# N215LA: 2024 Diamond Aircraft Ind DA20-C1

- Status: Valid registration
- Airframe: [Diamond Aircraft Ind DA20-C1](https://openairdocs.org/model/diamond-aircraft-ind-da20-c1) (registry code 2990001, 2 seats)
- Engine: [Continental IO-240-B](https://openairdocs.org/engine/continental-io-240-b) (registry code 17177)
- Data sheets: [TCDS TA4CH](https://openairdocs.org/tcds/TA4CH) (Diamond Aircraft Industries Inc.), [TCDS E7SO](https://openairdocs.org/tcds/E7SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: C0766
- Year built: 2024
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, utility
- Airworthiness date: May 9, 2024
- Certificate issued: June 6, 2024
- Expires: June 30, 2031
- Mode S code: A1CD10
- Registered owner: [Aurora Leasing LLC](https://openairdocs.org/faa-owner/AURORA%20LEASING%20LLC)
- Location: [Woods Cross, UT](https://openairdocs.org/faa-place/UT/Woods%20Cross)
- Owner type: LLC
- Owner's area on the map: 40.8891° N, 111.9282° W: Placed by OpenAirDocs at the center of ZIP code 84087, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=215LA
- Page: https://openairdocs.org/aircraft/N215LA

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): 5 in force

### Matched by airframe (Diamond Aircraft Ind DA20-C1)

- [AD 2026-15-18](https://openairdocs.org/ad/2026-15-18): Emergency Locator Beacon · Diamond Aircraft Industries DA20-C1. Effective Sep 8, 2026
- [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 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005

### Matched by engine (Continental IO-240-B)

- [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

### Historical (superseded or no longer in force)

- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more

## Information bulletins (advisory) (8 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-12-09](https://openairdocs.org/saib/CE-12-09): Landing Gear, Nose: Diamond DA20 Nose Landing Fork Assembly. Issued Dec 22, 2011
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-05-38](https://openairdocs.org/saib/NE-05-38): . Issued Mar 18, 2005
- [SAIB CE-98-21R1](https://openairdocs.org/saib/CE-98-21R1): . Issued Jun 10, 1998

## NTSB investigations

None matched to N215LA.

## FAA accident and incident reports

None matched to N215LA.

