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
synoptic page. The normal trim setting for takeoff (3 to 8 units) is depicted on the indicator as a
green band.
If stabilizer trim is not set in this range with the aircraft in the take-off mode, a CONFIG STAB
warning EICAS message will be displayed, and an aural “CONFIG TRIM” will sound.
Horizontal Stabilizer Trim Priority
The stabilizer trim can be operated manually with the pilot’s and copilot’s control wheel pitch trim
switches, or automatically with the autopilot or the Mach trim system. The order of priority and
rate of movement are as follows:
1. Pilot manual trim – The pilot’s control wheel pitch trim switch is highest in the order of
priority. The stabilizer rate of movement is 0.5°/sec.
2. Copilot manual trim – The copilot’s control wheel pitch trim switch is next highest in the
order of priority. The stabilizer rate of movement is 0.5°/sec.
3. Autopilot trim – The stabilizer rate of movement is 0.1°/sec. If a flap selection is made
with the autopilot engaged, the rate of movement reverts to the higher rate of 0.5°/sec
during flap transition.
4. Mach trim – The Mach trim is lowest in the order of priority. The stabilizer rate of
movement is between 0.03° and 0.06°/sec.
Horizontal Stabilizer Trim Clacker
If the horizontal stabilizer is in motion at a rate of more than 0.3°/sec for more than 3 seconds, a
clacker (“drumroll” sound) is activated, to alert the pilot of a possible horizontal stabilizer trim
runaway condition.
In the event of a runaway stabilizer trim condition, both channels can be quickly disconnected,
by pressing the STAB TRIM DISC button on either outboard control wheel horn.
FLIGHT CONTROLS
Description
Vol. 2 10−10−8
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
SECONDARY FLIGHT CONTROLS (CONT'D)
Mach Trim
At least one STAB TRIM channel must be engaged to have Mach trim engaged. The Mach trim
system, when engaged and active, compensates for the rearward shift of the aerodynamic
center of pressure as Mach number increases. The Mach trim system schedules inputs to the
HSTCU to command movement of the horizontal stabilizer, when hand-flying at speeds greater
than Mach 0.4.
Aileron Trim
Aileron trim is accomplished by activation of the AIL TRIM switches on the center pedestal.
Actuation of both switches provides arming and directional signals, which bias the control
circuits to actuate the PCUs and deflect the ailerons. Actuation of the aileron trim will cause the
control wheels to deflect in the direction of trim input. Aileron trim position is indicated on the
primary EICAS display.
Stab Trim Panel
Figure 10−10−5
Stab Trim Indications
Figure 10−10−6
FLIGHT CONTROLS
Description
Vol. 2 10−10−9
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
SECONDARY FLIGHT CONTROLS (CONT'D)
Rudder Trim
Rudder trim is accomplished by turning the RUD TRIM switch. Rudder trim input is applied by
the trim actuator into the yaw damper/trim mixer assembly, and will supplement the primary
rudder input, as applicable. Actuation of the rudder trim does not cause rudder pedal deflection.
The rudder trim position is indicated on the EICAS page.
Aileron/Rudder Trim Panel
Figure 10−10−7
Aileron/Rudder Trim Indications
Figure 10−10−8
Flaps
Two double-slotted flap panels (inboard and outboard) are externally hinged on the trailing edge
of each wing. A flap lever, located on the center pedestal, sends a signal to the flap control unit
(FCU) to initiate flap movement.
FLIGHT CONTROLS
Description
Vol. 2 10−10−10
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
SECONDARY FLIGHT CONTROLS (CONT'D)
The flaps may be set to one of four positions: 0, 20, 30, and 45 degrees. A flap gate is
incorporated within the flap lever 20-degree detent. This minimizes the possibility of accidental
flap retraction to 0 degrees during a go-around procedure. Flap position is displayed on the
EICAS page and the FLIGHT CONTROLS synoptic page, in both analog (colored bar) and
digital formats. The indications on the EICAS page are in view only if the flaps are extended, or
if the landing gear is not up and locked.
Maximum Flap Speeds
FLAP SETTING MAXIMUM AIRSPEED
20 degrees 231 KIAS
30 degrees 197 KIAS
45 degrees 189 KIAS
NOTE
To prevent damage, maximum indicated airspeeds for each flap
setting must not be exceeded. These are placarded on the
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605机组操作手册 CL605-FLIGHT_CONTROLS(4)
