Garmin GFC 600 Digital 2-Axis Autopilot, for A36 Bonanza & B55 Baron
$286.00
Aircraft Models Currently FAA Approved for GFC 600 Installation:
- Beechcraft Baron
- Models: B55, B55A, C55, C55A, D55, D55A, E55, E55A, 58, 58A, 58P, 58PA, 58TC*, 58TCA*
- Smart Rudder Bias Approved: 58, 58A, B55, B55A
- Beechcraft Bonanza
- Models: 36, A36, A36TC
- Cessna 182
- Models: P, Q, R, S, T, T182, T182T
- Cessna Grand Caravan
- Model: 208, 208B
- Cessna P210
- Models: P210N
- Cessna 310R
- Models: 310R*, T310R*
- Smart Rudder Bias Approved: 310R, T310R
- Cessna 340
- Models: 340, 340A
- Smart Rudder Bias Approved: 340, 340A
- Cessna 414
- Model: 414A
- Smart Rudder Bias Approved: 414A
- Cessna 421
- Model: 421C
- Cessna 425
- Model: 425
- Cessna 441
- Model: 441
- Cessna CitationJet
- Model: 525
- Beechcraft King Air
- Models: C90, C90-1, C90A, C90B, C90SE, C90GT, C90GTi, E90
- Beech King Air 200
- Models: 200, B200
- Beech King Air F90
- Models: F90, F90-1
- Pilatus PC-12
- Models: PC-12/41, PC-12/45, PC-12/47*
- Piper PA-31
- Models: 300*, 310*, 325, 325CR, 350
- Smart Rudder Bias Approved: 300, 310, 325, 325CR, 350
- Piper PA-46
- Models: 310P, 350P, 310P JetPROP, 350P JetPROP, 500TP Meridian
- Socata TBM
- Models: 700, A, B, C1, C2, N (TBM 850)
GFC 600 Certification Programs Currently In-progress: (Subject to change.)
- Cessna 421
- Models: 421B
GFC 600 Certification Programs Planned to Begin in the Next 12-months:
(Not currently under development and subject to change.)
- Cessna 310
- Models: 310P, T310P, 310Q, T310Q
- Piper PA-31T
- Models: Cheyenne II
Please note that G1000®, G1000 NXi and Collins Pro Line equipped aircraft are excluded from the list above.
*Certain serial numbers excluded, see authorized Garmin installation center for details.
Last Updated: 5/17/2023
Garmin GFC 600 Digital 2-Axis Autopilot, for Beechcraft & Cessna Models
Now You Can Fly a New Autopilot with Optional Pitch Trim & Yaw Dampener
- Cost-effective, superior in-flight characteristics, built-in self-monitoring capabilities and minimal maintenance needs when compared to older generation autopilot systems
- Designed for existing single- and twin-engine piston and turbine aircraft that have a wide range of aircraft speed and performance characteristics, initially available for the A36 Bonanza and B55 Baron aircraft with the 58 Baron to follow
- Standalone autopilot that boasts superior integration potential with G600/G500 glass flight displays, Garmin navigators, as well as a variety of third-party equipment
- Robust feature set, including safety features such as underspeed and overspeed protection, a dedicated return-to-level (LVL) mode button, Garmin ESP™ (Electronic Stability and Protection), Flight Director (FD), coupled approaches and missed approaches when paired with a compatible navigator and much more
- Offers 2-axis (pitch and roll) capabilities as well as pitch trim (provides automatic trim and manual electric trim); addition of optional fourth servo adds yaw damp capability
Designed for aftermarket installation on high-performance single- and twin-engine piston aircraft as well as turboprops and jets, the GFC 600 flight control system offers an impressive array of top-level safety and performance features. Leveraging technologies developed for our popular GFC 700 autopilot that drives our most advanced glass flight deck systems, these sophisticated features include Garmin ESP, underspeed and overspeed protection, automatic LVL mode, airspeed climb and decent (IAS) mode, flight director (FD) command cues and more.
Maximize Performance and Capability
Drawing on our top-end Garmin GFC 700 flight control technology, GFC 600 provides crisp, precise response and optimum performance over the entire airspeed envelope of your aircraft. Rather than depending on failure-prone mechanical gyros, the GFC 600 system is digitally controlled, using solid-state attitude and air data sensor reference — giving you ultra-smooth roundouts, intercepts and more while also enhancing system reliability. Offering a flexible upgrade solution, GFC 600 can be interfaced with a variety of Garmin and third-party instrumentation and navigation sources. The design of the GFC 600 includes environmentally hardened servos, allowing for installation in a wide range of airframes, including harsh operating conditions. The robust hardware used in the GFC 600 autopilot’s scalable architecture lets you tailor your system’s configuration to support the level of capability you want. Every component has been engineered to work seamlessly together to ensure optimum smoothness and comfort in flight — while helping to reduce pilot workload in the cockpit.
