# N808DE: 2021 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: 2267 - Year built: 2021 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: February 25, 2021 - Certificate issued: February 11, 2025 - Expires: February 29, 2032 - Mode S code: AAFFE5 - Registered owner: [Tabs Rental LLC](https://openairdocs.org/faa-owner/TABS%20RENTAL%20LLC) - Location: [St Simons Island, GA](https://openairdocs.org/faa-place/GA/St%20Simons%20Island) - Owner type: LLC - Owner's area on the map: 31.2572° N, 81.3420° W: Placed by OpenAirDocs at the center of ZIP code 31522, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=808DE - Page: https://openairdocs.org/aircraft/N808DE 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 N808DE. ## FAA accident and incident reports None matched to N808DE. ## Reports on N808DE not matched to an aircraft (1) They name N808DE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19940512022039I](https://openairdocs.org/incident/19940512022039I), May 12, 1994: Doug MD11 (N808DE), Salt Lake City, UT. Pilot lost consciousness sitting in jump seat. Long global flight. Relief pilot took over. Recovered.further tests. ## 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 N808DE not matched to an aircraft (21) They name N808DE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DLM11030396](https://openairdocs.org/sdr/DLM11030396), Apr 28, 2003: HANDLE. STUCK. DOOR 1L WAS ACTUATED BY THE EXTERIOR EMERGENCY HANDLE, DOOR ASSIST BOTTLE BLEW AND HANDLE STUCK IN EMERGENCY POSITION. DOOR WOULD NOT OPEN OR CLOSE ELECTRICALLY - [SDR DLM11020575](https://openairdocs.org/sdr/DLM11020575), May 21, 2002: ENGINE. STALLED. NR 3 ENG STALLED ON T/O ROLL AT 30 KNOTS. REMOVED AND REPLACED NR 3 ENG PER ROUTINE CARD DECK. - [SDR DLM11020256](https://openairdocs.org/sdr/DLM11020256), Mar 4, 2002: BATTERY. DISCHARGED. EMERGENCY FLASHLIGHT AT 4R INBOARD BATTERY LOW. REMOVED AND REPLACED FLASHLIGHT AND BATTERY, OPS NORMAL. - [SDR DLM11020036](https://openairdocs.org/sdr/DLM11020036), Jan 11, 2002: TIRE. FLAT. TIRE FAIL EICAS MESSAGE DURING CLIMB. TIRE PRESSURE ON RIGHT MAIN OUTSIDE AFT TIRE ZERO. TEMP INDICATIONS NORMAL. FOUND NR 8 TIRE AT 0 PSI. REPLACED NR 8 WHEEL - [SDR DLM11011773](https://openairdocs.org/sdr/DLM11011773), Nov 7, 2001: ACTUATOR. BENT. ATB DUE TO CENTER GEAR WILL NOT RETRACT. FOUND CENTER GEAR RETRACT ACTUATOR BENT. REPLACING SAME. - [SDR DLM11011560](https://openairdocs.org/sdr/DLM11011560), Sep 18, 2001: ADAPTER. BROKEN. OIL QTY ON ENG 3 DROPPED RAPIDLY TO 1 QT AFTER ABOUT 20 MINUTES IN FLIGHT . INITIALLY OIL PRESSURE WAS GOOD, SLOWLY DROPPED TO THE BOTTOM OF THE GREEN BAND 90 P - [SDR DLM11011152](https://openairdocs.org/sdr/DLM11011152), Jul 12, 2001: BATTERY. DISCHARGED. LED ON EMERGENCY FLASHLIGHT AT 4R NOT FLASHING. REPLACED BATTERY LIGHT, OPN CHECKS NORMAL. - [SDR DLM11010809](https://openairdocs.org/sdr/DLM11010809), May 20, 2001: LIGHT. INOPERATIVE. ON PRE FLT FOUND TEST SWITCH EMERGENCY LIGHT NR 6 BATTERY LOW MESSAGE ON. REMOVED AND REPLACED SEAT 54B LIGHT ASSY AND HARNESS