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时间:2010-09-27 08:10来源:蓝天飞行翻译 作者:admin
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END
Display Control Panel Failure
........Display Control Panel is inoperative
........CRS & HDG knobs on Flight Control Panel are inoperative
(1) DCP................................................................................SELECT
operative side.
(2) Autopilot XFER...............................................................SELECT
side corresponding to operative DCP.
NOTE
HDG knob remains inoperative until operable display
control panel is selected.
END
EFIS COMP INOP
Applicable comparator has failed:
(1) Affected flight instruments ...........................................MONITOR
(2) Standby instruments.......................................... CROSS CHECK
END
ABNORM 12-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
INSTRUMENTS
MALFUNCTIONS
EFIS COMP MON
PFD ACTION
ALT and/or
IAS
(1) Flight instruments and
standby flight instruments........ CROSS CHECK
(2) AIR DATA source selector....................SELECT
to reliable side.
Refer to Aircraft Flight Manual, Chapter 6,
PERFORMANCE – GENERAL, for alternate static
system position error correction charts.
ROL or PIT
(1) Flight instruments and
standby flight instruments........ CROSS CHECK
(2) IRS source selector ..............................SELECT
to reliable side.
HDG
IRS 1 (2) (3) IN ATT status message displayed:
Yes
(1) FMS................................................ENTER
present airplane heading on the
IRS CONTROL page.
No
(1) IRS mode selectors ............................... CHECK
set to NAV.
(2) Flight instruments and
standby flight instruments............... Cross check
(3) IRS source selector ..............................SELECT
to reliable side.
RA
(1) Radio Altimeter Failure
Procedure ...................................ACCOMPLISH
(See Page ABNORM 12–5)
LOC or GS If non-visual, during approach:
(1) Go-around ........................................... INITIATE
END
ABNORM 12-3
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
INSTRUMENTS
MALFUNCTIONS
ADC Failure
........Erratic primary display data
........Similar indications to EFIS comparator monitor failures
Pilot’s ADC has failed:
Yes
(1) ADC source selector.................................................. 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 .........................................................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
ABNORM 12-4
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15
INSTRUMENTS
MALFUNCTIONS
Radio Altimeter Failure
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
ABNORM 12-5
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
INSTRUMENTS
MALFUNCTIONS
IRS Failure
........Erratic primary flight display data
........Similar indications to EFIS comparator monitor failures
NOTE
If an IRS is in ATT mode, a heading drift of up to 15°/hr
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.
 
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