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− END −
No
Cowl anti-ice is selected off:
(Caution message may indicate a high pressure condition.)
(1) Affected engine thrust ............................................. REDUCE N2
to less than 85%.
(2) Affected 14TH STAGE bleed ........................................CLOSED
(3) Leave icing conditions.
If wing anti-ice is required:
(4) 14TH STAGE ISOL ........................................................... OPEN
END
Probe Heater Failure
AUX AOA CASE HEAT
or
AUX AOA VANE HEAT
or
L AOA HEAT
or
L PITOT BASE HEAT
or
L PITOT TUBE HEAT
or
L PROBE HEAT OFF
or
L STATIC HEAT
STBY PITOT HEAT
or
TAT PROBE HEAT
or
R AOA HEAT
or
R PITOT BASE HEAT
or
R PITOT TUBE HEAT
or
R PROBE HEAT OFF
or
R STATIC HEAT
(1) ANTI-ICE PROBES ................................................ OFF then ON
ABNORM 11-7
REV 72, Jan 22/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 ICE AND RAIN PROTECTION
Probe Heater Failure (Cont’d)
Applicable caution message still on:
Yes
MESSAGE ACTION
L (R) AOA HEAT Do not rely on stall protection system.
(2) No further action required.
AUX AOA CASE
HEAT
AUX AOA VANE
HEAT
Do not rely on low speed cue displayed
on both PFDs.
(2) No further action required.
L (R) PITOT TUBE
HEAT
L (R) PITOT BASE
HEAT
Do not rely on associated instruments:
• ATC transponder,
• Air Data Computer, and
• Inertial Reference System.
(2) Select ADC source to operative side.
L (R) STATIC
HEAT
Do not rely on associated instruments:
• Standby altimeter / airspeed indicator,
and
• Cabin pressure acquisition module.
(2) No further action required.
STBY PITOT HEAT
Do not rely on standby indicated airspeed
indicator.
(2) No further action required.
TAT PROBE HEAT
Do not rely on air temperature
indications.
(2) No further action required.
L (R) PROBE
HEAT OFF
During flight – No further action required.
Both L and R AOA HEAT caution messages persist:
Yes
(2) Avoid icing conditions.
(3) STALL FAIL Procedure ........................ ACCOMPLISH
(See Page ABNORM 8−2)
− END −
No
(2) No further action required.
END
ABNORM 11-8
REV 68, Apr 16/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ICE AND RAIN PROTECTION
Windshield/Window Heat Failure
L WSHLD HEAT
or
R WSHLD HEAT
L WINDOW HEAT
or
R WINDOW HEAT
(1) Affected ANTI-ICE,
WSHLD/WIND..................................................................RESET
then LO or HI, as applicable.
Caution message persists:
Yes
(2) CKPT HEAT ................................................................... ON
(3) AIR
(cockpit heat diverter valve)................................PULL OUT
− END −
No
(2) No further action required.
END
Windshield Outer Face Ply Failure
(1) Affected ANTI-ICE,
WSHLD/WIND...................................................................... OFF
(2) CKPT HEAT ........................................................................... ON
(3) AIR (cockpit heat diverter valve) ................................PULL OUT
END
ABNORM 11-9
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ICE AND RAIN PROTECTION
ABNORM 11-10
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ICE AND RAIN PROTECTION
THIS PAGE INTENTIONALLY LEFT BLANK
CONTENTS PAGE
• Primary Flight Display Failure .................................ABNORM 12−2
• Display Control Panel Failure..................................ABNORM 12−2
• EFIS COMP INOP ..................................................ABNORM 12−2
• EFIS COMP MON ..................................................ABNORM 12−3
• ADC Failure.............................................................ABNORM 12−4
• Radio Altimeter Failure............................................ABNORM 12−5
• IRS Failure ..............................................................ABNORM 12−6
ABNORM 12-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
INSTRUMENTS
MALFUNCTIONS
Primary Flight Display Failure
........PFD goes blank
On the reversionary panel:
(1) Applicable MFD ............................................... SELECT TO PFD
　
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