# N350TS: 2005 Diamond Aircraft Ind DA 42

- Status: Valid registration
- Airframe: [Diamond Aircraft Ind DA 42](https://openairdocs.org/model/diamond-aircraft-ind-da-42) (registry code 2990004, 4 seats)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Data sheets: [TCDS A57CE](https://openairdocs.org/tcds/A57CE) (Diamond Aircraft Industries GmbH) (OpenAirDocs)
- Serial number: 42.061
- Year built: 2005
- Type: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 23, 2006
- Certificate issued: December 14, 2006
- Expires: February 28, 2029
- Mode S code: A3E687
- Registered owner: [Utah State University](https://openairdocs.org/faa-owner/UTAH%20STATE%20UNIVERSITY)
- Location: [Logan, UT](https://openairdocs.org/faa-place/UT/Logan)
- Owner type: Government
- Owner's area on the map: 41.7990° N, 111.7276° W: Placed by OpenAirDocs at the center of ZIP code 84321, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=350TS
- Page: https://openairdocs.org/aircraft/N350TS

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): 18 in force

### Matched by airframe (Diamond Aircraft Ind DA 42)

- [AD 2026-14-08](https://openairdocs.org/ad/2026-14-08): Landing Gear Actuator · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Jul 20, 2026
- [AD 2025-24-07](https://openairdocs.org/ad/2025-24-07): Passenger/Crew Doors · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Feb 12, 2026
- [AD 2024-06-13](https://openairdocs.org/ad/2024-06-13): Flight Control System · Diamond Aircraft Industries DA 42, DA 42 NG and DA 42 M-NG. Effective May 28, 2024
- [AD 2022-06-08](https://openairdocs.org/ad/2022-06-08): Flight Control System · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective May 9, 2022
- [AD 2022-03-01](https://openairdocs.org/ad/2022-03-01): Fuel Storage · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Mar 17, 2022
- [AD 2021-22-03](https://openairdocs.org/ad/2021-22-03): Nose/Tail Landing Gear Attach Section · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Dec 21, 2021
- [AD 2018-10-10](https://openairdocs.org/ad/2018-10-10): Engine Exhaust · Diamond Aircraft Industries DA 42. Effective Jun 12, 2018
- [AD 2013-19-11](https://openairdocs.org/ad/2013-19-11): Landing Gear · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Oct 31, 2013
- [AD 2013-07-01](https://openairdocs.org/ad/2013-07-01): Landing Gear · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective May 20, 2013
- [AD 2012-17-07](https://openairdocs.org/ad/2012-17-07): Wings · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Oct 11, 2012
- [AD 2011-11-07](https://openairdocs.org/ad/2011-11-07): Landing Gear · Diamond Aircraft Industries DA 42. Effective Jul 6, 2011
- [AD 2011-10-13](https://openairdocs.org/ad/2011-10-13): Doors · Diamond Aircraft Industries DA 42, DA 42 M-NG and DA 42 NG. Effective Jun 17, 2011
- [AD 2008-23-08](https://openairdocs.org/ad/2008-23-08): Right hand engine support bracket · Diamond Aircraft Industries DA 42. Effective Dec 22, 2008
- [AD 2008-16-20](https://openairdocs.org/ad/2008-16-20): Aileron control system · Diamond Aircraft Industries DA 42. Effective Sep 17, 2008
- [AD 2007-23-14](https://openairdocs.org/ad/2007-23-14): Main aircraft battery · Diamond Aircraft Industries DA 42. Effective Dec 26, 2007
- [AD 2007-13-16](https://openairdocs.org/ad/2007-13-16): Surface roughness · Diamond Aircraft Industries DA 42. Effective Aug 10, 2007
- [AD 2007-12-24](https://openairdocs.org/ad/2007-12-24): Engine gearbox holding lines · Diamond Aircraft Industries DA 42. Effective Jul 19, 2007
- [AD 2007-12-05](https://openairdocs.org/ad/2007-12-05): Auxiliary fuel tank · Diamond Aircraft Industries DA 42. Effective Jul 16, 2007

### Matched by engine (Amateur-built UNKNOWN ENG)

None in force.

