# N53SH: 2021 Cirrus Design SR22

- Status: Valid registration
- Airframe: [Cirrus Design SR22](https://openairdocs.org/model/cirrus-design-sr22) (registry code 2130001, 4 seats)
- Engine: [Continental IO-550-N](https://openairdocs.org/engine/continental-io-550-n) (registry code 17215)
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) (Cirrus Design Corporation), [TCDS E3SO](https://openairdocs.org/tcds/E3SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 5008
- Year built: 2021
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 26, 2021
- Certificate issued: December 30, 2025
- Expires: December 31, 2032
- Mode S code: A6AFAC
- Registered owner: [James Robinson Homes LLC](https://openairdocs.org/faa-owner/JAMES%20ROBINSON%20HOMES%20LLC)
- Location: [Alpharetta, GA](https://openairdocs.org/faa-place/GA/Alpharetta)
- Owner type: LLC
- Owner's area on the map: 34.0257° N, 84.2473° W: Placed by OpenAirDocs at the center of ZIP code 30022, 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=53SH
- Page: https://openairdocs.org/aircraft/N53SH

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): 34 in force

### Matched by airframe (Cirrus Design SR22)

- [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 2009-26-01](https://openairdocs.org/ad/2009-26-01): Ice and Rain protection · Cirrus Design SR22. Effective Dec 21, 2009
- [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 2008-03-16](https://openairdocs.org/ad/2008-03-16): Rudder, aileron, and rudder-aileron interconnect rigging · Cirrus Design SR20 and SR22. Effective Mar 11, 2008
- [AD 2007-24-13](https://openairdocs.org/ad/2007-24-13): Install a drain hole in the left and right outboard wing tips · Cirrus Design SR22. Effective Dec 4, 2007
- [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 (Continental IO-550-N)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [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 2016-16-12](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 2014-05-29](https://openairdocs.org/ad/2014-05-29): SAP replacement parts manufacturer approval (PMA) investment cast cylinder assemblies · Continental Motors TSIO-520-A, TSIO-520-AE, TSIO-520-AF and 55 more. Effective Apr 25, 2014
- [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 2007-16-10](https://openairdocs.org/ad/2007-16-10): Kelly Aerospace Power Systems turbochargers · Turbonormalizing system (Engine Technologies STC SE10589SC or SA10588SC). Effective Aug 23, 2007
- [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 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993
- [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
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988

### 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
- [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
- [AD 2009-16-03](https://openairdocs.org/ad/2009-16-03) (historical): Cylinder assemblies · Continental Motors IO-520-A, IO-520-B, IO-520-BA and 55 more. Effective Sep 9, 2009
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

## Information bulletins (advisory) (28 in force)

- [SAIB AIR-21-05R1](https://openairdocs.org/saib/AIR-21-05R1): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [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 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-08-46](https://openairdocs.org/saib/CE-08-46): Powerplant Exhaust & Air Conditioning. Issued Sep 9, 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-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 NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-10-07](https://openairdocs.org/saib/NE-10-07): Reciprocating Engine Cylinder: Identification Information for Superior Air Parts, PMA Cylinder Heads for Teledyne Continental Motors (TCM) IO-520, TSIO-520,and IO-550 Series Engines.. Issued Nov 2, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002
- [SAIB AIR-21-05](https://openairdocs.org/saib/AIR-21-05) (historical): Engine Exhaust; Inlet check valves on turbochargers used in the Tornado Alley Turbo, Inc. turbonormalizing systems. Issued Mar 17, 2021
- [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
- [SAIB CE-08-12](https://openairdocs.org/saib/CE-08-12) (historical): Electrical Power. Issued Feb 27, 2008

## NTSB investigations

None matched to N53SH.

## FAA accident and incident reports

None matched to N53SH.

