward Type I emergency door is installed in lieu of forward baggage door 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 the event of a ditching procedure. This emergency exit can be operated by internal or external handles. NOTE: The type II/III emergency exit is de−activated for the extra capacity configuration. e. The aft passenger door which is a translating type door is installed on the aft left side 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 right side 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 the ladder or platform is placed more than this distance.
Model 400
Page 15 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL 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 door 3. 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 their enclosure (located in the aft baggage bulkhead, just inboard of the aft passenger door threshold) and are unfolded and extended by hand. The folding stairs are intended 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 door on 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 ditching procedure.
NOTE: The door will come out 16 inch (40 cm) before it swings to the right. Make sure the ladder or platform is placed more than this distance. 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 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. NOTE: This will lock the door in the open position. E. Type II/III Emergency Exit Door Operation
NOTE: The Type II/III emergency exit door is de−activated on aircraft with the extra capacity configuration.
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 CRASH−FIRE−RESCUE MANUAL 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
NOTE: The door will come out 16 inch (40 cm) before it swings to the right. Make sure the ladder or platform is placed more than this distance. 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 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. NOTE: This will lock the door in the open position.
Model 400
Page 17 Nov 05/2014 Model 400 WHILE LOWERING SUPPORT DOOR OUT ANDDOWN PULL HANDLE KEEP CLEAR WARNING OF DOOR TO OPEN EXTERIOR OFFORWARDPASSENGERDOOR PUSH ASNE N RWECP YTM (Sheet1of2) PASSENGER ANDCREW ESCAPESYSTEMS A CRASH−FIRE−RESCUE MANUAL Figure 00−9 PULL HANDLE AND TURN TO OPEN LOWERING ASSIST VENT DOOR EXTERIOR OFAFTPASSENGER DOOR DOOR B HANDLE INOPEN PULL HANDLE AND TURN (TYPICAL) POSITION TO OPEN Nov 05/2014 ae18 Page
brb90a01.dg, gv/kmw, sep11/2014 CRASH−FIRE−RESCUE MANUAL CREW EMERGENCY FLIGHT DESCENT ROPE COMPARTMENT (TYPICAL BOTH SIDES) ESCAPE HATCH
PUSH TO LOCK PUSH TO RELEASE PULL HANDLE AND TURN TO OPEN TURN HANDLE DOWN AND PUSH HATCH IN
PULL HANDLE AND TURN HANDLE IN TO OPEN OPEN POSITION
EXTERIOR OF TYPE II / III EMERGENCY EXIT DOOR VENT DOOR PUSH TO LOCK EXTERIOR OF AFT EXTERNAL OPERATING SERVICE DOOR HANDLE (CLOSED POSITION)
PULL HANDLE AND TURN PULL HANDLE TO OPEN AND TURN TO OPEN NOTES 1 Forward type I emergency exit door is installed only on aircraft with extra capacity configuration.
Type II/III emergency exit door is de−activated VENT DOOR for the extra capacity configuration. 1 EXTERIOR OF FORWARD BAGGAGE DOOR/ 3. The forward baggage door has a separate interior lockable door which can prevent exterior access.
FORWARD TYPE I EMERGENCY EXIT DOOR brb90a02.dg, gv/kmw, oct01/2014 PASSENGER AND CREW ESCAPE SYSTEMS (Sheet 2 of 2)
Figure 00 − 9 Model 400
Page 19 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
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 CRASH−FIRE−RESCUE MANUAL
NOTE Pull down to deploy ditching dam. 2 A
EXIT
LEGEND 1. Flight attendant seat. 1 2. Handle.
2 brl10a01.dg, sw, 23/07/99 FORWARD PASSENGER DOOR − DITCHING DAM OPERATION
Figure 00 − 10 Model 400
Page 21 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
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 exit door 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 optional galley stowage equipment and/or baggage and there is no handle on the baggage− compartment side of the door.
NOTE: The door will come out 16 inch (40 cm) before it swings to the right. Make sure the ladder or platform is placed more than this distance. 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 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. NOTE: This will lock the door in the open position.
