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PSP 604-15 MISCELLANEOUS SYSTEMS
CONTENTS PAGE
• EICAS Primary Display Failure ...............................ABNORM 15−2
• EICAS Secondary Display Failure ..........................ABNORM 15−2
• EICAS Control Panel Failure...................................ABNORM 15−2
• DCU Failure or DCU Aural Failure..........................ABNORM 15−3
• EICAS COMP INOP ...............................................ABNORM 15−3
• TCAS Failure...........................................................ABNORM 15−3
• TCAS RA Failure.....................................................ABNORM 15−4
• TCAS TA Failure.....................................................ABNORM 15−4
• TCAS TD Failure.....................................................ABNORM 15−4
ABNORM 15-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AURAL/VISUAL WARNING
SYSTEM
EICAS Primary Display Failure
........EICAS primary display goes blank
If the automatic transfer does not occur:
(1) Left MFD display control switch.........................................EICAS
(2) EICAS source selector .........................................................ED 2
END
EICAS Secondary Display Failure
........EICAS secondary display goes blank
(1) Right MFD display control switch ......................................EICAS
(2) EICAS source selector .........................................................ED 1
END
EICAS Control Panel Failure
........EICAS control panel buttons will not select synoptic/menu pages
The PRI, STAT, CAS and STEP buttons remain operable during
a microprocessor failure:
To display a synoptic page (HYD, ELEC or F/CTL):
(1) STEP switch ................................................................... UTILIZE
as required, to scroll to applicable page.
END
ABNORM 15-2
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AURAL/VISUAL WARNING
SYSTEM
DCU Failure or DCU Aural Failure
(1) Affected AUDIO WARNING ......................................... DISABLE
(2) Other AUDIO WARNING.............................................. NORMAL
END
EICAS COMP INOP
EICAS COMP INOP
Third DCU installed:
Yes
Two DCUs failed:
Yes
(1) Engine indications .......................................MONITOR
− END −
No
(1) EICAS displays (both) .................................................PRI PAGE
(2) Engine and instrument
parameters, messages...................................... CROSS CHECK
(3) PRI Page .............................................................................. USE
reliable side.
(4) Affected engine and/or system................................... MAINTAIN
within limits.
END
TCAS Failure
TCAS FAIL
........on PFD and/or MFD
(1) RTU, TCAS mode .............................................................. STBY
to select TCAS off.
END
ABNORM 15-3
REV 71, Oct 31/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AURAL/VISUAL WARNING
SYSTEM
TCAS RA Failure
TCAS RA FAIL
........on PFD
TCAS RA FAIL caution message displayed on both PFDs:
Yes
(1) RTU, TCAS mode................................................. TA ONLY
to select traffic advisory only.
− END −
No
TCAS RA FAIL caution message on one PFD:
(1) Pilot with functional RA-display would be required to carry out
any subsequent avoidance maneuvers.
END
TCAS TA Failure
TCAS TA FAIL
........on MFD
TCAS TA FAIL caution message displayed on both MFDs:
Yes
(1) No further action required.
Assume loss of traffic advisory data on both MFDs.
Resolution advisory data remains available.
− END −
No
TCAS TA FAIL caution message displayed on one MFD:
(1) Other MFD............................................................................ USE
to obtain traffic advisory data.
END
TCAS TD Failure
TCAS TD FAIL
........on MFD
(1) No further action required.
Assume loss of traffic advisory data on both MFDs.
Resolution advisory data remains available.
END
ABNORM 15-4
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AURAL/VISUAL WARNING
SYSTEM
The following are system response or acknowledgment-type
messages (green).
ENGINE
L (R) REV ARMED L (R) thrust reverser armed and ready.
APR ARM APR system is armed.
APR TEST 1 (2) (3) OK APR test successful at DCU 1 (2).
IGNITION A (B) Ignition system A (B) is activated.
　
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