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(5) HF 2................................................................... Attempt communication.
END
F. Flight Management System Tuning Failure
Indication: Unreliable FMS tuning data.
(1) FMS TUNE switch/light (centre
pedestal)............................................................Press in to inhibit FMS radio tuning
operation.
Check FMS TUNE INHIB light
on.
END
ABNORMAL PROCEDURES
Miscellaneous Systems
05−17−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. MISCELLANEOUS SYSTEMS (CONT'D)
G. Flight Management System CDU/FMC Failure
Indication: No data available on CDU.
(1) Reversionary panel, FMS 3 switch
(if installed) ............................................................... Set to failed FMS position.
On airplanes 5500 and subsequent and airplanes incorporating Service Bulletin
604–34–031:
(2) N1 setting value................................................Deselect active N1 thrust setting from
EICAS display. Use N1 thrust
setting value displayed on
CDU(s) only.
NOTE
The input parameters on the THRUST LIMIT, TAKEOFF REF and
APPROACH REF CDU pages must be re-confirmed by the pilot
following an FMS SYNC command, an FMS 3 reversion (if installed) or
an FMS cold start.
END
ABNORMAL PROCEDURES
Miscellaneous Systems
05−17−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Miscellaneous Systems
05−17−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. AURAL/VISUAL WARNING SYSTEM
A. EICAS Primary Display Failure
Indication: EICAS primary display goes blank.
The system automatically transfers the EICAS primary page data to the operational display
position.
If automatic transfer does not occur:
(1) Left MFD display control switch............................Select to EICAS.
(2) EICAS source selector .........................................Select to ED2.
Check the following:
• ED2 display reverts to PRI
(engines) page.
• Left MFD reverts to EICAS
STAT (status) page.
• All page functions are
selectable on the EICAS
control panel.
END
B. EICAS Secondary Display Failure
Indication: EICAS secondary display goes blank.
(1) Right MFD display control switch .........................Select to EICAS.
(2) EICAS source selector .........................................Select to ED 1.
Check the following:
• Right MFD reverts to EICAS
STAT (status) page.
• All page functions are
available on the EICAS
control panel.
END
C. EICAS Control Panel Failure
Indication: EICAS control panel buttons will not select synoptic/menu pages.
The PRI, STAT, CAS and STEP switches remain operable during a microprocessor failure:
To display a synoptic page (HYD, ELEC, or F/CTL):
(1) STEP switch ......................................................Press in and step as required, in order
to scroll to applicable page.
END
ABNORMAL PROCEDURES
Aural/Visual Warning System
05−18−1
REV 69, Jun 04/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AURAL/VISUAL WARNING SYSTEM (CONT'D)
D. Data Concentrator Unit Failure
Indication: DCU 1 (2) (3) INOP status message.
(1) Affected AUDIO WARNING switch.......................Select to DISABLE.
(2) Other AUDIO WARNING
switch(es) .............................................................Select to NORMAL.
END
E. Data Concentrator Unit Aural Failure
Indication: DCU 1 (2) (3) AURAL INOP status message.
(1) Affected AUDIO WARNING switch.......................Select to DISABLE.
(2) Other AUDIO WARNING
switch(es) .............................................................Select to NORMAL.
END
F. EICAS Comparator Inoperative
Indication: EICAS COMP INOP caution message.
Third DCU installed:
Yes
Two DCUs failed:
Yes
(1) Engine indications...............................Monitor
− END −
No
(1) EICAS displays (both) ..........................................Select to PRI page.
(2) Engine and instruments,
parameters and messages.........................Cross-check for any anomalies.
(3) EICAS, PRI page..................................................... Use reliable side.
(4) Affected engine and/or system......................... Maintain within limits.
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(29)