Guidance from a compatible navigation source (such as GTN™ 750 or GTN 650) lets the GFC 600 system automatically fly a wide range of precision, nonprecision and GPS-guided approaches as well as holds, procedure turns, missed approaches and more. GFC 600 also includes built-in GPS roll steering capability, allowing smoother navigation tracking and eliminating the need for external roll steering converters. For installations including a compatible flight display (such as G600 or G500), flight director cues are displayed as command bars and are always in view when the autopilot is doing the flying — and may also be used for visual guidance when you’re hand-flying the aircraft. Better still, with support for a remotely installed Takeoff/Go-around (TOGA) button, the autopilot can be cued to automatically capture the correct pitch attitude required to fly a missed approach and then follow the missed approach procedure loaded in your compatible GPS navigator.
Control from Your Avionics Stack
For selection and control of GFC 600 modes and functions, a compact autopilot controller comes standard with the system. Featuring backlit keys and a bright, sunlight-readable annunciator display, the mark-width controller mounts conveniently in your avionics stack. An intuitive up/down control wheel on the unit allows for easy and precise adjustment of aircraft pitch, airspeed and vertical speed modes. And for installations where the autopilot controller is out of the pilot’s primary field of view and a G600/G500 flight display is not installed for mode annunciation, a standalone mode annunciator is available that retains an identical footprint of third-party autopilot annunciators on the market. Support for a remotely-installed control wheel steering (CWS) button allows you to temporarily disengage the servos to hand-fly the aircraft. Then, to further enhance safety in potentially disorienting situations, a dedicated LVL mode button on the autopilot controller lets you command the autopilot to automatically return your aircraft to straight-and-level flight.
Silky-smooth Servo Control
Integrated “smart” servos linked to the flight control surfaces of your aircraft are used to apply the control inputs as commanded by the autopilot. Digitally controlled speed and torque limits on these inputs allow faster, crisper and more powerful response — enabling your GFC 600 system to track the intended flight path with smooth efficiency. For maximum reliability and safety, the GFC 600 servos incorporate brushless DC motors and a gear train that eliminate the need for a mechanical slip clutch. This design results in enhanced system efficiency — while also reducing maintenance/inspection requirements. The servos also provide virtually no control system friction with the autopilot turned off, decoupling the motor drives so you can hand-fly with ease.
Hand-fly with Stability Protection
As a standard feature, Garmin ESP works with GFC 600 to assist you in maintaining your aircraft in a safe, flight-stable condition when the aircraft is being hand-flown. This ESP feature functions independently of the autopilot — though it uses the same control servos — to gently nudge the controls toward stable flight whenever pitch or roll deviations exceed the recommended limits or underspeed/overspeed conditions occur. In the event of pilot incapacitation, after the system detects that it has been activated for a specified period of time, the autopilot will engage with the flight director in level mode, bringing the aircraft back to level flight and helping to avoid the onset of inadvertent stall/spins, steep spirals or other loss-of-control scenarios. Additionally, ESP can be manually disabled to allow for intentional flight maneuvers.
An Autopilot That Knows Its Limits
With the autopilot engaged, GFC 600 also provides overspeed and underspeed protection. In a high airspeed situation — for example, if you’re descending and your aircraft is approaching VNE or VMO — the system will increase the aircraft’s pitch attitude, preventing a further increase in airspeed and potential structural damage. Likewise, at the other end of the speed spectrum, GFC 600 provides underspeed (stall) protection. For example, in the event the pilot does not immediately advance the throttle to full power, with the autopilot engaged while flying a missed approach sequence, the autopilot will help prevent an aircraft stall by reducing pitch attitude and provide the pilot with an “airspeed, airspeed” audible alert.
It’s Confidence-inspiring Technology
With its extensive features and advanced technology, the GFC 600 system offers unprecedented value in a retrofittable autopilot solution. Backed by a comprehensive warranty and the industry’s No. 1-rated product support team, it’s truly a system you can own and fly with confidence. With supplemental type certification (STC) completed on select Beechcraft Bonanza and Baron model aircraft, with more to follow, it’s easy to select an approved installation that meets your mission requirements and budget. See your authorized Garmin installation center for more details on configuring a GFC 600 retrofit package for your aircraft.
