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Title
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
Commercial
Copyright © 2005
The Boeing Company
All Rights Reserved
June 27, 2014
2
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Document Information
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Manager, Flight Technical Data
Boeing Commercial Airplane Group
PO Box 3707, M/C 20-89
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Every attempt has been made to include as many of the Boeing Company’s
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Document Number: D6-7829
RevisionNumber: 10
RevisionDate: June 27, 2014
Table of Contents (tab)
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
Table of Contents
Title Page - - - - - - - - - - - - - - - - - - - - - - - - - - - - 00.Title
List of Effective Pages - - - - - - - - - - - - - - - - - - - -00.LEP
Revision Record - - - - - - - - - - - - - - - - - - - - - - - - 00.RR
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 727.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 727.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - - 727.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 727.0.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - - 727.0.6
707
707-100 & 200 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
707.0.1
707.0.1
707.0.2
707.0.3
707.0.4
707.0.5
707-300 & 400 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
707.1.1
707.1.1
707.1.2
707.1.3
707.1.4
707.1.5
717
717 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - -
717.0.1
717.0.1
717.0.2
717.0.3
717.0.4
717.0.5
717.0.6
717.0.7
720
720 & 720B SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
720.0.1
720.0.1
720.0.2
720.0.3
720.0.4
720.0.5
727
727 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 727.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 727.0.1
737
737-100/200/300/400/500 SERIES - - - - - - - - - - - - - - - - - - - 737.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 737.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 737.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 737.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - - 737.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 737.0.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - - 737.0.6
737-600/700/800/900/ER/BBJ/BBJ-2 - - - - - - - - - - - - - - - - - - 737.1.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 737.1.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 737.1.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 737.1.3
BATTERY LOCATION - - - - - - - - - - - - - - - - - - - - - - - - - - 737.1.4
FLIGHT DECK CNTRL SWITCH LOCATIONS - - - - - - - - - 737.1.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - - 737.1.6
AUX TANK CAPACITIES - - - - - - - - - - - - - - - - - - - - - - - - 737.1.7
747
747-100 & 200/-100 & 200 COMBI - - - - - - - - - - - - - - - - - - - 747.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 747.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 747.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 747.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - - 747.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 747.0.5
747-200 SPECIAL FREIGHTER - - - - - - - - - - - - - - - - - - - - - 747.1.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 747.1.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 747.1.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 747.1.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - - 747.1.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 747.1.5
747-300 & 300 COMBI SERIES - - - - - - - - - - - - - - - - - - - - - 747.2.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 747.2.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 747.2.2
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
6
June
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Table of Contents
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 747.8.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 747.8.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 747.8.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - 747.8.6
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 747.2.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 747.2.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - 747.2.5
747-300 SPECIAL FREIGHTER - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
747.3.1
747.3.1
747.3.2
747.3.3
747.3.4
747.3.5
747 SP SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
747.4.1
747.4.1
747.4.2
747.4.3
747.4.4
747.4.5
747 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
747.5.1
747.5.1
747.5.2
747.5.3
747.5.4
747.5.5
747-400 & 400 COMBI SERIES - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-3 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-4 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - -
747.6.1
747.6.1
747.6.2
747.6.3
747.6.4
747.6.5
747.6.6
747.6.7
747-400 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - -
747.7.1
747.7.1
747.7.2
747.7.3
747.7.4
747.7.5
747.7.6
747 LARGE CARGO FREIGHTER - - - - - - - - - - - - - - - - - - - 747.8.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 747.8.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 747.8.2
747-8 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - - - - - 747.9.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 747.9.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 747.9.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 747.9.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 747.9.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 747.9.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - 747.9.6
747-8I - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - -
747.10.1
747.10.1
747.10.2
747.10.3
747.10.4
747.10.5
747.10.6
757
757-200 & 200 COMBI SERIES - - - - - - - - - - - - - - - - - - - - - 757.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 757.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 757.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 757.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 757.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 757.0.5
757-200 PACKAGE FREIGHTER - - - - - - - - - - - - - - - - - - - - 757.1.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 757.1.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 757.1.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 757.1.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 757.1.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 757.1.5
757-300 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 757.2.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 757.2.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 757.2.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 757.2.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 757.2.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 757.2.5
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - 757.2.6
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
00.TOC.2
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767
787
767 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - -
767.0.1
767.0.1
767.0.2
767.0.3
767.0.4
767.0.5
767.0.6
767
767 -2C Freighter - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - -
767.0.1
767.0.1
767.0.2
767.0.3
767.0.4
767.0.5
767.0.6
787 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 787.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - - 787.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - - 787.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - - 787.0.3
EMERGENCY RESCUE ACCESS-3 - - - - - - - - - - - - - - - - 787.0.4
EMERGENCY RESCUE ACCESS-4 - - - - - - - - - - - - - - - - 787.0.5
EMERGENCY RESCUE ACCESS-5 - - - - - - - - - - - - - - - - 787.0.6
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - - 787.0.7
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - - 787.0.8
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - - - 787.0.9
DC-3
DC3 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-3.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - DC-3.0.1
DC-6
DC-6 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-6.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - DC-6.0.1
777
777 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 777.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - 777.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - 777.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - 777.0.3
EMERGENCY RESCUE ACCESS-3 - - - - - - - - - - - - - - - 777.0.4
EMERGENCY RESCUE ACCESS-4 - - - - - - - - - - - - - - - 777.0.5
EMERGENCY RESCUE ACCESS-5 - - - - - - - - - - - - - - - 777.0.6
EMERGENCY RESCUE ACCESS-6 - - - - - - - - - - - - - - - 777.0.7
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - 777.0.8
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - 777.0.9
COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - 777.0.10
777 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - COMPOSITE MATERIALS LOCATIONS - - - - - - - - - - - -
777.1.1
777.1.1
777.1.2
777.1.3
777.1.4
777.1.5
777.1.6
DC-7
DC-7 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-7.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - DC-7.0.1
EMERGENCY RESCUE ACCESS - - - - - - - - - - - - - - - - DC-7.0.2
EMERGENCY RESCUE ACCESS - - - - - - - - - - - - - - - - DC-7.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - DC-7.0.4
DC-7 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - - - - DC-7.1.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - DC-7.1.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - DC-7.1.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - DC-7.1.3
DC-8
DC-8 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-8.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - - DC-8.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - - DC-8.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - - DC-8.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - - DC-8.0.4
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
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Table of Contents
DC-8 FREIGHTER SERIES - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.1.1
DC-8.1.1
DC-8.1.2
DC-8.1.3
DC-8.1.4
DC-8-61 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.2.1
DC-8.2.1
DC-8.2.2
DC-8.2.3
DC-8.2.4
DC-8-62 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.3.1
DC-8.3.1
DC-8.3.2
DC-8.3.3
DC-8.3.4
DC-8-63 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.4.1
DC-8.4.1
DC-8.4.2
DC-8.4.3
DC-8.4.4
DC-8-71 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.5.1
DC-8.5.1
DC-8.5.2
DC-8.5.3
DC-8.5.4
DC-8-72 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.6.1
DC-8.6.1
DC-8.6.2
DC-8.6.3
DC-8.6.4
DC-8-73 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - -
DC-8.7.1
DC-8.7.1
DC-8.7.2
DC-8.7.3
DC-8.7.4
DC-9
DC-9 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-9.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - - DC-9.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - - DC-9.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - - DC-9.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - - DC-9.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - - DC-9.0.5
EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - - - - DC-9.0.6
DC-10
DC-10 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - DC-10.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - DC-10.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - DC-10.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - DC-10.0.3
EMERGENCY RESCUE ACCESS-3 - - - - - - - - - - - - - DC-10.0.4
EMERGENCY RESCUE ACCESS-4 - - - - - - - - - - - - - DC-10.0.5
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - DC-10.0.6
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - DC-10.0.7
EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - - - DC-10.0.8
MD-11
MD-11 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MD-11.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - MD-11.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - MD-11.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - MD-11.0.3
EMERGENCY RESCUE ACCESS-3 - - - - - - - - - - - - - MD-11.0.4
EMERGENCY RESCUE ACCESS-4 - - - - - - - - - - - - - MD-11.0.5
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - MD-11.0.6
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - MD-11.0.7
EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - - - MD-11.0.8
MD-80
MD-80 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - MD-80.0.1
FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - - MD-80.0.1
EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - - MD-80.0.2
EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - - MD-80.0.3
BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - - MD-80.0.4
FLIGHT DECK CONTROL SWITCH LOCATIONS - - - - MD-80.0.5
EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - - - MD-80.0.6
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00.TOC.4
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AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
Table of Contents
MD-90
MD-90 SERIES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - FLAMMABLE MATERIAL LOCATIONS - - - - - - - - - - EMERGENCY RESCUE ACCESS-1 - - - - - - - - - - - - EMERGENCY RESCUE ACCESS-2 - - - - - - - - - - - - BATTERY LOCATIONS - - - - - - - - - - - - - - - - - - - - - FLIGHT DECK CONTROL SWITCH LOCATIONS - - EXTERNAL APU FIRE CONTROLS - - - - - - - - - - - - -
MD-90.0.1
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MD-90.0.2
MD-90.0.3
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MD-90.0.5
MD-90.0.6
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Flight Crew Operations Manual
Revision Record
Revision Record
Revision
Record
Model
Revision Item
787
Updated fuel quantities for the 787-8 and added the 787-9.
767 -2C
Added new 767 -2C model.
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707-100 & 200 SERIES
FLAMMABLE MATERIAL LOCATIONS
707 (tab)
PORTABLE OXYGEN BOTTLES 8 PLACES
ON HATRACKS OR NEAR FLOOR LEVEL ON
PARTITIONS
434 GAL 1643 L
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
2333 GAL 8831 L
FIRE EXTINGUISHER
PORTS ON ENGINE RIGHT
COWLING (TYPICAL EACH
PASSENGER OXYGEN SYSTEM BOTTLES IN
AFT CARGO COMPARTMENT
2283 GAL 8642 L
UTILITY AND AUXILIARY RESERVOIR IN
LEFT FILLET AREA
CREW OXYGEN SYSTEM
BOTTLES IN FWD LOWERED
CEILING OR FWD CARGO
7306 GAL - 27656 L
2283 GAL - 8642 L
2333 GAL - 8831 L
434 GAL - 1643 L
FUEL TANK
ENGINE OIL TANK - EACH ENGINE
- RIGHT SIDE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
PORTABLE OXYGEN BOTTLE ON
Fans: Placing fans may place firefighters very close to the hazard zone.
FORWARD SIDE OF BULKHEAD
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across and maintain a cooling effect.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident. Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure,
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
with a pike pole, axe or any instrument used to sound surfaces for integrity.
fragmentation hazard.
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707.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
707-100 & 200 SERIES
1 ENTRY DOOR EXTERNAL
HANDLE
2 GALLEY DOOR
EXTERNAL HANDLE
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
3 EMERGENCY OVERWING
EXIT HATCHES PUSH
PANEL
TO OPEN HATCH:
1. PUSH IN PANEL.
2. PUSH HATCH INWARD.
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED FROM OUTSIDE.
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE
AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS
BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
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AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
707-100 & 200 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
2 AFT GALLEY DOOR
3 OVERWING ESCAPE
HATCHES
1
AFT ENTRY DOOR
4 CUT-IN AREAS (NOT
MARKED ON ALL
AIRPLANES)
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
2 FORWARD GALLEY
DOOR
1 FORWARD ENTRY
DOOR
1 FLIGHT DECK WINDOWS OPEN
FROM INSIDE
6 FT 1/2 IN. FLOOR LEVEL TO GROUND, WHEELS RETRACTED
9 FT 7 IN. FLOOR LEVEL TO GROUND, WHEELS EXTENDED
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
707.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
707-100 & 200 SERIES
BATTERY
MAIN BATTERY
NOSE WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
707.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
707-100 & 200 SERIES
ENGINE FIRE T-HANDLES - PULL
NOTE:
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
BATTERY
SWITCH - OFF
THRUST LEVERS - RETARD
APU FIRE SWITCH - PULL
ENGINE START
LEVERS - CUTOFF
APU MASTER
SWITCH - OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
707.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
707-100 & 200 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
707.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
707-300 & 400 SERIES
FLAMMABLE MATERIAL LOCATIONS
PORTABLE OXYGEN BOTTLES 8 PLACES ON
HATRACKS OR NEAR FLOOR LEVEL ON
PARTITIONS
434 GAL 1643 L
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
FUEL TANK
2285 GAL 8650 L
FIRE EXTINGUISHER PORTS ON
ENGINE RIGHT COWLING
(TYPICAL EACH ENGINE)
PASSENGER OXYGEN SYSTEM BOTTLES IN AFT
CARGO COMPARTMENT
4036 GAL 15278 L
UTILITY AND AUXILIARY RESERVOIR IN LEFT
FILLET AREA
CREW OXYGEN SYSTEM
BOTTLES IN FWD LOWERED
CEILING OR FWD CARGO AREA
10190 GAL - 38573 L
4036 GAL - 15278 L
2285 GAL - 8650 L
434 GAL - 1643 L
APU FUEL LINE
ENGINE OIL TANK EACH ENGINE - RIGHT SIDE
AUXILIARY POWER UNIT FWD CARGO
COMPARTMENT ON 25000 SERIES
PORTABLE OXYGEN BOTTLE ON
FORWARD SIDE OF BULKHEAD
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
pole, axe or any instrument used to sound surfaces for integrity.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
707.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
707-300 & 400 SERIES
2 ENTRY DOOR EXTERNAL
HANDLE
1 PILOT’S SLIDING
WINDOWS
P
U
L
L
4 EMERGENCY OVERWING
EXIT HATCHES PUSH
PANEL
3 GALLEY DOOR
EXTERNAL HANDLE
P
U
S
H
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN WINDOW FROM OUTSIDE
(RT SIDE ONLY)
1. PUSH IN EXTERNAL ACCESS
DOOR.
2. PULL EXTERNAL RELEASE
HANDLE.
3. SLIDE WINDOW OPEN.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN HATCH:
1. PUSH IN PANEL.
2. PUSH HATCH INWARD.
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED FROM OUTSIDE.
5 STATION 990 EMERGENCY EXIT
6 CUT-IN AREAS
CUT-IN AREAS
* NEW INTERIOR
HAS STOWAGE
BIN
*
NOTE:
CUT-INAREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT. BECAUSE
OF TYPE OF STRUCTURE AND POSSIBLE
INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES
AND DOORS. URGENCY OF SITUATION
WILL DICTATE THE NECESSITY FOR A CUTIN.
EMERGENCY EXIT
WARNING
STAND TO SIDE OF EXIT DOOR
DOOR FALLS OUT AND DOWN
ESCAPE SLIDE INFLATES IMMEDIATELY
TO OPEN LIFT HANDLE UP
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
707.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
707-300 & 400 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
3 AFT GALLEY DOOR
5 CARGO AIRPLANES
ONLY
2 AFT ENTRY DOOR
6 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
6 CUT-IN AREAS (NOT
MARKED ON ALL
AIRPLANES)
4 OVERWING
ESCAPE HATCHES
3 FORWARD GALLEY
DOOR
2 FORWARD ENTRY
DOOR
6 FT 1/2 IN. FLOOR LEVEL TO GROUND, WHEELS RETRACTED
1 FLIGHT DECK WINDOWS
OPEN FROM INSIDE
10 FT 1 IN. FLOOR LEVEL TO GROUND, WHEELS EXTENDED
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
707.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
707-300 & 400 SERIES
BATTERY
MAIN BATTERY
NOSE WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
707.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
707-300 & 400 SERIES
ENGINE FIRE T-HANDLES - PULL
NOTE:
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
BATTERY
SWITCH - OFF
THRUST LEVERS - RETARD
APU FIRE SWITCH - PULL
ENGINE START
LEVERS - CUTOFF
APU MASTER
SWITCH - OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
707.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
707-300 & 400 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
707.1.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
717 SERIES
FLAMMABLE MATERIAL LOCATIONS
717 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
PORTABLE OXYGEN
SYSTEM BOTTLE
FUEL VENT BOX
HYDRAULIC ACCUMULATOR
ENGINE OIL
TANKS
FIRE EXTINGUISHER
AGENT CONTAINERS
APU GROUND CONTROL
PANEL ON FUSELAGE
1383 GAL 5235 L
FUEL TANKS
HYDRAULIC FLUID RESERVIOR
1 IN EACH WHEEL WELL
907 GAL 3433 L
CREW OXYGEN SYSTEM
BOTTLES
FUEL TANKS
1383 GAL - 5235 L
FUEL VENT BOX
HYDRAULIC
ACCUMULATORS
PORTABLE OXYGEN
SYSTEM BOTTLE
CREW PORTABLE OXYGEN
SYSTEM BOTTLES
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
717.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
717 SERIES
1 PASSENGER AND SERVICE
DOORS
2 OVERWING EMERGENCY
EXITS
TO OPEN DOOR:
1. PULL HANDLE FROM RECCESS.
2. ROTATE HANDLE AFT.
3. PULL DOOR OPEN.
3 TAIL CONE JETTISON LATCH
TO OPEN DOOR:
1. PUSH HANDLE RELEASE.
2. PULL THE HANDLE AND, AT THE
SAME TIME, PUSH IN TOP OF
DOOR FORCIBLY.
EXTERIOR
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE
AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS
BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
717.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
717 SERIES
JETTISONABLE TAIL
CONE
AFT LOWER CARGO
COMPARTMENT DOOR
TAIL CONE ACCESS
DOOR
3 TAIL CONE
JETTISON LATCH
2 OVERWING EMERGENCY
EXITS
FORWARD LOWER
CARGO DOOR
1 FORWARD SERVICE
ENTRANCE DOOR
APU COMPARTMENT
ACCESS DOOR
CLEARVIEW WINDOWCHILL PANE WITH CO2
AND BREAK WITH HEAVY
FIRE AXE FOR ACCESS
TO HANDLE; SLIDE
WINDOW AFT
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 4 FT.
CLEARVIEW WINDOW
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
717.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
717 SERIES
BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
717.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
717 SERIES
APU CONTROL PANEL
AGENT
DISCH
1
2
L
E
N
G
FIRE
TEST
F
I
R
E
PULL
LH ENGINE
AGENT 1
LOW
AGENT 2
LOW
AGENT
DISCH
2
1
FAULT
TEST
R
4 FIRE AGENT NO. 2
E
N
G
3 FIRE AGENT NO. 1
F
I
R
E
PULL
APU
NO 1
FIRE AGENT
NO 2
AIR
OFF
OFF
DISCH
FIRE CONT
NORM
RH ENGINE
ON
1 MASTER OFF
MASTER
OFF
RUN
OFF &
AGENT ARM
B,D,E
START
2 FIRE CONT
C - “ENG FIRE”
HANDLES - PULL
APU SHUTDOWN AND FIRE PROCEDURE
1. APU “MASTER OFF” SWITCH TO “OFF” (UP)
2. IF”APU FIRE” ALERT ON EAD IS DISPLAYED...
3. FIRE CONT SW TO “OFF & AGENT ARM”
4. FIRE AGENT NO. 1 SWITCH TO “DISCH” (DOWN)
5. AFTER 30 SECONDS FIRE AGENT NO. 2 SWITCH TO
“DISCH” (DOWN)
ENGINE SHUTDOWN AND FIRE PROCEDURE
A. FUEL CONTROL SWITCH FROM “ON” TO “OFF” (DOWN)
B. IF LIGHT(S) IN HANDLES ARE ILLUMINATED...
C. PULL HANDLES FULLY OUT
D. ROTATE HANDLES CLOCKWISE
E. AFTER 30 SECONDS, ROTATE HANDLES COUNTERCLOCKWISE
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES
A - FUEL CONTROL
SWITCHES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
717.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
717 SERIES
2 FIRE LIGHT
3 FIRE AGENT 1
APU SHUTDOWN AND FIRE PROCEDURE
4 FIRE AGENT 2
1. “APU SHUT OFF” SWITCH TO “SHUT OFF” (UP)
2. IF “FIRE” LIGHT IS ILLUMINATED...
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP)
4. AFTER 30 SECONDS, FIRE AGENT NO 2 SWITCH TO “DISCHARGE” (UP)
1 APU SHUT
OFF SWITCH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
717.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
717 SERIES
ELEVATOR TABS
TIP CAP
HORIZONTAL
STABILIZER
FAIRING
TAILCONE
WING TO BODY FAIRING
FLAP HINGE
FAIRINGS
ENTRANCE
STAIR DOOR
RADOME
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
717.0.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
717 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
717.0.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
720 & 720B SERIES
FLAMMABLE MATERIAL LOCATIONS
720 (tab)
PORTABLE OXYGEN
BOTTLES ON HATRACKS
OR NEAR FLOOR LEVEL
ON PARTITIONS
434 GAL 1643 L
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
2333 GAL 8831 L
FIRE EXTINGUISHER PORTS ON
ENGINE RIGHT COWLING
(TYPICAL EACH ENGINE)
CREW OXYGEN SYSTEM
BOTTLES IN FWD LOWERED
CEILING OR FWD CARGO AREA
1
PASSENGER OXYGEN SYSTEM BOTTLES IN AFT
CARGO COMPARTMENT
2283 GAL 8642 L
UTILITY AND AUXILIARY RESERVOIR IN LEFT
FILLET AREA
2 GAL 5950
22523 L
FUEL TANK
2283 GAL - 8642 L
2333 GAL - 8831 L
FUEL TANK
434 GAL - 1643 L
FUEL TANK
ENGINE OIL TANK EACH ENGINE - RIGHT SIDE
PORTABLE OXYGEN BOTTLE ON
FORWARD SIDE OF BULKHEAD
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
720.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
720 & 720B SERIES
2 GALLEY DOOR EXTERNAL
HANDLE
1 ENTRY DOOR EXTERNAL
HANDLE
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
3 EMERGENCY OVERWING
EXIT HATCHES PUSH
PANEL
TO OPEN HATCH:
1. PUSH IN PANEL.
2. PUSH HATCH INWARD.
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED FROM OUTSIDE.
