Garmin GFC 500 Digital 2-Axis Autopilot
$286.00
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 GFC 500 Digital 2-Axis Autopilot, for Beechcraft, Piper & Cessna Models
It’s the Autopilot Solution You Have Been Waiting For with Optional Pitch Trim and Yaw Dampener
- Cost-effective, precise and smooth in-flight characteristics, built-in self-monitoring capabilities and lower cost of ownership when compared to older autopilot systems
- Designed for existing light single-engine piston, fixed-wing aircraft, initially available for select Cessna 172 and Cessna 182 models with more to follow
- Leverages certificated G5 electronic flight instrument for primary attitude reference — plus input and display of altitude preselect, heading, vertical speed, airspeed target and flight director cues
- 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 tailored to your aircraft; optional pitch-trim servo adds automatic trim and manual electric trim
The revolutionary GFC 500 autopilot brings unprecedented levels of capability, reliability and affordability to light single-engine, fixed-wing general aviation aircraft. GFC 500 leverages our advanced attitude-based flight control technology developed for the popular GFC 700 autopilot, which drives our most advanced glass flight deck systems.
To help prevent incidents caused by loss of control, the FAA and other regulators encourage the use of key technologies, such as angle-of-attack indicators and autopilots, to help increase situational awareness, reduce pilot workload and enhance safety of flight. GFC 500 is the right product — at the right price — for popular certified light GA aircraft such as select Cessna 172 and Cessna 182 models as well as Piper PA-28 series aircraft. Boasting a superior feature set, GFC 500 incorporates a number of safety-enhancing technologies, including Garmin ESP, underspeed and overspeed protection, automatic LVL mode, flight director (FD) command cues and more.>/p>
Smart Technology, Easily Accessible
Drawing on top-end Garmin flight control technology from our GFC 700, GFC 500 provides crisp, precise response and optimum performance over the entire airspeed envelope of your aircrcaft. Rather than depending on failure-prone mechanical gyros, the GFC 500 system is digitally controlled, using solid-state attitude and air data sensor reference — giving you ultra-smooth roundouts, intercepts and more while also enhancing the reliability of the system. Incorporating our crisp, easy-to-read 3.5” G5 electronic flight instrument¹, a mode controller and 2 “smart” servos, the autopilot’s architecture supports full pitch-and-roll axis control capabilities as well as optional pitch trim and manual electric trim with an additional servo.
With the optional GAD™ 29 nav data adapter, GFC 500 will interface with the GTN™ 650 and GTN 750 and legacy GNS™ 430 and GNS 530 (WAAS and non-WAAS) series navigators to fly a wide range of precision, nonprecision and GPS-guided approaches as well as holds, procedure turns, missed approaches and more. GFC 500 also includes built-in GPS roll steering capability, which allows smoother navigation tracking and eliminates the need for external roll steering converters. Flight director cues are displayed as command bars on the G5 electronic flight instrument. The command bars 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. With support for a remotely installed Takeoff/Go-around (TOGA) button, the flight director can be cued to automatically indicate and capture the correct pitch attitude required to fly a missed approach and then follow the missed approach procedure loaded in your compatible GPS navigator. Up to 2 G5 electronic flight instruments can be interfaced with the GFC 500 autopilot in your aircraft, providing full reversionary display capability.
Mode Control at Your Fingertips
A mode controller is included with your GFC 500 package, and its compact size and mark-width design require only minimal space in your avionics stack while providing easy access to all autopilot modes and functions. You can select advanced lateral and vertical modes such as pitch hold, altitude preselect, altitude hold, vertical speed and indicated airspeed hold as well as roll, track and selected heading. An intuitive control wheel integrated into the GFC 500 mode controller allows for easy and precise pitch, vertical speed and airspeed adjustments, while separate knobs allow quick twist control of heading and altitude. For added safety, a dedicated LVL button on the controller lets you command the autopilot to automatically return your aircraft to straight-and-level flight — and thus help avert a potential loss-of-control situation.
Silky-smooth Servo Control
For maximum reliability and safety, the GFC 500 servos incorporate brushless DC motors and a gear train that eliminates the need for a mechanical slip clutch and shear pins. 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 easily hand-fly or override the system without fighting the controls. The servos weigh only 1.4 lbs each, making them more than 40% lighter than most other autopilot servos of their class. Each servo is operated by its own built-in microprocessor, which provides the “smart” logic to significantly improve sensor performance, response and self-monitoring capabilities — while simplifying overall system configuration and installation.
