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flight time.
Select to display
elapsed time.
Bright/Dim Switch
B
D
1 hr up






Select for bright display.
Select for dim display.
Select momentary
position and release to
advance clock 1 hour.
Elapsed Time Switch
ZERO
STOP
RUN






momentary position
sets elapsed time to zero.
Also zeros flight time if
aircraft power is removed.
position stops elapsed
time meter.
position starts elapsed
time meter.
Press to Reset
Allow the clock's flight
time recorder to be reset
to zero without turning off
aircraft electrical power
Hours
Seconds
Minutes
Press To
Reset
FLIGHT INSTRUMENTS
For Training Purposes Only
May 03
11-51
P I LOT T R A I N I N G GU I D E
Clock A/C 5331 and Later
Figure 11-32
P604_11_049
SELECT CONTROL
GMT LT FT ET
SEL CTL
12 00
DAVTRON
CHRONOMETER
M877
Greenwich Mean Time
Local Time
12-hour format with
24-hour option
Flight Time
Elapsed Time
Audio Alarm
Speaker
Select Button

GMT LT FT ET


To select , , , and
back when momentarily pressed.
To turn off alarm.
Control Button
FT








Starts and resets elapsed time when
momentarily pressed.
Press and hold for 3 seconds for test mode.
With selected, press and hold for 3 secs
to reset flight time.
To turn off alarm.
Note:
Press SEL and CTL buttons simultaneously to enter set mode for GMT, LT, FT and ET Countdown
FLIGHT INSTRUMENTS
11-52 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Display Reversionary Panel
The display reversionary switches on the Display Reversionary Control Panel are used
to select the desired reversion mode of the L(R) MFD.
Both the L MFD and the R MFD can be set to one of three positions:
• Norm: The MFD operates in the NORM position and displays navigation, weather
radar, terrain or TCAS information as selected on the Display Control Panel
• PFD: By turning either the L MFD or the R MFD rotary selector to PFD, the
associated PFD is now transferred to the selected MFD
• EICAS: By turning either the L MFD or the R MFD rotary selector to EICAS, the
STATUS page will be displayed on the selected MFD. The EICAS Control Panel
then controls EICAS page selections
Abnormal Conditions
In the event of a DCP failure, a red boxed DCP shows on the affected PFD. To allow
selection of the operating DCP, a reversionary selector switch is provided on the
reversionary panel. This switch has three positions, NORM, 1, or 2. In the NORM
position, each DCP controls its own MFD. In either the 1 or the 2 position, the
remaining DCP controls the display on both MFDs.
FLIGHT INSTRUMENTS
For Training Purposes Only
May 03
11-53
P I LOT T R A I N I N G GU I D E
Display Reversionary Panel
Figure 11-33
VFE (45 FLAPS)
VFE (30 FLAPS)
VFE (20 FLAPS)
VA (MANEUVERING)
(AT SEA LEVEL 48,200LB)
(AT 20,000FT 26,000LB)
VNO (BELOW 8,000FT)
VNO (8,000 TO 22,150 FT)
AIRSPEED LIMITS - (INDICATED SPEEDS)
MMO (22,150FT TO 26,570FT)
VMO (26,570FT TO 30,990FT)
MMO (30,990FT TO 41,000FT)
VLO (EXT) (L/G EXTENSION)
VLO (RET) (L/G RETRACTION)
VLE (L/G EXTENDED)
189
197
231
248
187
300
348
0.78
318
0.85
197
197
250
PULL
PULLTOCAGE
CAGE
CLI MB
DI VE
OFF
BRT
BRT
BRT
0.0
0.0
0.0
0.0
180 180
N1
ITT
N2
STAB
- TRIM -
NU
ND
5.0
RUDDER
AIL
LWD RWD
NL NR
FF (PPH)
OIL PRESS
OIL TEMP
FAN VIB
0 4050
8100
0.0
33
0
0
0
- FUEL (LBS) - TOTAL
0
0
33
0.0
4050
DN DN DN
- GEAR - - FLAPS - 20
R ENG OIL PRESS
L ENG OIL PRESS
L WSHLD HEAT
L WINDOW HEAT
INBD BRAKE PRESS
R WSHLD HEAT
R WINDOW HEAT
OUTBD BRAKE PRESS
R PROBE HEAT OFF
L PROBE HEAT OFF
HYD 3 LO PRESS
BRT
CABIN TEMP
BLEED PRESS
FUEL TEMP
ENGINE
BULK
OXY
C ALT
RATE
P
47
23
0
36 35
1820
100
0
0.0
APU
100 323
RPM EGT
R FUEL PUMP ON
L FUEL PUMP ON
　
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