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
720.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
720 & 720B SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
2 AFT GALLEY DOOR
3 OVERWING
ESCAPE HATCHES
1 AFT ENTRY DOOR
4 CUT-IN AREAS (NOT
MARKED ON ALL
AIRPLANES)
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
2 FORWARD
GALLEY DOOR
1 FORWARD
ENTRY DOOR
1 FLIGHT DECK WINDOWS OPEN
FROM INSIDE
6 FT 1/2 IN. FLOOR LEVEL TO GROUND, WHEELS RETRACTED
9 FT 10 IN. FLOOR LEVEL TO GROUND, WHEELS EXTENDED
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
720.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
720 & 720B SERIES
BATTERY
MAIN BATTERY
NOSE WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
720.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
720 & 720B SERIES
ENGINE FIRE T-HANDLES - PULL
NOTE:
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
BATTERY
SWITCH - OFF
THRUST LEVERS - RETARD
APU FIRE SWITCH - PULL
ENGINE START
LEVERS - CUTOFF
APU MASTER
SWITCH - OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
720.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
720 & 720B SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
720.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
727 SERIES
FLAMMABLE MATERIAL LOCATIONS
727 (tab)
AFT CARGO FUEL TANKS (OPTIONAL)
1
2
860 GAL (FWD) - 3255 L
1070 GAL (AFT) - 4050 L
AIRSTAIR
HYDRAULIC RESERVOIR
FORWARD CARGO FUEL TANKS (OPTIONAL)
OXYGEN BOTTLES
(PORTABLE)
810 GAL (EACH CELL) - 3066 L
FUEL LINES
VENT SURGE TANK
APU
(WHEEL WELL)
AIRSTAIR HYDRAULIC
ACCUMULATOR
FUEL TANK
FIRE EXT PORT (OUTBD
ENG ONLY)
1793 GAL 6787 L
ENGINE OIL TANK
(TYPICAL)
1
HYDRAULIC ACCUMULATOR
(WHEEL WELL)
PORTABLE OXYGEN
BOTTLES
4004 GAL 15155 L
OXYGEN BOTTLES
(PASSENGERS AND CREW)
APU EMERGENCY CONTROL
PANEL LOCATED IN THE LEFT
WHEEL WELL AREA
1793 GAL - 6787 L
2
FUEL TANK
FUEL TANK
PORTABLE OXYGEN
BOTTLE
PORTABLE OXYGEN
BOTTLE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
VENT SURGE TANK
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
pole, axe or any instrument used to sound surfaces for integrity.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
727.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
727 SERIES
1 PILOT’S SLIDING WINDOW
(RH AND LH) CARGO AIRPLANES
(RH ONLY) PASSENGER AIRPLANES
P
U
L
L
2 FWD ENTRY DOOR
EXTERNAL HANDLE
3 MID/FWD GALLEY DOOR
EXTERNAL HANDLE
4 EMERGENCY OVERWING
EXIT HATCHES PUSH
PANEL
P
U
S
H
TO OPEN WINDOW FROM OUTSIDE:
1. PUSH IN EXTERNAL ACCESS
DOOR.
2. PULL EXTERNAL RELEASE
HANDLE.
3. SLIDE WINDOW OPEN.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN HATCH:
1. PUSH IN PANEL.
2. PUSH HATCH INWARD AND
UPWARD.
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED FROM OUTSIDE.
5 AFT EXIT DOORS EXTERNAL
HANDLE (200)L
TO OPEN DOOR:
1. PULL OUTWARD LOWER END OF
HANDLE AND ROTATE FORWARD.
2. PULL DOOR OUTWARD.
6 CUT-IN AREAS
NOTE:
CUT-IN AREAS
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT. BECAUSE OF
TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED
THAT MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE THE
NECESSITY FOR A CUT-IN.
NEW INTERIOR HAS
STOWAGE BIN
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
727.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
727 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
6 CUT-IN AREAS
AFT ENTRY DOOR OPENS FROM
INSIDE OF THE AFT STAIRS AREA
(Airstair must first be lowered)
4 OVERWING ESCAPE HATCHES
AFT AIRSTAIR EXTERIOR
CONTROL PANEL OPERATING
INSTRUCTIONS ON ACCESS
PANEL
6 CUT-IN AREA
AFT AIRSTAIR
3 GALLEY DOOR
(MOVED FORWARD ON 200
- REMOVED ON 200F)
5 AFT EXIT DOORS
(REMOVED ON 100 AND 200F)
2 FORWARD
ENTRY DOOR
4 OVERWING ESCAPE HATCHES
6 CUT-IN AREA
CARGO DOOR
1 PILOTS’ SLIDING
WINDOW
5 FT 8 IN. FLOOR LEVEL TO GROUND, WHEELS RETRACTED
9 FT 1 IN. FLOOR LEVEL TO GROUND, WHEELS EXTENDED
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
727.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
727 SERIES
MAIN BATTERY
ACCESS DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
727.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
TA 1
ON
TA 2
D.C. METERS
FIRE
D
I
S
C
H
NOTE:
WHEEL
WELL
PULL
TANK 1
D
I
S
C
H
D
I
S
C
H
D
I
S
C
H
D
I
S
C
H
D
I
S
C
H
BELL
CUTOUT
TANK 3
OPEN
CLOSE
OPEN
OPEN
HT
HT
0
0
0
CLOSE
VALVE ONTRANSIT
L NOZZLE
TRIP
DATE
BATTERY SWITCH
- LIFT GUARD
- SWITCH OFF
BRIG
TANK 2
OPEN
CLOSE
OFF
ENGINES
& W W
HT
CLOSE
FIRE TEST
PULL
HT
VALVE ONTRANSIT
FIREWALLS
PULL
HT
BRIG
FIRE
B
A
T
T
E
R
Y
BRIG
HT
ESS TR
BAT
OFF
BOTTLE
TRANSFER
FIRE
50 DC 50
AMPS
BRIG
20
0 DC VOLTS 40
BRIG
-0+
ENGINE FIRE T-HANDLES - PULL
BRIG
727 SERIES
0
0
R NOZZLE
0
R
E
P
E
A
T
E
V
RECORDING TIMEE
REMAINING
N
T
APU FIRE SWITCH
- PULL
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
THRUST LEVERS - RETARD
BRIG
HT
BRIG
HT
MASTER SWITCH
- OFF
ENGINE START
LEVERS - CUTOFF
OVER VOLTAGE
SYSTEM 1
OVER VOLTAGE
SYSTEM 2
OVER VOLTAGE
SYSTEM 3
UNDER VOLTAGE
SYSTEM 1
UNDER VOLTAGE
SYSTEM 2
UNDER VOLTAGE
SYSTEM 3
DIFF FAULT
SYSTEM 1
DIFF FAULT
SYSTEM 2
DIFF FAULT
SYSTEM 3
OVER EXCITER
SYSTEM 1
OVER EXCITER
SYSTEM 2
OVER EXCITER
SYSTEM 3
UNDER EXCITER
SYSTEM 1
UNDER EXCITER
SYSTEM 2
UNDER EXCITER
SYSTEM 3
PHASE
UNBALANCE
APU CHARGE
APU BLEED
RESET
TEST
BULKHEAD RIGHT OF
FLIGHT ENGINEERS
PANEL
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
727.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
727 SERIES
COMPOSITE MATERIALS LOCATIONS
FIN TIP FAIRING
RAIN GUTTER
WING TO BODY FAIRING
RADOME
LEADING EDGE ACCESS PANELS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
727.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
737-100/200/300/400/500 SERIES
FLAMMABLE MATERIAL LOCATIONS
737 (tab)
390/492/984 GAL 1476/1862/3725 L
1
WINGLETS
(AS INSTALLED)
OPTIONAL AUXILIARY FUEL
TANK IN LWR AFT CARGO
COMPARTMENT
VENT SURGE TANK
SYSTEM A, B AND STANDBY
HYDRAULIC RESERVOIRS IN
WHEEL WELL
AUXILIARY POWER UNIT OIL
TANK
FUEL TANK No. 2
PORTABLE OXYGEN BOTTLES
LOCATION VARIES THROUGHOUT
PASSENGER CABIN
1499 GAL 5674 L
APU FUEL LINE
APU EMERGENCY CONTROL PANEL LOCATED IN
THE RIGHT WHEEL WELL AREA
1
CREW OXYGEN BOTTLE
FWD CARGO AREA
HYDRAULIC BRAKE ACCUMULATORS
IN WHEEL WELL
2313 GAL 8755 L
FUEL TANK No. 1
VENT SURGE TANK
PASSENGER OXYGEN
(OPTIONAL)
1499 GAL - 5674 L
PORTABLE OXYGEN
BOTTLE BEHIND FIRST
OFFICER
CENTER FUEL TANK
ENGINE OIL TANK
RIGHT SIDE EACH
ENGINE - CFM-56
(LEFT SIDE ALL
OTHERS)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
737-100/200/300/400/500 SERIES
1 CO-PILOT’S SLIDING WINDOW
2 FWD AND AFT ENTRY DOOR
EXTERNAL HANDLE (LH SIDE)
(PILOT’S WINDOW - AS INSTALLED)
3 FWD AND AFT SERVICE DOOR
EXTERNAL HANDLE (RH SIDE)
EXTERNAL
RELEASE
HANDLE
EXTERNAL
ACCESS
DOOR
P
U
S
H
P
U
L
L
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN WINDOW FROM OUTSIDE:
1. PUSH IN EXTERNAL ACCESS DOOR.
2. PULL EXTERNAL RELEASE HANDLE.
3. SLIDE WINDOW OPEN.
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED FROM
OUTSIDE.
4 EMERGENCY OVERWING ESCAPE
HATCH
5 CARGO DOOR OPERATION
6 CUT-IN AREAS
CUT-IN AREAS
EMERGENCY EXIT
PRESS TO UNLATCH
PUSH HATCH INWARD
AND LIFT UP
CAUTION:
Make Sure Al l Per sons and
Eq uip me nt Are Cle ar of th e Doo r.
Do No t Ope n the Do or Wh en the
Air p lan e I s Pr e ss u ris e d.
Rem ove Class Divi der and Al l
L oo s e I t ems W it hin St o ra ge Bins
Be for e O pe nin g Car go Do or .
Car g o Doo r Mo ve me nt Ca n
Cause Injur y to Per sons and
Damage Equipment.
Loose Items Can Fall and
Cause Injur y.
TO OPEN CARGO DOOR 1.
UNLOCK THE EXT. DOOR
HANDLE
2. VERIFY UNLOCKED LIGHT
IS ON.
3. HOLD THE UP TO CANOPY
SWITCH IN POSITION UNTIL
DOOR MOTION STOPS.
TO OPEN HATCH FROM OUTSIDE:
1. PUSH IN PANEL.
2. PUSH HATCH INWARD & LIFT UP.
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE
AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS
BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
737-100/200/300/400/500 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE
3 AFT SERVICE DOOR
CARGO DOOR (RIGHT SIDE)
OPERATING INSTRUCTIONS ON
DOOR
4 EMERGENCY OVERWING
ESCAPE HATCHES (ALL)
4 EMERGENCY OVERWING
ESCAPE HATCHES (-400)
2 AFT ENTRY DOOR
6 CUT-IN AREAS
6 CUT-IN AREAS
CARGO DOOR ( RIGHT SIDE)
OPERATING INSTRUCTIONS ON
DOOR
3 FWD SERVICE DOOR
5 CARGO DOOR
(AS INSTALLED)
AVERAGE DISTANCE
1 PILOT’S SLIDING WINDOWS
(AS INSTALLED)
6 CUT-IN AREAS LOCATED
BETWEEN WING FRONT SPAR
AND ESCAPE HATCH (THREE
BAYS) BELOW WINDOWS AND
ABOVE FLOORS
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 5: FT
2 FWD ENTRY DOOR
WHEELS EXTENDED: 8 FT 6 IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
737-100/200/300/400/500 SERIES
BATTERY (-100 & -200)
BATTERY (-300, -400, -500)
E/E COMPARTMENT
ACCESS DOOR
OPTIONAL BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
737-100/200/300/400/500 SERIES FLIGHT DECK CONTROL SWITCH LOCATIONS
APU
APU
OFF
OR
OFF
DELAY
OFF
ON
START
ON
START
BATTERY SWITCH
- LIFT GUARD
- SWITCH - OFF
APU MASTER
SWITCH - OFF
THRUST LEVERS - RETARD
APU FIRE SWITCH - PULL
IDLE
START LEVERS
- CUTOFF
CUTOFF
1
2
ENGINE FIRE SWITCHES - PULL
(IF NOT ILLUMINATED, PUSH AND HOLD THE BUTTON
UNDER THE SWITCH TO RELEASE.)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
737-100/200/300/400/500 SERIES
VERTICAL STABILIZER TIP
HORIZONTAL STABILIZER
TRAILING EDGE AND TIP
RUDDER
TAILCONE
ASSEMBLY
ELEVATOR TAB
STRUCTURE
UPPER WING FIXED
TRAILING EDGE
PANELS
UPPER WING FIXED
LEADING EDGE
PANELS
NACELLE STRUT
FAIRING
WING TRAILING EDGE
MAIN FLAP ASSEMBLY
SPOILERS
AILERONS/TAB SKIN
AND STRUCTURE
RADOME
ENGINE COWL
LOWER WING FIXED
LEADING EDGE
PANELS
NOSE LANDING
GEAR DOORS
LOWER WING FIXED
TRAILING EDGE
PANELS
WING TO BODY
FAIRING
MAIN LANDING
GEAR DOORS
AND FAIRINGS
FLAP TRACK
FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
737-600/700/800/900/ER/BBJ/BBJ-2
1
FLAMMABLE MATERIAL LOCATIONS
AUXILIARY FUEL TANK
LOCATIONS (BBJ ONLY-SEE AUX
TANK CAPACITY PAGE)
WINGLETS
(AS INSTALLED)
VENT SURGE TANK
AUXILIARY POWER UNIT OIL
TANK
SYSTEM A, B AND STANDBY
HYDRAULIC RESERVOIRS IN
WHEEL WELL
FUEL TANK No. 2
PORTABLE OXYGEN BOTTLES
LOCATION VARIES THROUGHOUT
PASSENGER CABIN
1288 GAL 4876 L
APU FUEL LINE
1
CREW OXYGEN BOTTLE
FWD CARGO AREA
4299 GAL 16273 L
APU EMERGENCY CONTROL PANEL LOCATED IN
THE RIGHT WHEEL WELL AREA
HYDRAULIC BRAKE ACCUMULATORS
IN WHEEL WELL
1
1288 GAL - 4876 L
FUEL TANK No. 1
WINGLETS
(AS INSTALLED)
PORTABLE OXYGEN
BOTTLE BEHIND FIRST
OFFICER
CENTER FUEL TANK
ENGINE OIL TANK RIGHT
SIDE EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure,
visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
with a pike pole, axe or any instrument used to sound surfaces for integrity.
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
737-600/700/800/900/ER/BBJ/BBJ-2
2 FWD AND AFT ENTRY DOOR
EXTERNAL HANDLE (LH SIDE)
1 CO-PILOT’S SLIDING WINDOW
(PILOT’S WINDOW - AS INSTALLED)
EXTERNAL
RELEASE
HANDLE
EXTERNAL
ACCESS
DOOR
P
U
S
H
P
U
L
L
WARNING: PASSENGER AND SERVICE DOORS, SLIDE MAY AUTOMATICALLY DEPLOY WHEN DOORS ARE OPENED
FROM OUTSIDE
4 EMERGENCY OVERWING EXIT DOOR
PUSH TO OPEN
DOOR OPENS OUT AND UP
AUTOMATICALLY
EXTERIOR OVERWING
EMERGENCY EXIT
PUSH PANEL
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE COUNTERCLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN DOOR:
1. PULL HANDLE OUTWARD.
2. ROTATE CLOCKWISE.
3. PULL DOOR OUTWARD.
TO OPEN WINDOW FROM OUTSIDE:
1. PUSH IN EXTERNAL ACCESS DOOR.
2. PULL EXTERNAL RELEASE HANDLE.
3. SLIDE WINDOW OPEN.
EMERGENCY EXIT
ONLY
3 FWD AND AFT SERVICE DOOR
EXTERNAL HANDLE (RH SIDE)
5 CARGO DOOR OPERATION
6 CUT-IN AREAS
WARNING
DOOR SWINGS
OUT AND UP
HOLD YOUR
KNEE AGAINST
DOOR WHILE
OPENING OR
SERIOUS
INJURY CAN
OCCUR
TO OPEN DOOR FROM OUTSIDE:
1. HOLD KNEE AGAINST LOWER
PORTION OF DOOR.
2. PUSH IN EXTERIOR OVERWING
EMERGENCY EXIT PUSH PANEL.
3. DOOR OPENS OUT AND UP
AUTOMATICALLY.
CUT-IN AREAS
CAUTION:
Make Sure Al l Per sons and
Eq uip me nt Are Cle ar of th e Doo r.
Do No t Ope n the Do or Wh en the
Air p lan e I s Pr e ss u ris e d.
Rem ove Class Divi der and Al l
L oo s e I t ems W it hin St o ra ge Bins
Be for e O pe nin g Car go Do or .
Car g o Doo r Mo ve me nt Ca n
Cause Injur y to Per sons and
Damage Equipment.
Loose Items Can Fall and
Cause Injur y.
TO OPEN CARGO DOOR:
1. UNLOCK THE EXT. DOOR
HANDLE.
2. VERIFY UNLOCKED LIGHT
IS ON.
3. HOLD THE UP TO CANOPY
SWITCH IN POSITION UNTIL
DOOR MOTION STOPS.
NOTE:
WARNING: 737-600/700/800/900 MODELS HAVE A SPRING LOADED
UPWARD SWINGING OVERWING EXIT DOOR IN LIEU OF A HATCH.
FOLLOW THE OPENING PROCEDURE INDICATED ABOVE TO AVOID
INJURY.
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE
AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS
BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
737-600/700/800/900/ER/BBJ/BBJ-2
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE
WINGLETS
(AS INSTALLED)
3 AFT SERVICE DOOR
4 EMERGENCY OVERWING
EXIT DOORS (ALL)
CARGO DOOR (RIGHT SIDE)
OPERATING INSTRUCTIONS ON
DOOR
4 EMERGENCY OVERWING
EXIT DOORS (-800, -900)
2 AFT ENTRY DOOR
6 CUT-IN AREAS
6 CUT-IN AREAS
CARGO DOOR ( RIGHT SIDE)
OPERATING INSTRUCTIONS ON
DOOR
WINGLETS
(AS INSTALLED)
3 FWD SERVICE DOOR
5 CARGO DOOR
(737-700C)
1 PILOT’S SLIDING WINDOWS
(AS INSTALLED)
2 FWD ENTRY DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
6 CUT-IN AREAS LOCATED
BETWEEN WING FRONT SPAR
AND ESCAPE HATCH (THREE
BAYS) BELOW WINDOWS AND
ABOVE FLOORS
WHEELS RETRACTED: 5: FT
WHEELS EXTENDED: 8 FT 6 IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATION
737-600/700/800/900/ER/BBJ/BBJ-2
BATTERY (-600, -700, -800, -900, ER,
BBJ, BBJ-2)
ACCESSIBLE FROM FORWARD
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
737-600/700/800/900/ER/BBJ/BBJ-2 FLIGHT DECK CNTRL SWITCH LOCATIONS
APU
APU
OFF
OR
OFF
DELAY
OFF
ON
START
ON
START
BATTERY SWITCH
- LIFT GUARD
- SWITCH - OFF
APU MASTER
SWITCH - OFF
THRUST LEVERS - RETARD
APU FIRE SWITCH - PULL
START LEVERS CUTOFF
IDLE
CUTOFF
1
2
ENGINE FIRE SWITCHES - PULL
(IF NOT ILLUMINATED, PUSH AND HOLD THE BUTTON
UNDER THE SWITCH TO RELEASE.)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
737-600/700/800/900/ER/BBJ/BBJ-2
VERTICAL STABILIZER TIP
VERTICAL STABILIZER
TRAILING EDGE
RUDDER
WINGLETS
(As installed)
TAILCONE
ASSEMBLY
UPPER WING FIXED
TRAILING EDGE
PANELS
ELEVATOR TAB
STRUCTURE
UPPER WING FIXED
LEADING EDGE
PANELS
ELEVATOR UPPER
AND LOWER SKIN
DORSAL
FIN SKIN
NACELLE STRUT
FAIRING
WING TRAILING EDGE
MAIN FLAP ASSEMBLY
WINGLETS
(As installed)
RADOME
AILERONS/TAB SKIN
AND STRUCTURE
THRUST REVERSER
LOWER WING FIXED
LEADING EDGE
PANELS
NOSE LANDING
GEAR DOORS
LOWER WING FIXED
TRAILING EDGE
PANELS
FLAP TRACK
FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.1.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
AUX TANK CAPACITIES
737-600/700/800/900/ER/BBJ/BBJ-2
AUX FUEL
CELLS
3 AFT
GALLONS
LITERS
TOTAL
GALLONS
(ALL TANKS)
TOTAL
LITERS
(ALL TANKS)
3 AFT
1,485
5,685
8,360
31,710
4 AFT
2,010
7,676
8,885
33,701
3 AFT - 1 FWD
2,000
7,639
8,875
33,664
3 AFT - 2 FWD
2,530
9,647
9,405
35,672
4 AFT - 2 FWD
3,055
11,639
9,930
37,664
5 AFT - 2 FWD
3,360
12,797
10,235
38,822
5 AFT - 3 FWD
3,605
13,727
10,480
39,752
5 AFT - 4 FWD
3,850
14,656
10,725
40,681
5 AFT/3 FWD
3 AFT/1 FWD
4 AFT
5 AFT 4 FWD
3 AFT/2 FWD
4 AFT/2 FWD
5 AFT/2 FWD
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
737.1.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
737-600/700/800/900/ER/BBJ/BBJ-2
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
737.1.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-100 & 200/-100 & 200 COMBI
FLAMMABLE MATERIAL LOCATIONS
747 (tab)
PORTABLE OXYGEN BOTTLES
8 PLACES UNDER FIRST OUTBOARD
SEAT FORWARD OF DOOR
SURGE TANK
APU
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
788 GAL 2983 L
534
FUEL TANK
4482 GAL
- 16966 L
APU FUEL LINE
FUEL TANKS
PORTABLE OXYGEN BOTTLES 2 PLACES
UNDER FLIGHT ATTENDANT SEAT AFT OF
DOOR
12546 GAL
- 47492 L
SIDE CARGO DOOR (COMBI)
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
-100 13200 GAL 49967 L
-200 17164 GAL 64973 L
FUEL TANKS
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
12546 GAL - 47492 L
4482 GAL - 16966 L
534
SURGE TANK
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
PORTABLE OXYGEN BOTTLE ON
FWD CARGO COMPARTMENT CEILING
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-100 & 200/-100 & 200 COMBI
1 ENTRY DOORS (10) EXTERNAL HANDLE
HANDLE RELEASE
BUTTON
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
2 UPPER DECK CREW DOOR EXTERNAL HANDLE
(AS INSTALLED)
BUTTERFLY
BUTTERFLY WITH
SLIDE DISARM
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TEE
SLIDE DISARM HANDLE
TO OPEN DOOR:
1. DISARM SLIDE (ONLY REQUIRED ON BUTTERFLY WITH SLIDE DISARM)
2. PULL HANDLE FROM RECESS AND ROTATE 180° IN DIRECTION OF “OPEN” ARROW.
3. SLIDE DOOR AFT.
NOTE: THE ESCAPE SLIDE WILL REMAIN IN THE DOORWAY.