Hand-fly with Stability Protection
Any pilot who’s ever been startled to attention by a stall warning horn in a busy cockpit will appreciate the proactive stability augmentation of our ESP technology, which is standard on the GFC 500 system. When the aircraft is being hand-flown, this ESP feature functions independently of the autopilot — although it uses the same control servos — to 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 Knows Its Limits
With the autopilot engaged, GFC 500 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 500 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 a Total Peace-of-mind Investment
There is no substitute for a safe and vigilant pilot. But there are times when a “helping hand” at the controls can have a significant impact on the safety, comfort and enjoyment of your flight. Backed by a comprehensive warranty and the industry’s No. 1-rated product support team, our GFC 500 autopilot system is a price- and peace-of-mind breakthrough for pilots who want to add these valuable capabilities to their existing light piston GA aircraft. Installation approval via supplemental type certification (STC) is expected to be completed on a range of popular models. See your authorized Garmin installation center for more details on configuring a GFC 500 retrofit package for your aircraft.
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
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Manufacturer |
Model |
Notes/Info |
ADF Receiver |
Collins | ADF-60A/B | |
| Honeywell | KR 87 KDF 806 |
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| 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. |
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Cessna | 300B IFCS, 400B IFCS, 800B IFCS, 1000A IFCS | |
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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) |
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| Collins | APS 65 (APC-65/65E/65H/65J) | ||
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Autopilot - External Flight Director |
Bendix | M-4D | |
| Century | IV 41 2000 |
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| Cessna | 300B IFCS/400B IFCS/800B IFCS 1000A IFCS |
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Parallel tuning now available for DME-42. |
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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 |
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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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TAS/TCAS/TIS Traffic Display and Control |
Garmin | GTX 33( )/330( )/335 GTS 800/820/850 |
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ADS-B Traffic Display |
Garmin | GDL 88 GTX 345 |
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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 | ||
| 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 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 - 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″ Landscape 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) |
GTN 750 Xi Series 6.9″ Touchscreen GPS/NAV/COMM/MFD
- 750Xi TSO applicability: C34e; 2C34f; C36e Class A; 2C36f Class A; C40c; 2C40c; C74d Class A; C112e; C128a; 2C128; C146e Class 3; C151d Class A, B; C157b Class 1, 2; 165b; C169a Class C, E, 3, 4, 5, 6; 2C169a Class C, E, H2, 3, 4, 5, 6; C194; C195b Class B1, B3, B5, B7; C209
- 725Xi TSO applicability: C74d Class A; C112e; C146e Class 3; C151d Class A, B; C157b Class 1, 2; 165b; C194; C195b Class B1, B3, B5, B7; C209
- Display size: 6.9" (175 mm) diagonal
- Display resolution: 834 pixels (W) x 986 pixels (H)
- Unit bezel height: 6.00" (152 mm)
- Unit bezel width: 6.25" (159 mm)