## 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 N215LA not matched to an aircraft (55, newest 50)

They name N215LA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR KBM2006F00225](https://openairdocs.org/sdr/KBM2006F00225), Jun 29, 2006: INDICATOR. FAILED. NG INDICATOR, WENT TO ZERO, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00224](https://openairdocs.org/sdr/KBM2006F00224), Jun 29, 2006: PITCH LINK. EXCESS PLAY. T/R PITCH LINK, UNIT HAS NOTICEABLE PLAY IN ROD END, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00200](https://openairdocs.org/sdr/KBM2006F00200), Jun 13, 2006: CONTROL CABLE. BINDING. TAIL ROTOR CONTROL CABLE, UNIT BINDING, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00199](https://openairdocs.org/sdr/KBM2006F00199), Jun 5, 2006: BLOWER MOTOR. INOPERATIVE. AFT CLAP BLOWER IS INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00190](https://openairdocs.org/sdr/KBM2006F00190), May 25, 2006: GAUGE. ERRATIC. NG GAUGE, NEEDLE ERRATIC, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00166](https://openairdocs.org/sdr/KBM2006F00166), May 7, 2006: TRANSMITTER. INOPERATIVE. FUEL PRESSURE TRANSMITTER, FUEL GAUGE INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00165](https://openairdocs.org/sdr/KBM2006F00165), Apr 29, 2006: TACHOMETER. ERRATIC. DUAL TACH, READING ERRATIC DURING RUN UP, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00153](https://openairdocs.org/sdr/KBM2006F00153), Apr 17, 2006: GAUGE. STICKING. TOT GAUGE, T4 STICKS NEEDLE AT 4:00 AND 5:00 DEGREES, REMOVED AND REPLACED. (K)
- [SDR KBM2006F00164](https://openairdocs.org/sdr/KBM2006F00164), Mar 21, 2006: PUMP. LOW PRESSURE. FUEL PUMP NR 1 PRESSURE, READS LOW. PRESSURE CAUTION LIGHT DE-ACTIVATED. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00113](https://openairdocs.org/sdr/KBM2006F00113), Mar 9, 2006: GYRO. INOPERATIVE. ATTITUDE GYRO, UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2006F00103](https://openairdocs.org/sdr/KBM2006F00103), Feb 27, 2006: GYRO. INOPERATIVE. A.G., UNIT INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00338](https://openairdocs.org/sdr/KBM2005F00338), Nov 7, 2005: SWITCH. INTERMITTENT. FUEL PRESSURE LIGHT INTERMITTENT, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00308](https://openairdocs.org/sdr/KBM2005F00308), Oct 18, 2005: GYRO. FAILED. DIRECTIONAL GYRO WILL NOT HOLD CAGE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00307](https://openairdocs.org/sdr/KBM2005F00307), Oct 18, 2005: GYRO. FAILED. UNIT WILL NOT HOLD CAGE. REMOVED AND REPLACE. (K)
- [SDR KBM2005F00289](https://openairdocs.org/sdr/KBM2005F00289), Sep 19, 2005: DRAIN VALVE. LEAKING. ENGINE FUEL START DRAIN VALVE LEAKING IN THE WEEPING HOLE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00288](https://openairdocs.org/sdr/KBM2005F00288), Sep 19, 2005: BRUSHES. INOPERATIVE. LT CONDENSER BLOWER INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00287](https://openairdocs.org/sdr/KBM2005F00287), Sep 19, 2005: BEARING. TORN. LAMINATED BEARING, UNIT RUBBER TORN, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00260](https://openairdocs.org/sdr/KBM2005F00260), Sep 11, 2005: RADIO. INOPERATIVE. VHF RADIO KNOB WILL NOT ADJUST ITS NUMBERS, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00259](https://openairdocs.org/sdr/KBM2005F00259), Sep 10, 2005: STARTER GEN. INOPERATIVE. STARTER GEN - UNIT WILL NOT COME ON LINE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00250](https://openairdocs.org/sdr/KBM2005F00250), Aug 18, 2005: MOTOR. INOPERATIVE. A/C NOT BLOWING COLD AIR, MOTOR INOPERATIVE. REMOVED AND REPLACED MOTOR. (M)
- [SDR KBM2005F00172](https://openairdocs.org/sdr/KBM2005F00172), Aug 4, 2005: MOTOR. INOPERATIVE. 5 INCH MOTOR, UNIT INOPERATIVE, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00170](https://openairdocs.org/sdr/KBM2005F00170), Jul 28, 2005: INDICATION SYS. FLUCTUATES. ENGINE OIL PRESS, UNIT FLUCTUATES IN FLIGHT. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00156](https://openairdocs.org/sdr/KBM2005F00156), Jul 18, 2005: CONTROL CABLE. WORN. ENGINE GOVERNOR CABLE WORN, REMOVED AND REPLACED. (K)
- [SDR KBM2005F00219](https://openairdocs.org/sdr/KBM2005F00219), Jul 4, 2005: GEAR. MAKING METAL. M05 REDUCTION GEAR, SUSPECTED OF CAUSING CHIP LIGHT. (K)
- [SDR KBM2005F00129](https://openairdocs.org/sdr/KBM2005F00129), Jun 23, 2005: ELECTRICAL BOX. FAILED. GENERATOR LIGHT COMES ON IN FLIGHT. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00198](https://openairdocs.org/sdr/KBM2005F00198), May 20, 2005: MOTOR. INOPERATIVE. 5 INCH BLOWER MOTOR, INOPERATIVE. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00197](https://openairdocs.org/sdr/KBM2005F00197), May 20, 2005: MOTOR. BROKEN. 5 INCH BLOWER MOTOR, ONE BLOWER MOTOR BLADE BROKEN. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00196](https://openairdocs.org/sdr/KBM2005F00196), May 19, 2005: LIGHT. INOPERATIVE. ANTI-COLLISION LIGHT INOPERATIVE. REMOVED AND RELACED. (K)
