# N937DM: 2024 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: 10225 - Year built: 2024 - Type: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: October 1, 2024 - Certificate issued: October 17, 2024 - Expires: October 31, 2031 - Mode S code: AD0001 - Registered owner: [Punk Taco Love II LLC](https://openairdocs.org/faa-owner/PUNK%20TACO%20LOVE%20II%20LLC) - Location: [Okemos, MI](https://openairdocs.org/faa-place/MI/Okemos) - Owner type: LLC - Owner's area on the map: 42.7042° N, 84.3921° W: Placed by OpenAirDocs at the center of ZIP code 48864, 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=937DM - Page: https://openairdocs.org/aircraft/N937DM 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 N937DM. ## FAA accident and incident reports None matched to N937DM. ## 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 N937DM not matched to an aircraft (32) They name N937DM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DALA2023072405945](https://openairdocs.org/sdr/DALA2023072405945), Jul 19, 2023: UNKNOWN. UNKNOWN. (LOG 2874425) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR IB BALANCE BAY PANEL. REPAIRED CORRODED AREA PER DELTA ERA - [SDR DALA2023072405944](https://openairdocs.org/sdr/DALA2023072405944), Jul 19, 2023: UNKNOWN. UNKNOWN. (LOG 2874400) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR CENTER BALANCE BAY PANEL AT OB CORNER. REPAIRED CORRODED A - [SDR DALA2023072405942](https://openairdocs.org/sdr/DALA2023072405942), Jul 19, 2023: UNKNOWN. UNKNOWN. (LOG 2874325) LH HORIZONTAL STABILIZER AFT REAR SPAR UPPER ANGLE HAS AREA OF CORROSION ABOVE ELEVATOR OB BALANCE BAY PANEL. REPAIRED AREA OF CORROSION PER ERA 6 - [SDR DALA2023072405940](https://openairdocs.org/sdr/DALA2023072405940), Jul 19, 2023: UNKNOWN. UNKNOWN. (LOG 2874287) LH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28 FROM OB STABILIZER TIP. REPAIRED CORRODED AREA PER ERA 609520-14 - [SDR DALA2023071705741](https://openairdocs.org/sdr/DALA2023071705741), Jul 11, 2023: UNKNOWN. UNKNOWN. (LOG 2860460) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 500C + 15 AND BS 500L. LBL 26. LOCA - [SDR DALA2023071305697](https://openairdocs.org/sdr/DALA2023071305697), Jul 10, 2023: UNKNOWN. UNKNOWN. (LOG 2858953) DURING CHECK AT FLIGHTSTAR (VQQ), THE UPPER CHORD AT LH HORIZONTAL STAB REAR SPAR WAS FOUND WITH FOUR CORROSION SPOTS BETWEEN STAB STA 130 & STAB - [SDR DALA2023071105593](https://openairdocs.org/sdr/DALA2023071105593), Jul 7, 2023: UNKNOWN. UNKNOWN. (LOG 2853856) CORROSION IN AFT CARGO COMPARTMENT FLOOR STRUCTURE CARGO TRACK-TIE DOWN SUPPORT BETWEEN BS. 795 AND BS.835 RBL.13.84. REMOVED AND REPLACED TRACK I - [SDR DALA2023071005527](https://openairdocs.org/sdr/DALA2023071005527), Jul 6, 2023: UNKNOWN. UNKNOWN. (LOG 2852397) AFT CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT RAIL (CHANNEL) HAS A GOUGE AT FASTENER HOLE BS.727L+2 LBL.3.00. CUT AND REMOVED THE DAMAGE PART OF A - [SDR DALA2023071005525](https://openairdocs.org/sdr/DALA2023071005525), Jul 6, 2023: UNKNOWN. UNKNOWN. (LOG 2852489) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT FLOOR STRUCTURE RT SIDE TRANSITION PANEL SECTION BETWEEN BS.727I+10 AND BS.767 RBL.21.00. - [SDR