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• By depressing the MODE button once, the day digits are flashing and you can adjust the
display in the same way. The DT flag is lit.
• By depressing the MODE button once, the LT minutes digits are flashing and you can
adjust the display in the same way. The LT flag is lit.
• One more press on MODE button will lead to GMT minutes adjustment.
• Press the MODE button for more than 2 seconds to start the clock operation.
The default time and date for the SET mode at initialization of the clock will be: The 1st of
January 2002 at 00 hr and 00 min.
Set after Syncronization by GPS or Manual Starting
If the GPS data is valid, only the LT mode can be set.
The setting is obtained by means of the SET function which is available by pressing the MODE
pushbutton for a minimum of two seconds.
• By depressing the MODE button, the setting roll in LT time if the LT setting is chosen.
• By depressing the MODE button, the setting roll in DATE if the DT setting is chosen.
• By depressing the MODE button, the setting roll in INT time if the INT setting is chosen.
FLIGHT INSTRUMENTS
REV 46, Jul 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−51
PFD COMPARISON MONITOR ANNUNCIATIONS
Comparison monitor annunciations are displayed when the difference between the data received by
the pilot’s and copilot’s PFD, exceeds the predetermined trip thresholds.
Indicates a miscompare
of + 5° of pitch.
Indicates engine data
miscompare between the
sensors (DAU) and the
engine parameters for
more than 3 seconds.
Indicates a miscompare
of + 6° of roll.
IAS
Indicates a miscompare
of + 20 knots.
ALT
Indicates a miscompare
of + 200 feet.
ATT
Indicates a miscompare
of + 5° of pitch and + 6°
of roll.
HDG
Indicates a miscompare
of + 10°.
Indicates a miscompare
of + 1/2 dot.
LOC
RAD
Indicates a miscompare
of + 10 feet.
GS
Indicates a miscompare
of + 0.24°.
PIT
ROL
FWC
EICAS
Indicates CAS message miscompare
(warnings, cautions and advisories)
for more than 7 seconds.
GF1110_056
−
−
−
−
−
−
−
−
−
−
HDG
030
HDG
29.92 IN
104 00
9500
10500
100 00
ALT
AP1 ASEL
CRS
360
210
20
20
20
20
220
210
200
190
180
170
160
150
10 10
10 10
33
30
24 21
S
15
6
N 3
W
E
12
N
1000
VS 1000
0
1
2
3
1
2
3
IAS
ATT
HDG
LOC
EICAS
FWC
RAD
6
4
185
GS
The CHECK PFD warning message will be displayed on the EICAS display if both PFDs have
misleading data in flight or when the DC ESS and DC BUS 2 busses are powered on the ground.
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
11−10−52
FLIGHT INSTRUMENTS EICAS MESSAGES
ADC 1 (2)(3) MISCOMP
Indicates that
respective ADC has
miscompared.
CHECK PFD
Indicates that both PFDs
have misleading data.
ASCB CTRL 1 (2)(3) FAIL
Indicates loss of
communication with two of
three bus controllers.
ASCB FAIL
Indicates loss of
communication with all
three bus controllers. Loss
of all flight instruments and
AFCS functions.
IRS 1 (2)(3) OVHT
Indicates IRS has an
overtemperature condition
ALL ADC MISCOMP
Indicates that all three
ADCs have miscompared.
ALL IRS MISCOMP
Indicates that all three IRS
have miscompared.
IRS 1 (2)(3) MISCOMP
Indicates that
respective IRS has
miscompared.
DISP CTLRS FAIL
Indicates that both
display controllers
GF1110_100c
CHECK PFD
ALL ADC MISCMP
ADC 1 MISCMP
ADC 2 MISCMP
ADC 3 MISCMP
ALL IRS MISCMP
IRS 1 MISCMP
IRS 2 MISCMP
IRS 3 MISCMP
ASCB CTRL 1 FAIL
ASCB CTRL 2 FAIL
ASCB CTRL 3 FAIL
ASCB FAIL
DISP CTLRS FAIL
IRS 1 OVHT
IRS 2 OVHT
IRS 3 OVHT
have failed.
FLIGHT INSTRUMENTS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−53
FLIGHT INSTRUMENTS EICAS MESSAGES (CONT'D)
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航空翻译 www.aviation.cn
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