# N822RA: 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: 11214
- Year built: 2026
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 22, 2026
- Certificate issued: June 18, 2026
- Expires: June 30, 2033
- Mode S code: AB39C1
- Registered owner: [Ashworth Aviation LLC](https://openairdocs.org/faa-owner/ASHWORTH%20AVIATION%20LLC)
- Location: [Tampa, FL](https://openairdocs.org/faa-place/FL/Tampa)
- Owner type: LLC
- Owner's area on the map: 27.8913° N, 82.5057° W: Placed by OpenAirDocs at the center of ZIP code 33611, 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=822RA
- Page: https://openairdocs.org/aircraft/N822RA

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 N822RA.

## FAA accident and incident reports

None matched to N822RA.

## 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 N822RA not matched to an aircraft (40)

They name N822RA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR AALA016055](https://openairdocs.org/sdr/AALA016055), Jun 6, 2001: CONNECTOR. NOT SEATED. CCI-SNA - FOUND 15 DEF EMERGENCY LIGHTS INOPERATIVE. RESEATED CONNECTOR. OPS CHECK OK. (M)
- [SDR AALA016056](https://openairdocs.org/sdr/AALA016056), Jun 1, 2001: POWER SUPPLY. INOPERATIVE. CCI-LAX - EMERGENCY LIGHT IN TAIL CONE SECTION ON LEFT SIDE IS INOPERATIVE. REPLACED POWER SUPPLY AND LIGHTS. SECURED POWER SUPPLY, OPS CHECK OK. (M)
- [SDR AALA016046](https://openairdocs.org/sdr/AALA016046), Apr 26, 2001: BATTERY PACK. DEFECTIVE. CABIN EMERGENCY LIGHTS ON RIGHT SIDEWALL CAME ON IN FLIGHT. REPLACED EMERGENCY LIGHT POWER PACK AT AFT RIGHT EXIT DOOR. OPS CHECK GOOD. (M)
- [SDR AALA016042](https://openairdocs.org/sdr/AALA016042), Apr 8, 2001: WIRE. INOPERATIVE. EMERGENCY FLOOR LIGHTING SYSTEM BETWEEN ROWS 25-28 CAME ON UNCOMMANDED. BOTH PILOTS AND FA SWITCHES RECYCLED WITH NO AFFECT. FOUND LOOSE GROUND WIRE OF PLUG AT 
- [SDR AALA016002](https://openairdocs.org/sdr/AALA016002), Jan 9, 2001: CONNECTOR. DISCONNECTED. LAX - FOUND SEAT MOUNTED EMERGENCY LIGHT AT 15D INOPERATIVE. RECONNECTED ELECTRICAL PLUG AT SIDE WALL TO SEAT HARNESS. (M)
- [SDR AALA006157](https://openairdocs.org/sdr/AALA006157), Dec 25, 2000: WIRE. DAMAGED. CCI - THREE EMERGENCY LIGHTS INOPERATIVE IN TAIL. REPAIRED BROKEN WIRES, BATTERY PACK IN TAIL. (M)
- [SDR AALA006073](https://openairdocs.org/sdr/AALA006073), Apr 18, 2000: BATTERY PACK. INOPERATIVE. RNO-CCI - EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR EXTERIOR OVERWING EMERGENCY LIGHT CHECKED OK. (M)
- [SDR AALA006069](https://openairdocs.org/sdr/AALA006069), Apr 13, 2000: WIRE. BROKEN. RNO-CCI - EMERGENCY LIGHT IN TAIL CATWALK INOPERATIVE. REPAIRED BROKEN WIRE AT CHARGER. OPS CHECK GOOD. (M)