- Unit depth with connectors: 11.25" (286 mm) (measured from face of aircraft panel to rear of connector backshells)
- Unit weight: 7.1 lbs (3.22 kg)
- Input voltage range: 11 VDC - 33 VDC
- Operating temperature range: -20° C to 55° C (-4° F to 131° F)
- 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: 1,166 knots
- Position update Interval: 0.2 sec (5 Hz)
| Interface | Manufacturer | Model |
| Air Data Computer | B & D | 90004-003 |
| Honeywell (Bendix/King) | KDC 281 KDC 481 | |
| Insight | TAS 1000 | |
| Altitude Serializer/Encoder | Garmin | GTX 327 |
| ACK Technologies | A-30 (Mod 8 and above) | |
| ARNAV | FC-10 FT-10 | |
| Electronics International | FP-5L | |
| Icarus Instruments | 3000 | |
| JP Instruments | EDM-700 | |
| Sandia | SAE 5-35 | |
| Shadin | 833811-00 (AIS-380) 8800T 9000T 9200T F/ADC-200 F/ADC-2000 91204XT(38)D (Miniflo-L) 91053XP (Digiflo-L) 91053XT-D (Digiflo-L) 912802-( ) (Digidata) | |
| Trans-Cal Industries | IA-RS232-X SSD120 | |
| Audio Panel | Garmin | SL10 SL10MS SL10M SL10S SL15 SL15M GMA 340 GMA 347 GMA 35(c) GMA 350(c)/350H(c) |
| Honeywell (Bendix/King) | KMA 24 KMA 24H-70/71 KMA 26 KMA 28 | |
| PS Engineering | PMA 6000 PMA 7000 Series PMA 8000 Series | |
| Autopilot | Garmin | GFC 500 GFC 600 |
| Bendix | M4C M4D | |
| Century | I/II/III/IV 21/31/41 2000 Trident AK 1081 | |
| Cessna | 300B/400B/800B 300 IFCS/400 IFCS/800 IFCS/1000 IFCS | |
| Collins | APS 65 ( ) | |
| Honeywell (Bendix/King) | KAP 100/140/150 KFC 150/200/250/300 KFC 225/275/325 | |
| Sperry | SPZ 200A/500 | |
| S-TEC | System 20/30/40/50/55/60-1/60-2/60 PSS/65 System 55X ST-901 | |
| Datalink Weather Display and Control | Garmin | GDL 69/69A (also provides SiriusXM radio entertainment.) GSR 56 (also provides text/voice communication) |
| DME Control | Collins | DME 40 DME 42 |
| Honeywell (Bendix/King) | KN62/62A KN63 KN64 KDI 572/574 KDM 706 | |
| Narco | DME 890 IDME 891 | |
| EFIS | Garmin | G500/G600 TXi Series G5 G3X Touch |
| Avidyne | EXP5000 | |
| Honeywell (Bendix/King) | EFS 40/50 (SG 465) | |
| EHSI | Sandel | SN 3308 SN3500/4500 |
| FIS-B Weather Display and Control | Garmin | GDL 88 |
| Fuel/Air Data | Garmin | GTX 327 |
| ARNAV | FC-10 FT-10 | |
| Electronics International | FP-5L | |
| JP Instruments | EDM-700 | |
| Shadin | F/ADC-200 F/ADC-2000 91204XT(38)D (Miniflo-L) 91053XP (Digiflo-L) 91053XT-D (Digiflo-L) 912802-( ) (Digidata) | |
| IRU/AHRS | Collins | AHS-85E |
| Lightning Detection Display and Control | L-3 Communications | WX-500 |
| Multifunction Display | Garmin | GMX 200 MX20 |
| Avidyne | EX500 EX5000 | |
| NAV Indicator | Garmin | GI 102/A GI 106/A |
| Century | NSD 360A NSD 1000 | |
| Collins | 331A-6P 331A-9G PN101 (331A-3F/3G) IND-351D | |
| Honeywell (Bendix/King) | KI 202A/203/204/206 KI 208/A KI 209/A KI 525A KPI 552/B KPI 553/A/B | |
| Mid Continent | MD222-402 MD222-406 MD200-302/303/306/307 | |
| Sperry | RD 444 RD 550A RD 650 | |
| S-TEC | ST 180 | |
| Synchro Heading Source | Bendix/King | KI-525A |
| TAS/TCAS/TIS Traffic Display and Control | Garmin | GTS 800/820/850 GTX 330/33/330D/33D |
| Avidyne (Ryan) | TAS 6XX (TCAD 9900BX) | |
| Honeywell (Bendix/King) | KMH 880 (KMH 820) KMH 980 (KMH 920) KTA 870 (KTA 810) KTA 970 (KTA 910) | |
| L-3 Communications | SKY497 (Skywatch) SKY899 (Skywatch HP) | |
| Terrain Avoidance and Warning System | Honeywell (Bendix/King) | KGP 560 KMH 880 (KMH 820) KMH 980 (KMH 920) |
| Transponder Display and Control | Garmin | GTX 32 GTX 327 GTX 328 GTX 33/33D GTX 330/330D GTX 325/335(R)/345(R) |
| Weather Radar Display and Control | Garmin | GWX 68 GWX 70 GWX 75 |
| Bendix/King | RDS 81 (RS 811A) RDS 82 (RS 181A) RDR 2000 (ART 2000) RDR 2100 (ART 2100) |
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. |