- [SDR KBM2005F00073](https://openairdocs.org/sdr/KBM2005F00073), Mar 24, 2005: BEARING. WORN. LAMINATED BEARINGS WORN. REMOVED AND REPLACED. (K)
- [SDR KBM2005F00171](https://openairdocs.org/sdr/KBM2005F00171), Feb 28, 2005: BLOWER. BROKEN. EVAPORATOR BLOWER ASSY, BROKEN BRUSH HOLDER, REMOVED AND REPLACED. (K)
- [SDR KBM2004F00242](https://openairdocs.org/sdr/KBM2004F00242), Oct 4, 2004: DRAIN VALVE. LEAKING. START DRAIN VALVE, UNIT LEAKING, REMOVED AND REPLACED.
- [SDR KBM2004F00241](https://openairdocs.org/sdr/KBM2004F00241), Oct 4, 2004: MAGNETIC SEAL. LEAKING. MAGNETIC SEAL LEAKING, REMOVED AND REPLACED.
- [SDR KBM2004F00224](https://openairdocs.org/sdr/KBM2004F00224), Sep 20, 2004: GYRO. INOPERATIVE. DIRECTIONAL GYRO, INOPERATIVE (RED FLAG), WILL NOT HOLD HEADING. REMOVED AND REPLACED DIRECTIONAL GYRO.
- [SDR KBM2004F00223](https://openairdocs.org/sdr/KBM2004F00223), Sep 10, 2004: BEARING. WORN. BEARING HALF SHELLS WORN AND TORN. REMOVED AND REPLACED.
- [SDR KBM2004F00200](https://openairdocs.org/sdr/KBM2004F00200), Aug 17, 2004: ARMATURE. WORN. ARMATURE WORN, SPARKS DURING, INTERMITTENT OPERATION. REMOVED AND REPLACED.
- [SDR KBM2004F00199](https://openairdocs.org/sdr/KBM2004F00199), Aug 2, 2004: GYRO. INOPERATIVE. FLAG STAYS INOPERATIVE. REMOVED AND REPLACED DG.
- [SDR KBM2004F00139](https://openairdocs.org/sdr/KBM2004F00139), Jul 21, 2004: MOTOR. INOPERATIVE. A/C BLOWER WARM. RT CONDENSOR BLOWER INOPERATIVE. REMOVED AND REPLACED. RT CONDENSOR BLOWER.
- [SDR KBM2004F00138](https://openairdocs.org/sdr/KBM2004F00138), Jun 8, 2004: MAGNETIC SEAL. LEAKING. NR 5 MAG SEAL, LEAKING SEAL. REPLACED WITH RECONDITIONED UNIT.
- [SDR KBM2004F00137](https://openairdocs.org/sdr/KBM2004F00137), Jun 6, 2004: FUEL CONTROL. FAILED. FUEL CONTROL UNIT, UNABLE TO OBTAIN DESIRED NR. REPLACED WITH 0.0 TSO UNIT. OPS CHECK GOOD.
- [SDR KBM2004F00188](https://openairdocs.org/sdr/KBM2004F00188), May 6, 2004: DRIVE ASSY. DAMAGED. T/R DRIVE (SHORT SHAFT) FORWARD COUPLING ATT BOLTS TO ENGINE TAKE OFF FLANGE FAIL TORQUE LOAD CHECK REQUIRES UNIT TO BE SENT TO MANUFACTURER FOR INSPECTION. ASS
- [SDR KBM2004F00187](https://openairdocs.org/sdr/KBM2004F00187), May 6, 2004: SPIDER. WORN. T/R SPIDER BALL END WORN. REMOVED AND REPLACED.
- [SDR KBM2004F00186](https://openairdocs.org/sdr/KBM2004F00186), May 6, 2004: BOLT. UNDERTORQUED. ENGINE TO MGB POWER SHAFT FORWARD COUPLING BOLT TO PULLEY FAIL TORQUE LOAD CHECK, COUPLING REJECTION MANDATORY. REMOVED AND REPLACED.
- [SDR KBM2004FAA](https://openairdocs.org/sdr/KBM2004FAA), May 6, 2004: PULLEY. UNDERTORQUED. ENGINE TO MGB POWER SHAFT FORWARD PULLEY ATTACH HOLES ELONGATED DUE TO ATTACHMENT BOLT TORQUE LESS THAN MINIMUM TORQUE AT ORIGINAL INSTALLATION. REMOVED AND REP
- [SDR KBM2004F00051](https://openairdocs.org/sdr/KBM2004F00051), Apr 29, 2004: SWITCH. INOPERATIVE. NR 2 VHF VOLUME SWITCH, INOPERATIVE. REMOVED AND REPLACED.
- [SDR KBM2004F00050](https://openairdocs.org/sdr/KBM2004F00050), Apr 11, 2004: TRANSMITTER. FLUCTUATES. FLUCTUATION IN OIL PRESSURE. REMOVED AND REPLACED.
- [SDR KBM2004F00136](https://openairdocs.org/sdr/KBM2004F00136), Mar 20, 2004: STRAP. WORN. EXHAUST HEAT SHIELD STRAP. HEAT SHRINK WORN REGS REPLACEMENT. REMOVED AND REPLACED.
- [SDR KBM2004F00022](https://openairdocs.org/sdr/KBM2004F00022), Feb 19, 2004: DRAIN VALVE. LEAKING. START DRAIN VALVE, EXTERNAL LEAKING. 10 YR CALENDAR INSPECTION. REMOVED AND REPLACED WITH SERVICEABLE UNIT.
- [SDR KBM2005F00020](https://openairdocs.org/sdr/KBM2005F00020), Feb 18, 2004: CONTROL CABLE. FAILED. TAIL ROTOR CONTROL CABLE, BLACK GREASE COMING FROM BOTH ENDS. (OLD STYLE) REMOVED AND REPLACED. (K)
- [SDR KBM2004F00049](https://openairdocs.org/sdr/KBM2004F00049), Feb 18, 2004: PROBE. STICKING. FUEL PROBE, INTERMITTENTLY STICKS BETWEEN APPROX 25-35 PERCENT INDICATED. REMOVED AND REPLACED.
- [SDR KBM2004F00034](https://openairdocs.org/sdr/KBM2004F00034), Feb 18, 2004: PROBE. STICKS. FUEL PROBE INTERMITTENTLY STICKS BETWEEN APPROX. 25-35 PERCENT INDICATED. REMOVED AND REPLACED.

All 55: https://openairdocs.org/aircraft/N215LA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (89, 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 (Diamond Aircraft Ind DA20-C1)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems. J P Instruments
- [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 SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [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 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 SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [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 SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation
- [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 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

All 89: https://openairdocs.org/aircraft/N215LA/stcs.md

## Related

- Other Diamond Aircraft Ind DA20-C1 aircraft: https://openairdocs.org/model/diamond-aircraft-ind-da20-c1/aircraft.md
- The Continental IO-240-B engine: https://openairdocs.org/engine/continental-io-240-b.md

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