GTS-855 Traffic System
$0.00
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. |
Includes a Single GA 58 Directional Antenna
Optional GA58 Antenna & a Monopole Antenna or Dual GA58 Antenna Setups Available
GTS 855 TCAS I: A timely new dimension in collision avoidance
Advanced air traffic surveillance and collision avoidance systems.
For pilots operating high-performance aircraft in busy, high-density airspace, traffic separation requires a heightened sense of situational awareness — to “see and avoid” in all 3 dimensions. Pilot alertness and vigilance are essential. But for maximum protection, nothing beats having an extra set of “electronic eyes.” That’s why we developed the GTS™ family of ADS-B enhanced Traffic Advisory (TAS) and Traffic Collision Avoidance (TCAS I) Systems.
Featuring our exclusive CLEAR CAS™ technology, these attractively priced systems provide accurate, dynamic traffic surveillance — with ATC-like spoken audio alerts to help pilots quickly respond to potential flight path intrusions from other aircraft.
Separation Anxiety Terminated
Augmenting reports from radar-based air traffic control, the GTS 855 is able to use a synthesis of both active and passive surveillance technology (including 1090 MHz ADS-B “In”) to correlate target data and pinpoint traffic threats. This hybrid active/passive surveillance is enabled with installation of a GTX 330 ES “extended squitter” Mode-S transponder (sold separately), or other complementary class of ADS-B “Out” equipment, such as our GDL 88 datalink.
With this technology, aircraft are able to automatically report and receive more stable, and more detailed, traffic data — including aircraft flight ID, GPS-based positioning, relative altitude and direction of flight. Course trend vectors and vertical climb or descent information can also be shown on compatible displays. Thus, instead of just seeing random targets on a display, pilots can now identify and track specific aircraft flight trajectories with much greater precision. So, in busy airspace, they’re able to fly with a much clearer tactical picture of their immediate traffic situation.
More Integration Means Higher Awareness
Displaying traffic symbols and advisories on a variety of compatible display products in the cockpit, the GTS 855 can track up to 75 traffic targets simultaneously — and depict up to 30 intruder threats at a time, depending on the display being utilized. (There is no dedicated instrument or panel space required for TAS.) Creating a 360° zone of detection around your aircraft, the GTS 855 enables you to quickly see and identify targets in your airspace that may pose a potential collision hazard.
Voice Alerting Helps Keep Heads Up, Eyes Out
In place of the generic “Traffic, traffic” voice alerts of some earlier-generation systems, the GTS 855’s exclusive CLEAR CAS technology provides for expanded audio messaging in an ATC-like verbal format: “Traffic. One o’clock. High (or Low or Same Altitude). Two miles.” If surveillance bearing information is not available on the intruder, “Traffic, No Bearing” is called out.
By vocalizing more specific traffic-spotting information, pilots can stay “eyes out” while locating the intruder target on the cockpit display.. Sometimes, those vital split-seconds can make all the difference in a fast-converging situation.
Higher Speeds Call for Faster Response
The GTS family of TAS and TCAS I systems offers a full range of traffic surveillance capabilities to fit your specific aircraft and operational criteria.
Recommended for today’s higher-capability cabin class turboprops and business or regional jets, the GTS 855 TCAS I offers 400 W of nominal power output, a +/- 10,000-foot vertical separation maximum, and up to 80 nm of active interrogation range in the forward direction. All GTS units will operate to 55,000 feet. And a Mode-S transponder (sold separately) is required as part of the GTS 855 system installation.
For commuter aircraft (those with 10 to 30 passenger seats), TCAS I capability is required by the FAA. The GTS 855 system meets these stringent TCAS I performance criteria, providing the range and response to give early warning of fast-closing aircraft in high-traffic airspace. Targets are depicted using familiar TCAS-defined symbology. And selectable horizontal display ranges allow pilots to maintain the “big picture” of overall traffic activity in their airspace.
| GTS 800/820/825/850/855 Processor LRU | GA 58 Directional Antenna |
| Unit Size: 6.25″W x 2.7″H x 12.7″D (15.87 x 7.11 x 32.25 cm) excluding mounting rack |
Unit Size: 4.03″W x 2.97″H x 5.63″D (10.24 x 7.54 x 14.30 cm) |
| Weight: 9 lbs (4.08 kg) LRU; excludes connectors Vertical rack – 1.05 lbs (0.48 kg) Horizontal rack – 1.94 lbs (0.88 kg) |
Weight: 0.8 lb (0.36 kg); excludes connectors |
| Temperature: -55°C to +70°C | Omni-Directional Antenna (optional) |
| Operating Altitude: To 55,000 feet | Unit Size: 0.98″W x 3.30″H x 4.00″D (2.49 x 8.38 x 10.16 cm) |
| Power input: 14 or 28 VDC 40W max. (GTS 800); 45W max. (GTS 820, 825, 850, 855) |
Weight: 0.24 lb (0.10 kg); excludes connectors |
| Cooling input: Integrated | GPA 65 PA/LNA Module (GTS 820/850 only) (Built-in on 825/855 Units) |
| Environmental Compliance: RTCA DO-160E | Unit Size: 4.25″W x 1.00″H x 8.00″D (10.8 x 2.54 x 20.32 cm) |
| Software Compliance: RTCA DO-178B Level C | Weight: 1.75 lb (0.79 kg); excludes connectors |
| Hardware Compliance: RTCA DO-254, Level C | |
| TSO Compliance: GTS 800,820 TAS: TSO-C147, TSO-C166a, DO-197A, DO-260A; GTS 850 TCAS I: TSO-C118, TSO-C166a, DO-197A, DO-260A | |
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. |
Related products
G500 TXi 10.6″ 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 - 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 |
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. |
|
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) |
G500 TXi 10.6″ Primary Flight Display with AHRS
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 |
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. |
|
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) |
G500 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 - 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 |
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. | |
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) |
G600 TXi 10.6″ 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) |
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 600 Digital 2-Axis Autopilot, for A36 Bonanza & B55 Baron
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
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. |