# N320CA: 2014 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: 0822 - Year built: 2014 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: July 15, 2014 - Certificate issued: April 25, 2019 - Expires: April 30, 2029 - Mode S code: A36E83 - Registered owner: [Armstrong Resource Management Corp](https://openairdocs.org/faa-owner/ARMSTRONG%20RESOURCE%20MANAGEMENT%20CORP) - Location: [Knoxville, TN](https://openairdocs.org/faa-place/TN/Knoxville) - Owner type: Corporation - Owner's area on the map: 35.8605° N, 84.1005° W: Placed by OpenAirDocs at the center of ZIP code 37922, 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=320CA - Page: https://openairdocs.org/aircraft/N320CA 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 (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 ERA23LA145](https://openairdocs.org/ntsb/ERA23LA145), Mar 7, 2023: Cirrus Design SR22T (N320CA), Knoxville, TN, substantial damage. Probable cause: The pilot's failure to maintain directional control during the takeoff roll where a gusting and shifting crosswind prevailed. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20230307001339A](https://openairdocs.org/incident/20230307001339A), Mar 7, 2023: Cirrus Design Corp SR22T (N320CA), Knoxville, TN, Substantial damage. Pilot was taking off on runway 8 of Knoxville Downtown airport (dkx). As the aircraft began to lift off the runway the pilot felt the aircraft push left and… ## 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 N320CA not matched to an aircraft (24) They name N320CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR COMA9630152](https://openairdocs.org/sdr/COMA9630152), Oct 9, 1996: FITTING. CHAFED. 7-YEAR THRESHOLD, 4-YEAR INTERVAL CHECK. TASK 191-01I, UPPER ATTACH FITTING FOR LEFT WING AFT SPAR TO FUSELAGE FITTING HAS A DEEP GOUGE. C/W NDT INSPECION, BLEN - [SDR COMA9630151](https://openairdocs.org/sdr/COMA9630151), Oct 9, 1996: FLOORBOARD. CORRODED. C1 INSPECTION TASK 117/118-01I. CORROSION UNDER FLOORBOARDS ON RT SIDE OF COCKPIT THRESHOLD UNDER GALLEY AREA. REMOVED CORROSION, CLEANED, PRIMED, AND RESTORED - [SDR COMA9630126](https://openairdocs.org/sdr/COMA9630126), Jun 17, 1996: TRANSDUCER. MALFUNCTION. LEFT ENGINE LOW OIL PRESSURE WARNING SOUNDED DURING CLIMB. REPLACED THE LT ENGINE OIL PRESSURE TRANSDUCER. - [SDR COMA9630125](https://openairdocs.org/sdr/COMA9630125), Jun 11, 1996: OIL SYST. REQD SERVICE. LEFT ENGINE LOW OIL PRESSURE WARNING DURING FLIGHT. INSPECTED ENGINE FOR LEAKS AND FOUND NONE, ADDED 2 QUARTS OIL AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9630095](https://openairdocs.org/sdr/COMA9630095), Mar 31, 1996: WARMING POT. DEFECTIVE. BURNING ODOR NOTICED AT GALLEY AREA. REPLACED COFFEE WARMING POT. - [SDR COMA9630061](https://openairdocs.org/sdr/COMA9630061), Mar 9, 1996: FIRE EXT. CORRODED. CABIN FIRE EXTINGUISHER HANDLE IS HARD TO ROTATE. CLEANED AND REASSEMBLED FIRE EXTINGUISHER AND RETURNED TO SERVICE. PART TOTAL CYCLES, 22,156. - [SDR COMA9630041](https://openairdocs.org/sdr/COMA9630041), Feb 20, 1996: COMPUTER. FAILED. COPILOTS ATTITUDE AND HEADING RED FLAGGED. CIRCUIT BREAKER TRIPPED. REPLACED THE AHC-85 COMPUTER. - [SDR COMA9630031](https://openairdocs.org/sdr/COMA9630031), Feb 