Check Engine Display
3-22-12
PFD engine data suspect.
1.
Display........................................
Cross check pilot PFD data with copilot
PFD data
If data confirmed to be suspect:
2.
Reversion Controller...................
Set pilot PFD control knob to AGM2
If data remains suspect:
3.
Aircraft.........................................
Land as soon as practical using minimum
engine power to avoid exceeding engine
limits
---------- END -----------
ATT FAIL
3-22-13
1.
PFD pitch and roll.......................
Check
If shading is all blue and red crosses are shown, data has become invalid:
2.
Pitch and Roll data......................
Use Electronic Standby Instrument
System (ESIS)
3.
ADHRS pushbutton on PFD
Controller....................................
Press to bring the other ADAHRS
channel data onto PFD
---------- END -----------
RAD
3-22-14
Radar Altimeter data has become invalid.
Note
Autothrottle does not disconnect automatically when radar altimeter data is invalid
and/or the radar altimeter system has failed.
1.
Altitude data................................
Use Altimeter Indicator
---------- END -----------
HDG FAIL
3-22-15
Heading data has become invalid.
1.
Heading data...............................
Use Standby Magnetic Direction Indicator
Continued on next page
Section 3 - Emergency Procedures (EASA Approved)
APEX Failures
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3-22-7
12-C-A15-40-0322-00A-141A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