3 CREW OVERHEAD ESCAPE HATCH
EXTERNAL HANDLE
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT
FROM RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-100 & 200/-100 & 200 COMBI
EMERGENCY RESCUE ACCESS-2
2” WIDE BAND OF CONTRASTING
COLOR INDICATING DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
SIDE CARGO DOOR
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOORS (10)
C
D
A
B
2 UPPER DECK CREW DOOR
RH SIDE - STANDARD INSTALLATION
LH SIDE - AS INSTALLED
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-100 & 200/-100 & 200 COMBI
ACCESS DOOR
MAIN BATTERY
APU BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-100 & 200/-100 & 200 COMBI FLIGHT DECK CONTROL SWITCH LOCATIONS
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
WHEEL WELL FIRE DET
TEST
FIRE
WHEEL
WELL
PULL
PULL
APU
FIRE
120
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
80
PULL
DISCHARGE DISCHARGE
60
40
SQUIB
OK
3
OIL
QTY
2
1
10
EGT
6
C X 100
2
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
NOTE:
RPM
%
100
PULL
DISCHARGE DISCHARGE
FIRE
SMOKE
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-100 & 200/-100 & 200 COMBI
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-200 SPECIAL FREIGHTER
FLAMMABLE MATERIAL LOCATIONS
SURGE TANK
APU
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
788 GAL 2983 L
534
FUEL TANK
4482 GAL
- 16966 L
APU FUEL LINE
FUEL TANKS
12546 GAL
- 47492 L
SIDE CARGO DOOR
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
FUEL TANKS
17164 GAL 64973 L
12546 GAL - 47492 L
4482 GAL - 16966 L
534
SURGE TANK
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
PORTABLE OXYGEN BOTTLE ON
FWD CARGO COMPARTMENT CEILING
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-200 SPECIAL FREIGHTER
1 ENTRY DOORS (10) EXTERNAL HANDLE
HANDLE RELEASE
BUTTON
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
2 UPPER DECK CREW DOOR EXTERNAL HANDLE
(AS INSTALLED)
BUTTERFLY
BUTTERFLY WITH
SLIDE DISARM
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TEE
SLIDE DISARM HANDLE
TO OPEN DOOR:
1. DISARM SLIDE (ONLY REQUIRED ON BUTTERFLY WITH SLIDE DISARM)
2. PULL HANDLE FROM RECESS AND ROTATE 180° IN DIRECTION OF “OPEN” ARROW.
3. SLIDE DOOR AFT.
NOTE: THE ESCAPE SLIDE WILL REMAIN IN THE DOORWAY.
3 CREW OVERHEAD ESCAPE HATCH
EXTERNAL HANDLE
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT
FROM RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-200 SPECIAL FREIGHTER
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
1 ENTRY DOOR (5L)
SIDE CARGO DOOR
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOORS (10)
C
D
A
B
2 UPPER DECK CREW DOOR
RH SIDE - STANDARD INSTALLATION
LH SIDE - AS INSTALLED
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-200 SPECIAL FREIGHTER
ACCESS DOOR
MAIN BATTERY
APU BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-200 SPECIAL FREIGHTER
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
FIRE
WHEEL WELL FIRE DET
TEST
WHEEL
WELL
PULL
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
APU
FIRE
FIRE
120
SMOKE
PULL
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
80
PULL
DISCHARGE DISCHARGE
60
40
SQUIB
OK
3
OIL
QTY
2
1
10
EGT
6
C X 100
2
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
NOTE:
RPM
%
100
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-200 SPECIAL FREIGHTER
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.1.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-300 & 300 COMBI SERIES
FLAMMABLE MATERIAL LOCATIONS
SURGE TANK
APU
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
788 GAL 2983 L
FUEL TANK
534
FUEL TANK
4482 GAL
- 16966 L
APU FUEL LINE
FUEL TANKS
12546 GAL
- 47492 L
SIDE CARGO DOOR (COMBI)
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
FUEL TANKS
17164 GAL 64973 L
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
12546 GAL - 47492 L
4482 GAL - 16966 L
534
SURGE TANK
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
PORTABLE OXYGEN BOTTLE ON
FWD CARGO COMPARTMENT CEILING
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.2.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-300 & 300 COMBI SERIES
1 ENTRY DOORS (10) EXTERNAL HANDLE
HANDLE RELEASE
BUTTON
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 UPPER DECK EMERGENCY DOORS (2)
TO OPEN DOOR:
1. PUSH OUTSIDE DISARM LEVER.
2. LIFT DOOR HANDLE.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND
DISENGAGES THE EMERGENCY POWER SYSTEM.
NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR
AND AFT OF THE RH DOOR.
3. OPEN CONTROL ACCESS COVER
4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN.
EMER
DOOR
OPEN
CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL
OPEN RAPIDLY AND CANNOT BE STOPPED.
OFF
DOOR
OPEN
DOOR
CLOSE
PULL
PUSH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.2.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-300 & 300 COMBI SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
SIDE CARGO DOOR
3 UPPER DECK
EMERGENCY
DOORS (2)
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOORS (10)
C
D
B
A
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK EMERGENCY DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.2.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-300 & 300 COMBI SERIES
APU BATTERY
ACCESS DOOR
MAIN BATTERY
APU BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.2.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-300 & 300 COMBI SERIES
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
FIRE
WHEEL WELL FIRE DET
TEST
WHEEL
WELL
PULL
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
APU
FIRE
FIRE
120
SMOKE
PULL
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
80
PULL
DISCHARGE DISCHARGE
60
40
SQUIB
OK
3
OIL
QTY
2
1
10
EGT
6
C X 100
2
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
NOTE:
RPM
%
100
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.2.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-300 & 300 COMBI SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.2.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-300 SPECIAL FREIGHTER
FLAMMABLE MATERIAL LOCATIONS
SURGE TANK
APU
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
788 GAL 2983 L
FUEL TANK
534
FUEL TANK
4482 GAL
- 16966 L
APU FUEL LINE
FUEL TANKS
12546 GAL
- 47492 L
SIDE CARGO DOOR (COMBI)
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
FUEL TANKS
17164 GAL 64973 L
12546 GAL - 47492 L
4482 GAL - 16966 L
534
SURGE TANK
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
PORTABLE OXYGEN BOTTLE ON
FWD CARGO COMPARTMENT CEILING
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.3.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-300 SPECIAL FREIGHTER
1 ENTRY DOORS EXTERNAL HANDLE (2)
HANDLE RELEASE
BUTTON
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 UPPER DECK EMERGENCY DOORS (2)
TO OPEN DOOR:
1. PUSH OUTSIDE DISARM LEVER.
2. LIFT DOOR HANDLE.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND
DISENGAGES THE EMERGENCY POWER SYSTEM.
NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR
AND AFT OF THE RH DOOR.
3. OPEN CONTROL ACCESS COVER
4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN.
EMER
DOOR
OPEN
CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL
OPEN RAPIDLY AND CANNOT BE STOPPED.
OFF
DOOR
OPEN
DOOR
CLOSE
PULL
PUSH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.3.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-300 SPECIAL FREIGHTER
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
1 ENTRY DOOR (5L)
SIDE CARGO DOOR
3 UPPER DECK
EMERGENCY
DOORS (2)
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOOR (1L)
C
D
B
A
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK EMERGENCY DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.3.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-300 SPECIAL FREIGHTER
APU BATTERY
ACCESS DOOR
MAIN BATTERY
APU BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.3.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-300 SPECIAL FREIGHTER
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
FIRE
WHEEL WELL FIRE DET
TEST
WHEEL
WELL
PULL
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
APU
FIRE
FIRE
120
SMOKE
PULL
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
80
PULL
DISCHARGE DISCHARGE
60
40
SQUIB
OK
3
OIL
QTY
2
1
10
EGT
6
C X 100
2
OPTIONAL LOCATION
FOR T-HANDLES IS ON
THE PILOTS’ LIGHT
SHIELD
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
NOTE:
RPM
%
100
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.3.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-300 SPECIAL FREIGHTER
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.3.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 SP SERIES
FLAMMABLE MATERIAL LOCATIONS
OPTIONAL FUEL TANK
SURGE TANK
FUEL VENT AND
OVERFLOW
(BENEATH WING)
PORTABLE OXYGEN BOTTLES
8 PLACES UNDER FIRST OUTBOARD
SEAT FORWARD OF DOOR
788 GAL 2983 L
APU
534
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
FUEL TANK
4482 GAL
- 16966 L
FUEL TANK
FUEL TANKS
12546 GAL
- 47492 L
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
PORTABLE OXYGEN BOTTLE ON
UPPER DECK IN LH WALL AT TOP
OF STAIRS
APU FUEL LINE
PORTABLE OXYGEN BOTTLES 2
PLACES ON WALL
FUEL TANKS
-100 13200 GAL 49967 L
OPTIONAL FUEL TANK
12546 GAL - 47492 L
4482 GAL - 16966 L
534
PORTABLE OXYGEN SYSTEM BOTTLES ON
FWD CARGO COMPARTMENT
CEILING 3 TO 9 BOTTLES
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
FUEL VENT AND
OVERFLOW
(BENEATH WING)
SURGE TANK
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.4.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747 SP SERIES
1 ENTRY DOORS EXTERNAL HANDLE (8)
HANDLE RELEASE
BUTTON
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
2 UPPER DECK CREW DOOR EXTERNAL HANDLE
(AS INSTALLED)
BUTTERFLY
BUTTERFLY WITH
SLIDE DISARM
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TEE
SLIDE DISARM HANDLE
TO OPEN DOOR:
1. DISARM SLIDE (ONLY REQUIRED ON BUTTERFLY WITH SLIDE DISARM)
2. PULL HANDLE FROM RECESS AND ROTATE 180° IN DIRECTION OF “OPEN” ARROW.
3. SLIDE DOOR AFT.
NOTE: THE ESCAPE SLIDE WILL REMAIN IN THE DOORWAY.
3 CREW OVERHEAD ESCAPE HATCH
EXTERNAL HANDLE
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT
FROM RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.4.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747 SP SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOOR (8)
C
D
2 UPPER DECK CREW DOOR
RH SIDE - STANDARD INSTALLATION
LH SIDE - AS INSTALLED
B
A
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.4.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747 SP SERIES
ACCESS DOOR
APU BATTERY
APU BATTERY
MAIN BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.4.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747 SP SERIES
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
FIRE
WHEEL WELL FIRE DET
TEST
WHEEL
WELL
PULL
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
APU
FIRE
FIRE
120
SMOKE
RPM
%
PULL
80
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
100
60
40
OIL
QTY
1
10
EGT
6
C X 100
2
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
SQUIB
OK
3
2
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.4.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 SP SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.4.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
SURGE TANK
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
FUEL TANK
APU
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
788 GAL 2983 L
534
FUEL TANK
4482 GAL
- 16966 L
APU FUEL LINE
FUEL TANKS
12546 GAL
- 47492 L
SIDE CARGO DOOR (COMBI)
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
FUEL TANKS
17164 GAL 64973 L
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
12546 GAL - 47492 L
4482 GAL - 16966 L
534
SURGE TANK
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
PORTABLE OXYGEN BOTTLE ON
FWD CARGO COMPARTMENT CEILING
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
788 GAL - 2983 L
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.5.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 FREIGHTER SERIES
HANDLE RELEASE
BUTTON
1 ENTRY DOORS EXTERNAL
HANDLE (2)
EMERGENCY RESCUE ACCESS-1
2 UPPER DECK CREW DOOR EXTERNAL
HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD.
NOTE: ON FREIGHTERS AND SPECIAL
FREIGHTERS, THERE SHOULD BE NO
PERSONNEL ON THE MAIN DECK DURING TAXI,
TAKEOFF OR LANDING AND THE MAIN DOORS
ARE NOT CERTIFIED AS EMERGENCY EXITS.
THE EMERGENCY POWER ASSIST SYSTEM AND
THE ESCAPE SLIDES ARE NOT INSTALLED.
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS AND ROTATE 180° IN
DIRECTION OF “OPEN” ARROW.
2. SLIDE DOOR AFT.
NOTE: THE ESCAPE SLIDE WILL REMAIN IN THE DOORWAY.
3 CREW OVERHEAD ESCAPE HATCH
EXTERNAL HANDLE
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT
IS RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES
AND DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE
(HANDLE WILL SPRING OUT FROM RECESS
APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.5.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
1 ENTRY DOOR (5L)
SIDE CARGO DOOR
3 CREW OVERHEAD
ESCAPE HATCH
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
2 UPPER DECK CREW DOOR
RH SIDE ONLY
1 ENTRY DOOR (1L)
C
D
A
B
E
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.5.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747 FREIGHTER SERIES
APU BATTERY
ACCESS DOOR
MAIN BATTERY
APU BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.5.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747 FREIGHTER SERIES
ENGINE FIRE T-HANDLES - PULL
APU FIRE T-HANDLE - PULL
FIRE
FIRE
WHEEL WELL FIRE DET
TEST
WHEEL
WELL
PULL
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
APU
FIRE
FIRE
120
SMOKE
RPM
%
PULL
80
PULL
DISCHARGE DISCHARGE
DISCHARGE DISCHARGE
L BTL R BTL
PUSH PUSH
L BTL R BTL
PUSH PUSH
0
20
100
60
40
OIL
QTY
1
10
EGT
6
C X 100
2
FIRE
SQUIB TEST
U S QTS
APU
0
FIRE DET
FUEL
VALVE BLEED AIR
OPEN
DC PUMP
ON
APU
FAULT
CLOSE
APU
DOOR
A
START
ON
STOP
PULL
A
APU
8
4
SQUIB
OK
3
2
B
A
B
FIRE TEST
B
O
T
H
FAULT TEST
B
BTL
PUSH
APU MASTER SWITCH - STOP
THRUST LEVERS - RETARD
40
30
100
50 150
+
DC
0
AMPS
50 150
100
DC
VOLTS
20 10
0
DC METERS
BATTERY
ON
ON
APU
BATT
ON
ON
ESS
TR
ON
BATT
ON
OFF
TR 1
TR 2
TR 3
ON
BATTERY SWITCH
- LIFT GUARD
ENGINE START
LEVERS - CUTOFF
- SWITCH OFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.5.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 FREIGHTER SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.5.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 & 400 COMBI SERIES
CAUTION: Rescue crews wearing full PPE to
include SCBA’s must use caution
when moving across sections of
aircraft that have been exposed to
fatigue or fire as the result of an
accident. Crews need to verify the
integrity of the surface area before
moving their weight and equipment
across it. Signs could include but are
not limited to deformity of structure,
visual signs of flame impingement or
uneven surfaces. Surface integrity
can be checked with a pike pole, axe
or any instrument used to sound
surfaces for integrity.
FLAMMABLE MATERIAL LOCATIONS
FUEL VENT AND OVERFLOW
(BENEATH WING)
SURGE TANKS
HORIZONTAL STABILIZER
FUEL TANK AS INSTALLED,
PASSENGER MODELS ONLY
FUEL TANK
2644 GAL 10009 L
HYDRAULIC
ACCUMULATORS
IN RIGHT BODY
WHEEL WELL
8964 GAL 33932 L
PORTABLE OXYGEN
BOTTLES IN 8 PLACES
UNDER OUTBOARD SEAT
FORWARD OF DOOR IF
PASSENGER AREA
OTHERWISE 6 PLACES
APU
3300 GAL 12492 L
FUEL TANK
APU FUEL LINE
PORTABLE OXYGEN BOTTLES IN 2
PLACES AFT SIDE EACH CLOSET
WALL IF USED FOR PASSENGER
AREA
FUEL TANKS
UPPER DECK
PORTABLE OXYGEN
BOTTLES AT OUTBD
LEFT AND RIGHT
ATT. STA.
CREW OXYGEN
SYSTEM BOTTLE IN
FWD CARGO
COMPARTMENT
25092 GAL 94983 L
SIDE CARGO DOOR ON COMBI
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
17164 GAL 64973 L
FUEL TANKS
SURGE TANK
25092 GAL - 94983 L
8964 GAL - 33932 L
2644 GAL - 10009 L
FUEL TANK
FUEL VENT AND
OVERFLOW
(BENEATH WING)
(AS INSTALLED)
-400 3210 GAL - 12151 L
PASSENGER OXYGEN SYSTEM
BOTTLES ON FWD CARGO
COMPARTMENT WALL
IMMEDIATELY AFT OF DOOR
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when apporaching
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
hot brakes or fighting a wheel fire, as rims and tires may pose a fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.6.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-400 & 400 COMBI SERIES
1 ENTRY DOORS EXTERNAL HANDLE (10)
HANDLE RELEASE
BUTTON
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 UPPER DECK EMERGENCY DOORS (2)
TO OPEN DOOR:
1. PUSH OUTSIDE DISARM LEVER.
2. LIFT DOOR HANDLE.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND
DISENGAGES THE EMERGENCY POWER SYSTEM.
NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR
AND AFT OF THE RH DOOR.
3. OPEN CONTROL ACCESS COVER
4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN.
EMER
DOOR
OPEN
CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL
OPEN RAPIDLY AND CANNOT BE STOPPED.
OFF
DOOR
OPEN
DOOR
CLOSE
PULL
PUSH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.6.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 & 400 COMBI SERIES
EMERGENCY RESCUE ACCESS-2
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
SIDE CARGO DOOR ON COMBI
3 UPPER DECK
EMERGENCY DOORS (2)
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOORS (10)
C
D
B
E
A
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK EMERGENCY DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.6.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 & 400 COMBI SERIES
EMERGENCY RESCUE ACCESS-3
ON PASSENGER AIRCRAFT ONLY, DOOR
5R ALLOWS ACCESS TO THE OVERHEAD
CREW REST AREA. THE OVERHEAD CREW
REST AREA MAY BE OCCUPIED AND MUST
BE CHECKED FOR TRAPPED AND/OR
INJURED PEOPLE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.6.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 & 400 COMBI SERIES
EMERGENCY RESCUE ACCESS-4
FWD
STAIR ACCESS AT DOOR 5LFT
AFT OVERHEAD FLIGHT CREW REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.6.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-400 & 400 COMBI SERIES
APU BATTERY
MAIN BATTERY
ACCESS DOOR
NOSE GEAR COMPARTMENT
INBD
FWD
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.6.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-400 & 400 COMBI SERIES
ENGINE FIRE T-HANDLES - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
APU SELECTOR ROTATE OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
L
STANDBY POWER
AUTO
BAT
OFF
UTILITY
R
ON
ON
OFF
OFF
OFF
APU
ON
DISCH
A
B
DISCH
B
A
DISCH
A
B
DISCH
B
A
1
2
3
4
BTL A
DISCH
START
BATTERY
EXT PWR 1
A
V
A
I
L
ON
APU GEN 1
A
V
A
I
L
AUTO
AUTO
ISLN
ISLN
BUS
ON
APU GEN 2
A
V
A
I
L
OFF
ON
BUS
TIE
AUTO
A
V
A
I
L
ON
ON
ON
OFF
1
2
DRIVE
1
GEN
CONT
DRIVE
DISC
RUN
APU
BTL A BTL B
DISCH DISCH
CARGO FIRE
DISCH
MAIN
ARMED
FWD
ARMED
FWD
AFT
AFT
ARMED
DISCH
AFT
APU SWITCH - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
ISLN
BUS
OFF
DISCH
EXT PWR 2
APU BTL
DISCH
AUTO
ISLN
BUS
DRIVE
ON
BTL B
DISCH
MAIN DECK EXTINGUISHERS AVAILABLE ON -400 COMBI VERSION
BUS
ON
ON
OFF
OFF
3
4
DRIVE
DRIVE
FUEL CONTROL
2
3
THRUST LEVERS - RETARD
RUN
4
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
CUTOFF
CUTOFF
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.6.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 & 400 COMBI SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.6.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-400 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
SURGE TANKS
APU
FUEL VENT AND
OVERFLOW
(BENEATH WING)
1635 GAL 6189 L
FUEL TANK
5550 GAL 21009 L
HYDRAULIC
ACCUMULATORS
IN RIGHT BODY
WHEEL WELL
FUEL TANK
APU FUEL LINE
FUEL TANKS
14550 GAL 55078 L
SIDE CARGO DOOR
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
CREW OXYGEN
SYSTEM BOTTLE IN
FWD CARGO
COMPARTMENT
FUEL TANKS
SURGE TANK
17164 GAL - 64973 L
14550 GAL - 55078 L
5550 GAL - 21009 L
1635 GAL - 6189 L
FUEL VENT AND
OVERFLOW
(BENEATH WING)
FLIGHT DECK PORTABLE
OXYGEN BOTTLE
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
pole, axe or any instrument used to sound surfaces for integrity.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.7.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-400 FREIGHTER SERIES
1 ENTRY DOORS EXTERNAL HANDLE (2)
HANDLE RELEASE
BUTTON
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 UPPER DECK EMERGENCY DOOR
TO OPEN DOOR:
1. PUSH OUTSIDE DISARM LEVER.
2. LIFT DOOR HANDLE.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND
DISENGAGES THE EMERGENCY POWER SYSTEM.
NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR
AND AFT OF THE RH DOOR.
3. OPEN CONTROL ACCESS COVER
4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN.
EMER
DOOR
OPEN
CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL
OPEN RAPIDLY AND CANNOT BE STOPPED.
