Garmin Software Version 0321.19 Manual de usuario descargar pdf (Pagina 23)

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

FAA Approved Page 23 of 65

Note 2: Not applicable to DA 40 F. Manifold Pressure gauge is not installed in

the DA 40 F.

Note 3: To prevent nuisance alerts during normal takeoffs, the legend “RPM”

and digits will not turn red or flash until the RPM exceeds 2780.

Note 4: Fuel Pressure Gauge is optional for DA 40 aircraft.

2.6 WARNING, CAUTION AND STATUS MESSAGES

The following tables show the color and significance of the warning, caution,

and advisory messages which may appear on the G1000 displays.

NOTE

The G1000 Cockpit Reference Guide and the G1000 Pilot’s Guide contain

detailed descriptions of the annunciator system and all warnings, cautions and

advisories.

Warning annunciations – Red

Annunciation Cause

OIL PRES LO Oil pressure is less than 25 psi

FUEL PRES LO (DA40 Only) Fuel pressure is less than 14 psi

FUEL PRES HI (DA40 Only) Fuel pressure is greater than 35 psi

ALTERNATOR Alternator failure

STARTER ENGD

Operation of the starter without the key in

the start position, or failure of the starter

motor to disengage from the engine after

starting

DOOR OPEN

Front canopy and/or rear door not

completely closed and locked

Caution annunciations – Yellow

Annunciation Cause

PITOT OFF Pitot heat is not switched on

PITOT FAIL Fault in the pitot heating system

L FUEL LOW

Fuel quantity in the left tank is less than 3

US gal (+

1 US gal)

R FUEL LOW

Fuel quantity in the right tank is less than 3

US gal (+

1 US gal)

LOW VOLTS On-board voltage below 24 volts

1 2 ... 18 19 20 21 22 23 24 25 26 27 28 ... 64 65

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Garmin Software Version 0321.19 Manual de usuario Pagina 23

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