Aircraft Models Currently FAA Approved for GFC 600 Installation:
- Beechcraft Baron
- Models: B55, B55A, C55, C55A, D55, D55A, E55, E55A, 58, 58A, 58P, 58PA, 58TC*, 58TCA*
- Smart Rudder Bias Approved: 58, 58A, B55, B55A
- Beechcraft Bonanza
- Models: 36, A36, A36TC
- Cessna 182
- Models: P, Q, R, S, T, T182, T182T
- Cessna Grand Caravan
- Model: 208, 208B
- Cessna P210
- Models: P210N
- Cessna 310R
- Models: 310R*, T310R*
- Smart Rudder Bias Approved: 310R, T310R
- Cessna 340
- Models: 340, 340A
- Smart Rudder Bias Approved: 340, 340A
- Cessna 414
- Model: 414A
- Smart Rudder Bias Approved: 414A
- Cessna 421
- Model: 421C
- Cessna 425
- Model: 425
- Cessna 441
- Model: 441
- Cessna CitationJet
- Model: 525
- Beechcraft King Air
- Models: C90, C90-1, C90A, C90B, C90SE, C90GT, C90GTi, E90
- Beech King Air 200
- Models: 200, B200
- Beech King Air F90
- Models: F90, F90-1
- Pilatus PC-12
- Models: PC-12/41, PC-12/45, PC-12/47*
- Piper PA-31
- Models: 300*, 310*, 325, 325CR, 350
- Smart Rudder Bias Approved: 300, 310, 325, 325CR, 350
- Piper PA-46
- Models: 310P, 350P, 310P JetPROP, 350P JetPROP, 500TP Meridian
- Socata TBM
- Models: 700, A, B, C1, C2, N (TBM 850)
GFC 600 Certification Programs Currently In-progress: (Subject to change.)
- Cessna 421
- Models: 421B
GFC 600 Certification Programs Planned to Begin in the Next 12-months:
(Not currently under development and subject to change.)
- Cessna 310
- Models: 310P, T310P, 310Q, T310Q
- Piper PA-31T
- Models: Cheyenne II
Please note that G1000®, G1000 NXi and Collins Pro Line equipped aircraft are excluded from the list above.
*Certain serial numbers excluded, see authorized Garmin installation center for details.
Last Updated: 5/17/2023
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Notes/Info |
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| Honeywell (Bendix King) | KR 85 | KR 85 interface via GAD 43e. | |
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Garmin | GMA 340 GMA 342 GMA 345 GMA 347 GMA 35(c) GMA 350(c) SL15 SL15M | GMA 35(c) requires installation of GTN 7XX for control functions. |
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Autopilot - External Flight Director |
Bendix | M-4D | |
| Century | IV 41 2000 | ||
| Cessna | 300B IFCS/400B IFCS/800B IFCS 1000A IFCS | ||
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Engine Instrument Display System |
Meggitt (Cobham/S-TEC) | MAGIC Engine Instrumentation Display System (EIDS) | |
GPS Source |
Garmin | 400W/500W Series GNS 480 GTN 6XX/7XX | |
Marker Beacon via GAD 43e. |
Garmin | GMA 35/340/342/345/347/350(c) | |
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| Honeywell (Bendix King) | KMA 24/26/28/30 | ||
| PS Engineering | PMA 6000/7000/8000 | ||
Navigation Receiver |
Garmin | GNC 255( ) GNS 430W/530W GNS 480 (CNX80) GTN 650/750 SL30 | |
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Radar Altimeters |
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Weather Radar Display and Control |
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Manufacturer |
Model |
Notes/Info |
ADF Receiver |
Collins | ADF-60A/B | |
| Honeywell | KR 87 KDF 806 | ||
| Honeywell (Bendix King) | KR 85 | KR 85 interface via GAD 43e. | |
Audio Panels |
Garmin | GMA 340 GMA 342 GMA 345 GMA 347 GMA 35(c) GMA 350(c) SL15 SL15M | GMA 35(c) requires installation of GTN 7XX for control functions. |
| Honeywell (Bendix King) | KMA 24 KMA 26 KMA 28 KMA 30 | ||
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Autopilot - Alititude Preselect/Vertical Speed Select via GAD 43e |
Cessna | 300B IFCS, 400B IFCS, 800B IFCS, 1000A IFCS | |
| Collins | APS-65 ( ) | ||
| Honeywell (Bendix King) | KAP 150 KFC 150 KFC 200/250 KFC 275/325 | ||
| S-TEC | 55, 55X, 60-2, 65, 60PSS | ||