- [SDR AALA006067](https://openairdocs.org/sdr/AALA006067), Apr 1, 2000: BATTERY PACK. INOPERATIVE. LAX-CCI - FIRST CLASS EMERGENCY LIGHTS DIM TO TEST. REPLACED BATTERY PACK. (M)
- [SDR AALA006043](https://openairdocs.org/sdr/AALA006043), Mar 6, 2000: HARNESS. DAMAGED. RNO - FA REPORTS EMERGENCY LIGHTS ON ROWS 26, 27 AND 28 WITH SWITCH IN ARM. FOUND SHORTED WIRE. REPLACED BAD HARNESS AT ROW 25 DEF. SYSTEM OPS CHECKS GOOD. (M)
- [SDR AALA006040](https://openairdocs.org/sdr/AALA006040), Feb 25, 2000: BATTERY PACK. INOPERATIVE. LAX-CCI - INSEAT EMERGENCY LIGHTS IN SEATS 25 THROUGH 28 INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK NORMAL. (M)
- [SDR AALA006033](https://openairdocs.org/sdr/AALA006033), Feb 17, 2000: SLIDE. DISLODGED. RNO - AFT GALLEY EVAC SLIDE PACK FALLS OUT OF DOOR. REMOVED AND REPLACED AFT GALLEY SLIDE PER MM. (M)
- [SDR ORJA99251](https://openairdocs.org/sdr/ORJA99251), Aug 15, 1999: BATTERY CHARGER. INOPERATIVE. SJC - EMERGENCY PATH LIGHTS OUT IN ROWS 12, 14, 15 AND 17. CHANGED BATTERY PACK FOR EMERGENCY PATH LIGHTS. OPS CHECK GOOD. (M)
- [SDR ORJA99215](https://openairdocs.org/sdr/ORJA99215), Jul 2, 1999: BATTERY. DISCHARGED. RECHARGE LIGHTS ON FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS NOT BLINKING. REMOVED AND REPLACED BATTERY ASSY. ALL FLIGHT ATTENDANTS FLASHLIGHTS OPS CHECK OK. (X)
- [SDR ORJA99179](https://openairdocs.org/sdr/ORJA99179), May 25, 1999: ENGINE. FIRE. RNO - STARTED NR 1 ENGINE DURING PUSH BACK INFORMED BY GROUND NR 1 ENGINE ON FIRE, CUT FUEL AND IGNITION, MOTORED AND DISCHARGED NR 1 BOTTLE. INSPECTED ENGINE P
- [SDR ORJA98282](https://openairdocs.org/sdr/ORJA98282), Nov 6, 1998: POWER SUPPLY. INOPERATIVE. RNO - EXTERIOR LEFT AND RIGHT EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED OVERWING 'E' LIGHTS POWER SUPPLY, OPS CHECK GOOD. (M)
- [SDR ORJA98193](https://openairdocs.org/sdr/ORJA98193), Aug 13, 1998: OVERHEAT LOOP. MALFUNCTIONED. FROM RENO, AIR TURNBACK TO RENO, TAIL COMPT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF. STAYED ON FOR 3 MINUTES. WENT OUT ON FIRST POWER REDUCTION. RAN ENGINES NR 1 
- [SDR ORJA98188](https://openairdocs.org/sdr/ORJA98188), Aug 4, 1998: BATTERIES. DISCHARGED. RNO - O/H EMERGENCY LIGHTS INOP BETWEEN ROWS 18A-21AC, LEFT SIDE. REMOVED AND REPLACED BATTERIES, OPS CHECK OK. (M)
- [SDR ORJA98186](https://openairdocs.org/sdr/ORJA98186), Aug 3, 1998: BATTERY PACK. DISCHARGED. SJC - LEFT AND RIGHT AFT EMERGENCY EXI TLIGHTS INOP, UPPER. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK, OPS CHECK NORMAL. (M)