Model 400
Page 22 Nov 05/2014 PULL HANDLE Model 400 FORWARD BAGGAGEDOOR/TYPEI OWR AGG DOOR/FORWARDTYPEIEMERGENCYEXIT FORWARD BAGGAGE AND TURN EMERGENCY EXITDOOR (OPENPOSITION) TO OPEN EXTERIOR OFFORWARDBAGGAGEDOOR/ FORWARD TYPEIEMERGENCYEXITDOOR VENT DOOR VIEW LOOKINGDOWNONR/HSIDE CENTERLINE AIRCRAFT A PUSH TOLOCK 1 EXTERNAL OPERATING CRASH−FIRE−RESCUE MANUAL (CLOSED POSITION) PULL HANDLE AND TURN TO OPEN HANDLE Figure 00−11 1 2. Theforwardbaggagedoorhasaseparateinterior Forward typeIemergencyexitdoorisinstalled lockable doorwhichcanpreventexterioraccess. NOTES only onaircraftwithextracapacityconfiguration. VIEW LOOKINGINBOARDONR/HSIDE EXTERNAL OPERATING (OPEN POSITION) HANDLE DOOR OPERATION A Nov 05/2014 ae23 Page
br840a01.dg, sw/kmw, oct01/2014 CRASH−FIRE−RESCUE MANUAL
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 surround structure 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 CRASH−FIRE−RESCUE MANUAL
2
LEGEND 1. Ditching dam. 2. Type I emergency exit door. 1 3. Ditching dam handle. 4. Label, ditching dam operation.
3
VIEW LOOKING OUTBOARD
4 rbs45a01.dg, kmw, sep16/2014 b FORWARD TYPE I EMERGENCY EXIT DOOR − DITCHING DAM OPERATION
Figure 00 − 12 Model 400
Page 25 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
Aft Baggage Door Operation
A. Aft Baggage Door Operation 1. Push the pushbutton on the door operating handle to release the handle from the recess. 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 close easily. 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 Model 400 HANDLE INOPEN TELESCOPIC STAYASSY DOOR BALANCEDWITH POSITION A F AGG OPRMN OR−LOCATION ANDOPERATION AFT BAGGAGECOMPARTMENT DOOR PULL HANDLE AND TURN TO OPEN EXTERIOR OFAFTBAGGAGECOMPARTMENTDOOR SIDE VIEWOFDOORINOPEN POSITION CRASH−FIRE−RESCUE MANUAL (CLOSED POSITION) Figure 00−13 POSITION HANDLE A FLOOR LEVEL Z−100.032 Nov 05/2014 ae27 Page
br642a01.dg, sw/gw, jan25/2011 CRASH−FIRE−RESCUE MANUAL
Flight Compartment Escape Hatch
NOTE: In an emergency, you can try to get access by cutting through the outer skin to move the operating handle from the outside. Then push the hatch down.
WARNING:HOLD THE ESCAPE HATCH DURING THE PROCEDURE. IF YOU DO NOT DO THIS, THE ESCAPE HATCH CAN FALL AND CAUSE INJURIES TO PERSONS 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 1 in. 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 CRASH−FIRE−RESCUE MANUAL A
REAR SUPPORT BRACKET
FLIGHT COMPARTMENT EMERGENCY EXIT HATCH REAR SUPPORT FITTINGS
VENT
PULL HANDLE DOWN TO REMOVE HATCH
CLOSED
OPERATING HANDLE
ARM/SPRING 1 ROTATE HANDLE TO DETENT VENT POSITION MECHANISM 2 PULL DOWN ARM ON HANDLE TORQUE SHAFT 3 ASSEMBLY REMOVE HATCH A
VENT CLOSED VENT CLOSED
PULL HANDLE DOWN PULL HANDLE DOWN TO REMOVE HATCH TO REMOVE HATCH
OPERATING HANDLE OPERATING HANDLE r201a01.dg, pt, 21/08/97 b FLIGHT COMPARTMENT ESCAPE HATCH
Figure 00 − 14 Model 400
Page 29 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
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 latch and deadbolt location until the door frame distorts sufficiently to allow the flight compartment 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 the wardrobe maintenance panel. A white light will illuminate on the switch. The flight compartment door will automatically open after a timed delay of 40 seconds if there is no response by the flight crew. An amber light will illuminate on the Flight Attendant Access Switchlight indicating that the flight compartment door is unlatched. OR The Remote Access System can be disabled by removing electrical power from the aircraft (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 is engaged. NOTE: The key access feature for the deadbolt lock will be disabled if both arms of the rotary knob on the flight compartment side are set to the latched position .
Model 400
Page 30 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
1 1
−3 L628 P D C
3 28−
CDPL6
LEGEND 1. Fortified door. 2. Slide latch (operable from flight compartment only). 3. Deadbolt lock.
2 2 HUNTINGTON BEACH,CA
SERIAL NO.
GROSS WT. LBS
GROSS WT. KGS PART NO.