## 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 N53SH not matched to an aircraft (89, newest 50)

They name N53SH, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR KBM2006F00185](https://openairdocs.org/sdr/KBM2006F00185), May 6, 2006: BEARING. WORN. DAMPERS, BEARINGS ARE WORN, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00177](https://openairdocs.org/sdr/KBM2006F00177), Apr 27, 2006: TRANSMITTER. MALFUNCTIONED. ENGINE TRANSMITTER, DROP TO ZERO, OTHER GAUGES ARE NORMAL. REMOVED AND REPLACED WITH NEW. (K)
- [SDR KBM2006F00174](https://openairdocs.org/sdr/KBM2006F00174), Apr 27, 2006: RADIO. INOPERATIVE. VHT SIDE TONE EXCESSIVELY LOUD, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00193](https://openairdocs.org/sdr/KBM2006F00193), Apr 26, 2006: TRANSMITTER. READS LOW. ENGINE OIL TRANSMITTER, ENGINE OIL PRESSURE READS LOW, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00158](https://openairdocs.org/sdr/KBM2006F00158), Apr 18, 2006: ENTERTAIN SYS. DISTORTED. DMP PLAYER, UNIT SOUNDS DISTORTED, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00135](https://openairdocs.org/sdr/KBM2006F00135), Mar 14, 2006: STARTER GEN. INOPERATIVE. STARTER GENERATOR INOPERATIVE, MAKING NOISE DURING START. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00119](https://openairdocs.org/sdr/KBM2006F00119), Mar 13, 2006: METER. INOPERATIVE. HOBBS METER, INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00118](https://openairdocs.org/sdr/KBM2006F00118), Mar 13, 2006: PRESSURE SWITCH. INOPERATIVE. DIFF PRESSURE SWITCH, LOW AIR PRESSURE LIGHT FOR FDC FILTER CAME ON DURING HOVER, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00084](https://openairdocs.org/sdr/KBM2006F00084), Feb 4, 2006: TRANSMITTER. READS LOW. SUSPECTED TORQUE TRANSMITTER READS LOW, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00034](https://openairdocs.org/sdr/KBM2006F00034), Jan 3, 2006: BEARING. WORN. LAMINATED BEARINGS, BEARINGS ARE WORN. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00033](https://openairdocs.org/sdr/KBM2006F00033), Dec 4, 2005: SLEEVE. WORN. UNIT HAS WORN HOUSING SLEEVE. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00032](https://openairdocs.org/sdr/KBM2006F00032), Dec 4, 2005: SHUTOFF VALVE. INOPERATIVE. FUEL SHUTOFF VALVE INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00031](https://openairdocs.org/sdr/KBM2006F00031), Dec 4, 2005: BUSHING SLEEVE. WORN. UNIT HAS WORN BUSHING SLEEVE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00356](https://openairdocs.org/sdr/KBM2005F00356), Nov 27, 2005: TRANSMITTER. FAILED. ENGINE OIL GAUGE DROPS TO ZERO. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. (K)
- [SDR KBM2005F00355](https://openairdocs.org/sdr/KBM2005F00355), Nov 25, 2005: BATTERY. FAILED. SLOW START, REMOVED AND REPLACED BATTERY. (K)
- [SDR KBM2005F00354](https://openairdocs.org/sdr/KBM2005F00354), Nov 25, 2005: BATTERY. WEAK. BATTERY WEAK, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00353](https://openairdocs.org/sdr/KBM2005F00353), Nov 24, 2005: FCU. FAILED. SUSPECT HIGH SIDE FAILURE NTL GOVERNOR FUEL CONTROL UNIT. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00342](https://openairdocs.org/sdr/KBM2005F00342), Nov 12, 2005: GYRO. SPINNING. DIRECTIONAL GYRO, UNIT SPINS IN FLIGHT, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00318](https://openairdocs.org/sdr/KBM2005F00318), Oct 23, 2005: ICS BOX. INOPERATIVE. ICS BOX, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00317](https://openairdocs.org/sdr/KBM2005F00317), Oct 21, 2005: GYRO. INOPERATIVE. AG, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00251](https://openairdocs.org/sdr/KBM2005F00251), Aug 15, 2005: TRANSMITTER. INOPERATIVE. UNIT SHOWS NO INDICATION OF PRESSURE. REMOVED AND REPLACED ENG OIL TRANSMITTER. (M)
