# N653CA: 2026 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: 11226
- Year built: 2026
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 14, 2026
- Certificate issued: April 24, 2026
- Expires: April 30, 2033
- Mode S code: A89812
- Registered owner: [Aviation Insurance Managers Inc](https://openairdocs.org/faa-owner/AVIATION%20INSURANCE%20MANAGERS%20INC)
- Location: [Uniontown, OH](https://openairdocs.org/faa-place/OH/Uniontown)
- Owner type: Corporation
- Owner's area on the map: 40.9554° N, 81.4244° W: Placed by OpenAirDocs at the center of ZIP code 44685, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=653CA
- Page: https://openairdocs.org/aircraft/N653CA

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 N653CA.

## FAA accident and incident reports

None matched to N653CA.

## Reports on N653CA not matched to an aircraft (1)

They name N653CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20060908021049I](https://openairdocs.org/incident/20060908021049I), Sep 8, 2006: Cndair CL6002C10 (N653CA), Covington/Cinci, KY. (-23) Flight attendant reported smoke in the cabin during taxi. Aircraft was stopped, main cabin door opened. Fire/rescue was called and inspected the aircraft…

## 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 N653CA not matched to an aircraft (124, newest 50)

They name N653CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR N6WA2020100102](https://openairdocs.org/sdr/N6WA2020100102), Oct 1, 2020: CHANNEL. CORRODED. PAX DOOR FWD LOWER LATCH 'C' CHANNEL IS CORRODED. REMOVED AND REPLACED PAX DOOR FORWARD C CHANNEL, IAW CRJ700 SRM 51-40-00 AND REO 670-52-11-1167.
- [SDR N6WA2020100101](https://openairdocs.org/sdr/N6WA2020100101), Oct 1, 2020: CHANNEL. CORRODED. PAX DOOR FWD LOWER LATCH 'C' CHANNEL IS CORRODED. REMOVED AND REPLACED PAX DOOR FORWARD C CHANNEL, IAW CRJ700 SRM 51-40-00 AND REO 670-52-11-1167.
- [SDR N6WA2018072701](https://openairdocs.org/sdr/N6WA2018072701), Jul 27, 2018: WARNING SYSTEM. FALSE ACTIVATION. LT EMERGENCY DOOR CAUTION MESSAGE. PERFORMED OPS CHECK OF THE OVERWING EMERGENCY EXIT INDICATION SYS IAW AMM 52-21-00. NO MESSAGES NOTED AT THIS.
- [SDR N6WA201807131001](https://openairdocs.org/sdr/N6WA201807131001), Jul 10, 2018: WARNING SYSTEM. FALSE ACTIVATION. LEFT EMERG DOOR CAUTION MSG. PERFORMED OPS CHECK OF LEFT EMERGENCY DOOR PER AMM 52-21-00, OPS CHECK GOOD VERIFIED GREEN INDICATED ON EICAS AND VISUALLY AT DOOR 
- [SDR N6WA2018061801](https://openairdocs.org/sdr/N6WA2018061801), Jun 18, 2018: WARNING MESSAGE. ILLUMINATED. LEFT EMERGENCY EXIT CAUTION MESSAGE.
- [SDR N6WA2018030901](https://openairdocs.org/sdr/N6WA2018030901), Mar 9, 2018: WARNING MESSAGE. FALSE ACTIVATION. LEFT EMERGENCY EXIT DOOR CAUTION MESSAGE. PERFORMED AN OPS TEST OF THE EMERGENCY EXIT DOOR IAW AMM 52-21-00, NO ABNORMAL MESSAGES NOTED.
- [SDR V0XD20170921006](https://openairdocs.org/sdr/V0XD20170921006), Sep 21, 2017: STRINGER. CORRODED. STRINGER 26L CORRODED BETWEEN BS 250 AND 265. PERFORMED A STRINGER SPLICE REPAIR IAW SRM 53-00-03, 51-25-16, 51-21-11, 51-42-06, 51-42-21, 51-40-11, 51-25-06, A
- [SDR V0XD20170921005](https://openairdocs.org/sdr/V0XD20170921005), Sep 21, 2017: STRINGER. CORRODED. STRINGER 26R CORRODED BETWEEN BS 250 AND 265. PERFORMED A SPLICE REPAIR IAW SRM 53-00-03, 51-40-11, 51-25-06, 51-21-11, 51-42-21, 51-25-16, 51-42-06 AND NDTM PA
