Garmin Cessna Caravan G1000 Ergänzung zum Flughandbuch für Flugzeuge - Seite 15

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Garmin Cessna Caravan G1000 Ergänzung zum Flughandbuch für Flugzeuge
MOONEY
M20R
SECTION III - - EMERGENCY PROCEDURES
GENERAL
1. These checklists supercede those in the POH as a result of the
installation of the G1000 avionics system. All other emergency pro-
cedures in the POH remain in effect.
2. These checklists assume that the aircraft is equipped with a standby
alternator system installed by Mooney Airplane Company, Inc.
3. If GARMIN G1000 GPS navigation information is not available or in-
valid, utilize remaining operational navigation equipment as re-
quired.
4. If the "POSN ERROR" annunciation is displayed the system will flag
and no longer provide GPS based navigational guidance. The crew
should revert to the G1000 VOR/ILS receivers or an alternate
means of navigation other than the G1000 GPS receivers.
5. If the "POSN ERROR" annunciation is displayed in the enroute,
oceanic, terminal, or initial approach phase of flight, continue to nav-
igate using the GPS equipment or revert to an alternate means of
navigation other than the G1000 GPS receiver appropriate to the
route and phase of flight. When continuing to use GPS navigation,
position must be verified every 15 minutes using the G1000 VOR/
ILS receiver or another IFR--approved primary navigation system.
6. CAUTION: If the "POSN ERROR" annunciation is displayed while
on the final approach segment (between the Final Approach Fix and
the Missed Approach Point), GPS based navigation will continue for
up to 5 minutes with approach CDI sensitivity set at 0.3 nautical mile.
It is recommended that the pilot initiate the missed approach upon
receipt of this message from the G1000. Navigation guidance will
continue for 5 minutes allowing the pilot to initiate the missed ap-
proach while maintaining course guidance on the final approach
course. Then the system will flag and no longer provide course guid-
ance with approach sensitivity. Missed approach course guidance
may still be available with 1 nautical mile CDI sensitivity by executing
the missed approach. This is typically caused by the GPS sensor's
inability to provide adequate horizontal position accuracy for the fi-
nal approach segment. It is possible, however unlikely, that the GPS
position may degrade to the point where terminal operations cannot
be supported for the missed approach segment. Navigate using
other primary navigation equipment (VOR receivers, etc) if this oc-
curs.
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
AFM SUPPLEMENT
15 of 33
FAA APPROVED