6, 1996: WHEEL. DEPARTED. GRINDING NOISE COMING FROM NLG DURING TAKEOFF, LANDING, AND TAXI. THE RT NLG WHEEL ASSY DEPARTED AIRCRAFT DURING LANDING. PROBABLE CAUSE WAS BEARING FAILURE. RE - [SDR COMA9630020](https://openairdocs.org/sdr/COMA9630020), Jan 19, 1996: HYD TUBE. LEAKING. HYDRAULIC FLUID LEAKING FROM RT WHEEL WELL. REPLACED LEAKING BRAKE LINE WHICH WAS CHAFED THROUGH BY WOW HARNESS WIRING. - [SDR COMA9630009](https://openairdocs.org/sdr/COMA9630009), Jan 6, 1996: POWER SUPPLY. DEFECTIVE. EMERGENCY POWER WARNING LIGHT CAME ON. REPLACED THE EMERGENCY POWER SUPPLY. - [SDR COMA9630006](https://openairdocs.org/sdr/COMA9630006), Jan 5, 1996: RETRACT MECH. ICED UP. LANDING GEAR DID NOT RETRACT FULLY, GEAR CYCLED TWICE WITH SAME RESULT. DE-ICED LANDING GEAR AND RETRACTION CHECK NORMAL. - [SDR COMA9531180](https://openairdocs.org/sdr/COMA9531180), Oct 29, 1995: POS TRANSMITTER. DEFECTIVE. UNCOMMANDED MOVEMENT OF FLAPS DURING FLIGHT. REPLACED THE LT AND RT FLAP POSITION TRANSMITTER. - [SDR COMA9531174](https://openairdocs.org/sdr/COMA9531174), Oct 24, 1995: GCU. DEFECTIVE. THE LEFT ENGINE WILL NOT ROTATE DURING START CYCLE. REPLACED THE LEFT DC GENERATOR CONTROL UNIT. - [SDR COMA9531171](https://openairdocs.org/sdr/COMA9531171), Oct 9, 1995: CONTROLLER. DEFECTIVE. FLAP DISAGREEMENT INDICATOR FLASHES WITH EACH FLAP POSITION SELECTION. REPLACED THE FLAP CONTROL UNIT. - [SDR COMA9531165](https://openairdocs.org/sdr/COMA9531165), Sep 26, 1995: GOVERNOR. DEFECTIVE. LT PROPELLER RPM DROPS TO 1370 DURING FINAL APPROACH. REPLACED THE PROPELLER OVERSPEED GOVERNOR. - [SDR COMA9531163](https://openairdocs.org/sdr/COMA9531163), Sep 22, 1995: EEL BATTERY PACK. DISCHARGED. FLOOR PROXIMITY EMERGENCY LIGHTING AT ROW 5 IS INOP. REPLACED EMERGENCY LIGHTING BATTERY PACK. - [SDR COM31140](https://openairdocs.org/sdr/COM31140), Aug 22, 1995: CONTROL CABLE. BROKEN. RIGHT INBOARD MAIN GEAR DOOR WOULD NOT RETRACT AFTER GEAR EXTENSION. ACTION: FOUND RELEASE CABLE ON TELESCOPING ROD, BROKEN, REPLACED CABLE WITH SERVICEABLE UNI - [SDR COM31125](https://openairdocs.org/sdr/COM31125), Jul 28, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM - [SDR COM31087](https://openairdocs.org/sdr/COM31087), May 23, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND S - [SDR COM31080](https://openairdocs.org/sdr/COM31080), May 16, 1995: INLET. CHIPPED. LEFT ENGINE INTAKE, ANTI-ICE COATING IS DAMAGED. REPLACED INLET. - [SDR COM31059](https://openairdocs.org/sdr/COM31059), Apr 11, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. - [SDR COM31058](https://openairdocs.org/sdr/COM31058), Apr 11, 1995: INNER RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND S - [SDR COM31031](https://openairdocs.org/sdr/COM31031), Feb 6, 1995: BEARING RACE. SPUN. MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL SUB-ASSY HAS BEEN REMOVED FROM SERVICE AND SENT - [SDR COM31028](https://openairdocs.org/sdr/COM31028), Feb 6, 1995: PDU. DEFECTIVE. EMERGENCY BUS IS ACTIVATED WHEN ALL POWER IS OFF. REPLACED THE LT POWER DISTRIBUTION UNIT. ## 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/N320CA/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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.