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Revision 25 DOT Approved
DA20-C1 Flight Manual
.
5. Limitations on the right upper corner of the instrument panel
a.
b.
For aircraft operated in European Aviation Safety Agency (EASA) member countries only.
Doc # DA202-C1 April 06, 2010 Page S13 - 6
Revision 25 DOT Approved
DA20-C1 Flight Manual
6. Circuit breaker on the right side of the instrument panel
b.
Doc # DA202-C1 April 06, 2010 Page S13 - 7
Revision 25 DOT Approved
DA20-C1 Flight Manual
7.
8.
Trim placard on the upper left corner of the instrument panel
DA20-C1 Flight Manual
3. EMERGENCY PROCEDURES
3.1 Emergency Procedures
No change.
3.2 Abnormal Procedures
These procedures supersede those presented as markings or placards, or documented in the aircraft’s TCCA/FAA approved AFM as a result of the installation of the G500 PFD/MFD system. All other emergency procedures remain in effect.
1.
If primary flight information (Heading, Altitude or Airspeed) on the PFD is not available or appears invalid, utilize the standby instruments installed around and adjacent to the G500, as required.
2.
The AHRS requires at least one GPS or air data input to function properly. In the unlikely event that GPS data or air data is not received by the AHRS, the system will subsequently lose attitude and heading and the pilot will be required to use the standby instrumentation. In this instance, the PFD will not provide Attitude, Heading, Altitude, or Airspeed information; however, if the PFD is receiving valid GPS information, the reversionary data on the PFD provides GPS track and GPS Altitude data along with course information and deviations which are still valid and may be used to navigate.
3.
If navigation information on the PFD/MFD (HSI, RMI, WPT bearing and distance information, or Moving Map Data) is not available or appears invalid, select an alternate source (via CDI key or 1-2 key) or utilize the data directly from the navigation equipment as required.
4.
If any of the data sources from SVT become unreliable or unavailable, the display of synthetic terrain will automatically revert to the non-SVT PFD display of blue over brown. Additionally, if during the course of normal operations there is any discrepancy between actual terrain around the aircraft and terrain shown on the SVT display, the display of synthetic vision should be manually turned off using the procedure in paragraph 4.3 of this supplement.
5.
If GPS position information from the GNS430W is not valid due to an inability to track GPS, the own-ship icon on the MFD is removed and “NO GPS POSITION” text is overlaid on the MFD moving map. The system will annunciate a loss of integrity, “LOI” on the HSI. The LOI annunciation will be colored yellow and the HSI needle will flag. The pilot should select an alternate navigation source (via CDI key or 1-2 key). Pressing the CDI soft key will change the HSI navigation source. If GPS navigation is subsequently restored, the MFD moving map will display the own-ship icon, and the HIS navigation source may be selected to GPS; at that time the LOI annunciation will be removed.
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