OFF
DOOR
OPEN
DOOR
CLOSE
PULL
PUSH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.7.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-400 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
MAIN DECK TO UPPER
DECK LADDER
SIDE CARGO DOOR ON COMBI
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 UPPER DECK CREW DOOR
RH SIDE ONLY
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOOR (1L)
C
D
E
A B
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.7.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-400 FREIGHTER SERIES
APU BATTERY
MAIN BATTERY
ACCESS DOOR
NOSE GEAR COMPARTMENT
INBD
FWD
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.7.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-400 FREIGHTER SERIES
ENGINE FIRE T-HANDLES - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
APU SELECTOR ROTATE OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
L
STANDBY POWER
AUTO
BAT
OFF
DISCH
A
B
DISCH
B
A
1
UTILITY
R
ON
ON
OFF
OFF
OFF
APU
ON
2
BTL A
DISCH
START
A
V
A
I
L
APU GEN 1
ON
A
V
A
I
L
A
V
A
I
L
OFF
ON
AUTO
AUTO
ISLN
ISLN
BUS
APU GEN 2
ON
BUS
TIE
AUTO
ON
ON
ON
OFF
1
2
DRIVE
DRIVE
DISC
BTL A
DISCH
BTL B
DISCH
APU
BTL B
DISCH
CARGO FIRE
MAIN
ARMED
FWD
ARMED
AFT
MAIN DECK EXTINGUISHERS AVAILABLE ON FREIGHTER VERSION
DISCH
AFT
ARMED
DEPRESS
DISCH
AFT
APU SWITCH - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
BUS
ON
ON
OFF
OFF
3
4
DRIVE
DRIVE
GEN
CONT
4
FWD
ISLN
BUS
OFF
DISCH
EXT PWR 2
A
V
A
I
L
3
AUTO
ISLN
BUS
DRIVE
ON
DISCH
B
A
APU BTL
DISCH
BATTERY
EXT PWR 1
DISCH
A
B
THRUST LEVERS - RETARD
FUEL CONTROL
1
RUN
2
3
RUN
4
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
CUTOFF
CUTOFF
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.7.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
747-400 FREIGHTER SERIES
TIP FAIRING
RUDDER
VERTICAL STABILIZER
TRAILING EDGE PANELS
UPPER WING
LEADING EDGE
VERTICAL STABILIZER
FORWARD TORQUE BOX
ELEVATORS
AILERONS
ENGINE
PYLONS
STABILIZER TIP
SPOILERS
INLET, FAN, AND
REVERSER COWLS
WINGLETS
(-400 ONLY)
UPPER WING
TRAILING EDGE
RADOME
WING TO BODY
FAIRING
LOWER WING
TRAILING EDGE
LOWER WING
LEADING EDGE
FLAP TRACK FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.7.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 LARGE CARGO FREIGHTER
FLAMMABLE MATERIAL LOCATIONS
SURGE TANK
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
635 GAL 4254 L
FUEL TANK
HYDRAULIC ACCUMULATORS
(RIGHT WHEEL WELL AREA)
3080 GAL
- 20636 L
FUEL TANKS
CREW OXYGEN SYSTEM
BOTTLE IN FWD CARGO
COMPARTMENT
FUEL TANK
12546 GAL
- 47492 L
FUEL TANKS
-100 13200 GAL 49967 L
-200 17164 GAL 64973 L
FUEL VENT AND
OVERFLOW LOCATED
BENEATH WING
12546 GAL - 47492 L
3080 GAL - 20636 L
635 GAL - 4254 L
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
ENGINE OIL TANK FORWARD RIGHT SIDE
OR REAR LEFT SIDE
OF EACH ENGINE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure,
visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
with a pike pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANK
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the temperature
is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.8.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 LARGE CARGO FREIGHTER
EMERGENCY RESCUE ACCESS-1
1 ENTRY DOORS EXTERNAL HANDLE (2)
HANDLE RELEASE
BUTTON
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.8.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 LARGE CARGO FREIGHTER
EMERGENCY RESCUE ACCESS-2
MAIN DECK TO UPPER
DECK LADDER
2 CREW OVERHEAD
ESCAPE HATCH
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
1 ENTRY DOOR (1L)
B
C
B) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D
C) ENTRY DOOR HANDLE
A
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
D) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.8.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747 LARGE CARGO FREIGHTER
STANDBY BATTERY
MAIN BATTERY
ACCESS DOOR
INBD
FWD
NOSE GEAR COMPARTMENT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.8.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747 LARGE CARGO FREIGHTER FLIGHT DECK CONTROL SWITCH LOCATIONS
ENGINE FIRE T-HANDLES - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
APU SELECTOR ROTATE OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
L
STANDBY POWER
AUTO
BAT
OFF
DISCH
A
B
DISCH
B
A
1
UTILITY
R
ON
ON
OFF
OFF
OFF
APU
ON
2
BTL A
DISCH
START
BTL B
DISCH
DISCH
A
B
DISCH
B
A
3
4
BTL A
DISCH
BTL B
DISCH
BATTERY
EXT PWR 1
A
V
A
I
L
APU GEN 1
ON
A
V
A
I
L
AUTO
AUTO
ISLN
ISLN
BUS
APU GEN 2
ON
A
V
A
I
L
OFF
ON
BUS
TIE
AUTO
EXT PWR 2
A
V
A
I
L
ON
AUTO
ISLN
BUS
ISLN
BUS
ON
ON
OFF
OFF
1
2
DRIVE
ON
DRIVE
DRIVE
DISC
BUS
ON
ON
OFF
OFF
3
4
DRIVE
DRIVE
GEN
CONT
THRUST LEVERS - RETARD
FUEL CONTROL
1
RUN
2
3
RUN
4
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
CUTOFF
CUTOFF
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.8.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
747 LARGE CARGO FREIGHTER
TIP FAIRING
RUDDER
UPPER WING
LEADING EDGE
ENGINE
PYLONS
VERTICAL STABILIZER
TRAILING EDGE PANELS
VERTICAL STABILIZER
FORWARD TORQUE BOX
AILERONS
ELEVATORS
SPOILERS
STABILIZER TIP
INLET, FAN, AND
REVERSER COWLS
UPPER WING
TRAILING EDGE
RADOME
WING TO BODY
FAIRING
LOWER WING
TRAILING EDGE
LOWER WING
LEADING EDGE
FLAP TRACK FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.8.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-8 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
APU
SURGE TANKS
FUEL VENT AND
OVERFLOW
(BENEATH WING)
1635 GAL 6189 L
HYDRAULIC
ACCUMULATORS
IN RIGHT BODY
WHEEL WELL
FUEL TANK
APU FUEL LINE
FUEL TANK
5550 GAL 21009 L
FUEL TANKS
SIDE CARGO DOOR
12546 GAL 47492 L
CREW OXYGEN
SYSTEM BOTTLE IN
FWD CARGO
COMPARTMENT
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
FUEL TANKS
SURGE TANK
17164 GAL 64973 L
12546 GAL - 47492 L
4482 GAL - 16966 L
1322 GAL - 5004 L
FUEL VENT AND
OVERFLOW
(BENEATH WING)
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
FLIGHT DECK PORTABLE OF EACH ENGINE
OXYGEN BOTTLE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
pole, axe or any instrument used to sound surfaces for integrity.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.9.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-8 FREIGHTER SERIES
1 ENTRY DOORS EXTERNAL HANDLE (2)
HANDLE RELEASE
BUTTON
EMERGENCY RESCUE ACCESS-1
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.9.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-8 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
ACCESS DOOR Right Side
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
MAIN DECK TO UPPER
DECK LADDER
SIDE CARGO DOOR
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 UPPER DECK CREW DOOR
RH SIDE ONLY
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOOR (1L)
C
D
E
A
B
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.9.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-8 FREIGHTER SERIES
APU BATTERY
MAIN BATTERY
ACCESS DOOR
INBD
FWD
NOSE GEAR COMPARTMENT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.9.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-8 FREIGHTER SERIES
ENGINE FIRE T-HANDLES - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
APU SELECTOR ROTATE OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
L
STANDBY POWER
AUTO
BAT
OFF
DISCH
A
B
DISCH
B
A
1
UTILITY
R
ON
ON
OFF
OFF
OFF
APU
ON
2
A
V
A
I
L
ON
APU GEN 1
A
V
A
I
L
ON
A
V
A
I
L
OFF
ON
AUTO
AUTO
ISLN
ISLN
BUS
APU GEN 2
BUS
TIE
AUTO
ON
ON
ON
OFF
1
2
DRIVE
DRIVE
DISC
FWD
ARMED
AFT
DISCH
AFT
ARMED
DISCH
AFT
APU SWITCH - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
BUS
ON
ON
OFF
OFF
3
4
DRIVE
DRIVE
GEN
CONT
APU
MAIN DECK EXTINGUISHERS AVAILABLE ON FREIGHTER VERSION
CARGO FIRE
MAIN
ARMED
FWD
ISLN
BUS
OFF
DISCH
EXT PWR 2
A
V
A
I
L
4
AUTO
ISLN
BUS
DRIVE
ON
3
APU BTL
DISCH
BATTERY
EXT PWR 1
DISCH
B
A
BTL A BTL B
DISCH DISCH
BTL A BTL B
DISCH DISCH
START
DISCH
A
B
THRUST LEVERS - RETARD
FUEL CONTROL
1
RUN
CUTOFF
2
3
RUN
4
CUTOFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.9.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
747-8 FREIGHTER SERIES
TIP FAIRING
RUDDER
UPPER WING
LEADING EDGE
VERTICAL STABILIZER
TRAILING EDGE PANELS
VERTICAL STABILIZER
FORWARD TORQUE BOX
ELEVATORS
AILERONS
ENGINE
PYLONS
STABILIZER TIP
SPOILERS
INLET, FAN, AND
REVERSER COWLS
UPPER WING
TRAILING EDGE
RADOME
WING TO BODY
FAIRING
LOWER WING
TRAILING EDGE
LOWER WING
LEADING EDGE
FLAP TRACK FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.9.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
747-8I
FLAMMABLE MATERIAL LOCATIONS
SURGE TANKS
APU
FUEL VENT AND
OVERFLOW
(BENEATH WING)
3270 GAL 12378 L
HYDRAULIC
ACCUMULATORS
IN RIGHT BODY
WHEEL WELL
FUEL TANK
3300 GAL 12492 L
APU FUEL LINE
FUEL TANK
11102 GAL
- 42026 L
FUEL TANKS
29100 GAL 110155 L
CREW OXYGEN
SYSTEM BOTTLE IN
FWD CARGO
COMPARTMENT
HYDRAULIC RESERVOIR 4
PLACES ON ENGINE
STRUTS
FUEL TANKS
SURGE TANK
17164 GAL 64973 L
29100 GAL - 110155 L
11102 GAL - 42026 L
3270 GAL - 12378 L
FUEL VENT AND
OVERFLOW
(BENEATH WING)
ENGINE OIL TANK FORWARD RIGHT SIDE OR
REAR LEFT SIDE
FLIGHT DECK PORTABLE OF EACH ENGINE
OXYGEN BOTTLE
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
pole, axe or any instrument used to sound surfaces for integrity.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.10.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
747-8I
1 ENTRY DOORS EXTERNAL HANDLE (2)
HANDLE RELEASE
BUTTON
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
TO OPEN DOOR:
1. PUSH HANDLE RELEASE BUTTON AND
PULL HANDLE FROM RECESS.
2. ROTATE 180° IN DIRECTION OF “OPEN”
ARROW.
3. PULL DOOR OUTWARD
NOTE: OPENING A DOOR FROM THE OUTSIDE
DISENGAGES THE EMERGENCY EVACUATION
SYSTEM AND THE ESCAPE SLIDE WILL NOT
DEPLOY.
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM
RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180° CLOCKWISE.
3. PUSH HATCH INWARD.
3 UPPER DECK EMERGENCY DOOR
TO OPEN DOOR:
1. PUSH OUTSIDE DISARM LEVER.
2. LIFT DOOR HANDLE.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
NOTE: PUSHING IN THE DISARM LEVER DISARMS THE SLIDE AND
DISENGAGES THE EMERGENCY POWER SYSTEM.
NOTE: CONTROL ACCESS COVER FORWARD OF THE LH DOOR
AND AFT OF THE RH DOOR.
3. OPEN CONTROL ACCESS COVER
4. MOVE GUARDED EMERGENCY DOOR SWITCH TO OPEN.
EMER
DOOR
OPEN
CAUTION: STAND TO THE SIDE OF THE DOOR AS THE DOOR WILL
OPEN RAPIDLY AND CANNOT BE STOPPED.
OFF
DOOR
OPEN
DOOR
CLOSE
PULL
PUSH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.10.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
747-8I
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
ACCESS DOOR Right Side
4 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
APU ACCESS HATCH
APU EMERGENCY CONTROL PANEL
LOCATED ON RIGHT INBOARD MAIN
LANDING GEAR BULKHEAD
3 UPPER DECK CREW DOOR
RH SIDE ONLY
2 CREW OVERHEAD
ESCAPE HATCH
1 ENTRY DOOR (1L)
C
D
E
A
B
A) CONTROL CABIN/LOUNGE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 18 FT 4 IN. - WHEELS EXTENDED: 24 FT 6 IN.
B) UPPER DECK CREW DOOR HANDLE
WHEELS RETRACTED: 20 FT 4 IN. - WHEELS EXTENDED: 27 FT
C) PASSENGER CABIN FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT 10 IN. - WHEELS EXTENDED: 16 FT
D) ENTRY DOOR HANDLE
WHEELS RETRACTED: 13 FT - WHEELS EXTENDED: 19 FT 2 IN.
E) CREW OVERHEAD ESCAPE HATCH
WHEELS RETRACTED: 25 FT 10 IN. - WHEELS EXTENDED: 32 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.10.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
747-8I
APU BATTERY
MAIN BATTERY
ACCESS DOOR
INBD
FWD
NOSE GEAR COMPARTMENT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.10.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
747-8I
ENGINE FIRE T-HANDLES - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
APU SELECTOR ROTATE OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
L
STANDBY POWER
AUTO
BAT
OFF
DISCH
A
B
DISCH
B
A
1
UTILITY
R
ON
ON
OFF
OFF
OFF
APU
ON
2
A
V
A
I
L
ON
APU GEN 1
A
V
A
I
L
ON
A
V
A
I
L
OFF
ON
AUTO
AUTO
ISLN
ISLN
BUS
APU GEN 2
BUS
TIE
AUTO
ON
ON
ON
OFF
1
2
DRIVE
DRIVE
DISC
FWD
ARMED
AFT
DISCH
AFT
ARMED
DISCH
AFT
APU SWITCH - PULL
(IF NOT ILLUMINATED, MAY REQUIRE
PUSHING AND HOLDING THE BUTTON
UNDER THE SWITCH TO RELEASE)
BUS
ON
ON
OFF
OFF
3
4
DRIVE
DRIVE
GEN
CONT
APU
MAIN DECK EXTINGUISHERS AVAILABLE ON FREIGHTER VERSION
CARGO FIRE
MAIN
ARMED
FWD
ISLN
BUS
OFF
DISCH
EXT PWR 2
A
V
A
I
L
4
AUTO
ISLN
BUS
DRIVE
ON
3
APU BTL
DISCH
BATTERY
EXT PWR 1
DISCH
B
A
BTL A BTL B
DISCH DISCH
BTL A BTL B
DISCH DISCH
START
DISCH
A
B
THRUST LEVERS - RETARD
FUEL CONTROL
1
RUN
CUTOFF
2
3
RUN
4
CUTOFF
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
747.10.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
747-8I
TIP FAIRING
RUDDER
UPPER WING
LEADING EDGE
VERTICAL STABILIZER
TRAILING EDGE PANELS
VERTICAL STABILIZER
FORWARD TORQUE BOX
ELEVATORS
AILERONS
ENGINE
PYLONS
STABILIZER TIP
SPOILERS
INLET, FAN, AND
REVERSER COWLS
UPPER WING
TRAILING EDGE
RADOME
WING TO BODY
FAIRING
LOWER WING
TRAILING EDGE
LOWER WING
LEADING EDGE
FLAP TRACK FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
747.10.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 & 200 COMBI SERIES
FLAMMABLE MATERIAL LOCATIONS
757 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANKS
APU
HYDRAULIC RESERVOIR AND
ACCUMULATOR IN RIGHT
WHEEL WELL
CENTER FUEL TANK
RIGHT MAIN
FUEL TANK
APU FUEL LINE
2170 GAL 8214 L
HYDRAULIC RESERVOIR IN
LEFT WING FILLET
APU EMERGENCY
CONTROL PANEL
LOCATED ON THE
NOSE GEAR
6900 GAL 26119 L
LEFT MAIN FUEL TANKS
HYDRAULIC RESERVOIR IN
LEFT WHEEL WELL
SURGE TANK
2170 GAL - 8214 L
FLIGHT DECK PORTABLE
OXYGEN BOTTLE ON
BULKHEAD BEHIND
CAPTAIN
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
CREW OXYGEN BOTTLE IN
Water mist: Can be deployed from turret or handline.
RIGHT SIDE, FORWARD
Fans: Placing fans may place firefighters very close to the hazard zone.
CARGO COMPARTMENT AFT
WHEEL FIRE
OF DOOR
Apply large amounts of water initially with turrets. Transition to handline application to continue and
ENGINE OIL TANK - maintain a cooling effect.
LEFT OR RIGHT SIDE Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
OF EACH ENGINE
PORTABLE OXYGEN BOTTLES IN
FWD PASS CABIN
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 & 200 COMBI SERIES
1 ENTRY/SERVICE DOORS EXTERNAL HANDLE
EMERGENCY RESCUE ACCESS-1
2 OVERWING ESCAPE HATCHES
NOTE: ESCAPE SLIDE DISARMS
AUTOMATICALLY WHEN
DOOR OR HATCH IS OPENED
FROM THE OUTSIDE, EXCEPT
FOR TYPE 1 EMERGENCY
EXIT DOOR.
FLIGHT DECK WINDOWS
CANNOT BE OPENED FROM
THE OUTSIDE.
TO OPEN DOOR
1. PUSH HANDLE RELEASE LATCH.
2. PULL BUTTERFLY HANDLE FROM RECESS AND ROTATE 180° IN
DIRECTION OF “OPEN” ARROW.
3. PULL DOOR OUTWARD.
3 TYPE 1 EMERGENCY EXIT DOOR
TO OPEN HATCH:
1. LIFT LOWER PORTION OF HANDLE AWAY
FROM THE SIDE OF THE AIRPLANE.
2. PUSH INWARD AND UP ON THE HANDLE.
3. PUSH HATCH INWARD.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
FWD
TO OPEN DOOR:
1. PUSH ON “PUSH” PANEL TO GAIN ACCESS TO HANDLE.
2. PULL HANDLE FORWARD AND OUTWARD.
3. DOOR OPENS OUTWARD AND DOWN.
WARNING: STAND TO THE SIDE OF DOOR WHEN PULLING
HANDLE. ESCAPE SLIDE DOES NOT DISARM AND WILL
DEPLOY IMMEDIATELY WHEN A TYPE 1 DOOR IS OPENED
FROM THE OUTSIDE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
757-200 & 200 COMBI SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU ACCESS
1 ENTRY DOORS
4 CUT-IN AREAS
2 OVERWING ESCAPE HATCHES
(AS INSTALLED)
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
OPTIONAL CARGO DOOR ON
RIGHT SIDE - OPERATING
INSTRUCTIONS ON DOOR
4 CUT-IN AREAS
3 EMERGENCY EXITS
(AS INSTALLED)
CARGO DOOR ON COMBI
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
1 ENTRY DOORS
1 ENTRY DOORS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 6 FT 6 IN
WHEELS EXTENDED: 13 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
757-200 & 200 COMBI SERIES
AFT CARGO DOOR
FWD CARGO DOOR
MAIN BATTERY
AFT CARGO DOOR
NOSE GEAR COMPARTMENT
APU BATTERY
ACCESS DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 & 200 COMBI SERIES
FLIGHT DECK CONTROL SWITCH LOCATIONS
APU CONTROL
SWITCH - OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
THRUST LEVERS - RETARD
APU FIRE SWITCHES PULL (IF NOT
ILLUMINATED, PUSH
AND HOLD THE BUTTON
UNDER THE SWITCH TO
RELEASE)
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 & 200 COMBI SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 PACKAGE FREIGHTER
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANK
APU
HYDRAULIC RESERVOIR AND
ACCUMULATOR IN RIGHT
WHEEL WELL
CENTER FUEL TANK
RIGHT MAIN
FUEL TANK
APU FUEL LINE
2170 GAL 8214 L
HYDRAULIC RESERVOIR IN
LEFT WING FILLET
DRY BAY
6900 GAL 26119 L
APU EMERGENCY
CONTROL PANEL
LOCATED ON THE
NOSE GEAR
LEFT MAIN FUEL TANKS
HYDRAULIC RESERVOIR IN
LEFT WHEEL WELLS
SURGE TANK
2170 GAL - 8214 L
CREW OXYGEN BOTTLE IN
RIGHT SIDE, FORWARD
CARGO COMPARTMENT AFT
OF DOOR
FLIGHT DECK PORTABLE
OXYGEN BOTTLE ON
BULKHEAD BEHIND
CAPTAIN
PORTABLE OXYGEN BOTTLES IN
LAVATORY
ENGINE OIL TANK LEFT OR RIGHT SIDE
OF EACH ENGINE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 PACKAGE FREIGHTER
1 ENTRY/SERVICE DOORS EXTERNAL HANDLE
CRANK HANDLE
(SHOWN
EXTENDED)
ACCESS DOOR
EMERGENCY RESCUE ACCESS-1
2 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE
INJURY TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR
EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
PULL HANDLE
(SHOWN
EXTENDED)
TO OPEN DOOR:
1. PUSH HANDLE RELEASE LATCH.
2. PULL BUTTERFLY HANDLE FROM RECESS AND ROTATE 180° IN
DIRECTION OF “OPEN” ARROW.
3. PULL DOOR OUTWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
757-200 PACKAGE FREIGHTER
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU ACCESS
2 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
LOWER DECK CARGO
DOOR ON RIGHT SIDE OPERATING
INSTRUCTIONS ON DOOR
LOWER DECK CARGO DOOR ON
RIGHT SIDE - OPERATING
INSTRUCTIONS ON DOOR
PILOT’S WINDOW
ON RIGHT SIDE
SIDE CARGO DOOR
1 ENTRY DOOR
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 6 FT 6 IN
WHEELS EXTENDED: 13 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
757-200 PACKAGE FREIGHTER
AFT CARGO DOOR
FWD CARGO DOOR
MAIN BATTERY
NOSE GEAR COMPARTMENT
APU BATTERY
ACCESS DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 PACKAGE FREIGHTER FLIGHT DECK CONTROL SWITCH LOCATIONS
APU CONTROL
SWITCH - OFF
BATTERY SWITCH - PUSH
NOTE: ON SYMBOL IS
REMOVED
THRUST LEVERS - RETARD
APU FIRE SWITCHES PULL (IF NOT
ILLUMINATED, PUSH
AND HOLD THE BUTTON
UNDER THE SWITCH TO
RELEASE)
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
DEPR
CARGO
MAIN
FWD
AFT
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-200 PACKAGE FREIGHTER
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.1.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-300 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANKS
APU
HYDRAULIC RESERVOIR AND
ACCUMULATOR IN RIGHT
WHEEL WELL
CENTER FUEL TANK
RIGHT MAIN
FUEL TANK
APU FUEL LINE
2220 GAL 8404 L
HYDRAULIC RESERVOIR IN
LEFT WING FILLET
7050 GAL 26687 L
APU EMERGENCY
CONTROL PANEL
LOCATED ON THE
NOSE GEAR
LEFT MAIN FUEL TANKS
HYDRAULIC RESERVOIR IN
LEFT WHEEL WELLS
SURGE TANK
2220 GAL - 8404 L
CREW OXYGEN BOTTLE IN
RIGHT SIDE, FORWARD
CARGO COMPARTMENT AFT
OF DOOR
FLIGHT DECK PORTABLE
OXYGEN BOTTLE ON
BULKHEAD BEHIND
CAPTAIN
PORTABLE OXYGEN BOTTLES IN
FWD PASS CABIN
ENGINE OIL TANK LEFT OR RIGHT SIDE
OF EACH ENGINE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.2.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
757-300 SERIES
1 ENTRY/SERVICE DOORS EXTERNAL HANDLE
2 OVERWING ESCAPE HATCHES
NOTE: ESCAPE SLIDE DISARMS
AUTOMATICALLY WHEN
DOOR OR HATCH IS OPENED
FROM THE OUTSIDE, EXCEPT
FOR TYPE 1 EMERGENCY
EXIT DOOR.
FLIGHT DECK WINDOWS
CANNOT BE OPENED FROM
THE OUTSIDE.
TO OPEN DOOR
1. PUSH HANDLE RELEASE LATCH.
2. PULL BUTTERFLY HANDLE FROM RECESS AND ROTATE 180° IN
DIRECTION OF “OPEN” ARROW.
3. PULL DOOR OUTWARD.
3 TYPE 1 EMERGENCY EXIT DOOR
TO OPEN HATCH:
1. LIFT LOWER PORTION OF HANDLE AWAY
FROM THE SIDE OF THE AIRPLANE.