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

- [AD 2022-21-15](https://openairdocs.org/ad/2022-21-15) (historical): Fuselage Miscellaneous Structure · Diamond Aircraft Industries DA 42, DA 42 NG and DA 42 M-NG. Effective Dec 14, 2022
- [AD 2017-18-10](https://openairdocs.org/ad/2017-18-10) (historical): Flight Controls · Diamond Aircraft Industries DA-42-M-NG, DA-42-NG and DA 42. Effective Oct 11, 2017
- [AD 2017-15-09](https://openairdocs.org/ad/2017-15-09) (historical): Engine Exhaust · Diamond Aircraft Industries DA 42. Effective Aug 1, 2017
- [AD 2017-11-08](https://openairdocs.org/ad/2017-11-08) (historical): Engine Exhaust · Diamond Aircraft Industries DA 42. Effective May 31, 2017
- [AD 2017-01-12](https://openairdocs.org/ad/2017-01-12) (historical): Engine Exhaust · Diamond Aircraft Industries DA 42. Effective Feb 22, 2017

## Information bulletins (advisory) (3 in force)

- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB CE-08-45](https://openairdocs.org/saib/CE-08-45): Electrical - Airplane Flight Manual- Lightning Strike Procedures- Amendment. Issued Sep 3, 2008
- [SAIB CE-07-38](https://openairdocs.org/saib/CE-07-38): Airplane Flight Manual Clarification. Issued Jun 19, 2007

## 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 WPR21LA178](https://openairdocs.org/ntsb/WPR21LA178), Apr 27, 2021: Diamond Aircraft Ind DA 42 (N350TS), Brigham City, UT, substantial damage. Probable cause: The student pilot's unintentional selection of raising the landing gear instead of the flaps during a touch-and-go landing, and the flight instructor's delayed remedial action, which resulted in the…

## 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 20210427003979A](https://openairdocs.org/incident/20210427003979A), Apr 27, 2021: Diamond Aircraft Ind Gmbh DA 42 (N350TS), Brigham City, UT, Substantial damage. Pilot in control(student) was not multi engine qualified. Pilot in command was CFI. Student was practicing touch and go on airstrip. On second landing, student…

## Service difficulty reports (20)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 2025FA0000514](https://openairdocs.org/sdr/2025FA0000514), Jul 23, 2025: EXHAUST PIPE. INFLT SEPARATION. HEATSHIELD IS LOOSE ON THE EXHAUST PIPE TTSN 31.9 HOURS
- [SDR 2025FA0000466](https://openairdocs.org/sdr/2025FA0000466), Jul 9, 2025: EXHAUST PIPE. INFLT SEPARATION. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE. THE PROBLEM IS THE HEATSHIELD SPOT WEL
- [SDR 2025FA0000465](https://openairdocs.org/sdr/2025FA0000465), Jul 9, 2025: EXHAUST PIPE. INFLT SEPARATION. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE. THE PROBLEM IS THE HEATSHIELD SPOT WEL
- [SDR 2025FA0000461](https://openairdocs.org/sdr/2025FA0000461), Jul 9, 2025: EXHAUST PIPE. INFLT SEPARATION. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEATSHIELD TO BE TIGHT ON AND SPOT WELDED IN TWO PLACES TO THE EXHAUST PIPE.THE PROBLEM IS THE HEATSHIELD SPOT WELD
- [SDR 2025FA0000295](https://openairdocs.org/sdr/2025FA0000295), Apr 23, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOTS WELDS FAILED AND THE HEAT SHIELD I
- [SDR 2025FA0000272](https://openairdocs.org/sdr/2025FA0000272), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000271](https://openairdocs.org/sdr/2025FA0000271), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000270](https://openairdocs.org/sdr/2025FA0000270), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000269](https://openairdocs.org/sdr/2025FA0000269), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000268](https://openairdocs.org/sdr/2025FA0000268), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000267](https://openairdocs.org/sdr/2025FA0000267), Apr 15, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON THE AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON 
- [SDR 2025FA0000127](https://openairdocs.org/sdr/2025FA0000127), Feb 25, 2025: EXHAUST PIPE. SEPARATED. AD2018-10-10 DATED JUNE 12 2018 REQUIRES THE HEAT SHIELD TO BE TIGHT ON AND WELDED TO THE EXHAUST PIPE. THE HEAT SHIELD SPOT WELDS FAILED AND VERY LOOSE ON THE 
- [SDR 2025FA0000042](https://openairdocs.org/sdr/2025FA0000042), Jan 17, 2025: EXHAUST PIPE. SEPARATED. AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT
- [SDR 2025FA0000041](https://openairdocs.org/sdr/2025FA0000041), Jan 17, 2025: EXHAUST PIPE. SEPARATED. AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT
- [SDR 2025FA0000029](https://openairdocs.org/sdr/2025FA0000029), Jan 17, 2025: EXHAUST PIPE. SEPARATED. AD 2018-10-10 DATED JUNE 12 2018 REQUIRES US TO INSPECT THE EXHAUST PIPES TO MAKE SURE THE HEAT SHIELD IS TIGHT ON THE EXHAUST PIPE AND THE MOUNT CLAMPS ARE NOT
- [SDR 2023FA0000812](https://openairdocs.org/sdr/2023FA0000812), Dec 6, 2023: TENSIONER. DESTROYED. DURING FLIGHT THE PILOTS RECEIVED AN ALTERNATOR FAILURE FOR THE RH ALTERNATOR. UPON INSPECTION I NOTICED THE TENSIONER PULLEY FOR THE BELT DRIVEN ITEMS ON THE E
- [SDR 2017FA0000203](https://openairdocs.org/sdr/2017FA0000203), May 24, 2017: CLAMP. BROKEN. C/W AD 2017-01-12 DATED 2/22/17 INSTALLED NEW EXHAUST PIPE CLAMP IAW AD(F)(1) AND MSB 42-120/1 AND WI-MSB42-120 REV1. TAIL PIPE CLAMP P/N D60-7806-00-01 BROKE I
- [SDR 2017FA0000202](https://openairdocs.org/sdr/2017FA0000202), May 24, 2017: CLAMP. BROKEN. C/W AD 2017-01-12 DATED 2/22/17 INSTALLED NEW EXHAUST PIPE CLAMP IAW AD(F)(1) AND MSB 42-120/1 AND WI-MSB42-120 REV1. TAIL PIPE CLAMP P/N D60-7806-00-01 BROKE I
- [SDR 2013FA0000607](https://openairdocs.org/sdr/2013FA0000607), Sep 20, 2013: HOSE. RUPTURED. HOSE RUPTURED DURING FLIGHT TRAINING.
- [SDR 2007FA0000865](https://openairdocs.org/sdr/2007FA0000865), Aug 9, 2007: CYLINDER HEAD. FAILED. ENGINE BEGAN LOSING COOLANT BY PRESSURIZING THE COOLING SYSTEM WITH COMBUSTION PRESSURE AND BLOWING COOLANT OVERBOARD. WHEN CYLINDER HEAD WAS REMOVED, EACH CYLI

