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MFD L (R) switch..................................................Select to PFD.
Check applicable MFD reverts
to primary flight display.
END
B. Display Control Panel Failure
Indication: Display control panel is inoperative, course and HDG knob is inoperative.
(1) Reversionary panel, DCP switch..........................Select operative side.
(2) Autopilot XFR switch ............................................Select side corresponding to
operative display control
panel.
NOTE
HDG knob remains inoperative until operable display control panel is
selected.
END
C. EFIS Comparator Failure
Indication: EFIS COMP INOP caution message.
(1) Affected flight instruments ..................................Monitor
(2) Standby instruments................................................ Use to cross-check.
END
D. EFIS Comparator Monitor Failures
Indication: EFIS COMP MON caution message on, and one of the following comparator
warning annunciators shown on the primary flight display.
• ALT • IAS • ROL • LOC
• HDG • PIT • RA • GS
PFD ACTION
ALT and/or IAS
(1) Flight instruments and
standby flight instruments............Cross
check
(2) Centre pedestal, AIR
DATA source selector
switch.......................................... Select to reliable side
Refer to Chapter 6; PERFORMANCE, for alternate static system
position error correction charts.
ABNORMAL PROCEDURES
Instruments System
05−15−1
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. INSTRUMENTS SYSTEM (CONT'D)
D. EFIS Comparator Monitor Failures (Cont’d)
PFD ACTION
ROL or PIT
(1) Flight instruments and
standby flight instruments............Cross
check
(2) Reversionary panel, IRS
switch.......................................... Select to reliable alternate
source.
HDG
IRS 1 (2) (3) IN ATT status message displayed:
Yes
(1) FMS ......................................Enter present airplane
heading on the IRS
CONTROL page.
No
(1) Centre pedestal, IRS
switches......................................Check set to NAV.
(2) Flight instruments and
standby flight instruments............Cross
check
(3) Reversionary panel, IRS
switch.......................................... Select to reliable alternate
source.
RA
(1) Radio altimeter failure
procedure ...........................Accomplish
Refer to Radio Altimeter Failure procedure, in this section.
LOC or GS
If non-visual, during approach:
(1) Go-around ..................................Initiate
END
ABNORMAL PROCEDURES
Instruments System
05−15−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. INSTRUMENTS SYSTEM (CONT'D)
E. Air Data Computer Failure
Indication: Similar to EFIS comparator monitor failures; erratic primary flight display
data.
Pilot’s ADC has failed:
Yes
(1) ADC source selector.....................................Select to copilot’s side (ADC 2).
Check PFD 1 indicates single
air data source selected
(ADC 2).
NOTE
1. Ground proximity warning system (if installed) is
inoperative, GPWS FAIL status message comes on.
2. Windshear detection (if installed) is inoperative on both
sides.
3. For standby static system position error correction
charts, refer to Chapter 6; PERFORMANCE.
4. For RVSM operation, select the transponder associated
with the remaining ADC.
− END −
No
Copilot’s ADC has failed:
(1) ADC source selector ............................................Select to pilot’s side (ADC 1).
Check PFD 2 indicates single
air data source selected
(ADC 1).
NOTE
1. Windshear detection (if installed) is operative on pilot’s side
only.
2. For standby static system position error correction charts,
refer to Chapter 6; PERFORMANCE.
3. For RVSM operation, select the transponder associated with
the remaining ADC.
END
ABNORMAL PROCEDURES
Instruments System
05−15−3
REV 69, Jun 04/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. INSTRUMENTS SYSTEM (CONT'D)
F. Radio Altimeter Failure
Indication: False Radio Altimeter height and RA annunciation on applicable PFD.
(indications of a radio altitude miscompare)
Pilot’s radio altimeter has failed:
Yes
(1) No further action required.
　
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