曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

INTRODUCTION 11--10
Introduction 11--10--1
AILERONS 11--20
Ailerons 11--20--1
System Circuit Breakers 11--20--8
RUDDER 11--30
Rudder 11--30--1
System Circuit Breakers 11--30--9
ELEVATORS 11--40
Elevators 11--40--1
System Circuit Breakers 11--40--5
HORIZONTAL STABILIZER TRIM 11--50
Horizontal Stabilizer Trim 11--50--1
System Circuit Breakers 11--50--7
FLAPS AND SLATS 11--60
Flaps and Slats 11--60--1
System Circuit Breakers 11--60--6
SPOILERS 11--70
Spoilers 11--70--1
System Circuit Breakers 11--70--7
STALL PROTECTION SYSTEM 11--80
Stall Protection System 11--80--1
System Circuit Breakers 11--80--5
LIST OF ILLUSTRATIONS
INTRODUCTION
Figure 11--10--1 Flight Controls -- General 11--10--3
AILERONS
Figure 11--20--1 Aileron Control General Arrangement 11--20--2
Vol. 1 11--00--2
FLIGHT CONTROLS
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Figure 11--20--2 Ailerons -- Emergency Control 11--20--3
Figure 11--20--3 Ailerons Glareshield Emergency Control 11--20--3
Figure 11--20--4 EICAS Flight Control -- Synoptic Page 11--20--4
Figure 11--20--5 Aileron Trim Controls 11--20--5
Figure 11--20--6 Aileron Mistrim Flag 11--20--5
Figure 11--20--7 Aileron Trim EICAS Indications 11--20--6
Figure 11--20--8 Spoilerons and Roll Selection -- EICAS Indications 11--20--7
RUDDER
Figure 11--30--1 Rudder System 11--30--2
Figure 11--30--2 Rudder -- Flight Control Synoptic Page 11--30--3
Figure 11--30--3 Rudder Limiter -- EICAS Indications 11--30--4
Figure 11--30--4 Rudder Trim Control Panel and PFD Flag 11--30--5
Figure 11--30--5 Rudder Trim -- EICAS Indications 11--30--6
Figure 11--30--6 Yaw Damper Controls and PFD Flag 11--30--7
Figure 11--30--7 Yaw Damper -- EICAS Indications 11--30--8
ELEVATORS
Figure 11--40--1 Elevator System 11--40--2
Figure 11--40--2 Elevator Emer Controls and Flight Control --
Synoptic Page 11--40--3
Figure 11--40--3 Elevator -- EICAS Indications 11--40--4
HORIZONTAL STABILIZER TRIM
Figure 11--50--1 Horizontal Stabilizer Trim Control System Schematic 11--50--2
Figure 11--50--2 Stabilizer/ Mach Trim Control Panel 11--50--3
Figure 11--50--3 Stabilizer Trim -- Pilot’s Control Wheel 11--50--3
Figure 11--50--4 Elevator Mistrim Primary Flight Display Flag 11--50--4
Figure 11--50--5 Stabilizer Trim EICAS Indications 11--50--5
Figure 11--50--6 Stab Trim EICAS Indications 11--50--6
FLAPS AND SLATS
Figure 11--60--1 Slats/ Flaps Control System 11--60--2
Figure 11--60--2 Slats/ Flaps -- Control 11--60--3
Figure 11--60--3 Emergency Flap Deploy Control Panel 11--60--3
Figure 11--60--4 Slats/ Flaps Position -- Flight/Control Synoptic Page 11--60--4
Figure 11--60--5 Slats/ Flaps EICAS Indication 11--60--5
SPOILERS
Figure 11--70--1 Spoiler Control System 11--70--2
Figure 11--70--2 Spoiler Control Panel and Lever 11--70--3
Figure 11--70--3 Spoilers -- Flight/Control Synoptic Page 11--70--4
Vol. 1 11--00--3
FLIGHT CONTROLS
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Figure 11--70--4 Spoilers -- EICAS Indications -- Primary Page 11--70--5
Figure 11--70--5 Spoilers -- EICAS Indications -- Status Page 11--70--6
STALL PROTECTION SYSTEM
Figure 11--80--1 Stall Protection System Schematic 11--80--2
Figure 11--80--2 Stall Protection Controls 11--80--3
Figure 11--80--3 Stall Protection -- Test and EICAS Indications 11--80--4
Vol. 1 11--00--4
FLIGHT CONTROLS
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 11--10--1
FLIGHT CONTROLS
Introduction REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. INTRODUCTION
Flight controls are operated conventionally with control wheels, control columns and rudder
pedals for the pilot and copilot. The control surfaces are actuated either hydraulically or
electrically. The flight control systems include major control surfaces, components and
subsystems that control the attitude of the aircraft during flight. The flight controls are
divided into primary and secondary flight controls.
The primary flight controls include:
S Ailerons (roll control)
S Elevators (pitch control)
S Rudder (yaw control)
The ailerons, elevators and rudder are controlled by a network of cables, pulleys, push/pull
rods and levers that transmit control inputs to the related hydraulic power control units.
The aileron and elevator controls are equipped with control disconnects which permit the
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者手冊4(6)