• 热门标签

当前位置: 主页 > 航空资料 > 飞行资料 >

时间:2010-05-17 22:05来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

VS (Vertical Speed Hold).............................................................5-22
Go-Around .................................................................................... 5-22
Status Annunciators ..................................................................... 5-22A
Control Wheel Master Switches-Autopilot Function ................ 5-23
PITCH TRIM Selector Switch-Autopilot Function .................... 5-23
Control Wheel Switches (Figure 5-7) ............................................... 5-23
Control Wheel Trim Switches-Autopilot/Flight
Director Function ........................................................................... 5-24
Pedestal NOSE DN-OFF-NOSE UP Switch -Autopilot
Function ........................................................................................... 5-25
Learjet 31A
Pilot's Manual
TABLE OF CONTENTS (Cont)
Control Wheel Steering (CWS) Switches .........................................5-25
Control Wheel FD CLEAR Switches ................................................5-25
SYSTEM TEST Switch -A/P RESET Function .............................5-26
Yaw Damper System ................ .. ............................................................5-26
Yaw Damper Control .... ......................................................................5-26
Control Wheel Master Switches -Yaw Damper Function...........5-26
Rudder Boost System ............... ..............................................................5-27
RUDDER BOOST Switch ... .......... ......................................................5-27
Control Wheel Master Switches -Rudder Boost Function .........5-27
Rudder Boost Block Diagram (Figure 5-8) .......................................5-28
Attitude Heading System (AHS 1 and AHS 2) ....................... ...........5-29
Heading Control Switches .................................................................5-30
AHS 1 and AHS 2 Annunciator Lights ............................................. 5-30
AHS 1/AHS 2 Reversionary Mode ..................................................5-30
Electronic Flight Instruments System (EFIS) ......................................5-31
Electronic Attitude Director Indicator (EADI) ................... .............5-31
Electronic Horizontal Situation Indicator (EHSI) ...........................5-31
EFIS Control Panel ..............................................................................5-32
EFIS Control Panel (Figure 5-9) ........................................................5-32
Multifunction Display (MFD) ................. ..........................................5-32
MFD Control Panel .............................................................................5-32
MFD Control Panel (Figure 5-10) .....................................................5-33
EFIS Reversionary Control Panel ........................................ .............5-33
EFIS Reversionary Control Panel (Figure 5-11) ..............................5-34
Flight Instruments ..................................................................................5-34
Airspeed/Mach Indicators ................................................................5-34
Airspeed/Mach Indicator (Figure 5-12) ..........................................5-35
Altitude/Vertical Speed Indicators ..................................................5-35
Altitude/Vertical Speed Indicator (Figure 5-13) ............................5-36
Speed/Temperature Indicator ............................................. .............5-37
Speed/Temperature Indicator (Figure 5-14) ...................................5-37
Standby Airspeed/Mach Indicator ..................................................5-37
Standby Altimeter ............................................................................... 5-38
Standby Airspeed/Mach Indicator and
Altimeter (Figure 5-15) ........................................... .......................5-38
Standby Attitude Indicator ................................................................ 5-38
Standby Attitude Indicator (Figure 5-16) ................. ....................... 5-39
Standby Horizontal Situation Indicator (HSI) ................... .............5-40
Standby Horizontal Situation Indicator (Figure 5-17) ...................5-40
Pilot's Manual
Learjet 31A
TABLE OF CONTENTS (Copt)
Pitot-Static System .................................................................................. 5-41
STATIC SOURCE Switch ................................................................... 5-41
Pitot-Static System (Figure 5-18)........................................................ 5-42
Air Data System (ADC 1 and ADC 2) ................................................. 5-43
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:庞巴迪挑战者手册9(55)