DALA2023070505408](https://openairdocs.org/sdr/DALA2023070505408), Jul 1, 2023: UNKNOWN. UNKNOWN. (LOG 2844523) RH HORIZONTAL STABILIZER OB TE WEDGE UPPER ATTACH ANGLE HAS AREA OF CORROSION 28" FROM OB STABILIZER TIP. VIEWED THRU AFT ACCESS HOLE WITH STABILI - [SDR DALA2023070505407](https://openairdocs.org/sdr/DALA2023070505407), Jul 1, 2023: UNKNOWN. UNKNOWN. (LOG 2844472) AFT REMOVAL OF ADF ANTENNA #1 AND #2 FOUND MULTIPLE DOME NUT DAMAGE. REPAIRED ADF ANTENNA #1 AND #2 DOME NUTS PER DELTA ERA 608966-14 REV ORIGINAL - [SDR DALA2023070305325](https://openairdocs.org/sdr/DALA2023070305325), Jun 29, 2023: UNKNOWN. UNKNOWN. (LOG 2840745) FWD ADF ANTENNA AREA, ON TOP OF THE FUSELAGE, CORROSION AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609634-14 REV. ORIGINAL. - [SDR DALA2023070305324](https://openairdocs.org/sdr/DALA2023070305324), Jun 29, 2023: UNKNOWN. UNKNOWN. (LOG 2840722) AFT ADF ANTENNA AREA, CORROSION FOUND AROUND THE FASTENER HOLES. REPAIRED AFFECTED AREAS PER DELTA ERA 609424-14 REV ORIGINAL. - [SDR DALA2023062605114](https://openairdocs.org/sdr/DALA2023062605114), Jun 23, 2023: UNKNOWN. UNKNOWN. (LOG 2830670) LOCATED PREVIOUS BLENDOUT AT FUSELAGE SKIN STA 500A-500B, STR 22-21R. REPAIRED PREVIOUS BLENDOUT AREA OF FUSELAGE SKIN STA 500A-500B, STR 22-21R P - [SDR DALA2023062605112](https://openairdocs.org/sdr/DALA2023062605112), Jun 23, 2023: PANEL. CORRODED. (LOG 2830077) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 500A AND BS 500 L RBL 26. INSTALLED - [SDR DALA2023062605111](https://openairdocs.org/sdr/DALA2023062605111), Jun 22, 2023: UNKNOWN. UNKNOWN. (LOG 2828990) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE TRANSITION PANEL SECTION BETWEEN BS.727A AND BS.727I+8 LBL.21.00. - [SDR DALA2023062605110](https://openairdocs.org/sdr/DALA2023062605110), Jun 21, 2023: UNKNOWN. UNKNOWN. (LOG 2827423) AFT CARGO ENTRY PANEL UNDER THRESHOLD HAS MULTIPLE AREAS OF CORROSION. REPAIRED AREA PER DELTA ERA 609690-14 REV ORIGINAL. - [SDR DALA2023062605098](https://openairdocs.org/sdr/DALA2023062605098), Jun 20, 2023: SUPPORT FITTING. CORRODED. (LOG 2825881) RH AFT LAVATORY SUPPORT BEAM AT BS 953 HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN RBL 25 AND RBL 35. REMOVED AND REPLACED LAVATORY SUPPORT PE - [SDR DALA2023061904977](https://openairdocs.org/sdr/DALA2023061904977), Jun 17, 2023: UNKNOWN. UNKNOWN. (LOG 2821274) AFT CARGO FWD CUTOUT PANEL LWR CORNER DAMAGED. FABRICATE NEW AFT CARGO FWD CUTOUT PANEL DIM. 52.5 X 5.1 FROM MATERIAL 6013-T4 .050 IAW B737-900 SR - [SDR DALA2023061904975](https://openairdocs.org/sdr/DALA2023061904975), Jun 17, 2023: UNKNOWN. UNKNOWN. (LOG 2821178) CORROSION AROUND FASTENER HOLES IN AFT CARGO COMPARTMENT LT SIDE TRANSITION PANEL SECTION BETWEEN BS.727K+10 AND BS.847 LBL 21.00. REMOVED CORROSI - [SDR DALA2023061604928](https://openairdocs.org/sdr/DALA2023061604928), Jun 16, 2023: WEB. CORRODED. (LOG 2818886) FORWARD CARGO COMPARTMENT DOOR CUT OUT LOWER SILL HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 440 AND BS 490. INSTALLED NEW WEB AT FWD CARG - [SDR DALA2023061604927](https://openairdocs.org/sdr/DALA2023061604927), Jun 16, 2023: UNKNOWN. UNKNOWN. (LOG 2818839) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 