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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
Vol. 1 05−15−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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 Airplane Flight Manual, 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 Airplane Flight Manual, Chapter 6; PERFORMANCE.
3. For RVSM operation, select the transponder associated with
the remaining ADC.
END
ABNORMAL PROCEDURES
Instruments System
Vol. 1 05−15−3
REV 69, Jun 04/07
CL−604 Operating Manual
PSP 604−6
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.
− END −
No
Copilot’s Radio Altimeter has failed (if installed):
NOTE
With one radio altimeter failed, both TCAS (if installed) and
GPWS (if installed) remain operational.
(1) No further action required.
END
ABNORMAL PROCEDURES
Instruments System
Vol. 1 05−15−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. INSTRUMENTS SYSTEM (CONT'D)
G. Inertial Reference System Failure
Indication: Similar to EFIS comparator monitor failures; erratic primary flight display
data.
NOTE
If an IRS is in attitude mode, a heading drift rate of up to 15 degrees
per hour can occur. The FMS heading on the IRS CONTROL page
should be updated periodically from the best available alternate
navigation source.
Pilot’s IRS has failed:
Yes
(1) IRS source selector ......................................Select to an operative IRS.
Check PFD 1 indicates IRS 2
source selected (If IRS 3 is
installed and selected, PFD 1
indicates IRS 3 source
selected).
NOTE
1. Windshear detection (if installed) is operative on
copilot’s side only.
2. If IRS 3 is not installed, pilot’s flight director is
inoperative, FD 1 FAIL status message comes on.
− END −
No
Copilot’s IRS has failed:
(1) IRS source selector ..............................................Select to an operative IRS.
PFD 2 indicates IRS 1 source
selected (If IRS 3 is installed
and selected, PFD 2 indicates
IRS 3 source selected).
NOTE
1. Windshear detection (if installed) is inoperative on both
sides.
2. If IRS 3 is not installed, copilot’s flight director is inoperative,
FD 2 FAIL status message comes on.
END
ABNORMAL PROCEDURES
Instruments System
Vol. 1 05−15−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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庞巴迪挑战者604操作手册 Operating Manual 2(30)