- [SDR ORJA98194](https://openairdocs.org/sdr/ORJA98194), Jul 27, 1998: DETECTOR. MALFUNCTIONED. RETURN TO RENO, TAIL COMPT TEMP HI LIGHT CAME ON FOR 2 MINUTES AFTER TAKEOFF. OPERATING WITH LEFT THROTTLE RETARDED FOR 2 MINUTES, LIGHT WENT OUT. RESTORED THRO
- [SDR ORJA98123](https://openairdocs.org/sdr/ORJA98123), Jun 25, 1998: DUCT. CRACKED. AIR TURN BACK DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON DURING CLIMB. COMPLIED WITH EMERGENCY PROCEDURES. COULD EXTINGUISH LIGHT WITH POWER REDUCTION ONLY
- [SDR ORJA9889](https://openairdocs.org/sdr/ORJA9889), May 5, 1998: FUEL CONTROL. MALFUNCTIONED. ENGINE SHUT DOWN DUE TO THE FACT THAT THE RIGHT ENIGNE WOULD NOT IDLE BELOW 68 PERCENT N2. ENTERED DMI NR 13546. (M)
- [SDR ORJA9861](https://openairdocs.org/sdr/ORJA9861), Mar 25, 1998: WINDSHIELD. FAILED. AIR RETURN TO LAS, CLIMBING THROUGH 12,000 MSL CENTER WINDSHIELD POPPED AND STARTED LEAKING AT SEAMS. REMOVED AND REPLACED WINDSHIELD IAW MM 56-10-01 PRESSURED 
- [SDR ORJA97163](https://openairdocs.org/sdr/ORJA97163), Sep 26, 1997: LIGHT. FAILED. EMERGENCY LIGHTS (4 TOTAL, 2 RED, AND 2 WHITE) DO NOT TEST AT SEATS 17-20 A/C RT. REMOVED AND REPLACED EMERGENCY AISLE PATH AFT RT EMERGENCY EXIT IAW MM. OPS CH
- [SDR ORJA97155](https://openairdocs.org/sdr/ORJA97155), Sep 21, 1997: POWER PACK. INOPERATIVE. PAX - EMERGENCY LIGHTS ROW 8 THROUGH 11 INOP. REMOVED AND REPLACED POWER PACK. OPS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR ORJA97125](https://openairdocs.org/sdr/ORJA97125), Jul 30, 1997: FUEL CONTROL. MALFUNCTIONED. NR 1 ENGINE SURGING PLUS OR MINUS .03 EPR (INDICATING ALL ENGINE PARAMETERS). F/A REPORTS UNUSUAL VIBRATIONS AND NOISES. BORESCOPED ENGINE PER MM 72-00-04, ALL 
- [SDR ORJA97124](https://openairdocs.org/sdr/ORJA97124), Jul 30, 1997: SENSE LINE. DIRTY. NR 1 ENGINE SURGING PLUS OR MINUS .03 EPR ON CLIMB-OUT. ENGINE ANTI-ICE, NO AFFECT. ENGINE STABILIZED AT 1.6 EPR, RETURNED TO GPT. CLEANED OUT FUEL CONTROL MOIS
- [SDR ORJA97108](https://openairdocs.org/sdr/ORJA97108), Jun 29, 1997: FUEL FLOW TRANS. FAILED. DURING TAKEOFF FLASHING EGT 500 DEGREES RIGHT ENGINE. DISCONTINUED TAKEOFF AT 80 KNOTS WHEN RT FUEL FLOW FLASHED AT 500 DEGREES CELSIUS. MAINTENANCE NOTED NO FU
- [SDR ORJA97122](https://openairdocs.org/sdr/ORJA97122), Jun 1, 1997: SEAT TRACK. CORRODED. SEAT TRACK NR X22L CORRODED FROM BS 1145 TO 1160. FABRICATED AND DRILLED PARTS, TREATED PRIMED AND PAINTED. INSTALLED IAW SRM'S 53-05, 51-10. (M)
- [SDR ORJA9744](https://openairdocs.org/sdr/ORJA9744), Apr 5, 1997: BATTERY. DISCHARGED. OVERHEAD EMEGENCY EXIT LIGHTS INOP ROW 27. REPLACED BATTERIES IN CHARGER, OPS NORMAL. (M)