- [SDR KBM2005F00232](https://openairdocs.org/sdr/KBM2005F00232), Aug 14, 2005: INDICATOR. INOPERATIVE. NO ENGINE OIL PRESSURE INDICATION, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00231](https://openairdocs.org/sdr/KBM2005F00231), Jun 25, 2005: GYRO. MALFUNCTIONED. DIRECTIONAL GYRO FLAG GOES ON IN FLIGHT. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00139](https://openairdocs.org/sdr/KBM2005F00139), Jun 18, 2005: RADIO. INOPERATIVE. VHF FM, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00102](https://openairdocs.org/sdr/KBM2005F00102), Jun 6, 2005: CARGO HOOK. FAILED. CARGO HOOK WILL NOT HOLD LOAD. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00103](https://openairdocs.org/sdr/KBM2005F00103), May 30, 2005: BALL JOINT. WORN. BALL JOINTS, BOTH WORN, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00230](https://openairdocs.org/sdr/KBM2005F00230), May 5, 2005: INTAKE. CRACKED. ARRIEL ENGINE INTAKE HAS MULTIPLE CRACKS, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00227](https://openairdocs.org/sdr/KBM2005F00227), May 5, 2005: BALL JOINT. FAILED. BALL JOINTS, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00226](https://openairdocs.org/sdr/KBM2005F00226), May 5, 2005: SKID SHOE. CRACKED. RT FWD SKID SHOE CRACKED, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00081](https://openairdocs.org/sdr/KBM2005F00081), May 3, 2005: OIL TANK. CRACKED. OIL TANK, PORT NECK CRACKED. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00211](https://openairdocs.org/sdr/KBM2005F00211), Apr 23, 2005: WIRE. BROKEN. OIL TEMP PROBE TERMINAL BROKEN. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00210](https://openairdocs.org/sdr/KBM2005F00210), Apr 16, 2005: CROSSBEAM. ROTATED. CROSSBEAM ROTATING, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00209](https://openairdocs.org/sdr/KBM2005F00209), Apr 16, 2005: BEARING. ROTATED. LAMINATED BEARINGS ARE ROTATING, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00208](https://openairdocs.org/sdr/KBM2005F00208), Apr 16, 2005: BEARING. WORN. HALF SHELL LAMINATED BEARINGS, WORN BEYOND LIMITS. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00042](https://openairdocs.org/sdr/KBM2005F00042), Mar 12, 2005: TRANSMITTER. INOPERATIVE. OIL TRANSMITTER, ENGINE OIL PRESSURE INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00037](https://openairdocs.org/sdr/KBM2005F00037), Mar 5, 2005: BEARING. CUT. BEARING HAS MULTIPLE CUTS AROUND THE RUBBER. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00004](https://openairdocs.org/sdr/KBM2005F00004), Dec 4, 2004: BEARING. WORN. HALF SHELLS WORN, REMOVED AND REPLACED.(K)
- [SDR KBM2005F00005](https://openairdocs.org/sdr/KBM2005F00005), Dec 1, 2004: TRANSDUCER. FAILED. TRANSDUCER, NO INDACATED OIL PRESSURE AT START-UP. REMOVED AND REPLACED. (K)
- [SDR KBM2004F00240](https://openairdocs.org/sdr/KBM2004F00240), Sep 22, 2004: CONTROL CABLE. BINDING. PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW.
- [SDR KBM2004F00231](https://openairdocs.org/sdr/KBM2004F00231), Sep 22, 2004: CABLE. BINDING. PILOT REPORTS BINDING T/R PEDALS. REMOVED AND REPLACED T/R FLEX CABLE WITH NEW.
- [SDR KBM2005F00013](https://openairdocs.org/sdr/KBM2005F00013), Jul 22, 2004: GYRO. MALFUNCTIONED. DG, WILL NOT HOLD HEADING, REMOVED AND REPLACED. (K)
- [SDR KBM2004F00168](https://openairdocs.org/sdr/KBM2004F00168), Jul 22, 2004: GAUGE. READS LOW. OIL PRESSURE GAUGE READS LOW. REPLACED CLUSTER GAUGE WITH REPAIRED UNIT.
- [SDR KBM2004F00167](https://openairdocs.org/sdr/KBM2004F00167), May 16, 2004: GYRO. INOPERATIVE. DIRECTIONAL GYRO, WOULD NOT HOLD HEADING. REMOVED AND REPLACED.
- [SDR KBM2004F00166](https://openairdocs.org/sdr/KBM2004F00166), May 16, 2004: GAUGE. INOPERATIVE. FUEL AND ENGINE OIL PRESSURES READ ZERO IN FLIGHT. REMOVED AND REPLACED.
- [SDR KBM2004F00078](https://openairdocs.org/sdr/KBM2004F00078), May 14, 2004: MOUNT. CRACKED. RT FWD ENGINE COWLING SUPPORT LEG CRACKED AT MGB DECK HWD IAW STANDARD PRACTICES. REPAIRED RT ENGINE SUPPORT LEG W/STAINLESS STEEL BRACKET DOUBLER W/ EXISTING.
- [SDR KBM2004F00075](https://openairdocs.org/sdr/KBM2004F00075), May 1, 2004: DRAIN VALVE. FAILED. ENGINE WILL NOT START. NO RISE ON T4. REMOVED AND REPLACED.
- [SDR KBM2005F00014](https://openairdocs.org/sdr/KBM2005F00014), Apr 14, 2004: INDICATOR. INTERMITTENT. ATTITUDE INDICATOR, WILL NOT HOLD ATT, REMOVED AND REPLACED. (K)
- [SDR KBM2004F00104](https://openairdocs.org/sdr/KBM2004F00104), Apr 14, 2004: INDICATOR. INOPERATIVE. INDICATOR WILL NOT HOLD ATTITUDE. REMOVED AND REPLACED.
- [SDR KBM2004F00077](https://openairdocs.org/sdr/KBM2004F00077), Apr 6, 2004: MOTOR. SHORTED. OIL COOLER MOTOR HAS AN INTERNAL SHORT. REMOVED AND REPLACED.
- [SDR KBM2005F00035](https://openairdocs.org/sdr/KBM2005F00035), Feb 9, 2004: POWER SUPPLY. BURNED OUT. SMOKED POWER SUPPLY INTERNAL INPUT, REMOVED AND REPLACED. (K)

