Garmin G1000 Pilot's Training Guide (-05) - Page 15
Ground Lesson 3 - flight simulator
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Ground Lesson 3 POWER-UP, SELF-TEST, CHECKLIST Objectives Upon completion of this lesson, the pilot should be able to correctly identify proper alignment of the AHRS/ADC, complete a system self-test, and verify the database data. Resources • GIFD Pilot's Guide • GIFD PC-based Simulator Exercise 3.1: System Initialization 1. How does one verify the aircraft software upon power-up? The aircraft system version information is located on the top right corner of the MFD power-up splash screen and also on the AUX - System Status Page. It is very important to make sure the correct aircraft software is loaded, especially after the aircraft has undergone any maintenance action. 2. Is the aircraft required to remain stationary while the AHRS and ADC align? No, the AHRS/ADC can align while the aircraft is moving and even in flight at bank angles of up to 20°. 3. Is any warm-up time required for the engine instrumentation to be accurate? No, a warm-up period is not required for engine instrument display accuracy. 4. What pilot action should be taken if the MFD system self-test does not pass? The pilot should shut down the aircraft and contact maintenance. 5. Where can one verify the effective dates of the Jeppesen database during the initial system start-up? The Jeppesen database effective dates are located at the right-hand side of the MFD start up splash screen at the conclusion of the scrolled text sequence. 6. If the Jeppesen database is not current in the GIFD, can the system still be used for IFR flight? Yes, but one cannot file a "/G" flight plan for GPS use or use the GPS for instrument approach procedures. 7. How does one verify if the autopilot has passed its preflight system test? Upon completion of the preflight test, the AFCS Status Annunciation 'PFT' will extinguish and aural tone will be generated. 8. How does one verify if TAWS passed its preflight system test? Upon completion of the preflight test, the 'TAWS TEST' annunciation will extinguish and the voice alert, "TWAS system test OK", will be generated. 190-00368-05 Rev. B GIFD Pilot's Training Guide 11