Autopilot - Attitude Source via GAD 43e |
Century | 21/31/41/2000 | |
| Cessna | 300B IFCS/400B IFCS/800B IFCS (Type IF-550A) 400B (Type AF-550A) 1000A Series (Types AF/IF-1050A) | ||
| Collins | APS 65 (APC-65/65E/65H/65J) | ||
| Honeywell (Bendix King) | KAP 100 KAP 150/KFC 150 KAP 200/KFC 200 KFC 250 KFC 225/275/325 KFC 300 | ||
Autopilot - External Flight Director |
Bendix | M-4D | |
| Century | IV 41 2000 | ||
| Cessna | 300B IFCS/400B IFCS/800B IFCS 1000A IFCS | ||
| Collins | APS-65 AP-106/107 | ||
| Honeywell (Bendix King) | KFC 150/200/250 KFC 225/275/325 KFC 300 | ||
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| Sperry | SPZ-200A/500 | ||
Datalink Weather Display and Control |
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DME via GAD 43e |
Collins | DME-42 DME-442/4000 | Parallel tuning now available for DME-42. |
| Honeywell (Bendix King) | KDM 706(A) KN 62/64 KN 63 | Parallel tuning for 706(A) and 63 available. | |
Engine Instrument Display System |
Meggitt (Cobham/S-TEC) | MAGIC Engine Instrumentation Display System (EIDS) | |
GPS Source |
Garmin | 400W/500W Series GNS 480 GTN 6XX/7XX | |
Marker Beacon via GAD 43e. |
Garmin | GMA 35/340/342/345/347/350(c) | |
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| Honeywell (Bendix King) | KMA 24/26/28/30 | ||
| PS Engineering | PMA 6000/7000/8000 | ||
Navigation Receiver |
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ADS-B Traffic Display |
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Interface |
Manufacturer |
Model |
Notes/Info |
ADF Receiver |
Collins | ADF-60A/B | |
| Honeywell | KR 87 KDF 806 | ||
| Honeywell (Bendix King) | KR 85 | KR 85 interface via GAD 43e. | |
Audio Panels |
Garmin | GMA 340 GMA 342 GMA 345 GMA 347 GMA 35(c) GMA 350(c) SL15 SL15M | GMA 35(c) requires installation of GTN 7XX for control functions. |
| Honeywell (Bendix King) | KMA 24 KMA 26 KMA 28 KMA 30 | ||
| PS Engineering | PMA 6000 PMA 7000 Series PMA 8000 Series PAR 200 | ||
Autopilot - Alititude Preselect/Vertical Speed Select via GAD 43e |
Cessna | 300B IFCS, 400B IFCS, 800B IFCS, 1000A IFCS | |
| Collins | APS-65 ( ) | ||
| Honeywell (Bendix King) | KAP 150 KFC 150 KFC 200/250 KFC 275/325 | ||
| S-TEC | 55, 55X, 60-2, 65, 60PSS | ||
Autopilot - Attitude Source via GAD 43e |
Century | 21/31/41/2000 | |
| Cessna | 300B IFCS/400B IFCS/800B IFCS (Type IF-550A) 400B (Type AF-550A) 1000A Series (Types AF/IF-1050A) | ||
| Collins | APS 65 (APC-65/65E/65H/65J) | ||
| Honeywell (Bendix King) | KAP 100 KAP 150/KFC 150 KAP 200/KFC 200 KFC 250 KFC 225/275/325 KFC 300 | ||
Autopilot - External Flight Director |
Bendix | M-4D | |
| Century | IV 41 2000 | ||
| Cessna | 300B IFCS/400B IFCS/800B IFCS 1000A IFCS | ||
| Collins | APS-65 AP-106/107 | ||
| Honeywell (Bendix King) | KFC 150/200/250 KFC 225/275/325 KFC 300 | ||
| S-TEC | 55, 55X 60-2/65 1500/2100 | ||
| Sperry | SPZ-200A/500 | ||
Datalink Weather Display and Control |
Garmin | GDL 69/69A GDL 88 GSR 56 GTX 345 | GDL 69A also provides SiriusXM radio entertainment. GSR 56 also provides text/voice communication. GDL 88 and GTX 345 provide ADS-B data. |
DME via GAD 43e |
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| Honeywell (Bendix King) | KDM 706(A) KN 62/64 KN 63 | Parallel tuning for 706(A) and 63 available. | |
Engine Instrument Display System |
Meggitt (Cobham/S-TEC) | MAGIC Engine Instrumentation Display System (EIDS) | |
GPS Source |
Garmin | 400W/500W Series GNS 480 GTN 6XX/7XX | |
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Garmin | GMA 35/340/342/345/347/350(c) | |
| Collins | VIR-32/33 | ||
| Honeywell (Bendix King) | KMA 24/26/28/30 | ||
| PS Engineering | PMA 6000/7000/8000 | ||
Navigation Receiver |