- [SDR V0XD20170921004](https://openairdocs.org/sdr/V0XD20170921004), Sep 21, 2017: FITTING. CORRODED. FORWARD NOSE JACK FITTING HAS SIGNS OF CORROSION IN SEVERAL LOCATIONS. REPLACED THEJACK FITTING IAW SRM 51-21-11, 51-25-16, 51-40-11, 51-42-21, AND 51-42-06.
- [SDR V0XD20170921003](https://openairdocs.org/sdr/V0XD20170921003), Sep 21, 2017: FITTING. CORRODED. FORWARD NOSE JACK FITTING HAS SIGNS OF CORROSION IN SEVERAL LOCATIONS. REPLACED THE JACK FITTING IAW SRM 51-21-11, 51-25-16, 51-40-11, 51-42-21, AND 51-42-06.
- [SDR V0XD20170921002](https://openairdocs.org/sdr/V0XD20170921002), Sep 21, 2017: STRINGER. CORRODED. STRINGER 25R CORRODED IN SEVERAL PLACES BETWEEN BS 295 AND 349. REPLACED THE STRINGER IAW SRM 51-42-20, 51-42-06, 51-40-11, 51-42-00, 51-26-16, AND 51-21-11.
- [SDR V0XD20170921001](https://openairdocs.org/sdr/V0XD20170921001), Sep 21, 2017: SKIN SPLICE. CORRODED. SKIN SPLICE AT BS 280 TO 282.86 HAS SIGNS OF CORROSION BETWEEN STRINGERS 25 AND 27R. REPAIRED IAW REO 670-53-21-1446, REV -, SRM 51-25-16, 51-21-11, AND 51-25-0
- [SDR V0XD20170918001](https://openairdocs.org/sdr/V0XD20170918001), Sep 18, 2017: INTERCOSTAL. CORRODED. INTERCOSTAL BETWEEN BS 333 - 349, STRINGER 20R, FOUND CORRODED OUT OF LIMITS. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, 51-21-11, 51-25-06, 51-40-11, 51-25-16,
- [SDR V0XD2017092002](https://openairdocs.org/sdr/V0XD2017092002), Sep 14, 2017: STOP FITTING. CRACKED. PAX DOOR SURROUND FWD TOP STOP IS CRACKED. REMOVED AND REPLACED PAX DOOR SURROUND FWD TOP STOP IAW SRM 51-42-21, 51-25-16.
- [SDR V0XD20170913003](https://openairdocs.org/sdr/V0XD20170913003), Sep 13, 2017: ANGLE. CORRODED. PASSENGER DOOR KICK ANGLE AND MID CAP ANGLE HAVE SIGNS OF CORROSION. EVALUATED AND FOUND DAMAGE TO BE OUT OF LIMITS. REPLACED KICK ANGLE AND MID CAP IAW SRM 51-
- [SDR V0XD20170913001](https://openairdocs.org/sdr/V0XD20170913001), Sep 13, 2017: FRAME. CORRODED. FRAME BS 517 BETWEEN STRINGERS 26L AND 27L IS CORRODED. REPAIRED THE FRAME IAW REO 670-53-31-419.
- [SDR V0XD20170914004](https://openairdocs.org/sdr/V0XD20170914004), Sep 12, 2017: STRINGER. CORRODED. STRINGER 21R CORRODED OUT OF LIMITS AT BS 349. REPLACED THE STRINGER IAW SRM 53-21-03, 51-42-06, 51-21-00, 51-25-06, 51-25-16, 51-42-13, 51-42-21, AND 51-21-11.
- [SDR V0XD20170914002](https://openairdocs.org/sdr/V0XD20170914002), Sep 12, 2017: DOOR SILL. CORRODED. RT FLOOR SILL CORRODED OUT OF LIMITS AT FS 282. REPLACED RT FLOOR SILL IAW SRM 53-00-45 TR53-0080/51-42-13/51-42-06/51-40-11/51-21-11/51-25-16.
- [SDR V0XD20170914001](https://openairdocs.org/sdr/V0XD20170914001), Sep 12, 2017: INTERCOSTAL. CORRODED. INTERCOSTAL BETWEEN FS 310 - 319.70 AT STRINGER 20R CORRODED OUT OF LIMITS. REPLACED INTERCOSTAL IAW SRM 51-42-06/51-42-21/51-21-11/51-25-16.
- [SDR V0XD20170913002](https://openairdocs.org/sdr/V0XD20170913002), Sep 7, 2017: DRAG ANGLE. CRACKED. PASSENGER DOOR AFT DRAG ANGLE IS CRACKED HALF WAY. REMOVED AND REPLACED THE DRAG ANGLE IAW SRM 51-42-13, AND 51-42-06.
- [SDR V0XD20170906007](https://openairdocs.org/sdr/V0XD20170906007), Sep 6, 2017: ANGLE. CORRODED. AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE AT BS 939, HAS A CORRODED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-25-21, 51-42-06, AND 51-42-11.