SYSTEM CHK'S NORMAL PER MM, OK FO - [SDR DLM11001964](https://openairdocs.org/sdr/DLM11001964), Oct 8, 2000: BOTTLE. DISCHARGED. FOUR HOURS INTO FLIGHT, ENGINE FIRE AGENT LOW LIGHT ENG 1 WARNING CAME ON. REPLACED NR 1 ENGINE NR 1 FIRE BOTTLE. SQUIB NOT FIRED. SUSPECT AGENT LEAKED OUT AS S - [SDR DLM11001668](https://openairdocs.org/sdr/DLM11001668), Aug 29, 2000: WIRE. DAMAGED. DURING MTC CVG FOUND DAMAGED GALLEY AND EXTERNAL FEEDER WIRE. ALL DAMAGE WAS FOUND UNDER METAL CLAMPS. REPLACED CABLES. - [SDR DLM11001433](https://openairdocs.org/sdr/DLM11001433), Jul 30, 2000: WIRE. CHAFED. EMERGENCY LIGHTS FROM ROW 30 TO 41 INOP. REPAIRED CHAFED WIRE AT TERMINAL STRIP IN OVERHEAD LIGHTS, TEST OK. - [SDR DLM11000223](https://openairdocs.org/sdr/DLM11000223), Jan 30, 2000: SMOKE DETECTOR. MALFUNCTIONED. IN CRUISE, LAVATORY SMOKE ALERT ILLUMINATED FOR LAV H. CLOSE VISUAL INSP IN LAV COMPARTMENT SHOWED NO SMOKE, NO HEAT OR EXTINGUISHING AGENT DISCHARGE. PULLED AN - [SDR DLM11992181](https://openairdocs.org/sdr/DLM11992181), Sep 30, 1999: VIDEO UNIT. FAILED. FLIGHT ATTENDENTS REPORTED VIDEO DISPLAY AT SEAT 13G WAS VERY HOT EVEN THOUGH DISPLAY WAS OFF. NOTICEABLE ELECTRICAL SMELL WAS NOTICED BY PASSENGERS THROUGHOUT - [SDR DLM11991037](https://openairdocs.org/sdr/DLM11991037), May 10, 1999: SOCKET. SHORTED. EMERGENCY LIGHTS FAIL TEST BATTERY 5 AND BATTERY 6 LOW. FOUND SHORTED LIGHT SOCKETS AT SEAT 44 AND 45. REPLACED SAME, GROUND TEST OK. - [SDR DLM11981739](https://openairdocs.org/sdr/DLM11981739), Aug 22, 1998: WIRE HARNESS. FAILED. EMERGENCY LIGHT AT SEAT 37B INOP. REPLACED LIGHT/HARNESS ASSY. - [SDR DLM11971638](https://openairdocs.org/sdr/DLM11971638), Aug 21, 1997: SMOKE DETECTOR. DIRTY. LAVATORY SMOKE ALERT 8 PLUS 30 INTO FLIGHT APPEARED TO BE DUE TO PAX USE OF HAIR SPRAY INTO LAV 3L. ALERT MUST BE CLEARED ON GROUND. REPLACED DETECTOR. - [SDR DLM11971305](https://openairdocs.org/sdr/DLM11971305), Jul 6, 1997: WIRE. SHORTED. DURING A CHECK OF EMERGENCY TRACK LIGHTING AT THE GATE, A SECTION OF ESCAPE PATH TRACK LIGHTING WAS FOUND INOPERATIVE. IT WAS DETERMINED THAT TWO WIRE RUNS WERE - [SDR DLM11970602](https://openairdocs.org/sdr/DLM11970602), Apr 3, 1997: WARMING PLATE. FAILED. SMELL OF BURNING PLASTIC/INSULATION IN B/C CENTERLINE WARMING PLATE UPPER UNIT. - [SDR DLM11961668](https://openairdocs.org/sdr/DLM11961668), Jul 10, 1996: BATTERY. DISCHARGED. EMERGENCY BATT TEST FAILS, BATT 1 LOW. FOUND F/C FLOOR TRACK SHORTED OUT AND BATT MAKING LOUD NOISE WHEN SELECTED ON. REPLACED BATT AND REPAIRED TRACK. - [SDR DLM11960788](https://openairdocs.org/sdr/DLM11960788), Apr 7, 1996: BATTERY. DISCHARGED. BATTERY 3 LOW MSG ON TEST FOR EMERGENCY LIGHT SYSTEM. REPLACED BATTERY. - [SDR DLM11950830](https://openairdocs.org/sdr/DLM11950830), Feb 26, 1995: SKIN. WORN. DURING INSPECTION, FOUND WEAR DAMAGE TO WING LEADING EDGE AT THE INTERSECTION OF NR 1 AND NR 2 LEADING EDGE SLATS. REPAIRED PER SRM 57-10-00 PG 63. ## 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/N808DE/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.