2. PUSH INWARD AND UP ON THE HANDLE.
3. PUSH HATCH INWARD.
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY
TO PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO
GAIN ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF
SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
FWD
TO OPEN DOOR:
1. PUSH ON “PUSH” PANEL TO GAIN ACCESS TO HANDLE.
2. PULL HANDLE FORWARD AND OUTWARD.
3. DOOR OPENS OUTWARD AND DOWN.
WARNING: STAND TO THE SIDE OF DOOR WHEN PULLING
HANDLE. ESCAPE SLIDE DOES NOT DISARM AND WILL
DEPLOY IMMEDIATELY WHEN A TYPE 1 DOOR IS OPENED
FROM THE OUTSIDE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.2.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
757-300 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU ACCESS
1 ENTRY DOORS
4 CUT-IN AREAS
2 OVERWING ESCAPE HATCHES
(AS INSTALLED)
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
OPTIONAL CARGO DOOR ON
RIGHT SIDE - OPERATING
INSTRUCTIONS ON DOOR
4 CUT-IN AREAS
3 EMERGENCY EXITS
(AS INSTALLED)
CARGO DOOR ON COMBI
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
1 ENTRY DOORS
1 ENTRY DOORS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 6 FT 6 IN
WHEELS EXTENDED: 13 FT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.2.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
757-300 SERIES
AFT CARGO DOOR
FWD CARGO DOOR
MAIN BATTERY
AFT CARGO DOOR
NOSE GEAR COMPARTMENT
APU BATTERY
ACCESS DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.2.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
757-300 SERIES
FLIGHT DECK CONTROL SWITCH LOCATIONS
APU CONTROL
SWITCH - OFF
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
THRUST LEVERS - RETARD
APU FIRE SWITCHES PULL (IF NOT
ILLUMINATED, PUSH
AND HOLD THE BUTTON
UNDER THE SWITCH TO
RELEASE)
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
757.2.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
757-300 SERIES
VERTICAL STABILIZER TIP CAP
RUDDER
VERTICAL STABILIZER
PANELS
ELEVATORS AND TABS
HORIZONTAL STABILIZER
UPPER/LOWER TRAILING
EDGE PANELS
AILERONS
LEADING EDGE SLAT
AND FIXED PANELS
HORIZONTAL STABILIZER
UPPER/LOWER SKIN
PANELS
STRUT FAIRINGS
INBOARD/OUTBOARD
SPOILERS AND FLAPS
RADOME
PYLON FAIRING
PANELS
NOSE LANDING
GEAR DOORS
WING TO BODY
FAIRING
FLAP TRACK
FAIRINGS
INLET/FAN/ THRUST REVERSER
COWL
MAIN LANDING
GEAR DOORS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
757.2.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
767 SERIES
FLAMMABLE MATERIAL LOCATIONS
767 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft
that have been exposed to fatigue or fire as the result of an accident. Crews need to verify the integrity of the
surface area before moving their weight and equipment across it. Signs could include but are not limited to
deformity of structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
with a pike pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANK
APU
HYDRAULIC ACCUMULATOR IN
RIGHT WHEEL WELL
HYDRAULIC RESERVOIR IN
RIGHT WHEEL WELL
FUEL TANK
APU FUEL LINE
6070 GAL 22977 L
DRY BAY
OPTIONAL PORTABLE OXYGEN BOTTLES
THROUGHOUT CABIN
FUEL TANK
1
OPTIONAL PORTABLE OXYGEN BOTTLES ON
FORWARD SIDE OF BULKHEAD
SURGE TANK
6070 GAL - 22977 L
APU EMERGENCY
CONTROL PANEL
LOCATED ON THE
NOSE GEAR
FUEL TANK
CREW OXYGEN BOTTLE IN
RIGHT SIDE, E & E
COMPARTMENT
1
CENTER FUEL TANK CAPACITIES
ENGINE OIL TANK FORWARD RIGHT OR
REAR LEFT SIDE OF
EACH ENGINE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
MODEL
GALLONS
LITERS
STANDARD
-200 ER
-300 ER
4,560
8,310
12,000
17,261
31,457
45,425
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
-400 ER
12,000
45,425
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
767.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
767 SERIES
1 ENTRY/SERVICE DOOR
EXTERNAL HANDLE
2 OVERWING ESCAPE HATCHES
3 TYPE 1 EMERGENCY EXIT DOOR
FWD
TO OPEN DOOR:
1. PUSH IN DISARM LEVER (RED
SURFACE LABLED “PUSH”).
2. PULL AND LIFT OPERATING
HANDLE TO UNLATCH DOOR.
3. MOVE DOOR UPWARD.
TO OPEN HATCH:
1. LIFT LOWER PORTION OF HANDLE AWAY
FROM THE SIDE OF THE AIRPLANE.
2. PUSH INWARD AND UP ON THE HANDLE.
3. PUSH HATCH INWARD.
TO OPEN DOOR:
1. PUSH ON “PUSH” PANEL TO GAIN ACCESS TO HANDLE.
2. PULL HANDLE FORWARD AND OUTWARD.
3. DOOR OPENS OUTWARD AND DOWN.
WARNING: STAND TO THE SIDE OF DOOR WHEN PULLING
HANDLE. ESCAPE SLIDE DOES NOT DISARM AND WILL
DEPLOY IMMEDIATELY WHEN A TYPE 1 DOOR IS OPENED
FROM THE OUTSIDE.
NOTES:
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
1. FOR ENTRY/SERVICE DOORS AND OVERWING HATCHES, ESCAPE SLIDE DISARMS
AUTOMATICALLY WHEN DOOR OR HATCH IS OPENED FROM THE OUTSIDE.
2. ON PASSENGER AIRPLANES, COCKPIT WINDOWS CANNOT BE OPENED FROM
THE OUTSIDE.
3. ON 767 FREIGHTERS, THE RIGHT SIDE COCKPIT WINDOW CAN BE OPENED FROM
THE OUTSIDE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
767 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU ACCESS
4 CUT-IN AREAS
3 TYPE 1 EMERGENCY EXIT
(OPTIONAL ON 767-300,
ALL 767-400)
767-400 FREIGHTERS - RIGHT
SIDE COCKPIT CAN BE OPENED
FROM THE OUTSIDE
1 ENTRY/SERVICE DOORS
1 ENTRY/SERVICE
DOORS (OPTIONAL
ON 767-300, ALL
767-400)
4 CUT-IN AREAS
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
4 CUT-IN AREAS
CARGO DOOR ON
RIGHT SIDE OPERATING
INSTRUCTIONS ON
DOOR
2 OPTIONAL OVERWING
ESCAPE HATCHES
1 ENTRY/SERVICE DOORS
4 CUT-IN AREAS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 7 FT 6 IN
WHEELS EXTENDED: 13 FT 6 IN
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
767.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
767 SERIES
AFT CARGO DOOR
FWD CARGO DOOR
MAIN BATTERY
AFT CARGO DOOR
APU BATTERY
EQUIPMENT ACCESS DOOR
NOSE GEAR DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
767 SERIES
BAT
STBY POWER
APU
AUTO
OFF
ON
APU CONTROL
SWITCH - OFF
BAT
OFF
ON
START
OFF
O
F
F
BATTERY SWITCH - PUSH
NOTE: ON SYMBOL IS
REMOVED
THRUST LEVERS - RETARD
APU FIRE SWITCHES PULL (IF NOT
ILLUMINATED, PUSH
AND HOLD THE BUTTON
UNDER THE SWITCH TO
RELEASE)
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
L
FUEL CONTROL
R
RUN
RICH
CUT OFF
L ENG
OVHT
ENG BTL ENG BTL
1 DISCH 2 DISCH
L
E
F
T
R ENG
OVHT
ARMED
ARMED
FWD
AFT
R
I
G
H
T
APU BTL
DISCH
BTL DSCH
DISCH
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
767.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
767 SERIES
VERTICAL STABILIZER TIP
RUDDER
HF ANTENNA
WINDOW
RAKED TIP
(-400 ONLY)
HORIZONTAL STABILIZER
UPPER/LOWER TRAILING
EDGE PANELS
VERTICAL STABILIZER
FORWARD TORQUE
BOX PANELS
ELEVATORS AND TABS
HORIZONTAL
STABILIZER TIP
INBOARD/OUTBOARD
AILERON PANELS
LEADING EDGE SLAT
AND FIXED PANELS
HORIZONTAL STABILIZER
UPPER/LOWER SKIN
PANELS
NACELLE STRUT
FAIRING
INBOARD/OUTBOARD
SPOILERS AND FLAPS
RIGID CARGO BARRIER
(-300F/-400)
RADOME
PYLON FAIRING
PANELS
NOSE LANDING
GEAR DOORS
MAIN LANDING
GEAR DOORS
HEAT SHIELDS
WING TO BODY
FAIRING
INLET/FAN/ THRUST REVERSER
COWL
TAIL SKID FAIRING
MAIN LANDING
GEAR DOORS
AND VAPOR
BARRIER
FLAP TRACK
FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
767 -2C Freighter
FLAMMABLE MATERIAL LOCATIONS
767 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft
that have been exposed to fatigue or fire as the result of an accident. Crews need to verify the integrity of the
surface area before moving their weight and equipment across it. Signs could include but are not limited to
deformity of structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
with a pike pole, axe or any instrument used to sound surfaces for integrity.
SURGE TANK
APU
HYDRAULIC ACCUMULATOR IN
RIGHT WHEEL WELL
HYDRAULIC RESERVOIR IN
RIGHT WHEEL WELL
AFT BODY
TANKS
FUEL TANK
APU FUEL LINE
6010 GAL 22750 L
DRY BAY
OPTIONAL PORTABLE OXYGEN BOTTLES
THROUGHOUT CABIN
FWD BODY TANK
1805 GAL- 6832 L
OPTIONAL PORTABLE OXYGEN BOTTLES ON
FORWARD SIDE OF BULKHEAD
FUEL TANK
11940 GAL 45198 L
SURGE TANK
6010 GAL - 22750 L
APU EMERGENCY
CONTROL PANEL
LOCATED ON THE
NOSE GEAR
FUEL TANK
REAR CREW 6 X 115 CU FT
OXYGEN BOTTLES IN
FORWARD LOWER LOBE
PILOTS 2 X 115 CU FT OXYGEN
BOTTLES
ENGINE OIL TANK REAR LEFT SIDE OF
EACH ENGINE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
September 5, 2014
767.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
767 -2C Freighter
1 ENTRY/SERVICE DOOR
EXTERNAL HANDLE
2 OVERWING ESCAPE HATCHES
TO OPEN HATCH:
1. LIFT LOWER PORTION OF HANDLE AWAY
FROM THE SIDE OF THE AIRPLANE.
2. PUSH INWARD AND UP ON THE HANDLE.
3. PUSH HATCH INWARD.
TO OPEN DOOR:
1. PUSH IN DISARM LEVER (RED
SURFACE LABLED “PUSH”).
2. PULL AND LIFT OPERATING
HANDLE TO UNLATCH DOOR.
3. MOVE DOOR UPWARD.
NOTES:
4 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
1. FOR ENTRY/SERVICE DOORS AND OVERWING HATCHES, ESCAPE SLIDE DISARMS
AUTOMATICALLY WHEN DOOR OR HATCH IS OPENED FROM THE OUTSIDE.
2. ON PASSENGER AIRPLANES, COCKPIT WINDOWS CANNOT BE OPENED FROM
THE OUTSIDE.
3. ON 767 FREIGHTERS, THE RIGHT SIDE COCKPIT WINDOW CAN BE OPENED FROM
THE OUTSIDE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.1.2
September 5, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
767 -2C Freighter
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU ACCESS
4 CUT-IN AREAS
1 ENTRY/SERVICE DOORS
4 CUT-IN AREAS
MAIN CARGO DOOR
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
4 CUT-IN AREAS
CARGO DOOR ON
RIGHT SIDE OPERATING
INSTRUCTIONS ON
DOOR
2 OVERWING ESCAPE
HATCHES
1 ENTRY/SERVICE DOORS
4 CUT-IN AREAS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 7 FT 6 IN
WHEELS EXTENDED: 13 FT 6 IN
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
September 5, 2014
767.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
767 -2C Freighter
AFT CARGO DOOR
FWD CARGO DOOR
MAIN BATTERY
AFT CARGO DOOR
APU BATTERY
EQUIPMENT ACCESS DOOR
NOSE GEAR DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.1.4
September 5, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
767 -2C Freighter
BAT
STBY POWER
APU
ON
AUTO
OFF
ON
APU CONTROL
SWITCH - OFF
BAT
OFF
START
OFF
O
F
F
BATTERY SWITCH - PUSH
NOTE: ON SYMBOL IS
REMOVED
THRUST LEVERS - RETARD
APU FIRE SWITCHES PULL (IF NOT
ILLUMINATED, PUSH
AND HOLD THE BUTTON
UNDER THE SWITCH TO
RELEASE)
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
L
FUEL CONTROL
R
RUN
CUT OFF
L ENG
OVHT
ENG BTL ENG BTL
1 DISCH 2 DISCH
R ENG
OVHT
CARGO FIRE
APU BTL
DISCH
DEPR
CARGO
L
E
F
T
R
I
G
H
T
ARMED
MAIN
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
FUEL CONTROL SWITCHES - CUTOFF
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
September 5, 2014
767.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
767 -2C Freighter
VERTICAL STABILIZER TIP
RUDDER
HF ANTENNA
WINDOW
HORIZONTAL STABILIZER
UPPER/LOWER TRAILING
EDGE PANELS
VERTICAL STABILIZER
FORWARD TORQUE
BOX PANELS
ELEVATORS AND TABS
HORIZONTAL
STABILIZER TIP
INBOARD/OUTBOARD
AILERON PANELS
LEADING EDGE SLAT
AND FIXED PANELS
HORIZONTAL STABILIZER
UPPER/LOWER SKIN
PANELS
NACELLE STRUT
FAIRING
INBOARD/OUTBOARD
SPOILERS AND FLAPS
RIGID CARGO BARRIER
RADOME
PYLON FAIRING
PANELS
NOSE LANDING
GEAR DOORS
MAIN LANDING
GEAR DOORS
HEAT SHIELDS
WING TO BODY
FAIRING
EQUIPMENT FAIRING
MAIN LANDING
GEAR DOORS
AND VAPOR
BARRIER
FLAP TRACK
FAIRINGS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
767.1.6
September 5, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
777 SERIES
FLAMMABLE MATERIAL LOCATIONS
777 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft that have
been exposed to fatigue or fire as the result of an accident. Crews need to verify the integrity of the surface area
before moving their weight and equipment across it. Signs could include but are not limited to deformity of structure,
visual signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike pole, axe or any
instrument used to sound surfaces for integrity.
APU
OPTIONAL PASSENGER
OXYGEN BOTTLES
SURGE TANK
HYDRAULIC
RESERVOIR IN
RIGHT WHEEL
WELL
APU FUEL LINE
FUEL TANK
HYDRAULIC
RESERVOIR IN
LEFT AND RIGHT
ENGINE STRUTS
10300 GAL - 38990 L
1 AND 3 MAIN FUEL TANKS
-200
9300 GAL - 35200 L
-200ER 9560 GAL - 36200 L
-200LR 10300 GAL - 38990 L
-300
9560 GAL - 36200 L
-300ER 10300 GAL - 38990 L
FUEL TANK
(AS INSTALLED)
-200LR 1850 GAL - 7003 L
FUEL TANK
CENTER FUEL TANK
-200
-200ER
-200LR
-300
-300ER
12400 GAL - 46900 L
26100 GAL - 98790 L
27290 GAL - 103290 L
26100 GAL - 98790 L
27290 GAL - 103290 L
27290 GAL - 103290 L
PORTABLE OXYGEN BOTTLES
FUEL TANK
SURGE TANK
10300 GAL - 38990 L
HYDRAULIC
ACCUMULATOR
IN LEFT WHEEL
OPTIONAL PORTABLE
OXYGEN BOTTLES ON
FWD BULKHEAD FWD
RIGHT GALLEY
CREW OXYGEN BOTTLE IN EE
COMPARTMENT LEFT SIDE OF
WHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
ENGINE OIL TANK maintain a cooling effect.
FORWARD RIGHT SIDEWheels are equipped with fusible plugs designed to melt and deflate the tire when the
OF EACH ENGINE
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
777 SERIES
1 ENTRY/SERVICE DOOR/OVERWING EXIT EXTERNAL HANDLE
PUSH IN FLAPS (RED)
TO ACCESS HANDLE
2 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO PERSONNEL WITHIN, IT
IS RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE DIRECTED TO HATCHES
AND DOORS. URGENCY OF SITUATION WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN DOOR:
1. PUSH IN RED FLAPS.
2. PULL HANDLE FROM RECESS.
3. ROTATE HANDLE 180 DEGREES IN THE DIRECTION OF THE “OPEN” ARROW.
4. PULL DOOR OUTWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
777 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
BULK CARGO DOOR ON
RIGHT SIDE - OPERATING
INSTRUCTIONS ON DOOR
1 ENTRY/SERVICE DOORS
2 CUT-IN AREAS
(NOT MARKED ON ALL
AIRPLANES)
1 ENTRY/SERVICE DOORS
2 CUT-IN AREAS
(NOT MARKED ON ALL
AIRPLANES)
1 ENTRY/SERVICE DOORS
CARGO DOOR ON RIGHT
SIDE - OPERATING
INSTRUCTIONS ON DOOR
2 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
1 OVERWING EXIT DOORS
(300/300ER)
CARGO DOOR ON
RIGHT SIDE OPERATING
INSTRUCTIONS ON
DOOR
1 ENTRY/SERVICE DOORS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 8 FT 3 IN
WHEELS EXTENDED: 16 FT 6 IN
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-3
777 SERIES
UPPER CREW REST AS INSTALLEDENTRANCE AT DOORS, 3R, 4R, 5L
LOWER CREW REST AS INSTALLEDDOOR 3R
DOOR 1L - ALSO ALLOWS ACCESS
TO THE OVERHEAD CREW REST
AREA. THE OVERHEAD CREW REST
AREA MAY BE OCCUPIED AND MUST
BE CHECKED FOR TRAPPED AND/OR
INJURED PEOPLE.
UPPER AND LOWER CREW REST AREAS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-4
777 SERIES
BUNK MODULE
SEAT MODULE
ENTRANCE
ENCLOSURE
FORWARD OVERHEAD FLIGHT CREW REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
777 SERIES
EMERGENCY RESCUE ACCESS-5
AS INSTALLED
Main control panel
(inside enclosure)
AFT OVERHEAD FLIGHT CREW REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-6
777 SERIES
AS INSTALLED
Attendant
switch panel
Main entry hatch
(shown open)
Hinge
Hatch swings up
Center
handle
LOWER FLIGHT CREW REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.0.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
777 SERIES
AFT CARGO DOOR
AFT CARGO DOOR
APU BATTERY
EQUIPMENT ACCESS DOOR
MAIN BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.0.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
777 SERIES
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
ELECTRICAL
APU
ON
BATTERY
OFF
START
CARGO FIRE
APU BTL
DISCH
ON
ARM
OFF
APU GEN
APU SELECTOR OFF
ON
FWD
AFT
ARMED
ARMED
FWD
AFT
FAULT
OFF
DISCH
FIRE/
OVHT
TEST
R BUS TIE
L BUS TIE
AUTO
AUTO
DISCH
DISCH
ISLN
L
GEN
CTRL
SECONDARY
EXT PWR
PRIMARY
EXT PWR
ON
ON
AVAIL
AVAIL
L MAIN
L XFR
R XFR
OFF
ON
ON
OFF
OFF
APU FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND
HOLD THE BUTTON UNDER
THE SWITCH TO RELEASE)
R
GEN
CTRL
R MAIN
BACKUP GEN
L
R
ON
ISLN
ON
OFF
DRIVE
DRIVE
L
DRIVE DISC
R
THRUST LEVERS - RETARD
ENG BTL ENG BTL
1 DISCH 2 DISCH
1
FUEL CONTROL SWITCHES - CUTOFF
L
FUEL CONTROL
RUN
CUTOFF
R
DISCH
L
E
F
T
2
1
DISCH
R
I
G
H
T
2
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.0.9
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
777 SERIES
RUDDER
VERTICAL STABILIZER
TORQUE BOX SKIN/
STRINGERS/SPARS
OUTBOARD
AILERON
RUDDER TAB
ELEVATORS
UPPER/LOWER WING
LEADING EDGE
SPOILERS
FLAPERON
SPOILERS
HORIZONTAL STABILIZER
TORQUE BOX SKIN/
STRINGERS/SPARS
FORWARD AND AFT
STRUT FAIRINGS
ENGINE COWL INLET, FAN, THRUST
REVERSER
INBOARD FLAPS
OUTBOARD FLAPS
FAN COWL
SUPPORT BEAM
FAIRING
NOSE LANDING
GEAR DOORS
UPPER/LOWER WING
TRAILING EDGE
WING TO BODY
FAIRING
FLAP SUPPORT FAIRINGS
MAIN LANDING
GEAR DOORS
HORIZONTAL STABILIZER
LOWER/UPPER TRAILING
EDGE PANELS
AFT FUSELAGE
SKIN PANELS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.0.10
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
777 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
APU
PASSENGER OXYGEN
BOTTLES
SURGE TANK
HYDRAULIC
RESERVOIR IN
RIGHT WHEEL
WELL
APU FUEL LINE
FUEL TANK
HYDRAULIC
RESERVOIR IN
LEFT AND RIGHT
ENGINE STRUTS
10300 GAL - 38990 L
1 AND 3 MAIN FUEL TANKS
-200
9300 GAL - 35200 L
-200ER 9560 GAL - 36200 L
-200LR 10300 GAL - 38990 L
-300
9560 GAL - 36200 L
-300ER 10300 GAL - 38990 L
FUEL TANK
(AS INSTALLED)
-200LR 1850 GAL - 7003 L
FUEL TANK
CENTER FUEL TANK
-200
-200ER
-200LR
-300
-300ER
12400 GAL - 46900 L
26100 GAL - 98790 L
27290 GAL - 103290 L
26100 GAL - 98790 L
27290 GAL - 103290 L
27290 GAL - 103290 L
PORTABLE OXYGEN BOTTLES
FUEL TANK
SURGE TANK
10300 GAL - 38990 L
HYDRAULIC
ACCUMULATOR
IN LEFT WHEEL
WELL
OPTIONAL PORTABLE
OXYGEN BOTTLES ON
FWD BULKHEAD FWD
RIGHT GALLEY
CREW OXYGEN BOTTLE IN EE
COMPARTMENT LEFT SIDE OF
WHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
ENGINE OIL TANK Apply large amounts of water initially with turrets. Transition to handline application to continue and
FORWARD RIGHT SIDE maintain a cooling effect.
OF EACH ENGINE
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
777 FREIGHTER SERIES
1 ENTRY/SERVICE DOOR EXTERNAL HANDLE
PUSH IN FLAPS (RED)
TO ACCESS HANDLE
EMERGENCY RESCUE ACCESS-1
2 CUT-IN AREAS
NOTE: CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND POSSIBLE INJURY TO
PERSONNEL WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT TO GAIN
ACCESS BE DIRECTED TO HATCHES AND DOORS. URGENCY OF SITUATION
WILL DICTATE THE NECESSITY FOR A CUT-IN.