Garmin | GNC 255( ) GNS 430W/530W GNS 480 (CNX80) GTN 650/750 SL30 | |
| Collins | VIR-32/33 | VIR-32/33 interface via GAD 43e. | |
| Honeywell (Bendix King) | KX 155/155A/165/165A KX 170B/175B KN 53 | KX 155/155A/165/165A interface via GAD 43e. KN 53 interface via GAD 43e. | |
Radar Altimeters |
Collins | RAC-870 ALT-50A ALT-55B | ALT-50A interface via GAD 43e. ALT-55B interface via GAD 43e. |
| FreeFlight | RA-4500 | ||
| Honeywell (Bendix King) | KRA 405B KRA 10/10A KRA 405 | KRA 10/10A interface via GAD 43e. KRA 405 interface via GAD 43e. | |
| Sperry | AA-100 AA-100A AA-200 | AA-100 interface via GAD 43e. AA-100A interface via GAD 43e. AA-200 interface via GAD 43e. | |
TAS/TCAS/TIS Traffic Display and Control |
Garmin | GTX 33( )/330( )/335 GTS 800/820/850 | GTX 335 is TIS-A traffic only. |
| Honeywell | KTA 810/KMH 820 KTA 910/KMH 920 | ||
| L3 Communications (Goodrich) | SKY497/SKY899 | ||
| Avidyne (Ryan) | TAS 600/610/620 (9900BX) | ||
ADS-B Traffic Display |
Garmin | GDL 88 GTX 345 | |
Weather Radar Display and Control |
Garmin | GWX 68 GWX 70(R) | |
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G600 TXi 7″ Portrait Primary Flight Display
Interface |
Manufacturer |
Model |
Notes/Info |
ADF Receiver |
Collins | ADF-60A/B | |
| Honeywell | KR 87 KDF 806 | ||
| Honeywell (Bendix King) | KR 85 | KR 85 interface via GAD 43e. | |
Audio Panels |
Garmin | GMA 340 GMA 342 GMA 345 GMA 347 GMA 35(c) GMA 350(c) SL15 SL15M | GMA 35(c) requires installation of GTN 7XX for control functions. |
| Honeywell (Bendix King) | KMA 24 KMA 26 KMA 28 KMA 30 | ||
| PS Engineering | PMA 6000 PMA 7000 Series PMA 8000 Series PAR 200 | ||
Autopilot - HSI Output |
Bendix | M4C, M4D | |
| Century | II/III IV 21/31/41 2000 | ||
| Cessna | 400B 300 IFCS/400 IFCS/800 IFCS 300B IFCS/400B IFCS/800B IFCS 1000A IFCS | ||
| Collins | APS-65 ( ) AP-106/107 | ||
| Honeywell (Bendix King) | KAP 100/150/200 KFC 150/200/250 KAP 140 KFC 225/275/325 KFC 300 | ||
| Sperry | SPZ-200A/500 | ||
| S-TEC | 20/30/40/50/55/60-1/60-2/65 60 PSS 55X 1500/2100 | ||
Autopilot - Alititude Preselect/Vertical Speed Select via GAD 43e |
Collins | APS-65 ( ) | |
| Honeywell (Bendix King) | KAP 150 KFC 150 KFC 200/250 KFC 275/325 | ||
| S-TEC | 55, 55X, 60-2, 65, 60PSS | ||
Autopilot - Attitude Source via GAD 43e |
Century | 21/31/41/2000 | |
| Cessna | 300B IFCS/400B IFCS/800B IFCS (Type IF-550A) 400B (Type AF-550A) 1000A Series (Types AF/IF-1050A) | ||
| Collins | APS 65 (APC-65/65E/65H/65J) | ||
| Honeywell (Bendix King) | KAP 100 KAP 150/KFC 150 KAP 200/KFC 200 KFC 250 KFC 225/275/325 KFC 300 | ||
Autopilot - External Flight Director |
Bendix | M-4D | |
| Century | IV 41 2000 | ||
| Cessna | 300B IFCS/400B IFCS/800B IFCS 1000A IFCS | ||
| Collins | APS-65 AP-106/107 | ||
| Honeywell (Bendix King) | KFC 150/200/250 KFC 225/275/325 KFC 300 | ||
| S-TEC | 55, 55X 60-2/65 1500/2100 | ||
| Sperry | SPZ-200A/500 | ||
Datalink Weather Display and Control |
Garmin | GDL 69/69A GDL 88 GSR 56 GTX 345 | GDL 69A also provides SiriusXM radio entertainment. GSR 56 also provides text/voice communication. GDL 88 and GTX 345 provide ADS-B data. |
DME via GAD 43e |
Collins | DME-42 DME-442/4000 | Parallel tuning now available for DME-42. |
| Honeywell (Bendix King) | KDM 706(A) KN 62/64 KN 63 | Parallel tuning for 706(A) and 63 available. | |
Engine Instrument Display System |
Meggitt (Cobham/S-TEC) | MAGIC Engine Instrumentation Display System (EIDS) | |
GPS Source |
Garmin | 400W/500W Series GNS 480 GTN 6XX/7XX | |
Marker Beacon via GAD 43e. |
Garmin | GMA 35/340/342/345/347/350(c) | |
| Collins | VIR-32/33 | ||
| Honeywell (Bendix King) | KMA 24/26/28/30 | ||
| PS Engineering | PMA 6000/7000/8000 | ||
Navigation Receiver |
