ARFFPage Title AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION Commercial Copyright © 2005 The Boeing Company All Rights Reserved June 27, 2014 2 Copyright Information Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work. The right to reproduce, distribute, display, and make derivative works from this document, or any portion thereof, requires a license from Boeing. For more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124. Boeing 707, 717, 720, 727, 737, BBJ, 747, 757, 767, 777, 787, DC-3, DC-6, DC-7, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-90, the Boeing logo symbol and the Boeing livery are all trademarks owned by The Boeing Company and no trademark license (either expressed or implied) is granted in connection with this document or otherwise. Document Information Any questions about the content or use of this manual should be directed to: Manager, Flight Technical Data Boeing Commercial Airplane Group PO Box 3707, M/C 20-89 Seattle, Washington 98124-2207 USA Information contained in this document, including illustrations, depicts the Boeing Company’s standard airplane configuration. Diagrams are intended to be representative only. No attempt has been made to include customer variables or post-delivery modifications. For training purposes, this document is available in viewfoil format, Adobe Portable Document Format (PDF) on CD, and individual pages are available as 2’ x 3’ black and white wall charts. For ordering information, pleae contact: Boeing Commercial Airplanes Data and Services Management (DSM) PO Box 3707, Mail Stop 2H-65 Seattle, Washington 98124-2207, USA Telephone: 206-544-5000 FAX: 206-544-8899 Every attempt has been made to include as many of the Boeing Company’s airplane configuration variables as possible. 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 27, 2014 00.TOC.1 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION 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 June 27, 2014 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION Table of Contents 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 00.TOC.3 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION 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 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 00.TOC.4 June 27, 2014 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 MD-90.0.1 MD-90.0.2 MD-90.0.3 MD-90.0.4 MD-90.0.5 MD-90.0.6 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 27, 2014 00.TOC.5 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION Table of Contents Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 00.TOC.6 June 27, 2014 List of Effective Pages AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION List of Effective Pages 727 (tab) ARFF * Title Page 1-2 June 27, 2014 Table of Contents (tab) * 00.TOC.1-6 June 27, 2014 * * * * * * 727.0.1 727.0.2 727.0.3 727.0.4 727.0.5 727.0.6 * * * * * * * * * * * * * * 737.0.1 737.0.2 737.0.3 737.0.4 737.0.5 737.0.6 737.1.1 737.1.2 737.1.3 737.1.4 737.1.5 737.1.6 737.1.7 737.1.8 * * * * * * * * * * * * * * * * * * * * * * 747.0.1 747.0.2 747.0.3 747.0.4 747.0.5 747.0.6 747.1.1 747.1.2 747.1.3 747.1.4 747.1.5 747.1.6 747.2.1 747.2.2 747.2.3 747.2.4 747.2.5 747.2.6 747.3.1 747.3.2 747.3.3 747.3.4 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 List of Effective Pages * 00.LEP.1-2 Revision Record * 00.RR.1-2 June 27, 2014 707 (tab) * * * * * * * * * * * * 707.0.1 707.0.2 707.0.3 707.0.4 707.0.5 707.0.6 707.1.1 707.1.2 707.1.3 707.1.4 707.1.5 707.1.6 * * * * * * * * 717.0.1 717.0.2 717.0.3 717.0.4 717.0.5 717.0.6 717.0.7 717.0.8 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 717 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 720 (tab) * * * * * * 737 (tab) June 27, 2014 720.0.1 720.0.2 720.0.3 720.0.4 720.0.5 720.0.6 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 747 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * 747.3.5 747.3.6 747.4.1 747.4.2 747.4.3 747.4.4 747.4.5 747.4.6 747.5.1 747.5.2 747.5.3 747.5.4 747.5.5 747.5.6 747.6.1 