深夜福利✅_姐姐的朋友2完整视频有翻译英文吗_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
Vol. 1 13--00--1 REV 56, Jan 31/03 FUEL SYSTEM Table of Contents Flight Crew Operating Manual CSP A--013 MASTER CHAPTER 13 -- FUEL SYSTEM Page TABLE OF CONTENTS 13--00 Table of Contents 13--00--1 INTRODUCTION 13--10 Introduction 13--10--1 FUEL STORAGE 13--20 Fuel Storage 13--20--1 Collector Tanks 13--20--1 Venting 13--20--1 FUEL MANAGEMENT 13--30 Fuel Management 13--30--1 Fuel Transfer 13--30--1 Fuel Crossflow 13--30--1 System Circuit Breakers 13--30--8 FUEL DISTRIBUTION 13--40 Fuel Distribution 13--40--1 System Circuit Breakers 13--40--5 REFUELING AND DEFUELING 13--50 Refueling and Defueling 13--50--1 Control Panel 13--50--4 System Circuit Breakers 13--50--7 FUEL QUANTITY GAUGING 13--60 Fuel Quantity Gauging System 13--60--1 Magnetic Level Indicators 13--60--5 System Circuit Breakers 13--60--8 LIST OF ILLUSTRATIONS INTRODUCTION Figure 13--10--1 Fuel System -- General 13--10--2 FUEL STORAGE Figure 13--20--1 Collector Tank and Vent System -- General 13--20--2 FUEL MANAGEMENT Figure 13--30--1 Fuel System Schematic -- General 13--30--3 REV 56, Jan 31/03 Vol. 1 13--00--2 FUEL SYSTEM Table of Contents Flight Crew Operating Manual MASTER CSP A--013 Figure 13--30--2 Fuel Control Panel -- General 13--30--4 Figure 13--30--3 Fuel System EICAS Indications 13--30--5 Figure 13--30--4 Fuel System Controls -- Synoptic Page Indications 13--30--6 FUEL DISTRIBUTION Figure 13--40--1 Standby Fuel Feed System 13--40--2 Figure 13--40--2 Standby Fuel Feed System -- EICAS Messages 13--40--3 Figure 13--40--3 Standby Fuel Feed System -- Fuel Synoptic Page Indications 13--40--4 REFUELING AND DEFUELING Figure 13--50--1 Refuel/Defuel System 13--50--2 Figure 13--50--2 Fuel System Computer 13--50--3 Figure 13--50--3 Refuel/Defuel Control Panel 13--50--5 FUEL QUANTITY GAUGING Figure 13--60--1 Refuel/Defuel -- EICAS Messages 13--60--2 Figure 13--60--2 Refuel/Defuel System -- Fuel Synoptic Page Indications 13--60--3 Figure 13--60--3 Fuel System -- Menu Page 13--60--4 Figure 13--60--4 Magnetic Level Indicators 13--60--6 Figure 13--60--5 Pitch and Roll Inclinometers 13--60--7 Vol. 1 13--10--1 REV 56, Jan 31/03 FUEL SYSTEM Introduction Flight Crew Operating Manual CSP A--013 MASTER 1. INTRODUCTION The fuel system consists of three integral tanks within the wing box structure. Ejector pumps and electrical boost pumps supply fuel to each engine. The fuel system also provides facilities for pressure refueling/defueling and gravity refueling/defueling. Power and gravity crossflow systems allow fuel transfer between wing tanks and also provides fuel to the auxiliary power unit (APU). A fuel system computer (FSC) automatically controls refueling, powered fuel crossflow and fuel transfer. The FSC also measures the fuel quantity and temperature for display on the engine indication and crew alerting system (EICAS). The EICAS FUEL synoptic page shows a diagram of the fuel distribution system. Operation of the ejectors, pumps and shutoff valves are graphically displayed. Any fault detected by the FSC is annunciated in the form of visual and/or aural messages. Faults are also displayed on the refuel/defuel panel in the form of fault codes. REV 56, Jan 31/03 Vol. 1 13--10--2 FUEL SYSTEM Introduction Flight Crew Operating Manual MASTER CSP A--013 Fuel System --- General <MST> Figure 13---10---1 RH MAIN TANK RH MAIN FILL CAP CENTER TANK FILL CAP COLLECTOR CENTER TANK TANKS SINGLE POINT REFUEL/DEFUEL ADAPTER LH MAIN TANK REFUEL/DEFUEL CONTROL PANEL LH MAIN FILL CAP REFUEL/DEFUEL CONTROL PANEL <0017> Vol. 1 13--20--1 REV 56, Jan 31/03 FUEL SYSTEM Fuel Storage Flight Crew Operating Manual CSP A--013 MASTER 1. FUEL STORAGE Fuel is stored in two main wing tanks and one center wing tank. In flight, as the wing tank fuel quantity decreases, the FSC will automatically transfer fuel from the center tank to the wing tanks to maintain lateral balance. A. Collector Tanks Two collector tanks are located in the forward section of the center wing tank. Fuel from each wing tank is fed under pressure to its respective collector tank by scavenge ejectors. The collector tank capacity is 10 gallons (38 liters) and when the tank is full, excess fuel is vented back to the respective wing tank. Fuel can also be fed from the www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_CRJ_00-Fuel_System