Garmin | GNC 255( ) GNS 430W/530W GNS 480 (CNX80) GTN 650/750 SL30 | |
| Collins | VIR-32/33 | VIR-32/33 interface via GAD 43e. | |
| Honeywell (Bendix King) | KX 155/155A/165/165A KX 170B/175B KN 53 | KX 155/155A/165/165A interface via GAD 43e. KN 53 interface via GAD 43e. | |
Radar Altimeters |
Collins | RAC-870 ALT-50A ALT-55B | ALT-50A interface via GAD 43e. ALT-55B interface via GAD 43e. |
| FreeFlight | RA-4500 | ||
| Honeywell (Bendix King) | KRA 405B KRA 10/10A KRA 405 | KRA 10/10A interface via GAD 43e. KRA 405 interface via GAD 43e. | |
| Sperry | AA-100 AA-100A AA-200 | AA-100 interface via GAD 43e. AA-100A interface via GAD 43e. AA-200 interface via GAD 43e. | |
Stall Protection and Warning Unit |
EMCA | SPWG92 | |
TAS/TCAS/TIS Traffic Display and Control |
Garmin | GTX 33( )/330( )/335 GTS 800/820/850 | GTX 335 is TIS-A traffic only. |
| Honeywell | KTA 810/KMH 820 KTA 910/KMH 920 | ||
| L3 Communications (Goodrich) | SKY497/SKY899 | ||
| Avidyne (Ryan) | TAS 600/610/620 (9900BX) | ||
ADS-B Traffic Display |
Garmin | GDL 88 GTX 345 | |
Weather Radar Display and Control |
Garmin | GWX 68 GWX 70(R) | |
| Honeywell (Bendix King) | RDS 81 (RS 811A) RDS 82 (RS 181A) RDR 2000 (ART 2000) RDR 2100 (ART 2100) |
Garmin GFC 500 Digital 2-Axis Autopilot
Aircraft Models Currently FAA Approved for GFC 500 Installation:
- American Champion
- Models: 8GCBC Scout (metal wing spar equipped aircraft only)
- Aviat Husky
- Models: A-1, A-1A, A-1B, A-1C-180, A-1C-200
- Beechcraft Bonanza
- Models: A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC*, B36TC
- Beechcraft Bonanza/Debonair
- Models: 33, A33, B33, C33, C33A, E33, E33A, E33C, F33*, F33A, F33C*, G33*
- Beechcraft Musketeer*, Sport*, Sundowner, Sierra
- Models: 19, 23, 24
- Beechcraft
- Models: T-34 Mentor
- Cessna 172
- Models: A*, B*, C, D, E, F, G, H, I, K, L, M, N, P, Q, R, S, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, FR172K, P172D, R172K
- Cessna 172RG
- Models: 172RG
- Cessna 175
- Models: A*, B, C
- Cessna 177
- Models: 177, 177A 177B, 177RG, F177RG
- Cessna 180
- Models: 180, A, B, C, D, E, F, G, H, J, K
- Cessna 182
- Models: 182, A, B, C, D, E, F, G, H, J, K, L, M, N, P, Q, R, S, T, T182, T182T, F182P, F182Q
- Cessna 182RG
- Models: R182, FR182, TR182
- Cessna 185
- Models: 185, A, B, C, D, E, A185E, A185F
- Cessna 206
- Models: P206C, TP206C, U206C, TU206C, P206D, TP206D, U206D, TU206D, P206E, TP206E, U206E, TU206E, U206F, TU206F, U206G, TU206G, 206H, T206H
- Roberston STOL compatibility: U206F, TU206F U206F, TU206F, U206G, TU206G, 206H, T206H
- Cessna 210
- Models: 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N
- Cirrus SR22
- Models: SR20* SR22*
- Commander 112/114
- Models: Commander 112, 112A, 112B, 112TC, 112TCA, 114, 114A, 114B, 114TC
- Embraer Nieva (Brazil ANAC Approved Only)
- Models: EMB-710C, EMB-710D, EMB-711A, EMB-711B, EMB-711T, EMB-711ST, EMB-712, EMB-720C, EMB-720D, EMB-721C, EMB-721D
- Grumman (American General) AA-5 Series
- Models: AA-5 Traveler, AA-5A Cheetah, AA-5B Tiger, AG-5B Tiger
- Mooney M20
- Models: C, D, E, F, G, J, K, M, R, S (including 1962-1964 C, D and E Models)
- Piper PA-24
- Models: 180, 250, 260, 260B, 260C*
- Piper PA-28
- Models: 140, 150, 151, 160, 161, 180, 181, 201T, 235, 236 (and Overhead Trim Models)
- Piper PA-28R
- Models: 180, 200, 201, 201T
- Piper PA-28RT
- Models: 201, 201T
- Piper Twin Comanche
- Models: PA-301, PA-30B1, PA-30C1, PA-391 (including turbocharged models)
- Piper PA-32
- Models: 260, 300, 301, 301T, 301FT, 301XTC
- Piper PA-32R
- Models: 300, 301SP, 301HP, 301T
- Piper PA-32RT
- Models: 300, 300T
- Piper Seneca
- Models: PA-34-200T, PA-34-220T
- Socata Trinidad
- Models: TB-20*, TB-21*
GFC 500 Certification Programs Currently In-progress: (Subject to change.)