420 AND BS 440 RBL 26. LOCATED, DRI - [SDR DALA2023061604926](https://openairdocs.org/sdr/DALA2023061604926), Jun 16, 2023: PANEL. CORRODED. (LOG 2818828) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACE BETWEEN BS 490 AND BS 500A. RBL 26. - [SDR DALA2023061604937](https://openairdocs.org/sdr/DALA2023061604937), Jun 14, 2023: PANEL. CORRODED. (LOG 2815290) FORWARD CARGO COMPARTMENT LH FLOOR TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN BS 400 AND BS 500C + 15 LBL 26. LOCATE - [SDR DALA2023061204730](https://openairdocs.org/sdr/DALA2023061204730), Jun 9, 2023: UNKNOWN. UNKNOWN. (LOG 2807753) MAIN CABIN FLOOR SUPPORT STA 951-967 LBL 30 CORRODED AROUND HOLE DOT 45/018. REMOVED AND REPLACED FLOOR SUPPORT IAW B737-900 SRM 51-40-02. - [SDR DALA2023061204726](https://openairdocs.org/sdr/DALA2023061204726), Jun 7, 2023: SEAT TRACK. CRACKED. (LOG 2804399) MAIN CABIN LBL 45 SEAT TRACK LOWER SUPPORT IS CRACKED AT BS 727B. REMOVED AND REPLACED SEAT TRACK LOWER SUPPORT AT BS 727B LBL 45 IAW B737-900 SRM - [SDR DALA2023060604572](https://openairdocs.org/sdr/DALA2023060604572), Jun 3, 2023: SEAT TRACK. CRACKED. (LOG 2798299) MAIN CABIN RBL 45 SEAT TRACK LOWER SUPPORT IS CRACKED AT BS 727B. REMOVED AND REPLACE MAIN CABIN SEAT TRACK LOWER SUPPORT AT BS 727B RBL 45 PER B7 - [SDR DALA2023060604566](https://openairdocs.org/sdr/DALA2023060604566), Jun 3, 2023: UNKNOWN. UNKNOWN. MAIN CABIN BS 986.5 FLOOR BEAM UPPER SURFACE HAS AREAS OF CORROSION BETWEEN RBL 15 AND RBL 48. FABRICATED REPAIR PARTS REPAIR (1) STRAP FROM 7575T6 0.100" CLAD. - [SDR DALA2023032302260](https://openairdocs.org/sdr/DALA2023032302260), Mar 21, 2023: UNKNOWN. UNKNOWN. (LOG 2681789) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT LOWER OUTBD BORE PITTED ON OUTBD FACE. REMOVED BUSHING AND MACHINED .070 OFF OUTTER FACE TO R - [SDR DALA2023032302259](https://openairdocs.org/sdr/DALA2023032302259), Mar 21, 2023: UNKNOWN. UNKNOWN. (LOG 2681785) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT LOWER INBD BORE PITTED ON INBD FACE. REMOVED BUSHING AND MACHINED .090 OFF OUTTER FACE TO REM - [SDR DALA2023032302258](https://openairdocs.org/sdr/DALA2023032302258), Mar 21, 2023: UNKNOWN. UNKNOWN. (LOG 2681778) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT UPPER INBD BORE PITTED ON INBD FACE. REMOVED BUSHING AND MACHINED .062 OFF OUTTER FACE TO REM - [SDR DALA2023032302257](https://openairdocs.org/sdr/DALA2023032302257), Mar 21, 2023: UNKNOWN. UNKNOWN. (LOG 2681765) DURING INSPECTION FOUND LT WING H-BLOCK ATTACH POINT UPPER OUTBD BORE PITTED ON OUTBD FACE. REMOVED BUSHING AND MACHINED .042 OFF OUTTER FACE TO R ## 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/N937DM/stcs.md ## Earlier aircraft with N937DM The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N937DM before. - [Cancelled 2013-09-10](https://openairdocs.org/deregistered/N937DM-2013-09-10): Embraer-Empresa Brasileira De EMB-500, S/N 50000136, built 2010. Exported to Canada. Owner: [Embraer Executive Aircraft Inc](https://openairdocs.org/faa-owner/EMBRAER%20EXECUTIVE%20AIRCRAFT%20INC), [Melbourne, FL](https://openairdocs.org/faa-place/FL/Melbourne) ## 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.