TO OPEN DOOR:
1. PUSH IN RED FLAPS.
2. PULL HANDLE FROM RECESS.
3. ROTATE HANDLE 180 DEGREES IN THE DIRECTION OF THE “OPEN” ARROW.
4. PULL DOOR OUTWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
777 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
BULK CARGO DOOR ON
RIGHT SIDE (OPERATING
INSTRUCTIONS ON DOOR)
2 CUT-IN AREAS
(NOT MARKED ON ALL
AIRPLANES)
2 CUT-IN AREAS
(NOT MARKED ON ALL
AIRPLANES)
CARGO DOOR ON RIGHT
SIDE (OPERATING
INSTRUCTIONS ON DOOR)
2 CUT-IN AREAS
(NOT MARKED ON ALL AIRPLANES)
SIDE CARGO DOOR
CARGO DOOR ON
RIGHT SIDE
(OPERATING
INSTRUCTIONS ON
DOOR)
1 ENTRY/SERVICE DOORS
AVERAGE DISTANCE FLOOR LEVEL TO
GROUND
WHEELS RETRACTED: 8 FT 3 IN
WHEELS EXTENDED: 16 FT 6 IN
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
777 FREIGHTER SERIES
AFT CARGO DOOR
AFT CARGO DOOR
APU BATTERY
EQUIPMENT ACCESS DOOR
MAIN BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
777 FREIGHTER SERIES
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
ELECTRICAL
APU
ON
BATTERY
OFF
START
CARGO FIRE
APU BTL
DISCH
ON
ARM
OFF
APU GEN
APU SELECTOR OFF
ON
FWD
AFT
ARMED
ARMED
FWD
AFT
FAULT
OFF
DISCH
FIRE/
OVHT
TEST
R BUS TIE
L BUS TIE
AUTO
AUTO
DISCH
DISCH
ISLN
L
GEN
CTRL
SECONDARY
EXT PWR
PRIMARY
EXT PWR
ON
ON
AVAIL
AVAIL
L MAIN
L XFR
R XFR
OFF
ON
ON
OFF
OFF
APU FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND
HOLD THE BUTTON UNDER
THE SWITCH TO RELEASE)
R
GEN
CTRL
R MAIN
BACKUP GEN
L
R
ON
ISLN
ON
OFF
DRIVE
DRIVE
L
DRIVE DISC
R
THRUST LEVERS - RETARD
ENG BTL ENG BTL
1 DISCH 2 DISCH
1
FUEL CONTROL SWITCHES - CUTOFF
L
FUEL CONTROL
RUN
CUTOFF
R
DISCH
L
E
F
T
2
1
DISCH
R
I
G
H
T
2
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH
TO RELEASE)
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
777.1.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
COMPOSITE MATERIALS LOCATIONS
777 FREIGHTER SERIES
RUDDER
VERTICAL STABILIZER
TORQUE BOX SKIN/
STRINGERS/SPARS
OUTBOARD
AILERON
RUDDER TAB
ELEVATORS
UPPER/LOWER WING
LEADING EDGE
SPOILERS
FLAPERON
SPOILERS
HORIZONTAL STABILIZER
TORQUE BOX SKIN/
STRINGERS/SPARS
FORWARD AND AFT
STRUT FAIRINGS
ENGINE COWL INLET, FAN, THRUST
REVERSER
INBOARD FLAPS
OUTBOARD FLAPS
FAN COWL
SUPPORT BEAM
FAIRING
NOSE LANDING
GEAR DOORS
UPPER/LOWER WING
TRAILING EDGE
WING TO BODY
FAIRING
FLAP SUPPORT FAIRINGS
MAIN LANDING
GEAR DOORS
HORIZONTAL STABILIZER
LOWER/UPPER TRAILING
EDGE PANELS
AFT FUSELAGE
SKIN PANELS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
777.1.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
787 SERIES
FLAMMABLE MATERIAL LOCATIONS
787 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
PASSENGER OXYGEN UNITS
ARE LOCATED AT EACH PSU
STATION
APU
SURGE TANK
FUEL TANK 787-8
HYDRAULIC
RESERVOIR IN
LEFT AND RIGHT
ENGINE STRUTS
5570 GAL - 21085 L
HYDRAULIC
RESERVOIR IN
RIGHT WHEEL
WELL
FUEL TANK 787-9
APU FUEL LINE
5520 GAL - 20895 L
CARGO AND ENGINE FIRE
BOTTLES (UP TO 11)
HYDRAULIC
RESERVOIR IN
RIGHT WING TO
BODY FARING
FUEL TANK 787-8
22200 GAL - 84036 L
SURGE TANK
FUEL TANK 787-9
22340 GAL - 84566 L
FUEL TANK 787-8
5570 GAL - 21085 L
FUEL TANK 787-9
PORTABLE OXYGEN BOTTLES
5520 GAL - 20895 L
CREW OXYGEN BOTTLE IN EE
COMPARTMENT LEFT SIDE OF
WHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
HYDRAULIC
Water mist: Can be deployed from turret or handline.
ACCUMULATOR
Fans: Placing fans may place firefighters very close to the hazard zone.
IN LEFT WHEEL WELL
WHEEL FIRE
ENGINE OIL TANK FORWARD RIGHT SIDE Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
OF EACH ENGINE
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
787.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
787 SERIES
1 ENTRY/SERVICE DOOR EXTERNAL HANDLE
PUSH IN FLAP (RED) TO
ACCESS HANDLE
OPEN
PUSH
PUSH
(TYPICAL)
TO OPEN DOOR:
1. PUSH IN RED FLAP.
2. PULL HANDLE FROM RECESS.
3. ROTATE HANDLE 180 DEGREES IN THE DIRECTION OF THE “OPEN” ARROW.
4. PULL DOOR OUTWARD.
2 CREW OVERHEAD ESCAPE HATCH EXTERNAL HANDLE
W8MT-26-00-0005
W8MT-26-00-0005
TO OPEN HATCH:
1. PUSH RELEASE TRIGGER ON HANDLE (HANDLE WILL SPRING OUT FROM RECESS APPROXIMATELY 3 INCHES).
2. ROTATE HANDLE 180°.
3. PUSH HATCH INWARD.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
787.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
787 SERIES
CARGO DOOR ON RIGHT
SIDE (OPERATING
INSTRUCTIONS ON DOOR)
1 ENTRY/SERVICE DOORS
1 ENTRY/SERVICE DOORS
BULK CARGO DOOR ON
LEFT SIDE (OPERATING
INSTRUCTIONS ON DOOR)
1 ENTRY/SERVICE DOORS
3 CUT-IN AREA
(NOT MARKED ON ALL AIRPLANES)
3 CUT-IN AREA
(NOT MARKED ON ALL AIRPLANES)
CARGO DOOR ON RIGHT SIDE
(OPERATING INSTRUCTIONS
ON DOOR)
2 CREW OVERHEAD
ESCAPE HATCH
AVERAGE DISTANCE FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 7 FT 6 IN
WHEELS EXTENDED: 13 FT 6 IN
1 ENTRY/SERVICE DOORS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
787.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-3
787 SERIES
DOOR 4L - ALSO ALLOWS ACCESS
TO THE OVERHEAD FLIGHT
ATTENDANT REST AREA. THE
OVERHEAD FLIGHT ATTENDANT
REST AREA MAY BE OCCUPIED AND
MUST BE CHECKED FOR TRAPPED
AND/OR INJURED PEOPLE.
DOOR 1L - ALSO ALLOWS ACCESS
TO THE OVERHEAD FLIGHT CREW
REST AREA. THE OVERHEAD FLIGHT
CREW REST AREA MAY BE OCCUPIED
AND MUST BE CHECKED FOR
TRAPPED AND/OR INJURED PEOPLE.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
787.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-4
787 SERIES
SEAT MODULE
NOTE: SINGLE SEAT CONFIGURATION SHOWN
TWO SEAT CONFIGURATION ALSO
AVAILABLE.
BUNK MODULE
ENTRANCE ENCLOSURE
OVERHEAD FLIGHT CREW REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
787.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
787 SERIES
EMERGENCY RESCUE ACCESS-5
BUNK MODULE
ENTRANCE ENCLOSURE
OVERHEAD FLIGHT ATTENDANT REST AREA
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
787.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
787 SERIES
NOTE: The box containing the lithium-ion battery cells is secured
inside a reinforced stainless steel enclosure capable of
containing a lithium-ion battery event. Venting of vapor
during a battery failure event may be visible from an
exterior vent on the bottom of the aircraft under the
forward or aft E&E bay. During active venting, there is no
reason to make access to the E&E bay.
NOTE: If vapor is visible or odors are noticed, advise ground
personnel to stay clear of vapor if battery is still venting.
CAUTION: MAKE NO ATTEMPT TO DISCONNECT BATTERY
PACK FROM THE AIRCRAFT’S ELECTRICAL SYSTEM
USING QUICK DISCONNECT OR BY CUTTING THE
BATTERY CABLES.
APU BATTERY OVERBOARD VENT
(exterior, see note)
MAIN BATTERY OVERBOARD VENT
(exterior, see note)
AFT
AFT
ACCESS DOOR
FWD E&E BAY
LITHIUM-ION MAIN BATTERY
(stainless steel enclosure)
ACCESS DOOR
AFT E&E BAY
LITHIUM-ION APU BATTERY
(stainless steel enclosure)
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
787.0.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
787 SERIES
BATTERY SWITCH - PRESS
NOTE: ON SYMBOL IS
REMOVED
ELECTRICAL
IFE/PASS CABIN/
SEATS UTILITY
ON
ON
OFF
OFF
BATTERY
OFF
ON
APU
ON
START
CARGO FIRE
APU BTL
DISCH
A
P
U
FWD
OFF
APU GEN
L
R
FWD EXT PWR
L
R
ON
ON
OFF
OFF
ARM
AFT
ARMED
ARMED
FWD
AFT
FAULT
DISCH
FIRE/
OVHT
TEST
AFT EXT PWR
ON
ON
ON
AVAIL
AVAIL
AVAIL
DISCH
DISCH
AC BUSES
GEN CTRL
L1
L2
GEN CTRL
R1
R2
ON
ON
ON
ON
OFF
OFF
OFF
OFF
DRIVE
DRIVE
DRIVE
DRIVE
L1
L2
R1
R2
DRIVE DISC
APU FIRE SWITCH - PULL (IF NOT
ILLUMINATED, PUSH AND HOLD THE
BUTTON UNDER THE SWITCH TO
RELEASE)
THRUST LEVERS - RETARD
ENG BTL
1 DISCH
L
FUEL CONTROL
RUN
CUTOFF
FUEL CONTROL SWITCHES - CUTOFF
R
1
DISCH
L
E
F
T
2
ENGINE FIRE SWITCHES - PULL (IF
NOT ILLUMINATED, PUSH AND HOLD
THE BUTTON UNDER THE SWITCH TO
RELEASE)
ENG BTL
2 DISCH
1
DISCH
R
I
G
H
T
2
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
787.0.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
787 SERIES
COMPOSITE MATERIALS LOCATIONS
CARBON LAMINATE
CARBON SANDWICH
OTHER COMPOSITES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
787.0.9
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
787 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
787.0.10
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC3 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-3 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree
angle when apporaching hot brakes or fighting a wheel fire, as rims
and tires may pose a fragmentation hazard.
HYDRAULIC FLUID
TANK
FUEL TANKS
ENGINE OIL TANK
DEICER FLUID TANK
CARGO DOOR
MAIN CABIN ENTRANCE DOOR
804 GAL 3043 L
OXYGEN BOTTLE
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL EMERGENCY
EXITS AND FORCED ACCESS AREAS
PILOT’S ENTRANCE DOOR
BATTERIES
ENGINE OIL TANK
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
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June 27, 2014
DC-3.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC3 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-3.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-6 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-6 (tab)
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and maintain a
cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the temperature is
excessive.
FUEL TANK
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
FORCED ACCESS AREAS
DEICER FLUID TANK
ENGINE OIL TANK
FORCED ACCESS
AREA
CARGO DOOR (DC-6A ONLY)
2702 GAL - 10228 L
HYDRAULIC FLUID
TANK
MAIN CABIN ENTRANCE DOOR
OXYGEN BOTTLE
AUXILIARY OIL TANKS
PILOT’S ENTRANCE DOOR
2702 GAL - 10228 L
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL EMERGENCY
EXITS
FUEL TANK
ENGINE OIL TANKS
CARGO DOOR (DC-6A ONLY)
BATTERIES
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft that have been exposed to
fatigue or fire as the result of an accident. Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual signs of flame impingement or uneven
surfaces. Surface integrity can be checked with a pike pole, axe or any instrument used to sound surfaces for integrity.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-6.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-6 SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-6.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-7 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-7 (tab)
FLARES
FUEL TANK
2756 GAL 10433 L
ENGINE OIL TANKS
AUXILIARY OIL TANK ON
SOME AIRPLANES
PORTABLE OXYGEN
BOTTLES
FLARES
DC-7/7B
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
AUXILIARY OIL TANK
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
CAUTION: Rescue crews wearing full PPE to include SCBA’s must
PORTABLE OXYGEN
BOTTLES
3800 GAL 14385 L
ENGINE OIL TANKS
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
use caution when moving across sections of aircraft
that have been exposed to fatigue or fire as the result
of an accident. Crews need to verify the integrity of the
surface area before moving their weight and
equipment across it. Signs could include but are not
limited to deformity of structure, visual signs of flame
impingement or uneven surfaces. Surface integrity
can be checked with a pike pole, axe or any instrument
used to sound surfaces for integrity.
FUEL TANK
DC-7C
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June 27, 2014
DC-7.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS
DC-7 SERIES
1 CREW AND MAIN CABIN DOORS
EXTERNAL HANDLE
TO OPEN DOOR:
1. ROTATE HANDLE COUNTERCLOCKWISE.
2. PULL DOOR OUTWARD.
4 CUT-IN AREAS
CUT-IN AREAS
2 EMERGENCY EXIT DOORS
EXTERNAL HANDLE
TO OPEN DOOR:
1. PULL HANDLE OUT.
2. PUSH DOOR INWARD.
NOTE:
3 ESCAPE HATCH EXTERNAL HANDLE
TO OPEN HATCH:
1. PULL HANDLE OUT.
2. ROTATE HANDLE COUNTERCLOCKWISE.
3. PULL HATCH OUT.
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS. URGENCY OF SITUATION
WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-7.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS
DC-7 SERIES
1 MAIN CABIN DOOR
4 CUT-IN AREAS
2 EMERGENCY
EXIT DOOR
3 TYPICAL ESCAPE HATCHES
1 CREW AND CARGO DOOR
1 MAIN CABIN DOOR
4 CUT-IN AREAS
TYPICAL FIRE ACCESS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-7.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-7 SERIES
BATTERIES
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DC-7.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-7 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
FLARES
FUEL TANK
ENGINE OIL
TANKS
3800 GAL 14385 L
FIRE EXTINGUISHER
BOTTLES
AUXILIARY OIL TANK
3800 GAL 14385 L
ENGINE OIL TANKS
FUEL TANK
PORTABLE OXYGEN
BOTTLES
FIRE ACCESS
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-7.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-7 FREIGHTER SERIES
1 CREW AND MAIN CABIN DOORS
EXTERNAL HANDLE
TO OPEN DOOR:
1. ROTATE HANDLE COUNTERCLOCKWISE.
2. PULL DOOR OUTWARD.
4 CUT-IN AREAS
CUT-IN AREAS
2 EMERGENCY EXIT DOORS
EXTERNAL HANDLE
TO OPEN DOOR:
1. PULL HANDLE OUT.
2. PUSH DOOR INWARD.
NOTE:
3 ESCAPE HATCH EXTERNAL HANDLE
TO OPEN HATCH:
1. PULL HANDLE OUT.
2. ROTATE HANDLE COUNTERCLOCKWISE.
3. PULL HATCH OUT.
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE POWER
EQUIPMENT. BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL WITHIN, IT IS
RECOMMENDED THAT MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS. URGENCY OF SITUATION
WILL DICTATE THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-7.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-7 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE
2 EMERGENCY EXIT DOOR
4 CUT-IN AREAS
3 TYPICAL ESCAPE
HATCHES
1 CREW AND CARGO
DOOR
1 MAIN CABIN DOOR
4 CUT-IN AREAS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-7.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-7 FREIGHTER SERIES
Intentionally Blank
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-7.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-8 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC SUMP LOCATED
IN LEFT WHEEL WELL
HYDRAULIC ACCUMULATORS
LOCATED IN RIGHT WHEEL WELL
PASSENGER OXYGEN
BOTTLES
8950 GAL 33879 L
HYDRAULIC
ACCUMULATORS
LOCATED IN LEFT WHEEL
FUEL TANKS
CREW OXYGEN SYSTEM
BOTTLE
HYDRAULIC FLUID TANKS
LOCATED IN LEFT WING
ROOT
5800 GAL 21955 L
FUEL TANK
8950 GAL 33879 L
HYDRAULIC ACCUMULATOR
LOCATED IN LEFT WING
ROOT
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8 SERIES
1 PASSENGER AND
SERVICE DOORS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 CUT-IN AREAS
CUT-IN AREAS
2 EMERGENCY EXIT
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
1 AFT SERVICE
ENTRANCE DOOR
2 TYPICAL EMERGENCY
EXITS
2 AFT PASSENGER
ENTRANCE DOOR
BREAK GLASS FOR ACCESS
TO HANDLE AND SLIDE
WINDOW AFT
1 FORWARD SERVICE
ENTRY DOOR
3 CUT-IN AREAS
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
ACCESS TO ACCESSORY
COMPARTMENT
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
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June 27, 2014
DC-8.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8 FREIGHTER SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure,
visual signs of flame impingement or uneven surfaces. Surface integrity can be checked
with a pike pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC SUMP LOCATED
IN LEFT WHEEL WELL
HYDRAULIC ACCUMULATORS
LOCATED IN RIGHT WHEEL WELL
PASSENGER OXYGEN
BOTTLES
8800 GAL 33312 L
HYDRAULIC
ACCUMULATORS LOCATED
IN LEFT WHEEL WELL
FUEL TANKS
HYDRAULIC FLUID TANKS
LOCATED IN LEFT WING
ROOT
5800 GAL 21955 L
CREW OXYGEN SYSTEM
BOTTLE
FUEL TANK
8800 GAL 33312 L
HYDRAULIC ACCUMULATOR
LOCATED IN LEFT WING
ROOT
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.1.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8 FREIGHTER SERIES
1 PASSENGER AND
SERVICE DOORS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 CUT-IN AREAS
CUT-IN AREAS
EMERGENCY RESCUE ACCESS-1
2 EMERGENCY EXIT
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.1.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8 FREIGHTER SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
1 AFT SERVICE
ENTRANCE DOOR
2 TYPICAL EMERGENCY
EXITS
AFT CARGO
COMPARTMENT DOORS
1 AFT PASSENGER
ENTRANCE DOOR
REMOVAL OF DOOR IS RESTRICTED ON
SOME AIRPLANES
FORWARD CARGO
COMPARTMENT
DOORS
3 CUT-IN AREAS
1 FORWARD SERVICE
ENTRY DOOR
1 CARGO LOADING DOOR
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
ACCESS TO ACCESSORY
COMPARTMENT
FLOOR LEVEL TO GROUND
BREAK GLASS FOR ACCESS
TO HANDLE AND SLIDE
WINDOW AFT
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.1.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8 FREIGHTER SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.1.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-61 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC SUMP
LOCATED IN LEFT
WHEEL WELL
HYDRAULIC ACCUMULATORS
LOCATED IN RIGHT WHEEL
WELL
PASSENGER OXYGEN
BOTTLES
8950 GAL 33879 L
HYDRAULIC ACCUMULATOR LOCATED
IN LEFT WHEEL WELL
FUEL TANKS
HYDRAULIC FLUID TANKS
LOCATED IN LEFT WING
ROOT
6400 GAL 24227 L
CREW OXYGEN SYSTEM
BOTTLE
FUEL TANK
8950 GAL 33879 L
HYDRAULIC ACCUMULATOR
LOCATED IN LEFT WING
ROOT
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.2.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8-61 SERIES
1 PASSENGER AND
SERVICE DOORS
2 EMERGENCY EXIT
3 CUT-IN AREAS
CUT-IN AREAS
NOTE:
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
4 EMERGENCY EXIT DOORS
TO OPEN DOOR:
1. PULL HANDLE FROM
RECESS.
2. ROTATE HANDLE
FORWARD.
3. PULL DOOR OPEN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.2.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-61 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
1 AFT SERVICE
ENTRANCE
DOOR
4 TYPICAL EMERGENCY
EXIT DOORS
BREAK GLASS FOR ACCESS
TO HANDLE AND SLIDE
WINDOW AFT
2 OVERWING EMERGENCY
EXITS
3 CUT-IN AREA
1 GALLEY
SERVICE DOOR
1 AFT PASSENGER
ENTRANCE DOOR
4 TYPICAL EMERGENCY
EXIT DOORS
3 CUT-IN AREA
1 FORWARD SERVICE
ENTRY DOOR
AFT CARGO
COMPARTMENT DOORS
FORWARD CARGO
COMPARTMENT DOORS
1 FORWARD PASSENGER
ENTRANCE DOOR
ACCESS TO ACCESSORY
COMPARTMENT
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.2.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-61 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.2.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-62 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
TYPICAL HYDRAULIC
PUMP
HYDRAULIC ACCUMULATORS
LOCATED IN RIGHT WHEEL
WELL
PASSENGER OXYGEN
BOTTLES
FUEL TANKS
HYDRAULIC SUMP
LOCATED IN LEFT WHEEL
WELL
8950 GAL 33879 L
CREW OXYGEN SYSTEM
BOTTLE
HYDRAULIC ACCUMULATOR LOCATED
IN LEFT WING ROOT
MAIN HYDRAULIC
RESERVOIR LOCATED IN
LEFT WING ROOT
6400 GAL 24227 L
FUEL TANK
8950 GAL 33879 L
HYDRAULIC SUMPS
SURGE DAMPER
LOCATED IN LEFT
WING ROOT
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.3.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8-62 SERIES
1 PASSENGER AND
SERVICE DOORS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 CUT-IN AREAS
CUT-IN AREAS
2 EMERGENCY EXIT
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.3.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-62 SERIES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
1 AFT SERVICE
ENTRANCE DOOR
2 TYPICAL EMERGENCY
EXITS
1 AFT PASSENGER
ENTRANCE DOOR
BREAK GLASS FOR ACCESS
TO HANDLE AND SLIDE
WINDOW AFT
1 FORWARD SERVICE
ENTRY DOOR
3 CUT-IN AREAS
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
ACCESS TO ACCESSORY
COMPARTMENT
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.3.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-62 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.3.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-63 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
SURGE DAMPER
HYDRAULIC ACCUMULATORS
LOCATED IN RIGHT WHEEL WELL
TYPICAL
HYDRAULIC PUMP
PASSENGER OXYGEN
BOTTLES
HYDRAULIC SUMP
LOCATED IN LEFT WHEEL
WELL
HYDRAULIC ACCUMULATOR LOCATED
IN LEFT WING ROOT
8950 GAL 33879 L
FUEL TANKS
MAIN HYDRAULIC
RESERVOIR LOCATED IN
LEFT WING ROOT
6400 GAL 24227 L
FUEL TANK
8950 GAL 33879 L
OXYGEN BOTTLES
HYDRAULIC SUMPS
SURGE DAMPER
LOCATED IN LEFT
WING ROOT
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.4.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-63 SERIES
1 PASSENGER AND
SERVICE DOORS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
EMERGENCY RESCUE ACCESS-1
2 OVERWING EMERGENCY
EXITS
3 FORWARD UPPER CARGO DOOR
EXTERNAL CONTROL PANEL
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
4 EMERGENCY EXIT DOORS
TO OPEN DOOR:
1. PUSH LOCKPIN HANDLE DOWN AND HOLD.
2. INSERT WRENCH IN HEX END OF DOOR
HANDLE SHAFT AND ROTATE.
