Garmin G3000 Panel Avionics Unit Instruction Manual

Manual Garmin G3000 Panel Avionics Unit Instruction Manual

Garmin G3000 Panel Avionics Unit Instruction Manual

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Garmin G3000 Panel Avionics Unit

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Garmin G3000 Panel Avionics Unit

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Garmin G3000 Instructions

Here we offer the Garmin G3000 Panel Avionics Unit manual completely free and in English. We have cataloged this manual in the Panel Avionics Units section on Manualverse, and it has been rated by 1 users with an average rating of 5. If you have any specific questions about Garmin G3000 Panel Avionics Unit, we suggest checking the Frequently Asked Questions (FAQs) section of this manual.


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Garmin G3000 Panel Avionics Unit Specifications

Feature Specification
Aircraft Installation Daher TBM 930
Reference Documents Pilot's Guide 190-02046-02 Rev. A (05/29/2020); Cockpit Reference Guide 190-02047-02 Rev. A (06/2020)
System Software 2234.05 or later (GDU 20.92)
Display Units 3 × GDU 1200W (PFD1, MFD, PFD2), 12 in, 1280 × 800 px, LED backlight
Touchscreen Controllers 2 × GTC 580, infrared touchscreen, glove compatible
Integrated Avionics Units 2 × GIA 63W (SBAS GPS, VHF COM/NAV/GS, flight director)
Air Data Computer GDC 74B, ARINC 429 output, RVSM capable
AHRS / Magnetometer 2 × GRS 77 / 2 × GMU 44
Audio Panel GMA 36 remote audio unit
Engine/Airframe Units 2 × GEA 71 (RS-485)
Transponders GTX 33 ES, GTX 345R or GTX 33D ES; Mode S Level 2, EHS, ADS-B Out
AFCS Hardware GMC 710 controller, 4 × GSA 81 servos, GTA 82 yaw trim adapter
COM Frequency Range 118.000–136.975 MHz (760 ch, 25 kHz); 118.000–136.990 MHz (3040 ch, 8.33 kHz)
ADF Frequency Range 190.0–1799.5 kHz (2182.0 kHz excluded)
SBAS Support WAAS, EGNOS, MSAS
RAIM Protection Limits 2.0 nm oceanic/en route, 1.0 nm terminal, 0.3 nm non-precision approach
Weather Radar GWX 70, 40 W solid-state, 10 in antenna, ±30° pitch/roll stabilization
Radar Sector Scan 20°, 40°, 60° or FULL 90°
Radar Tilt / Gain Steps 0.25° / 0.5 (0.0 = calibrated gain)
Radar MPEL Distance 12 ft (1 mW/cm² at 9.3–9.5 GHz)
Traffic Advisory System GTS 820; tracks 45 Mode A/C and 30 Mode S intruders, ±10,000 ft, up to 40 nm
SVT Field of View 48° vertical; 71° horizontal (Full), 50° (Split)
Terrain Database Resolution 4.9 arc-seconds
Map Range 28 scales, 250 ft to 1000 nm
Stored Flight Plans 99 plans, 100 waypoints each
User Waypoints Up to 1000 (6-character name, 25-character comment)
Crew Profiles Up to 25 (16-character names)
Vertical Speed Mode Range −4000 to +3000 fpm, 100 fpm steps
FLC Mode Range 80–265 kt IAS; Mach 0.20–0.69
Bank Limits 25° normal; 15° Low Bank (automatic above 25,000 ft)
Flight Director Limits Pitch −15° to +25°; roll 25°
Database SD Cards 32 GB Garmin-supplied cards
Flight Data Logging SD up to 16 GB in upper MFD slot, 1 record per second
Navigation Database Cycle 28 days (Obstacle, SafeTaxi, Airport Directory 56 days; ChartView 14 days)
Clearance Recorder 2.5 minutes, erased at power-down
SafeTaxi Coverage More than 1,400 airports
SiriusXM Audio More than 170 channels

Garmin G3000 Panel Avionics Unit Details

The Garmin G3000 in the Daher TBM 930 is built around redundancy. If PFD1 fails, the MFD switches to a full reversionary display and PFD2 goes to Split mode. If the MFD fails, PFD1 becomes reversionary. You can also force reversionary mode with the red DISPLAY BACKUP switch. If one touchscreen controller fails, the other one still controls its own PFD and the MFD. Sensor comparators flag disagreements between the two sensors, for example altitude differences greater than 200 ft or heading differences greater than 6°.

