# N293AT: 2025 Cirrus Design SR20

- Status: Valid registration
- Airframe: [Cirrus Design SR20](https://openairdocs.org/model/cirrus-design-sr20) (registry code 2130000, 4 seats)
- Engine: [Lycoming IO-390-C3B6](https://openairdocs.org/engine/lycoming-io-390-c3b6) (registry code 42710)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E00006NY](https://openairdocs.org/tcds/E00006NY) (Lycoming Engines) (OpenAirDocs)
- Serial number: 10596
- Year built: 2025
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: April 12, 2025
- Certificate issued: May 12, 2025
- Expires: May 31, 2032
- Mode S code: A300B1
- Registered owner: [Alpha Tango Aviation LLC](https://openairdocs.org/faa-owner/ALPHA%20TANGO%20AVIATION%20LLC)
- Location: [Allendale, NJ](https://openairdocs.org/faa-place/NJ/Allendale)
- Owner type: LLC
- Owner's area on the map: 41.0327° N, 74.1338° W: Placed by OpenAirDocs at the center of ZIP code 07401, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=293AT
- Page: https://openairdocs.org/aircraft/N293AT

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 15 in force

### Matched by airframe (Cirrus Design SR20)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2008-14-13](https://openairdocs.org/ad/2008-14-13): Upper door hinge · Cirrus Design SR20 and SR22. Effective Aug 14, 2008
- [AD 2008-11-18](https://openairdocs.org/ad/2008-11-18): Heat exchanger · Cirrus Design SR20. Effective Jul 7, 2008
- [AD 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008
- [AD 2007-14-03](https://openairdocs.org/ad/2007-14-03): Cirrus Airplane Parachute System (CAPS) · Cirrus Design SR20 and SR22. Effective Aug 16, 2007
- [AD 2006-21-03](https://openairdocs.org/ad/2006-21-03): Brake caliper piston O-ring seals · Cirrus Design SR20 and SR22. Effective Nov 17, 2006
- [AD 2006-19-10](https://openairdocs.org/ad/2006-19-10): Adjust crew seat break-over bolts · Cirrus Design SR20 and SR22. Effective Oct 24, 2006
- [AD 2006-07-06](https://openairdocs.org/ad/2006-07-06): Wire harness · Cirrus Design SR20 and SR22. Effective May 11, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2002-24-08](https://openairdocs.org/ad/2002-24-08): Cable clamp · Cirrus Design SR20 and SR22. Effective Jan 24, 2003
- [AD 2002-21-02](https://openairdocs.org/ad/2002-21-02): Self-locking retaining nut · Cirrus Design SR20 and SR22. Effective Nov 8, 2002
- [AD 2001-25-03](https://openairdocs.org/ad/2001-25-03): Rivets In Elevator and Rudder · Cirrus Design SR20 and SR22. Effective Dec 17, 2001

### Matched by engine (Lycoming IO-390-C3B6)

- [AD 2026-04-11](https://openairdocs.org/ad/2026-04-11): Engine (Reciprocating) · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 605 more. Effective Apr 8, 2026

### Historical (superseded or no longer in force)

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 2005-17-19](https://openairdocs.org/ad/2005-17-19) (historical): Crew seat recline locks · Cirrus Design SR20 and SR22. Effective Oct 13, 2005
- [AD 2002-05-05](https://openairdocs.org/ad/2002-05-05) (historical): Limitation Section - Cirrus Aircraft Parachute System (CAPS) Activation Cable · Cirrus Design SR20 and SR22. Effective Mar 19, 2002

