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format, disables the radio tuning, and turns off the L−PFD. The MFD includes a compressed
EICAS page and a compressed PFD.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−51
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DISPLAY REVERSION (CONT'D)
Reversion L−PFD Failure
Figure 11−10−45
R-PFD Failure
Turning the R DISPLAYS selector knob to MFD REV reverts the R−MFD to a PFD format,
disables the radio tuning, and turns off the R−PFD. Maintenance and checklist functionality are
also lost.
Reversion R−PFD Failure
Figure 11−10−46
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−52
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DISPLAY REVERSION (CONT'D)
MFD Display Reversion
L-MFD Failure
When the L-MFD fails, EICAS data is automatically presented on the R-MFD, and radio tuning is
lost until PFD is reverted.
Turning the L DISPLAYS selector knob to PFD REV reverts the L-PFD to a compressed format
and turns off the L-MFD. The PFD includes a compressed EICAS page and a compressed PFD.
When compressed, the L-PFD can display a SUMMARY page (set via DCP FRMT pushbutton).
Reversion L−MFD Failure
Figure 11−10−47
R-MFD Failure
When the R−MFD fails, radio tuning is lost until PFD is reverted.
Turning the R DISPLAYS selector knob to PFD REV reverts the R−PFD to a compressed format
and turns off the R−MFD. The PFD includes a compressed EICAS page and a compressed
PFD.
When compressed, the R−PFD can display a SUMMARY page (set via DCP FRMT
pushbutton). Maintenance and checklist functionality are also lost.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−53
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
DISPLAY REVERSION (CONT'D)
Reversion R−MFD Failure
Figure 11−10−48
STANDBY FLIGHT INSTRUMENTS
Description
The standby flight instruments are comprised of a self−contained Thales model no. J42551AA
LCD integrated standby instrument (ISI) and a standby compass.
The standby flight instruments are used as an alternative source of flight and navigation data, or
as a cross−check to the electronic flight instrument system.
Integrated Standby Instrument (ISI)
The integrated standby instrument (ISI) replaces the 3 conventional standby flight instruments
(ADI, altimeter and airspeed). In addition, the ISI provides the flight crew with:
• Slip/skid indicator;
• VMO/MMO indications
• MACH number;
• Barometric unit in inches and/or hectopascals;
• Altitude in feet and meters;
• ILS deviation scales; and
• Static source error correction (SSEC).
The ISI receives air data information from the standby pitot static system (P3 and S3). The ISI
receives electrical power from the DC ESS BUS.
An internal inertial measurement unit measures the rotation speed and acceleration, in order to
compute and display the attitude (pitch and roll).
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−54
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
STANDBY FLIGHT INSTRUMENTS (CONT'D)
An internal pressure measurement unit measures the total and static pressures, in order to
compute and display the altitude and the airspeed, taking into account the static source error
correction (SSEC) law tables.
A yellow SSEC flag may be displayed if the ISI is not able to compute A/C airspeed and altitude,
by taking into account SSEC law correction tables.
Localizer and glideslope data comes from VHF NAV 1. The localizer and glideslope pointers and
scales do not come into view until a valid ILS frequency is received. If the localizer or glideslope
data becomes invalid, the appropriate red (LOC or GS) flag comes into view, and the
corresponding pointer and scale are removed.
ISI Alignment
When the ISI is first energized, a self−test is initiated (10 to 20 sec) for airspeed and altitude,
then an alignment is in progress (attitude) with an ALIGNING flag in view. After approximately
70 seconds, the flag is removed from view and ISI becomes operational.
ISI Alignment (Attitude)
Figure 11−10−49
ISI Functions
The brightness control buttons (+) and (−) provide adjustment independent of the instrument
panel lighting.
The cage button resets the attitude to zero when depressed for more than two seconds.
FLIGHT INSTRUMENTS
Description
Vol. 2 11−10−55
　
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