- [SDR V0XD20170906006](https://openairdocs.org/sdr/V0XD20170906006), Sep 6, 2017: FLOORBEAM. CRACKED. RIGHT BS 280 FLOORBEAM IS CRACKED. REMOVED AND REPLACED THE FLOORBEAM IAW 53-11-41, 51-25-06, 51-25-16, 51-21-11, 51-42-13, 51-42-06, 51-42-20, NDTM PART 1 51-2
- [SDR V0XD201709050005](https://openairdocs.org/sdr/V0XD201709050005), Sep 3, 2017: DRAG ANGLE. CRACKED. VERTICAL STABILIZER LT SIDE AFT DRAG ANGLE IS CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-55-31-018, REV A DATED 10 NOV 201
- [SDR V0XD20170901007](https://openairdocs.org/sdr/V0XD20170901007), Sep 1, 2017: BRACKET. CRACKED. RIGHT WING SLAT TRACK HOUSING BRACKET CRACKED. REMOVED THE DAMAGED BRACKET, FABRICATED AND INSTALLED A REPAIR IAW REO 670-57-42-577, SRM 51-25-34, 51-21-11, 51-
- [SDR V0XD20170925001](https://openairdocs.org/sdr/V0XD20170925001), Aug 31, 2017: STRINGER. CORRODED. AVIONICS BAY STRINGER 25R, BS 333 TO 349 SHOWING SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-25-06, 51-25-21, 51-42-20, 51-42-06, AND 51-40
- [SDR V0XD201709030001](https://openairdocs.org/sdr/V0XD201709030001), Aug 31, 2017: SEAT TRACK. CORRODED. RIGHT SIDE SEAT TRACK FROM BS 785.15 - 847 HAS CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK 
- [SDR V0XD20170830005](https://openairdocs.org/sdr/V0XD20170830005), Aug 30, 2017: SEAT TRACK. CORRODED. LEFT SEAT TRACK FROM BS 677 TO 708 HAS SIGNS OF CORROSION. EVALUATED SEAT RAIL AND FOUND CORROSION TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVED AND
- [SDR V0XD20170830004](https://openairdocs.org/sdr/V0XD20170830004), Aug 30, 2017: SLAT TRACK. CRACKED. LEFT WING SLAT TRACK (1-3) HOUSING BRACKET CRACKED. REPAIRED IAW REO 670-57-42-577.
- [SDR V0XD20170830003](https://openairdocs.org/sdr/V0XD20170830003), Aug 30, 2017: SEAT TRACK. CORRODED. RIGHT SEAT TRACK FROM BS 677 - 708 HAS SIGNS OF CORROSION. EVALUATED THE SEAT TRACK AND FOUND CORROSION TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REMOVE
- [SDR V0XD2017090701](https://openairdocs.org/sdr/V0XD2017090701), Aug 29, 2017: BRACKET. CRACKED. FORWARD BAG BAY RESTRAINT NET BRACKET AT FS 581 IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-11, 51-42-21, 51-42-06.
- [SDR V0XD201709030004](https://openairdocs.org/sdr/V0XD201709030004), Aug 29, 2017: SEAT TRACK. CORRODED. RIGHT SIDE SEAT TRACK FROM BS 501 - 565 HAS SIGNS OF CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT 
- [SDR V0XD201709030003](https://openairdocs.org/sdr/V0XD201709030003), Aug 29, 2017: SEAT TRACK. CORRODED. LEFT SIDE SEAT TRACK FROM BS 581 - 677 HAS CORROSION. BLENDED THE AREA, AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRACK IAW 
- [SDR V0XD201709030002](https://openairdocs.org/sdr/V0XD201709030002), Aug 29, 2017: SEAT TRACK. CORRODED. LEFT SIDE SEAT TRACK FROM BS 708 - 761.85 HAS SIGNS OF CORROSION. BLENDED THE AREA, AND FOUND OUT OF LIMITS IAW REO 670-53-00-013, REV J. REPLACED THE SEAT TRAC
- [SDR V0XD2017090702](https://openairdocs.org/sdr/V0XD2017090702), Aug 28, 2017: SKIN. CORRODED. FS 501-FS 523 BETWEEN STRINGERS 26L AND 26R EXTERNAL FUSELAGE SKIN IS CORRODED. REPAIRED FS 501-FS 523 BETWEEN STRINGERS 26L AND 26R EXTERNAL FUSELAGE SKIN IAW 
- [SDR V0XD2017083006](https://openairdocs.org/sdr/V0XD2017083006), Aug 24, 2017: SEAT TRACK. CORRODED. RT SIDE SEAT RAIL FROM FS 708-FS 761.85 HAS MULTIPLE SIGNS OF CORROSION. REMOVED AND REPLACED RT SIDE SEAT RAIL FROM FS 708-FS 761.85 IAW AMM 53-00-49.