MFG.DATE
PRY HERE FOR GROUNDDEADBOLT USE UNLY POSITIONS 3 UNLOCKED
LOCKED
KEY OPERABLE
LOCKED
CDPL600 WITH KEY INOPERABLE CROWBAR
3
CDPL595
PINS MUST BE FULLY ENGAGED AT ALL TIMES ray38a01.dg, gw, 01/03/05 b FORTIFIED FLIGHT COMPARTMENT DOOR DETAIL
Figure 00 − 15 Model 400
Page 31 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL 108 ft. 35 m LEGEND 100 Personnel danger areas 30 when engines are operating (areas shown are approximate).
20
50
HOT ENGINE 10 EXHAUST GASES VENTED REAR WARDS
0 0
APU EXHAUST (NOT ON ALL AIRCRAFT)
0 50 93 ft.
10 20 0 28.4 m rg35a01.dg, pt, 09/02/00 b PROPELLER / ENGINE EXHAUST DANGER AREAS (Sheet 1 of 2)
Figure 00 − 16 Model 400
Page 32 Nov 05/2014 Model 400 −200 −100 SLIPSTREAM VELOCITYCONTOURS(~18%TORQUE)(STATIONARYONGROUND) SLIPSTREAM VELOCITYCONTOURS(~43%TORQUE)(STATIONARYONGROUND) R(ft) 0 R(ft) 100 −100 100 0 RPLE NIEEHUTDNE RA (Sheet 2of2) PROPELLER /ENGINE EXHAUSTDANGERAREAS 90 ft/sec 80 ft/sec 100 70 ft/sec 100 60 ft/sec 0f/e 40ft/sec 50 ft/sec CRASH−FIRE−RESCUE MANUAL 200 Figure 00−16 50 ft/sec 40 ft/sec X(ft) X(ft) 200 30 ft/sec 300 30 ft/sec 25 ft/sec 400 300 20 ft/sec 20 ft/sec 500 Nov 05/2014 ae33 Page
brg35a02.dg, sb, may17/2011 I NTERIOR CONSTRUCTION−STRINGERS Model 400 RUN ABOVEANDBELOWWINDOWS −SKIN THICKNESS.006in.(1.50mm) WINDSHIELD (NON−OPENING) SIDE WINDOW CRASH−FIRE−RESCUE MANUAL CUT−THROUGH AREAS Figure 00−17 2. Cut−throughareasshowninredonRescueChart mayappearasothercoloursontheaircraft. "Cut−through" areasrequireportablemetalcutting equipment. Itisrecommendedthatmajoreffort due tothetypeofstructureandpossibleinjury NOTES to personnelwithin. to gainaccessbedirecteddoorsandhatches circumstances). areas. (Althoughanywindowissuitableinextreme are therecommendedfirstchoicecut−through The thirdwindowfwdoftheaftpassengerdoors 45.0 x20.0in.(1143508mm) AREA DIMENSIONS RECOMMENDED CUT−THROUGH COMPARTMENT PASSENGER WINDOWS Nov 05/2014 ae34 Page
brd22a01, gv/pt, 13/03/01 Model 400 NOTES ITEM 7 3 4 9 6 5 1 2 8 No. FLAMMABLE MATERIAL LOCATIONS(EXCLUDINGPASSENGERCABIN) 2 Fuel Tank Crew Oxygen anBteyadAuxiliaryBattery Main Batteryand o yrui Reservoir No. 1Hydraulic o yrui Reservoir No. 2Hydraulic Crew PBE oki oc RecorderandFlight Cockpit Voice No. 3Hydraulic Data Recorder Standby Battery 39.8 CuFtA.T. US Gal. Based onspecificgravityof0.816 1785 (single tank−divideby2) TOTAL FUELCAPACITY ITEM NAME 3 Imp. Gal. 1486 Cylinder Reservoir 4 6756 L 1 12138 CRASH−FIRE−RESCUE MANUAL LB 6 5506 Aft fuselage Aft fuselage Right nacelle Aft fuselage Integral Left nacelle Flight compartment, Nose lower oelwrcompartment−leftside Nose lower Kg Figure 00−18 compartment−right side ITEM LOCATION behind co−pilot’sseat Reservoir No. 3System No. 2System No. 1System Aux. System(Nose) HYDRAULIC FLUIDCAPACITY 5 4 9 ACCESS US Qt. 8 1.06 12.5 2.6 8.3 NOTE Standby batteryinnos with APUinstalled. 7 112AR 113AL 423CR 413CR 311AB 311AB 311AB PANEL/ Imp. Qt. 1.27 10.4 6.9 2.2 DOOR Nov 05/2014 1.20 11.8 7.9 2.5 L ae35 Page e brd50a01.dg, jp/pt, 05/06/00 Model 400 LMAL/AADU AEILLCTOSI ASNE AI (Sheet1of4) FLAMMABLE/HAZARDOUS MATERIALLOCATIONSINPASSENGER CABIN −1 ontopofdoghouse −1 onfwd.sideofdoghouse −2 indoghouse o 2 x 4 STANDARD CONFIGURATION CRASH−FIRE−RESCUE MANUAL Figure 00−19 −In doghouse x2 x 2 PBE PBE o 2 LEGEND PBE o 2 Fireextinguisher. Oxygenbottle. Breathing Equipment. Crew Protective Nov 05/2014 ae36 Page
