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
Flap position and condition are continuously monitored by the flap control unit. In the event of failure or overheat of a single flap motor (indicated by a FLAPS MOTOR OVHT status EICAS message), the remaining motor can operate the flaps at half speed. Complete failure of the flap system, including an asymmetry of >2.75°, will generate a FLAPS FAIL caution EICAS message, as well as an amber symbol on the FLIGHT CONTROLS synoptic page.
If the flaps are not set at 20° with the aircraft in takeoff mode, a CONFIG FLAPS warning EICAS message and aural warning will be displayed/sounded.
FLIGHT CONTROLS Description Vol. 2 10.10.12
Oct 05/06
Flap Schematic Figure 10.10.9
Flight Spoilers
These provide lift dumping and speed control when airborne, and reduce ground roll during landing and rejected takeoffs.
FLIGHT CONTROLS Description Vol. 2 10.10.13
Oct 05/06
Each flight spoiler panel is hydraulically operated by two identical PCUs, powered by hydraulic systems 1 and 2. The flight spoilers are mechanical controlled by the flight spoiler control lever on the center pedestal, and can be deployed up to a maximum of 40° in flight or on the ground. The flight spoiler control lever travels through nine detents, allowing the pilot to select variable amounts of flight spoiler deployment.
Spoiler position is indicated on both the EICAS page and FLIGHT CONTROLS synoptic page, using white arrows which move upward towards lines indicating relative extension (for flight spoilers only), and full extension (for both flight and ground spoilers). When the flight and ground spoilers are fully retracted, all EICAS spoiler icons and position arrows disappear.
An amber FLT SPLRS DEPLOY caution EICAS message appears if the flight spoilers are deployed in flight, and:
.
The aircraft radio altitude is between 10 and 300 feet AGL, or
.
The left or right engine N1 is greater than 79%, or
.
If radio altitude is not available, at any time the landing gear is extended.
If the flight spoilers are not stowed with the aircraft in takeoff mode, a CONFIG SPOILERS warning EICAS message and aural warning will be displayed/sounded.
20° Detent Mechanism
A 20° detent mechanism prevents asymmetrical deployment of the flight spoilers in the event of a disconnected input linkage. The PCU control valves are spring-loaded retracted, but the detent mechanism will apply force to hold a mid-position if the spoiler has been deployed to greater than 20°. When on the ground with hydraulic pressure available, a sensor on each detent mechanism will generate a FLT SPLRS caution EICAS message, and cause the appropriate flight spoiler outline to turn amber on the FLIGHT CONTROLS synoptic page, if the spoiler position does not correspond to the detent position.
FLIGHT CONTROLS Description Vol. 2 10.10.14
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-飞行操纵 FLIGHT_CONTROLS(7)
|
