Garmin G1000 Pilot’s Guide for the Socata TBM 850
190-00709-04 Rev. A
90
ENGINE & AIRFRAME SYSTEMS
In the event of a display failure, depending on the failed display(s), the functioning display(s) may be re-
configured to present Primary Flight Display (PFD) symbology together with engine and CAS information
(refer to the System Overview for more information about Reversionary Mode). In Reversionary Mode, engine,
pressurization, fuel, electrical, and trim data is presented in an abbreviated format on the left of the display.
CAS messages appear in a window on the right of the display. Synoptics are not available while in Reversionary
Mode.
EIS
Display
CAS
Window
Figure 3-2 Reversionary Mode
Содержание SOCATA TBM850
Страница 1: ...G1000 Integrated Flight Deck Pilot s Guide...
Страница 2: ......
Страница 10: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A vi REVISION INFORMATION Blank Page...
Страница 64: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 50 SYSTEM OVERVIEW Blank Page...
Страница 102: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 88 FLIGHT INSTRUMENTS Blank Page...
Страница 166: ...190 00709 04 Rev A Garmin G1000 Pilot s Guide for the Socata TBM 850 152 AUDIO PANEL AND CNS Blank Page...
Страница 482: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A 468 HAZARD AVOIDANCE Blank Page...
Страница 682: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 04 Rev A I 8 INDEX Blank Page...
Страница 683: ......