# N572CA: 2024 Cirrus Design SR22T

- Status: Valid registration
- Airframe: [Cirrus Design SR22T](https://openairdocs.org/model/cirrus-design-sr22t) (registry code 2130004, 5 seats)
- Engine: [Continental TSIO-550-K](https://openairdocs.org/engine/continental-tsio-550-k) (registry code 17410)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E5SO](https://openairdocs.org/tcds/E5SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 10301
- Year built: 2024
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: November 9, 2024
- Certificate issued: July 28, 2025
- Expires: July 31, 2032
- Mode S code: A7560A
- Registered owner: [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE)
- Location: [Casper, WY](https://openairdocs.org/faa-place/WY/Casper)
- Owner type: LLC
- Owner's area on the map: 43.0653° N, 106.3418° W: Placed by OpenAirDocs at the center of ZIP code 82601, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=572CA
- Page: https://openairdocs.org/aircraft/N572CA

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): 17 in force

### Matched by airframe (Cirrus Design SR22T)

- [AD 2024-24-11](https://openairdocs.org/ad/2024-24-11): Power Lever · Cirrus Design SR20, SR22 and SR22T. Effective Dec 23, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [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 2012-01-11](https://openairdocs.org/ad/2012-01-11): Engine Air Intake · Cirrus Design SR22T. Effective Feb 29, 2012

### Matched by engine (Continental TSIO-550-K)

- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-21-04](https://openairdocs.org/ad/2016-21-04): Oil cooler cross fitting assembly · Continental Motors TSIO-550-C, TSIO-550-K, TSIO-550-N and 2 more. Effective Nov 18, 2016
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2012-10-13](https://openairdocs.org/ad/2012-10-13): Starter adapters · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Jun 8, 2012
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993

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

- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2011-25-51](https://openairdocs.org/ad/2011-25-51) (historical): Starter Adapter Gear Shaft · Continental Motors IO-550-N, TSIO-520-B, TSIO-520-BB and 14 more. Effective Dec 28, 2011
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more

## Information bulletins (advisory) (8 in force)

- [SAIB CE-13-43R1](https://openairdocs.org/saib/CE-13-43R1): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Sep 30, 2013
- [SAIB CE-11-50](https://openairdocs.org/saib/CE-11-50): Flight Controls, Flaps. Issued Aug 26, 2011
- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB CE-13-43](https://openairdocs.org/saib/CE-13-43) (historical): Aircraft Fuel Distribution System and Ice/Rain Protection System. Issued Aug 30, 2013

## NTSB investigations

None matched to N572CA.

## NTSB investigations on N572CA not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA92IA065](https://openairdocs.org/ntsb/MIA92IA065), Jan 23, 1992: Boeing 757-23APF (N572CA), Miami, FL, incident, no damage. Probable cause: THE PILOT-IN-COMMAND'S IMPROPER SUPERVISION OF THE CO-PILOT/FIRST OFFICER. THIS RESULTED IN A TOTAL LOSS OF ENGINE POWER ON BOTH ENGINES WHILE AT LOW POWER SETTINGS IN KNOWN ICING CONDITIONS FOR…

## FAA accident and incident reports

None matched to N572CA.

## Reports on N572CA not matched to an aircraft (1)

They name N572CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19920123012139I](https://openairdocs.org/incident/19920123012139I), Jan 23, 1992: Boeing 75723APF (N572CA), Miami, FL. Multiple engine flameout after passing through thunderstorm. Restarted. Landed safely. Engine anti-ice off at time.

