Section 924
ASPEN EFD1000 PILOT PFD
924 - 10 Page Date: 31. March 2009
Pilot´s Operating Handbook
EXTRA 300L
924.7.10 MAP RANGE CONTROL
The EFD1000 PILOT PFD basemap range may be set to ranges of 2.5, 5, 10, 15, 20, 30, 40, 60,
80, 100, and 200 nautical miles. Map range is measured from the own ship position to the outside
of the compass arc.
To increase the range push the ‘+’ side of the range key located on the upper right side of the bezel.
To decrease the range push the ‘–‘ side of the key. The currently selected map range is displayed
in the lower left corner of the display.
924.7.11 DISPLAY REVERSION CONTROL AND ABNORMAL SHUTDOWN
Single PFD installations do not have a display reversion capability that can be activated by the REV
button. As such, the reversion function is inoperative in single display installations.
In addition to display reversion control, the REV button may be used to force the unit to power off
should, for example, the display stop responding to pilot inputs. When external power has been
removed by pulling the PFD circuit breaker, pressing and holding the REV button for 5 Seconds
will produce in an immediate system shut down. When external power is available (PFD circuit
breaker reset), pressing and holding the REV button for 5 seconds will result in a system restart.
924.7.12 WARNING, CAUTION, AND ADVISORY SUMMARY
WARNINGS
ON BAT
53% REM
Red annunciation presented below the aircraft symbol whenever the EFD1000 PILOT PFD is
operating on the internal battery. Will be accompanied by an indication of the estimated battery
charge remaining.
Function FAIL („X“)
Red annunciation presented whenever the EFD1000 PILOT PFD has determined that the
associated function is invalid or failed and should not be used. The data is removed from the display
and replaced by a red „X“ over the affected display feature.
CAUTIONS
CROSS CHECK
ATTITUDE
Amber annunciation presented centered in the lower half of the attitude indicator whenever the
EFD1000 AHRS internal integrity monitor determines that attitude is potentially degraded. If a
CROSS CHECK ATTITUDE annunciation is provided the pilot should cross check attitude, airspeed
and altitude indications against the real-life horizon and the primary instruments.
GPS1 and/or
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