## Information bulletins (advisory) (16 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011
- [SAIB CE-08-12R1](https://openairdocs.org/saib/CE-08-12R1): Electrical Power. Issued Mar 16, 2011
- [SAIB CE-11-09](https://openairdocs.org/saib/CE-11-09): Navigation  Flight Management Computing Software System. Issued Jan 5, 2011
- [SAIB CE-09-46](https://openairdocs.org/saib/CE-09-46): Landing Gear, Nose. Issued Jul 31, 2009
- [SAIB CE-09-32](https://openairdocs.org/saib/CE-09-32): Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount. Issued May 29, 2009
- [SAIB CE-09-01](https://openairdocs.org/saib/CE-09-01): Equipment - Emergency. Issued Oct 21, 2008
- [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006
- [SAIB CE-06-30](https://openairdocs.org/saib/CE-06-30): . Issued Feb 9, 2006
- [SAIB CE-06-07](https://openairdocs.org/saib/CE-06-07): . Issued Nov 4, 2005
- [SAIB CE-05-88](https://openairdocs.org/saib/CE-05-88): . Issued Sep 30, 2005
- [SAIB CE-05-77](https://openairdocs.org/saib/CE-05-77): . Issued Jul 27, 2005
- [SAIB CE-04-74](https://openairdocs.org/saib/CE-04-74): . Issued Aug 3, 2004
- [SAIB CE-03-09](https://openairdocs.org/saib/CE-03-09): . Issued Dec 16, 2002
- [SAIB CE-02-34](https://openairdocs.org/saib/CE-02-34): . Issued Jun 19, 2002
- [SAIB NE-19-08](https://openairdocs.org/saib/NE-19-08): Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve Cylinders. Issued May 2, 2019
- [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008

## NTSB investigations

None matched to N293AT.

## FAA accident and incident reports

None matched to N293AT.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N293AT not matched to an aircraft (31)