747.6.2 747.6.3 747.6.4 747.6.5 747.6.6 747.6.7 747.6.8 747.7.1 747.7.2 747.7.3 747.7.4 747.7.5 747.7.6 747.8.1 747.8.2 747.8.3 747.8.4 747.8.5 747.8.6 747.9.1 747.9.2 747.9.3 747.9.4 747.9.5 747.9.6 747.10.1 747.10.2 747.10.3 747.10.4 747.10.5 747.10.6 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 27, 2014 * 757 (tab) * * * * * * * * * * * * * * * * * * 757.0.1 757.0.2 757.0.3 757.0.4 757.0.5 757.0.6 757.1.1 757.1.2 757.1.3 757.1.4 757.1.5 757.1.6 757.2.1 757.2.2 757.2.3 757.2.4 757.2.5 757.2.6 * * * * * * 767.0.1 767.0.2 767.0.3 767.0.4 767.0.5 767.0.6 * * * * * * 767.0.1 767.0.2 767.0.3 767.0.4 767.0.5 767.0.6 * * * * * * * * * * 777.0.1 777.0.2 777.0.3 777.0.4 777.0.5 777.0.6 777.0.7 777.0.8 777.0.9 777.0.10 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 767 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 767 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 777 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 * = Revised, Added, or Deleted 00.LEP.1 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION List of Effective Pages * * * * * * 777.1.1 777.1.2 777.1.3 777.1.4 777.1.5 777.1.6 * * * * * * * * * * 787.0.1 787.0.2 787.0.3 787.0.4 787.0.5 787.0.6 787.0.7 787.0.8 787.0.9 787.0.10 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 787 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 DC-3 (tab) * DC-3.0.1 * DC-3.0.2 June 27, 2014 June 27, 2014 * * * * * * * * * * * * * * * * * * * * * * DC-8.2.3 DC-8.2.4 DC-8.3.1 DC-8.3.2 DC-8.3.3 DC-8.3.4 DC-8.4.1 DC-8.4.2 DC-8.4.3 DC-8.4.4 DC-8.5.1 DC-8.5.2 DC-8.5.3 DC-8.5.4 DC-8.6.1 DC-8.6.2 DC-8.6.3 DC-8.6.4 DC-8.7.1 DC-8.7.2 DC-8.7.3 DC-8.7.4 * * * * * * DC-9.0.1 DC-9.0.2 DC-9.0.3 DC-9.0.4 DC-9.0.5 DC-9.0.6 DC-6 (tab) * DC-6.0.1 * DC-6.0.2 June 27, 2014 June 27, 2014 DC-7 (tab) * * * * * * * * DC-7.0.1 DC-7.0.2 DC-7.0.3 DC-7.0.4 DC-7.1.1 DC-7.1.2 DC-7.1.3 DC-7.1.4 * * * * * * * * * * DC-8.0.1 DC-8.0.2 DC-8.0.3 DC-8.0.4 DC-8.1.1 DC-8.1.2 DC-8.1.3 DC-8.1.4 DC-8.2.1 DC-8.2.2 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 DC-8 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 * = Revised, Added, or Deleted 00.LEP.2 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 * MD-11.0.7 * MD-11.0.8 June 27, 2014 June 27, 2014 MD-80 (tab) * * * * * * MD-80.0.1 MD-80.0.2 MD-80.0.3 MD-80.0.4 MD-80.0.5 MD-80.0.6 * * * * * * MD-90.0.1 MD-90.0.2 MD-90.0.3 MD-90.0.4 MD-90.0.5 MD-90.0.6 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 MD-90 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 (blank tab) DC-9 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 DC-10 (tab) * * * * * * * * DC-10.0.1 DC-10.0.2 DC-10.0.3 DC-10.0.4 DC-10.0.5 DC-10.0.6 DC-10.0.7 DC-10.0.8 * * * * * * MD-11.0.1 MD-11.0.2 MD-11.0.3 MD-11.0.4 MD-11.0.5 MD-11.0.6 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 MD-11 (tab) June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 June 27, 2014 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 27, 2014 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. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 2 June 27, 2014 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 00.RR.1 Flight Crew Operations Manual Revision Record Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 00.RR.2 June 27, 2014 AIRPLANE RESCUE AND FIRE FIGHTING INFORMATION 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. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 27, 2014 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. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 707.0.2 June 27, 2014 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. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 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 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 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 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 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. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 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