bru16a01.dg, sw/cs, aug25/2014 Model 400 LMAL/AADU AEILLCTOSI ASNE AI (Sheet2of4) FLAMMABLE/HAZARDOUS MATERIALLOCATIONSINPASSENGER CABIN PBE o 2 STANDARD CONFIGURATION X 3 CRASH−FIRE−RESCUE MANUAL Figure 00−19 −In drawerbehindseats,opensaft −On aftbaggagebulkhead PBE o 2 PBE LEGEND PBE o 2 Fireextinguisher. Oxygenbottle. Breathing Equipment. Crew Protective Nov 05/2014 ae37 Page
bru16a02.dg, sw/cs, aug25/2014 Model 400 −1 onfwd.sideofenclosure −2 indrawerbehindseats, LMAL/AADU AEILLCTOSI ASNE AI (Sheet3of4) FLAMMABLE/HAZARDOUS MATERIALLOCATIONSINPASSENGER CABIN opens aft o 2 x 3 STANDARD CONFIGURATION CRASH−FIRE−RESCUE MANUAL Figure 00−19 −1 onfwd.sideofdoghouse −1 ontopofdoghouse −In doghouse x 2 PBE x 2 o 2 PBE x 2 o 2 LEGEND PBE o 2 FireExtinguisher. Oxygenbottle. Breathing Equipment. Crew Protective Nov 05/2014 ae38 Page
bru16a03.dg, sw/cs, aug25/2014 Model 400 LEGEND LMAL/AADU AEILLCTOSI ASNE AI (Sheet4of4) FLAMMABLE/HAZARDOUS MATERIALLOCATIONSINPASSENGER CABIN o 2 Fire extinguisher. Oxygen bottle. o 2 EXTRA CAPACITYCONFIGURATION x 3 CRASH−FIRE−RESCUE MANUAL Figure 00−19 o 2 x 2 x 2 o 2 Nov 05/2014 ae39 Page
bru16a04.dg, cs, aug25/2014 CRASH−FIRE−RESCUE MANUAL
Fire Control Recommendations
A. Fire Area Extinguisher Type Notes Preferred Alternative Avoid Aircraft Foam Halon 1211* Dry chemical Structural Fire powder/Carbon dioxide may be used as complimentary agents in conjunction with foam Engine Fire Halon 1211* Dry chemical Foam Avoid foam unless adjacent powder structures are at risk (corrosive) Carbon dioxide (can damage engine) Fuel Fire 1. Dry chemical powder for leaking fuel 2. Water fog or foam on ground spill area Wheel Fire Dry chemical Halon 1211* Carbon Dioxide− 1. Wheels are equipped powder or water wheel breakage with fusible plugs which will fog (intermittent is possible blow between 342°F to application) 360°F (172°C to 182°C) Approach landing gear from forward or aft. Stand upwind of fire to avoid ’Skydrol’ fumes Electrical Fire Halon 1211* Dry chemical Water powder/Carbon dioxide Hydraulic Halon 1211* Dry chemical Water Service Bay powder/Carbon Fire dioxide Galley Fire Halon 1211* Dry chemical Water powder Flight Halon 1211* Dry chemical Water Water can be used in flight Compartment/ powder compartment/cabin if Cabin Fire electrical/flammable liquids not involved (eg. upholstery) Cargo Halon 1211* Dry chemical Water Compartment powder/Carbon Fire dioxide
Model 400
Page 40 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL * Use of Halon 1211 may be restricted by local authority.