They name N293AT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SIMA200114702](https://openairdocs.org/sdr/SIMA200114702), May 27, 2001: LIGHT. INOPERATIVE. MIA - FLT 5305 - CREW REPORTED THE CABIN DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND 
- [SDR SIMA20010592](https://openairdocs.org/sdr/SIMA20010592), Feb 28, 2001: POWER SUPPLY. INOPERATIVE. MIA - FLT 5370 - CREW REPORTED FLOOR PROXIMITY LIGHTS OUT AT ROW 10, 11, 12. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 15WL. OPS CHECK WAS GOOD AND AIR
- [SDR SIMA200101501](https://openairdocs.org/sdr/SIMA200101501), Jan 15, 2001: LIGHT. INOPERATIVE. MIA - FLT 5229 - CREW REPORTED EXTERIOR EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAITNENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW ATR MM. OPS CHECK 
- [SDR SIMA2801](https://openairdocs.org/sdr/SIMA2801), Oct 6, 2000: GCU. FAILED. MIA - FLT 5371 - AFTER TAKEOFF FROM MIA, THE NR 2 DC GENERATOR FAULTED. THE CREW C/W THE QRH AND RETURNED TO MIA WITHOUT FURTHER INCIDENTS. REMOVED AND INSTALLE
- [SDR SIMA2271](https://openairdocs.org/sdr/SIMA2271), Aug 14, 2000: COVER. MISSING. APF - FLT 5208 - SERVICE DOOR LEFT EMERGENCY LIGHT LENS COVER MISSING. REPLACED COVER. (M)
- [SDR SIMA1203](https://openairdocs.org/sdr/SIMA1203), Apr 29, 2000: BRACKET. CORRODED. SAW - STRINGER 16R FRAME 33 BRACKET CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET IAW SRM 51-25-02. (M)
- [SDR SIMA1201](https://openairdocs.org/sdr/SIMA1201), Apr 29, 2000: STRINGER. CORRODED. SAW - STRINGER 17R BETWEEN FRAMES 32 AND 33 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER IAW SRM 53-00-00. (M)
- [SDR SIMA1202](https://openairdocs.org/sdr/SIMA1202), Apr 29, 2000: FLOORBEAM. CORRODED. SAW - FLOORBEAM 39 BETWEEN 14L AND 14R CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF FLOORBEAM IAW SRM 53-00-00. (M)
- [SDR SIMA10411](https://openairdocs.org/sdr/SIMA10411), Apr 13, 2000: GUIDE. CORRODED. DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD DEFLECTOR NUMBER 1, 3 AND 4 FROM INBOARD TO OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AN
- [SDR 20000609AP001](https://openairdocs.org/sdr/20000609AP001), Apr 13, 2000: GUIDE. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED INBOARD
- [SDR SIMA10410](https://openairdocs.org/sdr/SIMA10410), Apr 13, 2000: GUIDE. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED INBOARD
- [SDR SIMA1049](https://openairdocs.org/sdr/SIMA1049), Apr 13, 2000: FITTING. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD FORWARD AND AFT BEAM ATTACH FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT OUTBO
- [SDR SIMA1048](https://openairdocs.org/sdr/SIMA1048), Apr 13, 2000: FRAME. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND FRAME 36 AT SERVICE DOOR SILL PLATE CORRODED BEYOND LIMITS. REPAIRED FRAME 36 IAW SRM 53-61-40. AIRCRAFT RETURNED TO SERVI
- [SDR SIMA1042](https://openairdocs.org/sdr/SIMA1042), Apr 13, 2000: BEAM. CORRODED. SAW - DURING HMBV-1 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD FLAP BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLAP BEAM IAW JIC 575300-RAI
- [SDR SIMA1043](https://openairdocs.org/sdr/SIMA1043), Apr 13, 2000: ROD. CORRODED. SAW - DURING HMBV-1 INSPECTION, FOUND RIGHT ELEVATOR TRIM TAB DUAL LOAD PATH ROD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ROD. AIRCRAFT RETURNED TO
- [SDR SIMA1044](https://openairdocs.org/sdr/SIMA1044), Apr 13, 2000: ROD. CORRODED. SAW - DURING HMBV-1 INSPECTION, FOUND LEFT ELEVATOR TRIM TAB DUAL LOAD PATH ROD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ROD IAW JIC 273142-RAI-100
- [SDR SIMA1045](https://openairdocs.org/sdr/SIMA1045), Apr 13, 2000: WEB. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT WEB BETWEEN FRAMES 39 AND 40 AT CREASE BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED WEB IAW SRM 51-25-
- [SDR SIMA1046](https://openairdocs.org/sdr/SIMA1046), Apr 13, 2000: STRINGER. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER 17R BETWEEN FRAMES 27 AND 28 CORRODED BEYOND LIMITS. REPAIRED STRINGER 17R IAW SRM 53-00-00. AIRCRAFT RETURNED TO
- [SDR 20000620AP002](https://openairdocs.org/sdr/20000620AP002), Apr 13, 2000: FLOORBEAM. CORRODED. SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-01. AIRCRAFT RETURNED T
- [SDR SIMA1047](https://openairdocs.org/sdr/SIMA1047), Apr 13, 2000: FLOORBEAM. CORRODED. DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERV
- [SDR SIMA0196](https://openairdocs.org/sdr/SIMA0196), Jan 19, 2000: LAMP. INOPERATIVE. FLT 5360 - MIA - EMERGENCY FLOOR LIGHTS AT ROWS6 AND 13 INOPERATIVE. REMOVED AND REPLACED LAMPS AT ROWS 6 AND 13. OPS CHECKS GOOD. (M)
- [SDR SIMA992873](https://openairdocs.org/sdr/SIMA992873), Oct 14, 1999: BATTERY PACK. DISCHARGED. SAW - DURING PS-2 INSPECTION FOUND SEVERAL CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL IAW JIC 
- [SDR SIMA991412](https://openairdocs.org/sdr/SIMA991412), May 21, 1999: BATTERY PACK. DISCHARGED. SAW - DURING PS-2 INSPECTION, FOUND FORWARD EMERGENCY FLOOR, EXTERIOR AND EMERGENCY EXIT DOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BAT
- [SDR SIMA983232](https://openairdocs.org/sdr/SIMA983232), Nov 19, 1998: FAN. FAILED. MIA - FLT 5714 - AFT CARGO/LAV SMOKE WARNING ACTIVATED AFTER TAKEOFF. RETURNED TO FIELD. FOUND THE SMOKE DETECTOR FAN SMOKING DURING NORMAL OPERATION. REMVOED A
- [SDR SIMA982391](https://openairdocs.org/sdr/SIMA982391), Aug 27, 1998: SEAT TRACKS. CORRODED. DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. RE
- [SDR 98ZZZM710](https://openairdocs.org/sdr/98ZZZM710), Aug 27, 1998: SEAT TRACKS. CORRODED. DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. RE
- [SDR 98ZZZM709](https://openairdocs.org/sdr/98ZZZM709), Aug 27, 1998: SEAT TRACKS. CORRODED. DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. RE
- [SDR 98ZZZM708](https://openairdocs.org/sdr/98ZZZM708), Aug 27, 1998: SEAT TRACKS. CORRODED. DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. RE
- [SDR 98ZZZM707](https://openairdocs.org/sdr/98ZZZM707), Aug 27, 1998: SEAT TRACKS. CORRODED. DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. RE
- [SDR NVEA9700018](https://openairdocs.org/sdr/NVEA9700018), Nov 18, 1997: DRAIN LINE. BROKEN. ALB - DURING ROUTINE OVERNIGHT MAINTENANCE, RIGHT ENGINE COWLING WAS OPENED UP AND EVIDENCE OF FIRE WAS PRESENT. THE FIRE OCCURRED IN AN ISOLATED AREA LOCATED A
- [SDR 95ZZZX6786](https://openairdocs.org/sdr/95ZZZX6786), Nov 1, 1995: DEICE BOOT. SHORTED/BURNED. CREW REPORTS RIGHT PROPELLER BLADE DE-ICE BOOT SHORTED OUT CAUSING SPARKS AND A RED GLOW. DEACTIVATED THE SYSTEM AND LANDED WITHOUT INCIDENT. REPLACED PROPELLER