- Cessna 210
- Models: 210-5, 210-5A
- Beechcraft
- Models: A35, B35
GFC 500 Certification Programs Planned to Begin in the Next 12-months:
(Not currently under development and subject to change.)
- Cessna 170
- Models: 170B
- Cessna 172
- Models: 172
- Cessna 175
- Models: 175
- Cessna 180 and 185
- Robertson STOL compatibility: Cessna 180 and 185 models
- Cessna
- Models: 190, 195
Please note that G1000® equipped aircraft are excluded from the list above.
*Certain serial numbers excluded, see authorized Garmin installation center for details.
1Light twin aircraft will require a GI 275 Electronic Flight Instrument
Last Updated: 9/13/2023
Garmin GNX 375 WAAS GPS Navigator with ADS-B “Out”/”In” Transponder & GA-35 GPS Antenna
- TSO applicability: C88b; C112e Category 1, Level 2 els; C146e Class 3; C154c Category A1S; C157b Category 1; C165a; C166b Category A1S; C195b Category B1, B3, B5, B7, C1, C2, C3, C5, C7
- Display size: 4.8" (122.5 mm) diagonal
- Display resolution: 732 pixels (W) x 240 pixels (H)
- Unit bezel height: 2.02" (51.0 mm)
- Unit bezel width: 6.25" (159.0 mm)
- Unit depth with connectors: 10.85" (276.0 mm) (measured from face of aircraft panel to rear of connector backshells)
- Unit weight: 3.2 lbs (1.44 kg)
- Maximum altitude: 30,000 ft with optional GAE module. 35,000 ft without optional GAE module.
- Input voltage range: 9 VDC - 33 VDC
- Maximum display brightness: 260 fL
- Operating temperature range: -20° C to 55° C (-4° F to 131° F)
- Bluetooth version: 4.2
- Number of GPS channels: 15 (12 GPS and 3 GPS/WAAS/SBAS)
- LAT/LON position accuracy: <1.25 meter RMS horizontal, < 2 meter vertical, with WAAS
- Maximum velocity: 1,000 knots (above 60,000 feet)
- Position update interval: 0.2 sec (5 Hz)
- ADS-B “Out”: yes, 1090 ES
- ADS-B “In”: yes, Dual-link
| Interface | Manufacturer | Model |
| ADS-B In Displays | Aspen | EFD 1000/500 |
| Garmin | G500/G600 | |
| TXi Series | ||
| G3X Touch | ||
| GTN 6XX/7XX | ||
| GMX 200 | ||
| MX20 | ||
| Altitude Sources | ACK Tech | A-30 |
| B&D | 90004-003 | |
| Bendix/King (Honeywell) | KDC 281 | |
| KDC 481 | ||
| Garmin | G500/G600 | |
| GAE 12 | ||
| TXi Series | ||
| G3X Touch | ||
| Icarus Instruments | 3000 | |
| Sandia | SAE 5-35 | |
| Shadin | 8800T | |
| F/ADC-200 | ||
| F/ADC-2000 | ||
| Trans-Cal Industries | IA-RS232-X | |
| SSD120 | ||
| Autopilots | Honeywell (Bendix/King) | KAP 100/140/150, KFC 150/200/250 |
| KFC 225/275/325 | ||
| Century | I/II/III/IV, 21/31/41, 2000, Triden | |
| AK 1081 [1] | ||
| S-TEC | System 20/30/40/50/55/60-2/60 PSS/65 | |
| System 55X | ||
| ST-901 [1] | ||
| Cessna | 300B/400B/800B | |
| 300 IFCS/400 IFCS | ||
| Garmin | GFC 500 | |
| GFC 600 | ||
| Navigation Indicators | Garmin | GI 106/106B (IFR) |
| GI 102/102A (VFR) | ||
| Honeywell (Bendix/King) | KI 204/209/209A (IFR) | |
| KI 203/208/208A (VFR) | ||
| KI 206/209A/525A, KPI 552/552B/553/553A/553B (IFR) | ||
| KI 202/208A (VFR) | ||
| ARC (Cessna) | IN-386A, IN-481AC (IFR) | |
| IN-385AC (VFR) | ||
| Century | NSD 360A, NSD 1000 (IFR) | |
