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DESCRIPTION General 08−10−1 Placards 08−10−1 Oxygen 08−10−2 Flight Compartment 08−10−2 Oxygen Bottle 08−10−3 Oxygen Ground Service Panel 08−10−4 Crew Mask Storage 08−10−5 Crew Mask 08−10−6 Passenger Oxygen 08−10−8 Oxygen System EICAS Messages 08−10−9 Oxygen System Quantity Readout 08−10−10 Crew Oxygen Consumption Data 08−10−11 Evacuation Devices 08−10−13 Exit Lighting 08−10−14 Emergency Exit − Passenger Door 08−10−14 Overwing Emergency Exit 08−10−15 Overwing Emergency Exit − External 08−10−15 Overwing Emergency Exit − Internal 08−10−16 Fire Fighting Equipment 08−10−17 Portable Fire Extinguisher 08−10−17 Over Water Emergency Equipment 08−10−19 Life Vest 08−10−19 EMS CIRCUIT PROTECTION CB − Oxygen 08−20−1 EMERGENCY EQUIPMENT TABLE OF CONTENTS CHAPTER 8 08−00−1 Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 08−00−1 Page TABLE OF CONTENTS EMERGENCY EQUIPMENT TABLE OF CONTENTS Flight Crew Operating Manual Rev 2A, Apr 11, 2005 CSP 700−5000−6 Volume 2 08−00−2 THIS PAGE INTENTIONALLY LEFT BLANK GENERAL This chapter describes the systems and equipment which are essential to the safety of passengers and crew during a fire, rapid decompression, ditching and emergency evacuation. These include the following equipment: · Oxygen equipment (portable and fixed). · Evacuation devices (crash axe, emergency lighting and emergency exits). · Fire fighting equipment (portable and fixed). · Over water emergency equipment (life vests). PLACARDS GF0810_001 EXTINGUISHER OXYGEN CYLINDER FIRST AID KIT HALON FIRE o2 CREW MEMBER LIFE−VEST UNDER SEAT EMERGENCY EQUIPMENT Rev 2A, Apr 11, 2005 Flight Crew Operating Manual CSP 700−5000−6 Volume 2 08−10−1 OXYGEN A gaseous oxygen system is supplied by four cylinders to serve the flight crew and passengers. FLIGHT COMPARTMENT The flight compartment oxygen system consists of the following: · Four oxygen bottles (with a pressure regulator unit, bottle gauge and shutoff valve). · Ground servicing panel (with a gauge and filler valve). · Fuselagemounted overboard relief valve (frangible disc). · Two oxygen mask/regulator units and goggles. GF0810_002a INDICATOR OVERBOARD DISCHARGE SERVICE−PANEL GROUND PRESSURE−GAUGE FILLER VALVE CYLINDERS STORAGE SERVICE−PANEL GROUND PRESSURE GAUGE STORAGE CYLINDER REGULATOR CHECK VALVE SUPPLY LINE CABIN OXYGEN ALTIMETRIC VALVE STOWAGE BOXES AND PILOT/COPILOT CREW OXYGEN MASKS SWITCH PRESSURE TRANSDUCER PRESSURE EICAS Cockpit/cabin supply line Storage−cylinder fill line HP Discharge line LP Discharge line HP Capillary lines for indication EICAS EMERGENCY EQUIPMENT Flight Crew Operating Manual Rev 2A, Apr 11, 2005 CSP 700−5000−6 Volume 2 08−10−2 OXYGEN BOTTLE The oxygen bottles [1416 liter (50.0 cubic feet)] are located in the forward fuselage underfloor area. Normal charge pressure at 21 °C (70 °F) is 1850 psi. Charge pressure is indicated as follows: · Gauge on the bottle regulator · Gauge on the ground servicing panel · Oxygen quantity is indicated on the EICAS status page When bottle pressure becomes excessive, approximately 2600 psi, all oxygen is vented overboard by a pressure regulator unit working in conjunction with a fuselagemounted relief valve. Overpressure causes the OXY HP RELIEF disc, located on the left front fuselage to blow out. The pressure regulator unit regulates flow to the crew mask regulator unit to 72.5 psi and the unit’s strain gauge transmits pressure signals to EICAS. The crew mask/regulator unit regulates the flow to the crew masks. Oxygen is supplied via the regulator at either ambient or slightly over ambient pressure dependent upon crew setting of the flow controls. The flight crew oxygen system is a diluter demand system. The flight crew oxygen masks are of the www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Emergency_Equipment