## STCs that may be installed (OpenAirDocs) (121, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cirrus Design SR20)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc
- [STC SA12227IB](https://openairdocs.org/stc/SA12227IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-B/188-50(). MT-Propeller Entwicklung GmbH
- [STC SA02216SE](https://openairdocs.org/stc/SA02216SE): Removal of mechanical link between engine throttle control and propeller RPM control. Installation of a separate RPM control lever, linkage between Cirrus RPM cable/cam followers, center console to accommodate three-lever configuration, new knobs for all levers, and new installation hardware (nuts, bolts, etc). Skyryse Inc
- [STC SA12064WI](https://openairdocs.org/stc/SA12064WI): Hardware and software updates for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA12084BO](https://openairdocs.org/stc/SA12084BO): Installation of the 700-00212-110 and the 700-00212-010 12-inch Vantage Displays Systems with Attitude Reference System and the 700-00236-000 Air Data Computers System. Avidyne Corporation
- [STC SA12080BO](https://openairdocs.org/stc/SA12080BO): Installation of Prodigy model 90901() LED Landing Light. Whelen Aerospace Technologies
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02551AK](https://openairdocs.org/stc/SA02551AK): Installation of SKYDISPLAY Aircraft Interface Device (AID). AeroDisplay LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA03303CH](https://openairdocs.org/stc/SA03303CH): Installation of MT propeller model MTV-12-D/188-59(). McFarlane Aviation LLC
- [STC SA04575CH](https://openairdocs.org/stc/SA04575CH): Installation of access panel in accordance with Kelly Aerospace Thermal Systems Installation Manual NC-19-092, revision E, or later FAA approved revision. Kelly Aerospace Thermal Systems LLC
- [STC SA00199BO](https://openairdocs.org/stc/SA00199BO): Installation of Aerox Oxygen System. Aerox Aviation Oxygen Systems LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA01170LA](https://openairdocs.org/stc/SA01170LA): : Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List, Document No. ST8691LA-A-01, Revision "B", dated May 14, 2001, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement, Document No. ST8691LA-A-09, Revision "N/C", dated June 01, 2001, or later FAA approved revision. Sandel Avionics LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02329AK](https://openairdocs.org/stc/SA02329AK): Installation of a fixed-mounted Max-Viz® Enhanced Vision System (EVS) Model 100 or Model 600 to include a sensor with conformal housing that displays imagery on any FAA-approved monitor with NTSC RS-170 video interface capability. PECO Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01234WI-D](https://openairdocs.org/stc/SA01234WI-D): Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). Honeywell International Inc
- [STC SA04449CH](https://openairdocs.org/stc/SA04449CH): Retirement life extension of Cirrus Design Corporation aircraft model SR20 in accordance with FAA approved Master Drawing List, E00002953, Revision E, dated February 26, 2020, or later FAA approved revision. Cirrus Design Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [STC SA00378BO](https://openairdocs.org/stc/SA00378BO): Installation of integrated wingtip exterior light assemblies. Cirrus Design Corporation

All 121: https://openairdocs.org/aircraft/N293AT/stcs.md

## Earlier aircraft with N293AT

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N293AT before.

- [Cancelled 2012-03-02](https://openairdocs.org/deregistered/N293AT-2012-03-02): Airbus Industrie A320-111, S/N 006. Owner: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)

## Related

- Other Cirrus Design SR20 aircraft: https://openairdocs.org/model/cirrus-design-sr20/aircraft.md
- The Lycoming IO-390-C3B6 engine: https://openairdocs.org/engine/lycoming-io-390-c3b6.md

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