Garmin Cessna Caravan G1000, Manual Supplement

Page: 38 / 65

FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
DIAMOND MODEL DA 40
DIAMOND MODEL DA 40 F
190-00492-10 Rev 5 Diamond DA 40 / DA 40F
Page 38 of 65
3.8.2 AHRS FAILURE
NOTE
A failure of the Attitude and Heading Reference System (AHRS) is indicated by
removal of the sky/ground presentation and a red X and a yellow “AHRS
FAILURE” shown on the PFD. The digital heading presentation will be
replaced with a yellow “HDG” and the compass rose digits will be removed.
The course pointer will indicate straight up and course may be set using the
digital window.
1. Use Standby Attitude Indicator, magnetic compass and Navigation Map
2. Course .......................................................................... Set using digital window
3.8.3 AIR DATA COMPUTER (ADC) FAILURE
NOTE
Complete loss of the Air Data Computer is indicated by a red X and yellow text
over the airspeed, altimeter, vertical speed, TAS and OAT displays. Some FMS
functions, such as true airspeed and wind calculations, will also be lost.
1. Use Standby Airspeed Indicator and Altimeter
2. Land as soon as practical at a suitable airport
3.8.4 ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS
NOTE
Loss of an engine parameter is indicated by a red X through the data field.
Erroneous information may be identified by indications that do not agree with
other system information. Erroneous indications may be determined by
comparing a display with other displays and other system information.
1. Set power based on throttle lever position, engine noise, and speed.
2.
Monitor other indications to determine the health of the engine.
3.
Use known power settings from the AFM for approximate fuel flow values.
4.
Use other system information, such as annunciator messages, ENGINE
SYSTEM page, and AUX – TRIP PLANNING page to safely complete the
flight.