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. G1000 guide for designated pilot examiners and certified flight instructors. Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors 190-00368-02 Rev.

1. Robert A Duff
2. Randall L Brukardt
3. Erhard Ploedereder

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any stor- age medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this. Figure 2 GDU 1040 (PFD Shown).3 Figure 3 Reversionary Mode.6 Figure 4 G1000 System Failure Indications Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors TABLE OF CONTENTS & LIST OF FIGURES TABLE OF CONTENTS.8.10 LIST OF FIGURES.6. NOTE: As part of Garmin’s commitment to flight safety, any specific questions or recommendations about both this document and the G1000 system as it is to be used for the instrument check-ride can be sent via e-mail to “CFITools@garmin.com”. For general questions, please visit “to correspond with Garmin’s aviation technical support specialists. (or three) liquid crystal displays (LCDs) and one (or two) audio panels.

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All of the components of the G1000 system are line-replaceable units (LRUs). This modular approach allows the various components to be mounted either behind each of the displays, or in remote locations in the aircraft, based upon the needs of the aircraft manufacturer. The main components of the G1000 system are the two GDU 1040 displays used for the Primary Flight Display (PFD) and the Multi Function Display (MFD), and the two GIA 63 Integrated Avionics Units (IAUs). These components are interfaced with each other via a proprietary Ethernet-based, high-speed digital databus system. GIA 63 The GIA 63 units serve as the main interface hub for the individual components of the G1000 system. All key components, such as the GRS 77 AHRS, GDC 74A ADC, GTX 33 Mode-S transponder and GEA 71 Engine/Airframe Interface, provide inputs to both GIA 63 units.

GTX 33/GTX 32 The GTX 33 Mode-S and GTX 32 Mode-C transponders provide the ground radar surveillance capability to the G1000 system. Both transponders are solid-state units and require no warm-up time. As installed in most aircraft, these units transition to an ALT reporting mode at a ground speed of 30 kt. Engine Airframe Unit GIA 63 Integrated Avionics Units Engine Control Unit (ECU) GDC 74A Air Data Computer Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors G1000 SYSTEM COMPONENTS Figure 3 Reversionary Mode GIA 63 Integrated Avionics Units DME/ADF Source. In the same section, the applicant is required to demonstrate the ability to utilize an autopilot and/or flight management system (FMS). In the G1000 system, the FMS functions are very similar to those used in the Garmin 400/500 series units.

This should help pilots familiar with these units make the transition to the G1000 system. The tasks listed in this section cover flight by reference to instruments.

Robert A Duff

According to the PTS, the examiner is expected to evaluate the applicant’ s use of the backup instruments with both a full panel and a partial panel. In the case of the G1000-equipped aircraft, failures can be simulated in two ways. ADC should be avoided in Class B and C airspaces, or within the Mode C veil of Class B airspace. 190-00368-02 Rev. A Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors Examiner Action Pull AHRS and ADC circuit breakers.

AREAS OF OPERATION SECTION IV: RECOMMENDATIONS FOR FAILURE SIMULATION Cessna does not recommend pulling circuit breakers as a means of simulating failures on the Garmin G1000. Pulling circuit break- ers—or using them as switches—has the potential to weaken the circuit breaker to a point at which it may not perform its intended function. Direct-to navigation DISPLAY BACKUP button 3, 5, 8, 10 E6B calculations 3, 5 Emergency mode 190-00368-02 Rev. A Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors INDEX Engine/airframe interface 3, 4, 5 Engine instrumentation 1, 5 ENT key. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. P: 44/08 f: 44/08 Garmin Corporation No.

68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2004 Garmin Ltd. Or its subsidiaries 190-00368-02 Rev.

Randall L Brukardt

Screenshot of Default Baron 58 panel. How to use it: The Manual/Checklist is intended to start with a 'dark and cold' panel/engine. If you want to get the maximum from this booklet, you should create an adequate starting situation. If you are used to start flight simulator with running engines and avionics ready for takeoff, place the aircraft at a gate, or a parking position, use the Manual/Checklist items at its end from 'Taxi to ramp' until 'Shutdown' and 'Securing'; then you should have the desired situation.

Erhard Ploedereder

As a guideline, I gave the Manifold pressure values for different sections of the flight. The manifold pressure values my be incorrect, if you takeoff and/or land on airports much above 2500ft MSL.