COUNTERCLOCKWISE TO UNLATCH
3. ATTACH SLING TO DOOR AND HOIST DOOR
OPEN.
5 CUT-IN AREAS
CUT-IN AREAS
TO OPEN DOOR:
1. PULL HANDLE FROM
RECESS.
2. ROTATE HANDLE
FORWARD.
3. PULL DOOR OPEN.
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.4.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-63 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
1 AFT SERVICE
ENTRANCE DOOR
4 EMERGENCY EXIT
DOORS ON SOME
AIRPLANES
2 OVERWING
EMERGENCY EXITS
1 GALLEY SERVICE
DOOR ON SOME
AIRPLANES
1 AFT PASSENGER
ENTRANCE DOOR
4 TYPICAL EMERGENCY
EXIT DOORS
5 CUT-IN AREA
AFT CARGO
COMPARTMENT DOORS
1 FORWARD SERVICE
ENTRY DOOR
5 CUT-IN AREA
FORWARD CARGO
COMPARTMENT DOORS
3 EXTERNAL CONTROL
PANEL
1 FORWARD UPPER
CARGO DOOR
1 FORWARD PASSENGER
ENTRANCE DOOR
ACCESS TO ACCESSORY
COMPARTMENT
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOW
EXTERIOR ACCESS
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.4.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-63 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.4.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-71 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC
ACCUMULATORS LOCATED
IN RIGHT WHEEL WELL
HYDRAULIC ACCUMULATOR
SPOILER RESERVOIR
LOCATED IN RIGHT
WHEEL WELL
PASSENGER OXYGEN
BOTTLES
HYDRAULIC RUDDER
RESERVOIR LOCATED IN
LEFT WHEEL WELL
HYDRAULIC
ACCUMULATOR LOCATED
IN LEFT WHEEL WELL
8950 GAL 33879 L
FUEL TANKS
HYDRAULIC RESERVOIRS
LOCATED IN LEFT WING
ROOT
6400 GAL 24227 L
FUEL TANK
8950 GAL 33879 L
OXYGEN BOTTLES
OPTIONAL APU
AUXILIARY HYDRAULIC
PUMP
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.5.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8-71 SERIES
1 PASSENGER AND
SERVICE DOORS
2 OVERWING EMERGENCY
EXITS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 FORWARD UPPER CARGO DOOR
EXTERNAL CONTROL PANEL
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
4 EMERGENCY EXIT DOORS
TO OPEN DOOR:
1. PUSH LOCKPIN HANDLE DOWN AND HOLD
2. INSERT WRENCH IN HEX END OF DOOR
HANDLE SHAFT AND ROTATE.
COUNTERCLOCKWISE TO UNLATCH
3. ATTACH SLING TO DOOR AND HOIST DOOR
OPEN.
5 CUT-IN AREAS
CUT-IN AREAS
TO OPEN DOOR:
1. PULL HANDLE FROM
RECESS.
2. ROTATE HANDLE
FORWARD.
3. PULL DOOR OPEN.
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.5.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-71 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
1 AFT SERVICE
ENTRANCE DOOR
4 EMERGENCY EXIT
DOORS ON SOME
AIRPLANES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
2 OVERWING
EMERGENCY EXITS
1 GALLEY SERVICE
DOOR ON SOME
AIRPLANES
1 AFT PASSENGER
ENTRANCE DOOR
4 TYPICAL EMERGENCY
EXIT DOORS
5 CUT-IN AREA
AFT CARGO
COMPARTMENT DOORS
1 FORWARD SERVICE
ENTRY DOOR
5 CUT-IN AREA
FORWARD CARGO
COMPARTMENT DOORS
3 EXTERNAL CONTROL
PANEL
1 FORWARD UPPER
CARGO DOOR
1 FORWARD PASSENGER
ENTRANCE DOOR
ACCESS TO ACCESSORY
COMPARTMENT
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOW
EXTERIOR ACCESS
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.5.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-71 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.5.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-72 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC
ACCUMULATORS LOCATED
IN RIGHT WHEEL WELL
HYDRAULIC ACUMULATOR
TYPICAL
HYDRAULIC PUMP
PASSENGER OXYGEN
BOTTLES
HYDRAULIC RUDDER
RESERVOIR IN LEFT
WHEEL WELL
FUEL TANKS
8950 GAL 33879 L
HYDRAULIC ACCUMULATOR
LOCATED IN LEFT WING ROOT
MAIN HYDRAULIC
RESERVOIR LOCATED IN
LEFT WING ROOT
6400 GAL 24227 L
FUEL TANK
8950 GAL 33879 L
OXYGEN BOTTLES
OPTIONAL
APU
HYDRAULIC
RESERVOIR
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.6.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8-72 SERIES
1 PASSENGER AND
SERVICE DOORS
2 OVERWING EMERGENCY
EXITS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 FORWARD UPPER CARGO DOOR
EXTERNAL CONTROL PANEL
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
4 EMERGENCY EXIT DOORS
TO OPEN DOOR:
1. PUSH LOCKPIN HANDLE DOWN AND HOLD.
2. INSERT WRENCH IN HEX END OF DOOR
HANDLE SHAFT AND ROTATE
COUNTERCLOCKWISE TO UNLATCH.
3. ATTACH SLING TO DOOR AND HOIST DOOR
OPEN.
5 CUT-IN AREAS
CUT-IN AREAS
TO OPEN DOOR:
1. PULL HANDLE FROM
RECESS.
2. ROTATE HANDLE
FORWARD.
3. PULL DOOR OPEN.
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.6.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-72 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
1 AFT SERVICE
ENTRANCE DOOR
4 EMERGENCY EXIT
DOORS ON SOME
AIRPLANES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
2 OVERWING
EMERGENCY EXITS
1 AFT PASSENGER
ENTRANCE DOOR
5 CUT-IN AREA
5 CUT-IN AREA
AFT CARGO
COMPARTMENT DOORS
1 FORWARD SERVICE
ENTRY DOOR
1 FORWARD PASSENGER
ENTRANCE DOOR
3 EXTERNAL CONTROL
PANEL
1 FORWARD UPPER
CARGO DOOR
AVERAGE DISTANCE
ACCESS TO ACCESSORY
COMPARTMENT
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
CLEARVIEW WINDOW
EXTERIOR ACCESS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.6.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-72 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.6.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-8-73 SERIES
FLAMMABLE MATERIAL LOCATIONS
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
HYDRAULIC ACCUMULATOR
TYPICAL HYDRAULIC
PUMP IN 4 PLACES
HYDRAULIC
ACCUMULATORS LOCATED
IN RIGHT WHEEL WELL
SPOILER RESERVOIR
LOCATED IN RIGHT
WHEEL WELL
PASSENGER OXYGEN
BOTTLES
HYDRAULIC RUDDER
RESERVOIR LOCATED IN
LEFT WHEEL WELL
8950 GAL 33879 L
FUEL TANKS
HYDRAULIC ACCUMULATOR
LOCATED IN LEFT WING ROOT
MAIN HYDRAULIC
RESERVOIR LOCATED IN
LEFT WING ROOT
6400 GAL 24227 L
FUEL TANK
8950 GAL 33879 L
OXYGEN BOTTLES
HYDRAULIC SUMPS
OPTIONAL APU
ENGINE OIL TANKS
HYDRAULIC ACCUMULATORS LOCATED IN
NOSEWHEEL WELL
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.7.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-8-73 SERIES
1 PASSENGER AND
SERVICE DOORS
2 OVERWING EMERGENCY
EXITS
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE FORWARD.
3. PULL DOOR OPEN.
3 FORWARD UPPER CARGO DOOR
EXTERNAL CONTROL PANEL
TO OPEN DOOR:
1. HOLD HANDLE.
2. PUSH RELEASE PLATE (HANDLE
ON SOME AIRPLANES ONLY).
4 EMERGENCY EXIT DOORS
TO OPEN DOOR:
1. PUSH LOCKPIN HANDLE DOWN AND HOLD.
2. INSERT WRENCH IN HEX END OF DOOR
HANDLE SHAFT AND ROTATE.
COUNTERCLOCKWISE TO UNLATCH
3. ATTACH SLING TO DOOR AND HOIST DOOR
OPEN.
5 CUT-IN AREAS
CUT-IN AREAS
TO OPEN DOOR:
1. PULL HANDLE FROM
RECESS.
2. ROTATE HANDLE
FORWARD.
3. PULL DOOR OPEN.
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.7.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-8-73 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
1 AFT SERVICE
ENTRANCE DOOR
4 EMERGENCY EXIT
DOORS ON SOME
AIRPLANES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
2 OVERWING
EMERGENCY EXITS
1 GALLEY SERVICE
DOOR ON SOME
AIRPLANES
1 AFT PASSENGER
ENTRANCE DOOR
4 TYPICAL EMERGENCY
EXIT DOORS
5 CUT-IN AREA
AFT CARGO
COMPARTMENT DOORS
1 FORWARD SERVICE
ENTRY DOOR
5 CUT-IN AREA
FORWARD CARGO
COMPARTMENT DOORS
3 EXTERNAL CONTROL
PANEL
1 FORWARD UPPER
CARGO DOOR
1 FORWARD PASSENGER
ENTRANCE DOOR
ACCESS TO ACCESSORY
COMPARTMENT
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOW
EXTERIOR ACCESS
WHEELS RETRACTED: 9 FT.
WHEELS EXTENDED: 13 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-8.7.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-8-73 SERIES
MAIN BATTERY
LOCATED IN RIGHT
WHEEL WELL
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-8.7.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-9 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-9 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use
caution when moving across sections of aircraft that have
been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before
moving their weight and equipment across it. Signs could
include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface
integrity can be checked with a pike pole, axe or any
instrument used to sound surfaces for integrity.
780/1000 GALLONS
2953/3785 LITERS
2
APU EXHAUST DUCT ON
RIGHT SIDE ONLY
FUEL VENT BOX
ENGINE OIL
TANKS
FUEL OVERFLOW
STAND PIPE
HYDRAULIC
ACCUMULATORS
OPTIONAL AUXILIARY
FUEL TANK
OPTIONAL AUXILIARY
FUEL TANK
FIRE EXTINGUISHER AGENT
CONTAINERS
1386 GAL 5247 L
1
580/780/100/1250 GALLONS
2196/2953/3785/4732 LITERS
APU GROUND CONTROL
PANEL ON FUSELAGE
2
PORTABLE OXYGEN
BOTTLE
FUEL TANKS
907 GAL 3433 L
HYDRAULIC ACCUMULATORS
1
FUEL TANK
1386 GAL - 5247 L
CREW OXYGEN SYSTEM
BOTTLES
FUEL VENT BOX
HYDRAULIC FLUID
RESERVOIR 1 PLACE IN
EACH WHEEL WELL
RAIN REPELLENT
CONTAINERS
PORTABLE OXYGEN
SYSTEM BOTTLE
CREW PORTABLE OXYGEN
SYSTEM BOTTLES
FUEL OVERFLOW
STAND PIPE
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-9.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-9 SERIES
1 PASSENGER AND SERVICE DOORS
2 OVERWING EMERGENCY EXIT
3 TAIL CONE JETTISON LATCH
INTERIOR
TO OPEN DOOR:
1. PUSH HANDLE.
2. PULL HANDLE AND AT THE SAME TIME, PUSH
IN ON TOP OF DOOR.
3. LIFT UP FORCIBLY.
TO OPEN DOOR:
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE.
3. PULL DOOR OPEN.
EXTERIOR
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-9.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-9 SERIES
JETTISONABLE TAIL
CONE
APU COMPARTMENT
ACCESS DOOR
TAIL CONE ACCESS
DOOR
AFT LOWER CARGO
COMPARTMENT DOOR
3 TAIL CONE
JETTISON LATCH
2 OVERWING
EMERGENCY EXITS
FORWARD LOWER
CARGO DOOR
PASSENGER AFT ENTRANCE STAIRWAY
INTERRIOR CONTROL PANEL ON SOME
AIRPLANES
1 FORWARD SERVICE
ENTRANCE DOOR
ENGINE NACELLE LOWER
COWL DOOR
CLEARVIEW WINDOWCHILL PANE WITH CO2
AND BREAK WITH HEAVY
FIRE AXE FOR ACCESS
TO HANDLE; SLIDE
WINDOW AFT
4 CUT-IN AREAS
MAIN CARGO DOOR AND
EXTERNAL CONTROL PANEL ON
CARGO AIRPLANES ONLY
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOW- EXTERIOR ACCESS
KNOCKOUT PANEL ON CARGO
AIRPLANES
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
WHEELS RETRACTED: 4 FT.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-9.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-9 SERIES
BATTERY
BATTERY QUICK
DISCONNECT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-9.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
DC-9 SERIES
APU CONTROL PANEL
AGENT
1
LOW
1
AGENT
DISCH
E
N
G
F
I
R
E
PULL
2
LOOPS A
TEST
AGENT
2
LOW
FIRE
BELL OFF
6
1
LOOPS B
TEST
AGENT
DISCH
2
5 FIRE AGENT NO 2
E
N
G
F
I
R
E
PULL
7
8
APU
5
0
4 `C x 1001
3 2
4 FIRE AGENT NO 1
FIRE AGENT
NO 1
NO 2
OFF
DISCH
FIRE CONT
NORM
OFF &
AGENT ARM
B,D,E - “ENG FIRE”
HANDLES
9 01
10
8
2
20
7
3 APU
6
30
1005 4
PERCENT40
90 RPM
80 6050
70
EXHTEMP
APU
AIR
OFF
ON DOORS
AUTO
AIR COND
COLDER
MASTER OFF
OFF
NON
RAM
RUN
RAM
START
1 MASTER OFF
3 FIRE CONT
C - PULL
WARNING
MISC CAUTION
APU OIL
TEMP HI
APU OIL
PRESS LOW
APU FIRE
2 “APU FIRE” LIGHT
ENGINE SHUTDOWN AND FIRE PROCEDURE:
APU SHUTDOWN AND FIRE PROCEDURE:
A. FUEL CONTROL LEVER(S) FROM “ON” TO “OFF” (DOWN).
1. APU “MASTER OFF” SWITCH TO “OFF” (UP).
B. IF LIGHT(S) IN HANDLES ARE ILLUMINATED...
2. IF “APU FIRE” LIGHT IN OVERHEAD PANEL IS
ILLUMINATED...FIRE CONT SW TO “OFF & AGENT ARM”.
C. PULL HANDLES FULLY OUT.
D. ROTATE HANDLE CLOCKWISE.
E. AFTER 10 SECONDS, ROTATE HANDLES
COUNTERCLOCKWISE.
A - FUEL CONTROL LEVERS
3. FIRE AGENT NO 1 SWITCH TO “DISCH” (DOWN).
4. AFTER 10 SECONDS FIRE AGENT NO 2 SWITCH TO
“DISCH” (DOWN).
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-9.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
DC-9 SERIES
2 FIRE LIGHT
3 FIRE AGENT 1
APU SHUTDOWN AND FIRE PROCEDURE:
4 FIRE AGENT 2
1. “APU SHUT OFF” SWITCH TO “SHUT OFF” (UP.)
2. IF “FIRE” LIGHT IS ILLUMINATED:
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP)
4. AFTER 10 SECONDS, FIRE AGENT NO 2 SWITCH TO
“DISCHARGE” (UP.)
1 APU SHUT
OFF SWITCH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-9.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
DC-10 SERIES
FLAMMABLE MATERIAL LOCATIONS
DC-10 (tab)
HOT BRAKES
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
Water mist: Can be deployed from turret or handline.
fragmentation hazard.
ENGINE 2 FUEL FIRE SHUTOFF VALVE
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
ENGINE 2 HYDRAULIC FIRE SHUTOFF VALVE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
ENGINE 2 / APU FIRE EXTINGUISHER AGENT CONTAINERS
temperature is excessive.
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across sections of aircraft that
have been exposed to fatigue or fire as the result of an accident. Crews need to verify the integrity of the surface
area before moving their weight and equipment across it. Signs could include but are not limited to deformity of
structure, visual signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike pole,
axe or any instrument used to sound surfaces for integrity.
PORTABLE OXYGEN
BOTTLES
OVERBOARD VENT
OUTLET
FUEL VENT BOX
ENGINE 2 OIL
TANK
HYDRAULIC FLUID
RESERVOIR
FUEL
TANKS
HYDRAULIC
ACCUMULATORS
IN RIGHT WHEEL
WELL
TYPICAL PRESSURE
REFUELING ADAPTER
APU EXHAUST DUCT ON
RIGHT SIDE ONLY
ENGINE 3 FUEL FIRE SHUTOFF VALVE
ENGINE 3 HYDRAULIC FIRE SHUTOFF VALVE
6000 GAL 22712 L
ENGINE 3 FIRE EXTINGUISHER
AGENT CONTAINERS
FIRE EXTINGUISHERS
HYDRAULIC ACCUMULATORS IN
LEFT WHEEL WELL
OPTIONAL AUXILIARY
FUEL TANK
9700 GAL 36718 L
HYDRAULIC RESERVOIRS IN
WHEEL WELLS
ENGINE 3 OIL TANK
FUEL TANK
14600GAL 55267 L
CREW OXYGEN SYSTEM
BOTTLES
6000 GAL - 22712 L
FUEL VENT BOX
OVERBOARD
VENT OUTLET
OXYGEN
BOTTLES
RAIN REPELLENT
CONTAINERS
ENGINE 1 FUEL FIRE SHUTOFF VALVE
LOWER CARGO FIRE
EXTINGUISHER
CONTAINER
ENGINE 1 OIL TANK
PORTABLE OXYGEN
BOTTLES
FIRE EXTINGUISHERS
ENGINE 1 HYDRAULIC FIRE SHUTOFF VALVE
ENGINE 1 FIRE EXTINGUISHER
AGENT CONTAINERS
FIRE
EXTINGUISHERS
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-10.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
DC-10 SERIES
1 PASSENGER AND SERVICE DOORS
PUSH BUTTON TYPE
NOTE:
NON PUSH BUTTON TYPE
WHEN MOVED TO “EMERGENCY” POSITION AND HELD, ALLOWS DOOR
CONTROL HANDLE TO BE MOVED TO “EMERGENCY” POSITION FOR
EMERGENCY OPENING OF THE DOOR IF ELECTRICAL POWER IS NOT
AVAILABLE.
NOTE:
WHENPLACED IN “EMERGENCY” POSITION, DOOR CONTROL HANDLE WILL
REMAIN IN THAT POSITION.
EMERGENCY
OPENING
BUTTON
EMERGENCY
OVERRIDE LEVER
AUXILARY HANDLE
AUXILARY
HANDLE
DOOR
CONTROL
SWITCH
DOOR CONTROL
HANDLE
DOOR CONTROL
HANDLE
POSITIVE
STOP AT
CLOSE
POSITION
NEUTRAL
DETENT
POSITIVE STOP AT
OPEN POSITION DURING
NORMAL OPERATION
MANUAL DRIVE
(LEFT FWD DOOR
ONLY) (SOME
AIRPLANES)
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-10.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
DC-10 SERIES
2 CARGO ACCESS DOORS
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF
STRUCTURE AND POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT
TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE
NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-10.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-3
DC-10 SERIES
3 UPPER CARGO DOOR
(CONVERTIBLE FREIGHTER AIRPLANES ONLY)
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-10.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-4
DC-10 SERIES
AFT ACCESSORY
COMPARTMENT DOOR
APU COMPARTMENT DOOR
1 PASSENGER AND
SERVICE DOORS
2 FORWARD
CARGO DOOR
PRESSURE BULKHEAD
HORIZONTAL STABILIZER JACK SCREWS
AND MOTORS ACCESS DOOR
4 CUT-IN AREAS
2 AFT CARGO DOOR
1 FORWARD SERVICE
ENTRANCE DOOR
2 CENTER CARGO DOOR
4 CUT-IN AREAS
1 PASSENGER
ENTRANCE DOOR
3 UPPER CARGO DOOR ON
CONVERTIBLE FREIGHTER
AIRPLANES ONLY
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOW CUT-IN AREA
WHEELS RETRACTED: 4 FT.
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-10.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
DC-10 SERIES
CENTER ACCESSORY
COMPARTMENT LOOKING
AFT
TYPICAL BATTERY SENSOR
ELECTRICAL CONNECTOR
MAIN BATTERY
BATTERY
CHARGER
TYPICAL OVERBOARD
VENT IN 2 PLACES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-10.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
DC-10 SERIES
3 - ENG FIRE HANDLE
COVERS
80
70
90 100110
120
60
50
40
30 20
2
1 APU MASTER
0
80
70
% RPM
1
QT
0 OIL QTY
APU
CYL 1
CYL 2
DISCH
7
EXH TEMP
APU
90 100110
120
60
50
40
30 20
N2
APU
% RPM
5 CYL 2
OFF
APU
FIRE
FIRE CONTROL
APU OFF
AGENT ARM
10 0
NORM
APU OIL APU FUEL
APU USING PRESS
LO/
BAT PWR
TEMP HI PRESS LO
APU MASTER
START
4 CYL 1
APU
FIRE AGENT
5
6
6 7 8
5
4
3
2
10 0
4
3
1
N1
APU
STBY
ON
FUEL
PUMP
CONT SYS
STBY
OFF
NORM
2 APU FIRE
3 APU OFF &
AGENT ARE
RUN
OFF
ELEC PWR SYS
4,5,6 - ENG FIRE HANDLE
OFF
2 - ENG FIRE HANDLE
FLIGHT ENGINEER’S UPPER
INSTRMENT PANEL NO. 1
APU SHUTDOWN AND FIRE PROCEDURE
1. “APU MASTER” SWITCH TO “OFF” (DOWN).
NOSE
DN
UP
UP
0
0
RET
3. “APU OFF & AGENT ARM” SWITCH TO “AGENT
ARM” (UP)
ALTN
LONG TRIM
RET
4. APU FIRE AGENT “CYL 1” SWITCH TO
“DISCHARGE” (UP)
T.O.
EXT
PARK
BRK
1/3
2
0
SPD
BRK
4
15
15
15
22
22
22
2/3
2
ON
ON
35
FULL
UP
35
LAND
EXT
8
FUEL
10
FUEL
50
50
NOSE
UP
GROUND
SPOILER
OFF
OFF
LONG TRIM
7
8
9
0
11
12
14
ENGINE SHUTDOWN AND FIRE PROCEDURE:
FLAP T.O.
SEL
6
PARK
2. IF “APU FIRE” LIGHT IS ILLUMINATED:
SLAT
FLAP
GEAR
HORN
OFF
1. FUEL LEVER(S) FROM “ON” TO “OFF” (DOWN)
5. AFTER 30 SECONDS , APU FIRE AGENT “CYL 2”.
SWITCH TO “DISCHARGE” (UP.)
2. IF LIGHT(S) IN FUEL LEVER(S) OR “ENG FIRE”
HANDLE(S) ARE ILLUMINATED:
3. LIFT “ENG/FIRE” HANDLE COVER(S)
4. PULL HANDLE(S) DOWN AND FORWARD
5. WHILE HOLDING FORWARD PRESSURE ON HANDLE,
TWIST HANDLE CLOCKWISE AND HOLD
1,2 - FUEL LEVERS
6. AFTER 30 SECONDS, TWIST HANDLE
COUNTERCLOCKWISE.