Model 400
Page 41 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL LEGEND COPILOT’S OXYGEN 1. Oxygen cylinder. SUPPLY 2. Low pressure oxygen 11 OUTLET 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. 7 11. Flight compartment oxygen pressure gauge. A TO OVERBOARD DISCHARGE INDICATOR PILOT’S OXYGEN 4 SUPPLY 6 OUTLET B
2 C 3 TO FLIGHT 1 COMPARTMENT OXYGEN PRESSURE GAUGE 1000 4 500 1500 8 A 0 2000 1 CREW OXYGEN USE NO PSI CYLINDER ASSEMBLY OIL OXYGEN 2 SUPPLY PRESSURE MADE IN USA
5 C 9 3 10 OXYGEN CYLINDER PRESSURE GAUGE VIEW ON ARROW B brd51a01, gv, 04/11/98 CREW OXYGEN SYSTEM
Figure 00 − 20 Model 400
Page 42 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL
INTAKE TO EXHAUST TO GROUND LEVEL GROUND LEVEL 7.60 FT. (2.32 m) 10.96 FT. (3.34 m)
NOTES 1. Approximately 3 ft. lower in wheels−up situation. 2. There are no externally accessible fire access panels. brd49a01, gv, 05/11/98 ENGINE FIRE ACCESS LOCATIONS
Figure 00 − 21 Model 400
Page 43 Nov 05/2014 Model 400 C EXTINGUISHER BOTTLES ENGINE FIRE IEETNUSIGSSESLCTOS(Sheet1of2) FIRE EXTINGUISHING SYSTEMS LOCATIONS B CRASH−FIRE−RESCUE MANUAL A Figure 00−22 VIEW LOOKINGINBOARD ON LHSIDE A
OUTBD Nov 05/2014 ae44 Page
brb95a01.dg, rm, 02/10/98
Model 400 INBD FIRE EXTINGUISHERBOTTLES IEETNUSIGSSESLCTOS(Sheet2of2) FIRE EXTINGUISHING SYSTEMS LOCATIONS CARGO BAY B CRASH−FIRE−RESCUE MANUAL Figure 00−22 APU FIREEXTINGUISHER BOTTLE
C INBD Nov 05/2014 ae45 Page
brb95a02.dg, rm, 02/10/98 CRASH−FIRE−RESCUE MANUAL A
BAGGAGE AFT SMOKE VENT VENT EXTG INLT OTLT
CLOSED 1 TEST 2 FIRE BLT AFT ARM LOW AFT FWD ARM LOW FWD
BAGGAGE FWD SMOKE TEST EXTG
ENGINE FIRE A 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 FIRE 1. 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.
BAGGAGE AFT COMPARTMENT FIRE 1. 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.
NOTE The FIRE BOTTLE FWD LOW advisory light will illuminate approximately seven minutes after the FIRE BOTTLE AFT LOW advisory light illuminates.
BAGGAGE FWD COMPARTMENT FIRE 1. Check for illumination of FIRE BOTTLE FWD ARM advisory light. 2. Illuminated SMOKE/EXTG switch − Press. Check FIRE BOTTLE FWD LOW and AFT LOW advisory lights illuminate and FIRE BOTTLE FWD ARM advisory light out. FIRE EXTINGUISHING SYSTEMS OPERATIONS (STANDARD CONFIGURATION) brd48a01.dg, gv/cs, sep09/2014 FIRE EXTINGUISHING SYSTEMS OPERATIONS (Sheet 1 of 2)
Figure 00 − 23 Model 400
Page 46 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL A
BAGGAGE AFT SMOKE VENT VENT EXTG INLT OTLT
CLOSED 1 TEST 2 FIRE BLT AFT ARM LOW AFT ARM LOW
ENGINE FIRE A 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 FIRE 1. 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.
BAGGAGE AFT COMPARTMENT FIRE 1. 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.
NOTE The FIRE BOTTLE FWD LOW advisory light will illuminate approximately seven minutes after the FIRE BOTTLE AFT LOW advisory light illuminates.
FIRE EXTINGUISHING SYSTEMS OPERATIONS (EXTRA CAPACITY CONFIGURATION) brd48a02.dg, cs, sep09/2014 FIRE EXTINGUISHING SYSTEMS OPERATIONS (Sheet 2 of 2)
Figure 00 − 23 Model 400
Page 47 Nov 05/2014 CRASH−FIRE−RESCUE MANUAL A
DC CONTROL
OFF OFF OFF OFF
STBY AUX MAIN BATTERY BATT BATT BATT MASTER
OFF OFF OFF OFF OFF
GEN 1 GEN 2 MAIN BUS BUS FAULT EXT PWR TIE RESET
A
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. brd47a01, gv, 05/11/98 BATTERY POWER SWITCH LOCATIONS
Figure 00 − 24 Model 400
Page 48 Nov 05/2014