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时间:2010-05-17 21:29来源:蓝天飞行翻译 作者:admin
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Indicates position of respective spoiler.
Indicator is not displayed when respective
spoiler is retracted or input data is invalid.
Ground Spoiler Outline
Green -- Spoiler is operative.
White -- Loss of redundancy.
Amber -- Spoiler is inoperative.
IB or OB FLT SPLRS (amber)
Indicates loss of proportional lift dumping
capability for respective multi--function spoilers.
IB or OB SPOILERONS (amber)
Indicates loss of roll assist capability for
respective multi--function spoilers.
SPLR/STAB IN TEST (green)
Indicates that the spoiler and stabilizer
control system is in self test mode.
NOTE
To prevent nuisance messages, no other
cockpit function should be carried out while
SPLR / STAB IN TEST is displayed
(about 60 seconds)
Flight Controls Page
BRT
Vol. 1 11--70--5
FLIGHT CONTROLS
Spoilers REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Spoilers --- EICAS Indications --- Primary Page <1001>
Figure 11---70---4
IB FLT SPLRS
OB FLT SPLRS
IB GND SPLRS
OB GND SPLRS
IB SPOILERONS
OB SPOILERONS
FLT SPLR DEPLOY
GND SPLR DEPLOY
GLD NOT ARMED
GLD UNSAFE
IB or OB FLT SPLRS caution (amber)
Indicates loss of proportional lift dumping
capability for respective multi--function spoilers.
IB or OB SPOILERONS caution (amber)
Indicates loss of roll assist capability for
respective multi--function spoilers.
IB or OB GND SPLRS caution (amber)
Indicates that respective ground spoilers
are inoperative.
GND SPLR DEPLOY caution (amber)
Indicates that a ground spoiler is deployed
and airplane is not on the ground.
GLD NOT ARMED caution (amber)
Indicates that ground lift dumping is not
armed and airplane is in either approach
or take--off configuration.
GLD UNSAFE caution (amber)
Indicates that ground lift dumping mode is
unsafe (possible inadvertant deployment of
spoilers due to failure of two or more input
sensors).
Primary Page
of the 0 position with the aircraft either in
go--around or the radio altitude is below 300 feet.
FLT SPLR DEPLOY caution (amber)
Vol. 1 11--70--6
FLIGHT CONTROLS
Spoilers REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Spoilers --- EICAS Indications --- Status Page
Figure 11---70---5
GND SPLR DEPLOY advisory (green )
Indicates that a ground spoiler is deployed
and airplane is on the ground.
GLD MAN ARM advisory (green)
Indicates that ground lift dumping is
manually armed.
SPLR/STAB IN TEST advisory (green)
Indicates that the spoiler and stabilizer
control system is in self test mode.
IB or OB FLT SPLR FAULT status (white)
Indicates a loss in redundancy of proportional
lift dumping capability for respective
multi--function spoilers.
GLD MAN DISARM status (white)
Indicates that ground lift dumping is
manually disarmed.
SPLR/STAB FAULT status (white)
Indicates a fault in the spoiler and
stabilizer control unit.
IB or OB GND SPLR FAULT status (white)
Indicates a loss in redundancy of respective
ground spoilers.
IB or OB SPLRONS FAULT status (white)
Indicates a loss in redundancy of roll assist
capability for respective multi--function spoilers.
SSCU 1 or 2 FAULT status (white)
Indicates that one of two spoiler and
stabilizer control modules has failed or
is not powered.
Status Page
FLT SPLR DEPLOY
GND SPLR DEPLOY
GLD MAN ARM
SPLR/STAB IN TEST
GLD MAN DISARM
SPLR/STAB FAULT
SSCU 1 FAULT
SSCU 2 FAULT
IB FLT SPLR FAULT
OB FLT SPLR FAULT
IB GND SPLR FAULT
OB GND SPLR FAULT
IB SPLRONS FAULT
OB SPLRONS FAULT
Vol. 1 11--70--7
FLIGHT CONTROLS
Spoilers REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
SSCU 1 CH A DC BUS 1 1 F1
Spoilers Control Unit
SSCU 1 CH B DC BUS 2 F1
SSCU 2 CH A DC
2 R3
SSCU 2 CH B
ESSENTIAL R4
Vol. 1 11--70--8
FLIGHT CONTROLS
Spoilers REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 11--80--1
FLIGHT CONTROLS
Stall Protection System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
1. STALL PROTECTION SYSTEM
The purpose of the stall protection system is to provide warning of an impending stall when
the aircraft attitude approaches a high angle--of--attack (AOA) and to prevent stall
 
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