| Collins | 331A-6P, PN-101, IND-351D (IFR) | |
| S-TEC | ST 180 (IFR) | |
| Mid Continent | MD222-406, MD200-306, MD200-307 (IFR) | |
| MD222-402, MD200-302, MD200-303 (VFR) | ||
| Narco | VOA 5/9/50M (IFR) | |
| VOA 4/8 (VFR) | ||
| EFIS Displays | Aspen | EFD 1000/500 |
| Garmin | G500/G600 | |
| TXi Series | ||
| G5 (ADI) | ||
| G3X Touch | ||
| EHSI Displays | Garmin | G5 (HSI) |
| Sandel | SN 3308 | |
| SN 3500/4500 | ||
| Heading Reference Sources | Aspen | EFD 1000 |
| Garmin | GAD 42 | |
| G500/G600 | ||
| TXi Series | ||
| G3X Touch | ||
| Sandel | SN3500 | |
| SN3308 | ||
| Multifunction Displays | Garmin | GMX 200 |
| MX20 |
|
aera® 796/795/660 |
Garmin Pilot™ |
FltPlan Go |
|
| Backup Attitude |
X |
X |
X |
| GPS Position |
X |
X |
|
| Flight Plan Transfer |
X |
X |
X |
| ADS-B Weather |
X |
X |
X |
| ADS-B Traffic |
X* |
X* |
X |
GTS-825 Traffic System
GARMIN TAS / TCAS COMPARISON: |
GTS 800 |
GTS 820/825 |
GTS 850/855 |
| Traffic system type | TAS | TAS | TCAS 1 |
| Transmitter power output (nominal) | 40 watt | 250 watt | 250 watt |
| Active surveillance range (typical) | 20 nm | 40 nm | 40 nm |
| Number of targets tracked | 60 | 60 | 60 |
| Number of targets displayed (dependent on display system capability) | 30 | 30 | 30 |
| Display range | 2/6/12 | 2/6/12/24/40 | 2/6/12/24/40 |
| Range accuracy | +/- .05 nm | +/- .05 nm | +/- .05 nm |
| Bearing accuracy | 5° RMS | 5° RMS | 5° RMS |
| Altitude accuracy | +/- 200 ft | +/- 200 ft | +/- 200 ft |
| Altitude resolution | +/- 100 ft | +/- 100 ft | +/- 100 ft |
| Max vertical separation | +/- 10,000 ft | +/- 10,000 ft | +/- 10,000 ft |
| Audible target threat position callouts | Yes | Yes | Yes |
| 1090ES ADS-B receiver (requires ADS-B “Out” capability) | Yes | Yes | Yes |
| Correlated display capability | Yes | Yes < | Yes |
| Selective Mode-S interrogation | No | Yes | Yes |
| Maximum Operating Altitude | 55,000 ft. | 55,000 ft. | 55,000 ft. |
GTS-855 Traffic System
GARMIN TAS / TCAS COMPARISON: |
GTS 800 |
GTS 820/825 |
GTS 850/855 |
| Traffic system type | TAS | TAS | TCAS 1 |
| Transmitter power output (nominal) | 40 watt | 250 watt | 250 watt |
| Active surveillance range (typical) | 20 nm | 40 nm | 40 nm |
| Number of targets tracked | 60 | 60 | 60 |
| Number of targets displayed (dependent on display system capability) | 30 | 30 | 30 |
| Display range | 2/6/12 | 2/6/12/24/40 | 2/6/12/24/40 |
| Range accuracy | +/- .05 nm | +/- .05 nm | +/- .05 nm |
| Bearing accuracy | 5° RMS | 5° RMS | 5° RMS |
| Altitude accuracy | +/- 200 ft | +/- 200 ft | +/- 200 ft |
| Altitude resolution | +/- 100 ft | +/- 100 ft | +/- 100 ft |
| Max vertical separation | +/- 10,000 ft | +/- 10,000 ft | +/- 10,000 ft |
| Audible target threat position callouts | Yes | Yes | Yes |
| 1090ES ADS-B receiver (requires ADS-B “Out” capability) | Yes | Yes | Yes |
| Correlated display capability | Yes | Yes < | Yes |
| Selective Mode-S interrogation | No | Yes | Yes |
| Maximum Operating Altitude | 55,000 ft. | 55,000 ft. | 55,000 ft. |