A guided initialization sequence takes the crew through four tasks: crew profile, flight plan, system tests, and weight and fuel. After those, the crew selects Accept Initialization. The weight and fuel page calculates zero-fuel weight, takeoff weight and estimated landing weight. Excess values are shown in amber. Trip Planning works in automatic or manual mode. It reports ETE, ETA, ESA, fuel efficiency, endurance, total range, density altitude and sunrise or sunset times for stored or active flight plans.

The Electronic Stability and Protection (ESP) system only works above 200 ft AGL with the autopilot disengaged. It starts to push back at 45° of bank, at +20°/−22° of pitch, or above 268 kt IAS. If ESP stays active for more than 10 seconds within a 20-second window, the system engages the autopilot in LVL mode. In Emergency Descent Mode, the autopilot descends at 255 KIAS, turns 90° to the left, and levels off at 15,000 ft whenever cabin altitude gets too high.

For situational awareness, the system combines several weather sources: SiriusXM, FIS-B, Iridium-based Connext, the WX-500 Stormscope and the onboard radar. Each data product shows its age, which turns amber as it approaches expiration. Terrain protection comes as Terrain-SVT or TAWS-B, with callouts such as "Pull Up", "Sink Rate", "Don't Sink" and "Five-Hundred". SurfaceWatch warns about taxiway takeoffs and landings, runways that are too short, and remaining runway distance from 5,000 ft down to 100 ft.

VNAV builds vertical paths from barometric altitude, using constraints that are designated, advisory or entered by the pilot. Temperature compensation raises approach altitudes in cold weather; adjusted altitudes carry a snowflake icon. Electronic charts from Jeppesen ChartView or FliteCharts meet the Type B EFB requirements of AC 120-76D. The system also handles electronic checklists in .gcl format, PDF documents of up to 9,999 pages, Iridium voice calls, and SMS messages of up to 160 characters.

You can update the databases with SD cards or wirelessly. For wireless updates, the Flight Stream 510 connects to Garmin Pilot over Bluetooth and moves the files over WiFi using Database Concierge. Never cut power while a database is loading. Garmin recommends at least one power cycle for every 4 days of continuous operation, to avoid an autonomous restart. If GPS is lost, dead reckoning keeps guidance available for up to 20 minutes in en route and oceanic phases.

Frequently Asked Questions (FAQs)

Can't find the answer you need? Here are some frequently asked questions about the Garmin G3000 Panel Avionics Unit, and we answer them below.


How long does the AHRS take to align after power-up?
The AHRS displays "AHRS ALIGN: Keep Wings Level" and normally becomes valid in about 1 minute. All display windows should be working within 1 minute of power-up.

Where are attitude and heading unreliable?
Do not rely on them north of 72°N or south of 70°S. Some additional high-latitude areas are also excluded, such as north of 65°N between 75°W and 120°W.

How often should the system be power cycled?
Cycle power at least once for every 4 days of continuous operation. This prevents an autonomous system restart.

What SD cards can be used for database updates?
Use only 32 GB SD cards supplied by Garmin, the OEM or an authorized dealer. Insert the cards in the lower slot of each GDU.

What happens if a microphone gets stuck?
After 35 seconds the transmitter is cut off, and a CAS message appears: "L MIC STUCK ON" or "R MIC STUCK ON".

What triggers the Emergency Descent Mode?
EDM activates when the autopilot is engaged, pressure altitude is above 15,000 ft, and cabin altitude is too high. The autopilot then descends at 255 KIAS toward 15,000 ft, turning 90° to the left.

What is the minimum safe distance from the radar when it is transmitting?
For the 10-inch GWX 70 antenna, the MPEL boundary is 12 ft. Do not transmit while anyone is inside that distance.

How long can the system navigate in Dead Reckoning mode?
DR mode works only in the en route and oceanic phases. The amber CDI is removed after 20 minutes, and the autopilot stays coupled as long as lateral guidance is available.

What are the autopilot underspeed (MINSPD) values?
MINSPD is 88 kt with flaps up, 84 kt with flaps at takeoff, and 74 kt with flaps fully extended.

When is SiriusXM music muted automatically?
Music is muted on the ground above 40 KIAS, below 10,000 ft MSL or 2,000 ft AGL, below 150 KIAS, during unusual attitudes, and in reversionary mode.

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