All 89: https://openairdocs.org/aircraft/N53SH/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (147, 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 SR22)

- [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 SA12273IB](https://openairdocs.org/stc/SA12273IB): Installation of the MT-Propeller Entwicklung GmbH MTV-9-D/198-52() propeller. 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 SA12027IB](https://openairdocs.org/stc/SA12027IB): Installation of the MT-Propeller Entwicklung GmbH MTV-14-D/195-30() propeller. MT-Propeller Entwicklung GmbH
- [STC SA02558CH](https://openairdocs.org/stc/SA02558CH): Installation of a L-3 Communications Avionics Systems SmartDeck Flight Guidance and Display System. Acron Aviation Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [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 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 SA10532SC](https://openairdocs.org/stc/SA10532SC): Installation of XM Satellite Radio Wireless equipment. Heads Up Technologies Inc
- [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 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 SA04468CH](https://openairdocs.org/stc/SA04468CH): Installation of Hartzell Propeller model 4C1-F650A1/76C04-0.6 or 4C1-F650A1/76C04B-0.6 i. Hartzell Propeller 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 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 SA10195SC](https://openairdocs.org/stc/SA10195SC): Installation of an engine driven vapor cycle air conditioning system. Air Comm 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

All 147: https://openairdocs.org/aircraft/N53SH/stcs.md

## Related

- Other Cirrus Design SR22 aircraft: https://openairdocs.org/model/cirrus-design-sr22/aircraft.md
- The Continental IO-550-N engine: https://openairdocs.org/engine/continental-io-550-n.md

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