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庞巴迪挑战者300公务机机组操作手册 Bombardier Challenger-防冰和排雨(2)

时间:2011-11-16 11:51来源:蓝天飞行翻译 作者:公务机
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Description.................................................................................................................14-01-07
Components and Operation.......................................................................................14-01-07
Pitot Static Probes......................................................................................................14-01-07
Standby Pitot Probe...................................................................................................14-01-07
Standby Static Ports...................................................................................................14-01-07
Angle-of-Attack Vanes (AOA) ....................................................................................14-01-07
Total Air Temperature Probe (TAT).............................................................................14-01-07

Windshield Ice and Rain Protection ....................................................................................14-01-08
Description.................................................................................................................14-01-08
Components and Operation.......................................................................................14-01-08
Windshield and Side Window Heating.......................................................................14-01-08
Control Switches and Function..................................................................................14-01-08

Controls and Indications......................................................................................................14-01-09
Description.................................................................................................................14-01-09
Anti-Ice Control Panel................................................................................................14-01-09

Anti-Ice Synoptic Page........................................................................................................14-01-10

EICAS Messages ................................................................................................................ 14-01-11

May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP 100-6
14-00-01

INTRODUCTION
The wing leading edges and the engine intake cowls are heated using engine bleed air. The windshields, windows and the air data probes are heated using electrical power. Anti-icing of the aircraft tail surface is not required.
Two ice detectors provide indication to the flight crew of icing conditions.
The anti-ice protection system (AIPS) is controlled by the integrated air system controllers (IASC) with indications dis-played on the EICAS. The ANTI ICE synoptic display provides an overview of status of the pneumatically operated anti-icing systems.
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
14-01-01 ICE DETECTION SYSTEM
 
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