## 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 N572CA not matched to an aircraft (24)

They name N572CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2000ZZZX215](https://openairdocs.org/sdr/2000ZZZX215), Oct 1, 1999: LINE. RUPTURED. KMIA/KSAL - FLT 067 AT 21:30 Z - LEFT HYDRAULIC QUANTITY INDICATOR DECREASED TO 0.03 GALLON. ENGINE DRIVEN PUMP DEPRESSURIZED AND ELECTRIC PUMP OFF, QUANTITY IN
- [SDR CLCA9903](https://openairdocs.org/sdr/CLCA9903), Mar 19, 1999: CIRCUIT BREAKER. TRIPPED. FLT 33 - MIA-SAP - AIR TURN BACK, CLIMBOUT OF FL240 THE FOLLOWING OCCURED. THE LEFT IRS DISPLAYED ON DC AND EICAS MESSAGE. THE CTR AUTOPILOT DISENGAGED AND AUTO
- [SDR CLCA9801](https://openairdocs.org/sdr/CLCA9801), Nov 1, 1998: SKIN. DAMAGED. FLT 56 - BOG-MIA - UPON APPROACH, CREW LOGGED 'FLAPS MAKE LOUD GRINDING NOISE IN FLIGHT WHEN FLAPS MOVING FROM POSITION 0 TO 1.' UPON GROUND INSPECTION AT MAI, 
- [SDR CLCA9902](https://openairdocs.org/sdr/CLCA9902), Sep 29, 1998: PANEL. CORRODED. ON 9-29-98 DURING ROUTINE 'A' CHECK, FOUND CORROSION AT THE RIGHT FUELING STATION WS 481.50, BOEING AUTHORIZED CAC TO CONTINUE OPERATIONS WITH REPEAT INSPECTION
- [SDR 98ZZZM1](https://openairdocs.org/sdr/98ZZZM1), Dec 5, 1997: NLG. BIRDSTRIKE. FLT 96, ON APPROACH TO MIA, EICAS MSG GEAR DISA DISP WITH GEAR HANDLE UP. GEAR AMB LT ILLUM DOORS AMB LT AND ALL GREEN DOWN LTS EXTINGUISHED. NOSE GEAR GREEN DO
- [SDR 98ZZZM21](https://openairdocs.org/sdr/98ZZZM21), Nov 28, 1997: LINE. CRACKED. ON CAC - FLT 89 - A/C AIR RETURNED TO MIA, DUE TO LEFT HYD QTY LOSS OVERWEIGHT LANDING OCCURRED (98,000). ON GROUND MAINTENANCE, REMOVED AND REPLACED NR 1 ENGIN
- [SDR 97ZZZX4551](https://openairdocs.org/sdr/97ZZZX4551), Oct 15, 1997: SEAT TRACK. CORRODED. LT OUTBOARD FLOATING SEAT TRACK STA 880 TO STA 900 HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED UPPER SECTION PER SRM 53-00-52. TAT: 2,628.8 HOURS. TAC: 5,
- [SDR 97ZZZX4550](https://openairdocs.org/sdr/97ZZZX4550), Oct 15, 1997: SEAT TRACK. CORRODED. INTERGRANULAR CORROSION ON SEAT TRACK SUPPORT RT, SECOND TRACK FROM CENTER PALLET POSITION NR 7 AT FS 970 RT. CLEANED AND TREATED CORROSION AND INSTALLED STRAP 
- [SDR 97ZZZX4549](https://openairdocs.org/sdr/97ZZZX4549), Oct 15, 1997: SEAT TRACK. CORRODED. FLOATING SEAT TRACK LT SIDE STA 880 TO STA 900 HAS INTERGRANULAR CORROSION AND IS CRACKED. FABRICATED AND INSTALLED REPAIR ON SEAT TRACK PER DER DWG 97039. TAT:
- [SDR 97ZZZX4548](https://openairdocs.org/sdr/97ZZZX4548), Oct 15, 1997: FLOOR BEAM. CORRODED. FLOOR BEAM CORRODED AT FS 879 OUTBOARD OF SECOND SEAT TRACK FROM CENTER RT. REPAIR FLOOR BEAM PER SRM 53-00-51. TAT: 2,628.8 HOURS. TAC: 5,944.
- [SDR 97ZZZX4547](https://openairdocs.org/sdr/97ZZZX4547), Oct 15, 1997: SEAT TRACK. CORRODED. INTERGRANULAR CORROSION AROUND FASTENER HOLES BETWEEN CENTER AND RT NR 1 SEAT TRACK AT BS 900. REPAIRED FLOOR BOARD CHANNEL BETWEEN CENTER AND NR 1 SEAT TRACK P
- [SDR 97ZZZX4546](https://openairdocs.org/sdr/97ZZZX4546), Oct 15, 1997: SEAT TRACK. CORRODED. RIGHT SEAT TRACK SECOND FROM CENTER SUPPORT STIFFENER CORRODED AT FS 880. REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-30-51 AND SRM 51-30-40. TAT: 2,628.8 HO