- [SDR V0XD2017082901](https://openairdocs.org/sdr/V0XD2017082901), Aug 24, 2017: SEAT TRACK. CORRODED. RT FLOOR SEAT RAIL FROM FS 581-677 HAS SIGNS OF CORROSION. REMOVED AND REPLACED RT FLOOR SEAT TRACK RAIL AT FS 581-677 IAW AMM 53-00-49.
- [SDR N6WA2017041501](https://openairdocs.org/sdr/N6WA2017041501), Apr 15, 2017: WARNING MESSAGE. FALSE ACTIVATION. LEFT EMERGENCY DOOR CAUTION MESSAGE AFTER LANDING. PERFORMED AN OPS TEST OF THE LEFT OVERWING EMERGENCY DOOR IAW AMM 52-21-00. OK FOR SERVICE, NO FAULTS FOUND.
- [SDR N6WA201612051001](https://openairdocs.org/sdr/N6WA201612051001), Dec 5, 2016: SEAL. DIRTY. WATER COMING THROUGH FLT DECK ESCAPE HATCH. CLEANED THE SEAL IAW AMM 52-22-00.
- [SDR N6WA2016100701](https://openairdocs.org/sdr/N6WA2016100701), Oct 7, 2016: ENGINE. FAILED. RIGHT ENGINE FAILED. R & R THE NR 2 ENGINE IAW AMM 71-00-00. OPS AND LEAK CHECKED GOOD.
- [SDR N6WA2016072602](https://openairdocs.org/sdr/N6WA2016072602), Jul 26, 2016: WARNING MESSAGE. ILLUMINATED. PAX DOOR LATCH CAUTION MESSAGE.
- [SDR N6WA2016F00053](https://openairdocs.org/sdr/N6WA2016F00053), Feb 3, 2016: FLOOR SUPPORT. CORRODED. SIDE FLOOR SUPPORT CORRODED BETWEEN FS 1000-1015 AT RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 01-27-2016 .
- [SDR N6WA2016F00052](https://openairdocs.org/sdr/N6WA2016F00052), Feb 3, 2016: FLOOR SUPPORT. CORRODED. SIDE BEAM CORRODED BETWEEN FS 1015-1031 AT RBL 42. R & R IAW SRM 51-42-06-001-001-A01 AND REO 670-53-61-1205, REV DATED 01-27-2016 .
- [SDR N6WA2016F00051](https://openairdocs.org/sdr/N6WA2016F00051), Feb 3, 2016: FLOORBEAM. CORRODED. FS 1015 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 1-27-2016.
- [SDR N6WA2016F00050](https://openairdocs.org/sdr/N6WA2016F00050), Feb 3, 2016: FLOORBEAM. CORRODED. FS 1031 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO 670-53-61-1205, REV DATED 1-27-2016.
- [SDR N6WA2016F00048](https://openairdocs.org/sdr/N6WA2016F00048), Feb 3, 2016: FLOORBEAM. CORRODED. FS 1051 FLOORBEAM CORRODED RBL 42. REPAIRED IAW REO670-53-61-1205 REV, DATED 1-27-2016.
- [SDR N6WA2016F00047](https://openairdocs.org/sdr/N6WA2016F00047), Feb 3, 2016: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BETWEEN FS 1000-1015 AT LBL 9. REPAIRED IAW REO670-53-61-1205, REV DATED 1-27-2016.
- [SDR N6WA2016F00046](https://openairdocs.org/sdr/N6WA2016F00046), Feb 3, 2016: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BETWEEN BS 1031-1051 AT RBL 9. REPAIRED IAW REO 670-53-61-1203, REV DATED 1-23-2016.
- [SDR N6WA2015080601](https://openairdocs.org/sdr/N6WA2015080601), Aug 6, 2015: DOOR SEAL. DIRTY. MAIN CABIN DOOR SQUEALS IN FLIGHT. CLEANED & LUBED MAIN CABIN DOOR SEAL IAW AMM 12-20-52.
- [SDR N6WA2015050702](https://openairdocs.org/sdr/N6WA2015050702), May 7, 2015: HAND RAIL. LOOSE. BOTH HAND RAILS ON THE PAX DOOR LOOSE. R & R BOTH HANDRAILS ON PAX DOOR IAW AMM 52-11-05. OPERATIONS CHECKED GOOD.
- [SDR V0XD20150303083](https://openairdocs.org/sdr/V0XD20150303083), Mar 3, 2015: STRINGER. CORRODED. MAIN AVIONICS BAY STRINGER 27R BETWEEN FS 295.0 & 310.0 HAS CORROSION. CUT OUT & SPLICED IN NEW STRINGER 26R BETWEEN FS 295.0 & 310.0 IAW REO 670-53-21-1162, DA

All 124: https://openairdocs.org/aircraft/N653CA/unmatched-reports.md

## 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/N653CA/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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