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
DC-10.0.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
DC-10 SERIES
3 FIRE AGENT 1
4 FIRE AGENT 2
APU SHUTDOWN AND FIRE PROCEDURE:
2 APU FIRE LIGHT
APU
FIRE
AGENT
1
LOW
AGENT
2
LOW
1. TURN APU SWITCH TO “OFF” (UP).
FIRE AGENT 1
DISCHARGE
2. IF APU FIRE LIGHT IS ON...
DISCHARGE
SERVICE
INTERPHONE
APU OFF
AGENT ARM
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP).
4. AFTER 30 SECONDS, FIRE AGENT 2 SWITCH TO
“DISCHARGE” (UP).
FIRE AGENT 2
OFF
1 APU SWITCH
HORN
NORMAL
NORMAL
NORMAL
NORMAL
ON
OFF
SERVICE LIGHT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
DC-10.0.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
MD-11 SERIES
FLAMMABLE MATERIAL LOCATIONS
MD-11 (tab)
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
ENGINE 2 FUEL FIRE SHUTOFF VALVE
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
ENGINE 2 HYDRAULIC FIRE SHUTOFF VALVE
ENGINE 2 / APU FIRE EXTINGUISHER AGENT CONTAINERS
ENGINE 2 OIL
TANK
PORTABLE OXYGEN
BOTTLES
UPPER CARGO FIRE
EXTINGUISHER ON
COMBI ONLY
OVERBOARD VENT
OUTLET
FUEL VENT BOX
FUEL
TANKS
HYDRAULIC FLUID
RESERVOIR
HYDRAULIC
ACCUMULATORS
IN RIGHT WHEEL
WELL
TYPICAL PRESSURE REFUELING
ADAPTER
1958 GALLONS
7412 LITERS
APU EXHAUST DUCT ON
RIGHT SIDE ONLY
ENGINE 3 FUEL FIRE SHUTOFF VALVE
ENGINE 3 HYDRAULIC FIRE SHUTOFF VALVE
ENGINE 3 FIRE EXTINGUISHER
AGENT CONTAINERS
FIRE EXTINGUISHERS
6100 GAL 23091 L
HYDRAULIC ACCUMULATORS IN LEFT WHEEL WELL
AUXILIARY FUEL TANK
HYDRAULIC RESERVOIRS IN WHEEL WELLS
9700 GAL 36718 L
ENGINE 3 OIL TANK
ENGINE 2 FORWARD FUEL FIRE SHUTOFF VALVE
FUEL VENT BOX
14600 GAL 55267 L
FUEL TANK
CREW FIXED OXYGEN
SYSTEM BOTTLES
OVERBOARD
VENT OUTLET
6100 GAL - 23091 L
APU FUEL FIRE SHUTOFF VALVE
RAIN REPELLENT
CONTAINERS
ENGINE 1 FUEL FIRE SHUTOFF VALVE
ENGINE 1 HYDRAULIC FIRE SHUTOFF VALVE
LOWER CARGO FIRE
EXTINGUISHER CONTAINER
PORTABLE OXYGEN FIRE EXTINGUISHERS
BOTTLES
ENGINE 1 FIRE EXTINGUISHER
AGENT CONTAINERS
ENGINE 1 OIL TANK
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-11.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
MD-11 SERIES
1 PASSENGER AND SERVICE DOORS
PUSH BUTTON TYPE
NOTE:
NON PUSH BUTTON TYPE
WHEN MOVED TO “EMERGENCY” POSITION AND HELD, ALLOWS DOOR
CONTROL HANDLE TO BE MOVED TO “EMERGENCY” POSITION FOR
EMERGENCY OPENING OF THE DOOR IF ELECTRICAL POWER IS NOT
AVAILABLE.
NOTE:
WHENPLACED IN “EMERGENCY” POSITION, DOOR CONTROL HANDLE WILL
REMAIN IN THAT POSITION.
EMERGENCY
OPENING
BUTTON
EMERGENCY
OVERRIDE LEVER
AUXILARY HANDLE
AUXILARY
HANDLE
DOOR
CONTROL
SWITCH
DOOR CONTROL
HANDLE
DOOR CONTROL
HANDLE
POSITIVE
STOP AT
CLOSE
POSITION
NEUTRAL
DETENT
POSITIVE STOP AT
OPEN POSITION DURING
NORMAL OPERATION
MANUAL DRIVE
(LEFT FWD DOOR
ONLY) (SOME
AIRPLANES)
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-11.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
MD-11 SERIES
2 CARGO ACCESS DOORS
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING PORTABLE
POWER EQUIPMENT. BECAUSE OF TYPE OF
STRUCTURE AND POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT MAJOR EFFORT
TO GAIN ACCESS BE DIRECTED TO HATCHES AND
DOORS. URGENCY OF SITUATION WILL DICTATE THE
NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-11.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
MD-11 SERIES
EMERGENCY RESCUE ACCESS-3
3 UPPER CARGO DOOR
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-11.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-4
MD-11 SERIES
AFT ACCESSORY
COMPARTMENT DOOR
APU COMPARTMENT DOOR
1 PASSENGER AND
SERVICE DOORS
FORWARD CARGO
DOOR
PRESSURE BULKHEAD
HORIZONTAL STABILIZER JACK SCREWS
AND MOTORS ACCESS DOOR
4 CUT-IN AREAS
2 AFT CARGO DOOR
UPPER CARGO DOOR ON COMBI ONLY
1 FORWARD SERVICE
ENTRANCE DOOR
2 CENTER CARGO DOOR
AVIONICS
COMPARTMEN
T DOORS
4 CUT-IN AREAS
1 PASSENGER
ENTRANCE DOOR
3 UPPER CARGO DOOR ON
CONVERTIBLE FREIGHTER
AIRPLANES ONLY
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
CLEARVIEW WINDOWCUT-IN AREA
WHEELS RETRACTED: 4 FT.
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-11.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
MD-11 SERIES
CENTER ACCESSORY
COMPARTMENT LOOKING
AFT
TYPICAL BATTERY SENSOR
ELECTRICAL CONNECTOR
MAIN BATTERY
BATTERY
CHARGER
TYPICAL OVERBOARD
VENT IN 2 PLACES
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-11.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
MD-11 SERIES
2,3 APU FIRE HANDLE
3 - ENG/FIRE HANDLE GUARD
4 - ENG/FIRE HANDLE
ENG/APU
FIRE TEST
AGENT DISCH
APU FIRE
1 PULL/TURN 2
APU START/STOP SWITCH
START/
STOP
ON
OFF
APU
FUEL
FAIL
DOOR
APU
GEN
OFF
2,5,6 - ENG/FIRE HANDLE
AFT OVERHEAD PANEL
AFT OVERHEAD PANEL
APU SHUTDOWN AND FIRE PROCEDURE
1. PUSH APU START/STOP SWITCH TO OFF.
2. IF “APU FIRE” LIGHT IN HANDLE IS ILLUMINATED:
1
ENG START
2
3. PULL AND ROTATE APU FIRE HANDLE IN EITHER
DIRECTION
3
4. AFTER 30 SECONDS , PULL AND ROTATE APU FIRE
HANDLE IN THE OPPOSITE DIRECTION.
ENGINE SHUTDOWN AND FIRE PROCEDURE:
ON
FUEL
ON
ON
1. FUEL SWITCH(ES) FROM “ON” TO “OFF” (DOWN.)
2. IF LIGHT(S) IN FUEL SWITCH(ES) OR “ENG FIRE”
HANDLE(S) ARE ILLUMINATED:
OFF
OFF
OFF
1 - ENGINE FUEL SWITCHES
3. LIFT “ENG/FIRE” HANDLE GUARD(S)
4. PULL HANDLE(S) DOWN AND FORWARD
5. WHILE HOLDING FORWARD PRESSURE ON HANDLE,
TWIST HANDLE CLOCKWISE AND HOLD
6. AFTER 30 SECONDS, TWIST HANDLE
COUNTERCLOCKWISE.
CONTROL STAND
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-11.0.7
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
MD-11 SERIES
3 FIRE AGENT 1
4 FIRE AGENT 2
APU SHUTDOWN AND FIRE PROCEDURE:
2 APU FIRE LIGHT
APU
FIRE
AGENT
1
LOW
AGENT
2
LOW
1. TURN APU SWITCH TO “OFF” (UP).
FIRE AGENT 1
DISCHARGE
2. IF APU FIRE LIGHT IS ON...
DISCHARGE
SERVICE
INTERPHONE
APU OFF
AGENT ARM
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP).
4. AFTER 30 SECONDS, FIRE AGENT 2 SWITCH TO
“DISCHARGE” (UP).
FIRE AGENT 2
OFF
1 APU SWITCH
HORN
NORMAL
NORMAL
NORMAL
NORMAL
ON
OFF
SERVICE LIGHT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-11.0.8
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
MD-80 SERIES
FLAMMABLE MATERIAL LOCATIONS
MD-80 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
565/780/1160 GALLONS
2
APU EXHAUST DUCT ON
RIGHT SIDE ONLY
HYDRAULIC
ACCUMULATORS
FUEL VENT BOX
ENGINE OIL
TANKS
FUEL OVERFLOW
STAND PIPE
HYDRAULIC
ACCUMULATORS
OPTIONAL AUXILIARY
FUEL TANK
FIRE EXTINGUISHER AGENT
CONTAINERS
565/780 GALLONS
1
APU GROUND CONTROL
PANEL ON FUSELAGE
1397 GAL 5288 L
OPTIONAL AUXILIARY
FUEL TANK
HYDRAULIC FLUID
RESERVOIR 1 PLACE IN
EACH WHEEL WELL
2
FUEL TANKS
3044 GAL 11523 L
FUEL TANK
FUEL OVERFLOW
STAND PIPE
1397 GAL - 5288 L
FUEL VENT BOX
PORTABLE OXYGEN
BOTTLES
HYDRAULIC ACCUMULATORS
1
RAIN REPELLENT
CONTAINERS
CREW PORTABLE OXYGEN
SYSTEM BOTTLES
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-80.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
MD-80 SERIES
1 PASSENGER AND SERVICE
DOORS
TO OPEN DOOR
1. PULL HANDLE FROM RECESS.
2. ROTATE HANDLE.
3. PULL DOOR OPEN.
2 OVERWING EMERGENCY EXIT
3 TAIL CONE JETTISON LATCH
TO OPEN DOOR
1. PUSH HANDLE.
2. PULL HANDLE AND PUSH IN ON TOP OF DOOR.
3. LIFT UP FORCIBLY.
4 CUT-IN AREAS
CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL DICTATE
THE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-80.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
MD-80 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU COMPARTMENT
ACCESS DOOR
JETTISONABLE TAIL
CONE
AFT LOWER CARGO
COMPARTMENT DOOR
TAIL CONE ACCESS
DOOR
2 OVERWING
EMERGENCY EXITS
3 TAIL CONE
JETTISON LATCH
FORWARD CARGO
COMPARTMENT DOOR
1 FORWARD SERVICE
ENTRANCE DOOR
PASSENGER AFT ENTRANCE STAIRWAY
INTERIOR CONTROL PANEL ON SOME
AIRPLANES
ENGINE NACELLE LOWER
COWL DOOR
MID CARGO
COMPARTMENT DOOR
4 CUT-IN AREAS
CLEARVIEW WINDOWCHILL PANE WITH CO2
AND BREAK WITH HEAVY
FIRE AXE FOR ACCESS
TO HANDLE; SLIDE
WINDOW AFT
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 4 FT.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-80.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
MD-80 SERIES
BATTERY
BATTERY QUICK
DISCONNECT
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-80.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
MD-80 SERIES
APU CONTROL PANEL
AGENT
1
LOW
1
AGENT
DISCH
E
N
G
F
I
R
E
PULL
2
LOOPS A
TEST
AGENT
2
LOW
FIRE
BELL OFF
6
1
LOOPS B
TEST
AGENT
DISCH
5
2
5 FIRE AGENT NO 2
E
N
G
F
I
R
E
PULL
7
8
APU
0
4 `C x 1001
3 2
4 FIRE AGENT NO 1
FIRE AGENT
NO 1
NO 2
OFF
DISCH
FIRE CONT
NORM
OFF &
AGENT ARM
B,D,E - “ENG FIRE”
HANDLES
9 01
10
8
2
20
7
3 APU
6
30
1005 4
PERCENT40
90 RPM
50
80 60
70
EXHTEMP
APU
AIR
OFF
ON DOORS
AUTO
AIR COND
COLDER
MASTER OFF
OFF
NON
RAM
RUN
RAM
START
1 MASTER OFF
3 FIRE CONT
C - PULL
WARNING
MISC CAUTION
APU OIL
TEMP HI
APU OIL
PRESS LOW
APU FIRE
2 “APU FIRE” LIGHT
ENGINE SHUTDOWN AND FIRE PROCEDURE:
APU SHUTDOWN AND FIRE PROCEDURE
A. FUEL CONTROL LEVER(S) FROM “ON” TO “OFF” (DOWN).
1. APU “MASTER OFF” SWITCH TO “OFF” (UP).
B. IF LIGHT(S) IN HANDLES ARE ILLUMINATED...
2. IF “APU FIRE” LIGHT IN OVERHEAD PANEL IS
ILLUMINATED...FIRE CONT SW TO “OFF & AGENT ARM”
C. PULL HANDLES FULLY OUT.
D. ROTATE HANDLE CLOCKWISE.
E. AFTER 10 SECONDS, ROTATE HANDLES
COUNTERCLOCKWISE.
A - FUEL CONTROL LEVERS
3. FIRE AGENT NO 1 SWITCH TO “DISCH” (DOWN).
4. AFTER 10 SECONDS FIRE AGENT NO 2 SWITCH TO
“DISCH” (DOWN).
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-80.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
MD-80 SERIES
2 FIRE LIGHT
3 FIRE AGENT 1
APU SHUTDOWN AND FIRE PROCEDURE:
4 FIRE AGENT 2
1. “APU SHUT OFF” SWITCH TO “SHUT OFF” (UP.)
2. IF “FIRE” LIGHT IS ILLUMINATED:
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP)
4. AFTER 10 SECONDS, FIRE AGENT NO 2 SWITCH TO
“DISCHARGE” (UP.)
1 APU SHUT
OFF SWITCH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-80.0.6
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
MD-90 SERIES
FLAMMABLE MATERIAL LOCATIONS
MD-90 (tab)
CAUTION: Rescue crews wearing full PPE to include SCBA’s must use caution when moving across
sections of aircraft that have been exposed to fatigue or fire as the result of an accident.
Crews need to verify the integrity of the surface area before moving their weight and
equipment across it. Signs could include but are not limited to deformity of structure, visual
signs of flame impingement or uneven surfaces. Surface integrity can be checked with a pike
pole, axe or any instrument used to sound surfaces for integrity.
APU EXHAUST DUCT ON
RIGHT SIDE ONLY
HYDRAULIC
ACCUMULATORS
FUEL VENT BOX
ENGINE OIL
TANKS
FUEL OVERFLOW
STAND PIPE
HYDRAULIC
ACCUMULATORS
OPTIONAL AUXILIARY
FUEL TANK
FIRE EXTINGUISHER AGENT
CONTAINERS
1397 GAL 5288 L
APU GROUND CONTROL
PANEL ON FUSELAGE
HYDRAULIC FLUID
RESERVOIR 1 PLACE IN
EACH WHEEL WELL
FUEL TANKS
3044 GAL 11522 L
PORTABLE OXYGEN
BOTTLES
FUEL TANK
FUEL OVERFLOW
STAND PIPE
1397 GAL - 5288 L
FUEL VENT BOX
HYDRAULIC ACCUMULATORS
RAIN REPELLENT
CONTAINERS
CREW PORTABLE OXYGEN
SYSTEM BOTTLES
HOT BRAKES
Normal cooling: Move aircraft to a suitable location and allow brakes to cool on their own.
Water mist: Can be deployed from turret or handline.
Fans: Placing fans may place firefighters very close to the hazard zone.
WHEEL FIRE
Apply large amounts of water initially with turrets. Transition to handline application to continue and
maintain a cooling effect.
Wheels are equipped with fusible plugs designed to melt and deflate the tire when the
temperature is excessive.
WARNING: Approach landing gear trucks from forward or aft at a 45 degree angle when
apporaching hot brakes or fighting a wheel fire, as rims and tires may pose a
fragmentation hazard.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-90.0.1
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-1
MD-90 SERIES
1 PASSENGER DOOR AND STAIRWAY
2 OVERWING EMERGENCY EXIT
3 TAIL CONE JETTISON/SLIDE
DEPLOYMENT
EMERGENCY
EXIT
FOR TAIL CONE
JETTISON
PUSH DOOR
PULL HANDLE
INSIDE LOCK CABLE
MUST BE RE-INSTALLED
IF HANDLE IS PULLED
TO OPEN DOOR:
1. UNLATCH AND OPEN SLIGHTLY.
2. UNLATCH STAIR DOOR, TURN AND HOLD
BATTERY SWITCH “BATT.”
3. PRESS AND HOLD “DN” BUTTON UNTIL STAIR
FULLY EXTENDS.
4. RELEASE BATTERY SWITCH.
5. MOVE DETENT LATCH TO LOCKED POSITION.
6. MANUALLY EXTEND HANDRAILS INTO
DOORWAY.
NOTE:
TO OPEN DOOR:
1. UNLATCH.
2. PULL HANDLE.
3. LIFT OUT.
TO JETTISON TAIL CONE AND INFLATE SLIDE
1. PUSH DOOR.
2. PULL HANDLE.
3. SLIDE INFLATES AUTOMATICALLY.
NOTE:
HANDLE IS 10 FEET ABOVE THE GROUND.
FORWARD LEFT DOOR HAS SLIDE. STAND CLEAR
WHILE OPENING DOOR.
4 CUT-IN AREAS
NOTE:
CUT-IN AREAS REQUIRE METAL CUTTING
PORTABLE POWER EQUIPMENT.
BECAUSE OF TYPE OF STRUCTURE AND
POSSIBLE INJURY TO PERSONNEL
WITHIN, IT IS RECOMMENDED THAT
MAJOR EFFORT TO GAIN ACCESS BE
DIRECTED TO HATCHES AND DOORS.
URGENCY OF SITUATION WILL
DICTATETHE NECESSITY FOR A CUT-IN.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-90.0.2
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EMERGENCY RESCUE ACCESS-2
MD-90 SERIES
GENERAL NOTE:
1. OBSERVE MARKINGS ON ALL DOORS FOR OPERABILITY. DO
NOT ATTEMPT TO OPEN DOORS WHICH ARE BANDED OR
MARKED INOPERABLE.
2. DO NOT STAND IN FRONT OF PASSENGER SERVICE OR
EMERGENCY EXIT DOORS WHEN OPENING. ESCAPE SLIDE
WILL INFLATE AUTOMATICALLY WHEN DOOR IS OPENED
AND DROP OVER LOWERED DOOR.
2” WIDE BAND OF CONTRASTING
COLOR INDICATING ALL DOORS,
HATCHES AND WINDOWS
EXTERNALLY OPERABLE.
APU COMPARTMENT
ACCESS DOOR
JETTISONABLE TAIL
CONE
AFT LOWER CARGO
COMPARTMENT DOOR
TAIL CONE ACCESS
DOOR
2 OVERWING
EMERGENCY EXITS
3 TAIL CONE JETTISON/SLIDE
DEPLOY
FORWARD CARGO
COMPARTMENT DOOR
1 FORWARD SERVICE
ENTRANCE DOOR
PASSENGER AFT ENTRANCE STAIRWAY
INTERRIOR CONTROL PANEL ON SOME
AIRPLANES
MID CARGO
COMPARTMENT DOOR
4 CUT-IN AREAS
CLEARVIEW WINDOWCHILL PANE WITH CO2
AND BREAK WITH HEAVY
FIRE AXE FOR ACCESS
TO HANDLE; SLIDE
WINDOW AFT
1 FORWARD PASSENGER
ENTRANCE DOOR
AVERAGE DISTANCE
FLOOR LEVEL TO GROUND
WHEELS RETRACTED: 4 FT.
WHEELS EXTENDED: 8 FT.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-90.0.3
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
BATTERY LOCATIONS
MD-90 SERIES
BATTERY
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-90.0.4
June 27, 2014
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
FLIGHT DECK CONTROL SWITCH LOCATIONS
MD-90 SERIES
APU CONTROL PANEL
4 FIRE AGENT NO 1
FIRE AGENT
NO 1 OFF NO 2
ENG
DISCH
APU FIRE
FIRE CONT
NORM
APU
ON
AIR COND
COLDER
MASTER
OFF
RUN
START
OFF &
AGENT ARM
EMER PWR
OFF ARM ON
3 FIRE CONT
ENGINE SHUTDOWN AND FIRE PROCEDURE:
2 “APU FIRE” LIGHT
A. FUEL SWITCHES FROM “ON” TO “OFF” (DOWN.)
B. IF LIGHT(S) IN HANDLES ARE ILLUMINATED:
5 FIRE AGENT NO 2
AIR
OFF
EMER
PWR
IN USE
BATT
OFF
C. PULL HANDLES FULLY OUT
1 MASTER OFF
CKPT
DOOR
ON
D. ROTATE HANDLE CLOCKWISE
E. AFTER 10 SECONDS, ROTATE HANDLES
COUNTERCLOCKWISE.
APU SHUTDOWN AND FIRE PROCEDURE
1. APU “MASTER OFF” SWITCH TO “OFF” (UP).
B,C,D,E - “ENG
FIRE” HANDLES
1
AGENT
DISCH
L
E
N
G
2
FIRE
TEST
F
I
R
E
PULL
LH ENGINE
A - FUEL SWITCHES
AGENT 1
LOW
AGENT 2
LOW
FIRE
BELL OFF
2. IF “APU FIRE” LIGHT IN OVERHEAD PANEL IS
ILLUMINATED...FIRE CONT SW TO “OFF & AGENT ARM”.
1
FAULT
TEST
AGENT
DISCH
2
R
3. FIRE AGENT NO 1 SWITCH TO “DISCH” (DOWN).
4. AFTER 10 SECONDS FIRE AGENT NO 2 SWITCH TO
“DISCH” (DOWN).
E
N
G
F
I
R
E
PULL
RH ENGINE
CRITICAL SWITCH LOCATIONS AND THEIR OPERATION ARE SHOWN WITH THE
EXPANDED VIEWS OF THE CONTROL MODULES.
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
June 27, 2014
MD-90.0.5
AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION
EXTERNAL APU FIRE CONTROLS
MD-90 SERIES
2 FIRE LIGHT
3 FIRE AGENT 1
APU SHUTDOWN AND FIRE PROCEDURE:
4 FIRE AGENT 2
1. “APU SHUT OFF” SWITCH TO “SHUT OFF” (UP.)
2. IF “FIRE” LIGHT IS ILLUMINATED:
3. FIRE AGENT 1 SWITCH TO “DISCHARGE” (UP)
4. AFTER 10 SECONDS, FIRE AGENT NO 2 SWITCH TO
“DISCHARGE” (UP.)
1 APU SHUT
OFF SWITCH
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
MD-90.0.6
June 27, 2014
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