- [SDR 97ZZZX4545](https://openairdocs.org/sdr/97ZZZX4545), Oct 15, 1997: SEAT TRACK. CORRODED. RIGHT SEAT TRACK FIRST FROM CENTER SUPPORT STIFFENER CORRODED AT FS 880. REMOVED AND REPLACED ATTACH BRACKET PER SRM 51-30-51 AND SRM 51-30-40. TAT: 2,628.8 HOU
- [SDR 97ZZZX4544](https://openairdocs.org/sdr/97ZZZX4544), Oct 15, 1997: SEAT TRACK. CORRODED. RIGHT SEAT TRACK SECOND FROM CENTER SUPPORT CORRODED AT FS 880 TO FS 900. CLEANED AND TREATED CORROSION PER SRM 53-00-52. TAT: 2,628.8 HOURS. TAC: 5,944.
- [SDR 97ZZZX4543](https://openairdocs.org/sdr/97ZZZX4543), Oct 15, 1997: FLOOR BEAM. CORRODED. STA 880 FLOOR BEAM BETWEEN LBL 45.5 AND LBL 24.75, FORWARD UPPER CHORD OUTBOARD, FLOOR BOARD FASTENERS HOLE LOWER SIDE, HAS INTERGRANULAR CORROSION. REPAIR SEAT
- [SDR 97ZZZX4542](https://openairdocs.org/sdr/97ZZZX4542), Oct 15, 1997: SEAM TAPE. WRONG PART. SEAM TAPE IN MAIN CARGO COMPARTMENT DOES NOT MEET FAR 25.853 REQUIREMENTS. REMOVED TAPE AND RETAPED WITH APPROVED TAPE. TAT: 2,628.8 HOURS. TAC: 5,944.
- [SDR 97ZZZX4541](https://openairdocs.org/sdr/97ZZZX4541), Oct 15, 1997: TRACK SUPPORT. CORRODED. RIGHT SEAT TRACK SUPPORT, SECOND FROM CENTER BS 860 TO BS 880, HAS INTERGRANULAR CORROSION. REPAIRED SEAT TRACK PER SRM 53-00-52. TAT: 2,628.8 HOURS. TAC: 5,944
- [SDR 97ZZZX2965](https://openairdocs.org/sdr/97ZZZX2965), Jun 16, 1997: PITOT TUBE. PLUGGED. MIZ/LIMA - FLT 087 - ON OR ABOUT 0430, A/C ABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON CAPTAIN'S AIRSPEED INDICATOR, CAPTAIN'S AUX AND F/O'S AIRSPEED INDIC
- [SDR 97ZZZM554](https://openairdocs.org/sdr/97ZZZM554), Apr 10, 1997: WINDSHIELD. HIGH RESISTANCE. FLT 47 - APPROX 1 HOUR INTO FLIGHT, SMOKE AND ODOR WAS DETECTED IN COCKPIT. ALL WINDOW HEAT TURNED OFF, AIRCRAFT DESCENDED TO 10,000 FT AND RETURNED TO MIA WITH
- [SDR USAA960724](https://openairdocs.org/sdr/USAA960724), Aug 29, 1996: SKIN. DENT. CLT - INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT FRAME STATION 345 LEFT ZONE 838. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER AS PER SR
- [SDR USAA960723](https://openairdocs.org/sdr/USAA960723), Aug 29, 1996: SKIN. DENT. CLT INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT STATION 1480, ABOVE STRINGER 26L. DAMAGE CUTOUT AND INSTALLED REPAIR ANGLE AND FILLER AS PER SRM 
- [SDR USAA960722](https://openairdocs.org/sdr/USAA960722), Aug 29, 1996: SKIN. DENT. CLT - INSPECTION VISUALLY FOUND A 1 INCH DENT IN SKIN LOCATED AT STATION 1520 ABOVE STRINGER 26R. DAMAGED REMOVED AND INSTALLED REPAIR ANGLE AND FILLER AS PER S
- [SDR 96ZZZM1046](https://openairdocs.org/sdr/96ZZZM1046), Jun 10, 1996: WINDOW. CRACKED. FLT 39 - KMIA-MNMG - DURING FLIGHT, THE L1 WINDOW CRACKED. AIRCRAFT RETURNED TO MIAMI, FLORIDA. REMOVED AND REPLACED WINDOW. AIRCRAFT RETURNED TO SERVICE.
- [SDR 95ZZZW774](https://openairdocs.org/sdr/95ZZZW774), May 8, 1995: HYD LINES. BROKEN. FLT NR 92 - AFTER TAKEOFF FROM BOGOTA, LOST HYDRAULIC SYSTEM QUANTITY AND PRESSURE. ABNORMAL CHECK LIST COMPLIED WITH. AIRCRAFT DIVERTED TO CALI. FOUND THREE BR