## STCs that may be installed (OpenAirDocs) (31)

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 DA 42)

- [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 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 SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA04681NY](https://openairdocs.org/stc/SA04681NY): Installation of MT-Propeller Entwicklung GmbH model MTV-6-( )-C-F/CF190-69( ) 3-blade, constant speed, full feathering propellers and spinners. MT- Propeller Entwicklung GmbH
- [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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne 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 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 SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [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 SA03804NY](https://openairdocs.org/stc/SA03804NY): Engine Refit: The presently installed versions of the TAE 125-01 or TAE 125-02-99 engine are replaced by the TAE 125-02-114 engine. This STC includes two propeller configurations: 1) MTV-6-A-C-F / CF187-129 without noise suppressor or 2) MTV-6-A-C-F / CF190-69 with noise suppressor;. Crosby Aviation (Jersey) Ltd
- [STC SA03701NY](https://openairdocs.org/stc/SA03701NY): Installation of RF-006(A) Main Wheel and RA-002(B) Nose Wheel with EA-003.7N(A) Brake System. Beringer Aero
- [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 SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [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 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 SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA02226SE](https://openairdocs.org/stc/SA02226SE): Installation of vortex generators on the wings and tail surfaces. Micro AeroDynamics Inc
- [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation
- [STC SA01918LA](https://openairdocs.org/stc/SA01918LA): Installation of AmSafe Inflatable Restraint System on the pilot and passenger seats. AMSAFE Inc
- [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation
- [STC SA02725NY](https://openairdocs.org/stc/SA02725NY): Installation of Lycoming IO-360 M1A series engines with MTV-12-B-C-F series propellers. Diamond Aircraft Industries Inc
- [STC SA03254CH](https://openairdocs.org/stc/SA03254CH) (historical): Installation of an Electric Vapor Air Cycle System. Standard Aero Business Aviation Services LLC
- [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC

## Related

- Other Diamond Aircraft Ind DA 42 aircraft: https://openairdocs.org/model/diamond-aircraft-ind-da-42/aircraft.md
- The Amateur-built UNKNOWN ENG engine: https://openairdocs.org/engine/amateur-built-unknown-eng.md

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