- [SDR ORJA9699](https://openairdocs.org/sdr/ORJA9699), Nov 11, 1996: LOCK RING. CRACKED. FOUND C-1 BLADE LOCK RING BROKEN AT PULL HOLE APPROXIMATELY 2 INCHES FROM END. REPLACED C-1 BLADE LOCK RING. PART TOTAL CYCLES, 11,904. (X)
- [SDR ORJA9669](https://openairdocs.org/sdr/ORJA9669), Oct 12, 1996: BATTERY. DISCHARGED. AFT SECTION OF E-LIGHT FLOOR PATH INOP. REMOVED AND REPLACED APPLICABLE BATTERIES FOR AFT SECTION. E-PATH LIGHTING OPS CHECKS GOOD. (M)
- [SDR ORJA9628](https://openairdocs.org/sdr/ORJA9628), May 2, 1996: BATTERIES. DISCHARGED. CEILING EMERGENCY LIGHTS ROW 11-16 WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERIES FOR ROWS 11-16. OPS CHECK NORMAL. (M)
- [SDR ORJA96017](https://openairdocs.org/sdr/ORJA96017), Mar 18, 1996: BATTERIES. DISCHARGED. AFT GALLEY OVERHEAD EMERGENCY LIGHTS INOPERATIVE. INSTALLED NEW BATTERIES IN CHARGER. OPS CHECK NORMAL. (X)
- [SDR ORJA95138](https://openairdocs.org/sdr/ORJA95138), Dec 14, 1995: BOLT. BROKEN. NR 2 WHEEL THROUGH-BOLT SHEARED. REPLACED NR 4 WHEEL ASSY. (X)
- [SDR ORJA9552](https://openairdocs.org/sdr/ORJA9552), Jun 22, 1995: ENGINE. FAILED. IRW - RIGHT ENGINE OIL QUANTITY DECREASED TO 12 QUARTS. TEMPERATURE INCREASED TO 140 DEGREES. REMOVED AND REPLACED 'R' ENGINE PER MD-80 MM 71-00. OPS CHECK GOOD
- [SDR ORJA9550](https://openairdocs.org/sdr/ORJA9550), Jun 20, 1995: EEL BATTERY. DISCHARGED. AFT SECTION OF FLOOR TRACK INOP (EMERGENCY). INSTALLED NEW EMERGENCY FLOOR TRACK LIGHTING SUPPLY POWER PACK. OPS TESTS NORMAL. (X)
- [SDR ORJA9551](https://openairdocs.org/sdr/ORJA9551), Jun 17, 1995: EEL BATTERY. DISCHARGED. SECTION 15 THROUGH SECTION 20, RIGHT SIDE EMERGENCY FLOOR LIGHTS OUT. REPLACED POWER PACK BATTERY ON SECTION 15. OPS GOOD. (X)
- [SDR ORJA95001](https://openairdocs.org/sdr/ORJA95001), Jan 31, 1995: CONTROLLERS. MALFUNCTIONED. AT 26,000 FEET, NOTED CABIN ALTITUDE INCREASING, WHILE STILL CLIMBING TO ASSIGNED ALTITUDE. AIRCRAFT LEVELED AND DESCENT REQUESTED. RED CABIN LIGHT CAME ON AT 1
- [SDR ORJA95003](https://openairdocs.org/sdr/ORJA95003), Jan 17, 1995: EEL. INOPERATIVE. EMERGENCY FLOOR LIGHTS INOP AT 6 AND 7 DEF. REPLAMPED AND RESECURED FLOOR TRACK LIGHTING. OPS CHECK OKAY. (X)

## 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/N822RA/stcs.md

## Earlier aircraft with N822RA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N822RA before.

- [Cancelled 2017-10-03](https://openairdocs.org/deregistered/N822RA-2017-10-03): Cessna 172S, S/N 172S9727, built 2004. Exported to Canada. Owner: [Crossen Leasing LLC](https://openairdocs.org/faa-owner/CROSSEN%20LEASING%20LLC), [Aptos, CA](https://openairdocs.org/faa-place/CA/Aptos)

## 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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