## STCs that may be installed (OpenAirDocs) (53, 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 SR22T)

- [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 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 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 SA12274IB](https://openairdocs.org/stc/SA12274IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-D/198-52() and MTV-9-D/198-58() propellers. MT-Propeller Entwicklung GmbH
- [STC SA12064WI](https://openairdocs.org/stc/SA12064WI): Hardware and software updates for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA12080BO](https://openairdocs.org/stc/SA12080BO): Installation of Prodigy model 90901() LED Landing Light. Whelen Aerospace Technologies
- [STC SA12027IB](https://openairdocs.org/stc/SA12027IB): Installation of the MT-Propeller Entwicklung GmbH MTV-14-D/195-30() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02924CH](https://openairdocs.org/stc/SA02924CH): Installation of M-T Propeller model MTV-14-D/195-30( ) 4 bladed propeller. McFarlane Aviation LLC
- [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 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 SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA01076DE](https://openairdocs.org/stc/SA01076DE): Installation of main battery replacement with Concorde Valve Regulated Lead Acid battery. Concorde Battery Corporation
- [STC SA04440CH](https://openairdocs.org/stc/SA04440CH): Installation of Hartzell propeller model 4C1-F650A1/76C04-0.6 or 4C1-F650A1/76C04B-0.6. Hartzell Propeller Inc
- [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 SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA00378BO](https://openairdocs.org/stc/SA00378BO): Installation of integrated wingtip exterior light assemblies. Cirrus Design Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA03869NY](https://openairdocs.org/stc/SA03869NY): Installation of a Safetyplane Flight Monitoring System. ISEI International Services
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA03777NY](https://openairdocs.org/stc/SA03777NY): Installation of RF-006(A) Main Wheel and RA-002(A) Nose Wheel with EA-003.3N Brake System. Beringer Aero
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc
- [STC SA02554LA](https://openairdocs.org/stc/SA02554LA): Installation of a strut mounted Sensor Pod and wiring for a passenger operated monitoring system. Sky IMD Inc
- [STC SA02247SE](https://openairdocs.org/stc/SA02247SE): Removal of rear seats and installation of cargo shelf and restraint system. Tamarack Aerospace Group
- [STC SA04037CH](https://openairdocs.org/stc/SA04037CH): Installation of an Air Conditioning System, Kelly Aerospace kit #KATS-14-003. Installation Instructions as listed on NC-14 -022, revision D, dated November 19, 2015, and drawing list NC-14-021, revision D, dated September 24, 2015, or later FAA approved revision. Kelly Aerospace Thermal Systems LLC
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA04154AT](https://openairdocs.org/stc/SA04154AT): Installation of a PM Firesystems LLC, Fire Suppression System. PM Fire Systems LLC
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation
- [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC
- [STC SA03372NY](https://openairdocs.org/stc/SA03372NY): Installation of RF-006(A) main wheel well and RA-002(A) nose wheel well with EA-003.4N(B) brake system. Beringer Aero
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc
- [STC SA5156NM](https://openairdocs.org/stc/SA5156NM): Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System. AvTek
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc
- [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC

### Approved for the engine (Continental TSIO-550-K)

- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp

All 53: https://openairdocs.org/aircraft/N572CA/stcs.md

## Related

- Other Cirrus Design SR22T aircraft: https://openairdocs.org/model/cirrus-design-sr22t/aircraft.md
- The Continental TSIO-550-K engine: https://openairdocs.org/engine/continental-tsio-550-k.md

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