Garmin g1000 manual da40

G/DA40 Installation Drawing, (Ref STC #SAWI N/A Replace After Suspected / Actual Lighting Event TVS Unit Replacement (Qty 7) Replace all five voltage suppressor units. Refer to G/DA40 Installation Drawing, (Ref STC #SAWI) and TVS Installation Drawing: 9Battery, Alternator, GMA , and. Garmin G Cockpit Reference Guide for the DA40/40F Rev. A WARNINGS, CAUTIONS, NOTES NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge. Garmin G Cockpit Reference Guide for the DA40/40F WARNINGS, CAUTIONS, NOTES WARNING: The Garmin G, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical.

Rev. B Garmin G Annunciations and Alerts Pilot's Guide for the DA40 ANNUNCIATIONS ALERTS INTRODUCTION NOTE: The Aircraft Flight Manual (AFM) takes precedence over any conflicting information found in this document. The G Alerting System conveys alerts to the pilot using a combination of the following items. Table below is provided as a reference to aid in identifying which original G STC configuration is installed on the aircraft to be upgraded (SAWI). All previously certified configurations under the original G / DA40 STC are listed below. It is not necessary that the installation be up to date with. The information that is provided in this document is applicable to the installation of the G system in the Diamond DA For additional information on the installation, refer to the documents below. Table Referenced Documentation Part Number Document Required Equipment List, Garmin G, Diamond Model DA

Garmin G EIS Pilot’s Guide for the DA40 Rev. A ENGINE INDICATION SYSTEM Manifold Pressure Gauge (Constant Speed) The Manifold Pressure gauge displays the engine power in inches of mercury (in Hg). • White (bottom of arc) – Below normal operating range. • Green – Normal operating range. For a complete description and breakdown of each Configuration Mode page, refer to the G Configuration Manual, Garmin part number Loader Card Interface. The G/DA 40 SW Loader Card interface exists to provide a means of loading software and configuration files to the system and LRUs. Garmin G Cockpit Reference Guide for the DA40/40F WARNINGS, CAUTIONS, NOTES WARNING: The Garmin G, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical.