# N424AM: 2006 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 2990104, 4 seats)
- Engine: [Austro E4 series](https://openairdocs.org/engine/austro-e4-series) (registry code 06400)
- Data sheets: [TCDS A57CE](https://openairdocs.org/tcds/A57CE) (Diamond Aircraft Industries GmbH), [TCDS E00081EN](https://openairdocs.org/tcds/E00081EN) (Austro Engine GmbH) (OpenAirDocs)
- Serial number: 42.AC024
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: December 16, 2006
- Certificate issued: March 1, 2025
- Expires: March 31, 2032
- Mode S code: A50A87
- Registered owner: [Skywarrior Flight Training LLC](https://openairdocs.org/faa-owner/SKYWARRIOR%20FLIGHT%20TRAINING%20LLC)
- Location: [Pensacola, FL](https://openairdocs.org/faa-place/FL/Pensacola)
- Owner type: LLC
- Owner's area on the map: 30.4730° N, 87.1865° W: Placed by OpenAirDocs at the center of ZIP code 32504, 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=424AM
- Page: https://openairdocs.org/aircraft/N424AM

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. The registry lists only the engine series, so ADs for every Austro E4 model are included.

## ADs that may apply (OpenAirDocs): 29 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 (Austro E4 series)

- [AD 2025-02-12](https://openairdocs.org/ad/2025-02-12): Reciprocating Engine Cylinder Section; Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Apr 1, 2025
- [AD 2024-19-10](https://openairdocs.org/ad/2024-19-10): Engine (Reciprocating) · Austro Engine E4 and E4P. Effective Oct 9, 2024
- [AD 2024-05-01](https://openairdocs.org/ad/2024-05-01): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Mar 11, 2024
- [AD 2022-03-03](https://openairdocs.org/ad/2022-03-03): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Feb 14, 2022
- [AD 2021-24-10](https://openairdocs.org/ad/2021-24-10): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Dec 27, 2021
- [AD 2021-17-01](https://openairdocs.org/ad/2021-17-01): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Aug 23, 2021
- [AD 2020-22-14](https://openairdocs.org/ad/2020-22-14): Reciprocating Engine Supercharger · Austro Engine E4 and E4P. Effective Dec 10, 2020
- [AD 2020-15-05](https://openairdocs.org/ad/2020-15-05): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Aug 31, 2020
- [AD 2020-14-07](https://openairdocs.org/ad/2020-14-07): Fuel Control/Reciprocating Engines and Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Aug 25, 2020
- [AD 2014-08-10](https://openairdocs.org/ad/2014-08-10): Gate controllers · Austro Engine E4. Effective Jun 3, 2014
- [AD 2011-18-19](https://openairdocs.org/ad/2011-18-19): High-pressure (HP) fuel pumps · Austro Engine E4. Effective Oct 6, 2011

### 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
- [AD 2023-20-03](https://openairdocs.org/ad/2023-20-03) (historical): Reciprocating Engine Cylinder Section, Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective Dec 11, 2023
- [AD 2021-22-20](https://openairdocs.org/ad/2021-22-20) (historical): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Nov 16, 2021
- [AD 2021-09-04](https://openairdocs.org/ad/2021-09-04) (historical): Reciprocating Engine Oil System · Austro Engine E4 and E4P. Effective May 10, 2021
- [AD 2018-18-02](https://openairdocs.org/ad/2018-18-02) (historical): Reciprocating Engine Power Section · Austro Engine E4 and E4P. Effective Nov 29, 2018
- [AD 2018-07-16](https://openairdocs.org/ad/2018-07-16) (historical): Reciprocating Engine Supercharger · Austro Engine E4 and E4P. Effective Apr 27, 2018
- [AD 2013-14-08](https://openairdocs.org/ad/2013-14-08) (historical): Waste gate controller lever · Austro Engine E4. Effective Aug 21, 2013
- [AD 2010-23-09](https://openairdocs.org/ad/2010-23-09) (historical): High pressure (HP) fuel pumps · Austro Engine E4. Effective Nov 22, 2010

## 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

None matched to N424AM.

## 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.

- [Incident 20130226002139I](https://openairdocs.org/incident/20130226002139I), Feb 26, 2013: Diamond Aircraft Ind Inc DA 42 (N424AM), Ft Lauderdale, FL, Minor damage. On 2-26-2013 at 1720Z N425AM departed runway 13 at Ft Lauderdale (fxe). On climb out pilots reported losing lt rear door. Airport security found door on the…

## 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 N424AM not matched to an aircraft (37)

They name N424AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR RAIA9912034](https://openairdocs.org/sdr/RAIA9912034), Dec 23, 1999: PROP HEAT. FAILED. 7027-STL- LEFT PROPELLER HEAT WAS INOPERATIVE. MAINTENANCE REPLACED LEFT PROPELLER ASSEMBLY.
- [SDR RAIA9910030](https://openairdocs.org/sdr/RAIA9910030), Oct 21, 1999: PUMP. FAILED. 7510 - STL - RIGHT HYD PUMP FAILED. MAINTENANCE REPLACED RIGHT HYD PUMP.
- [SDR RAIA9910014](https://openairdocs.org/sdr/RAIA9910014), Oct 12, 1999: RADIUS ROD. FAILED. 7486 - STL - LIGHT LANDING GEAR INTRANSIT LIGHT ON CONSTANTLY. MAINTENANCE REPLACED RIGHT RADIUS ROD.
- [SDR RAIA990703](https://openairdocs.org/sdr/RAIA990703), Jul 2, 1999: TRANSMITTER. FAILED. FLT 7098 - STL - LEFT FUEL PRESSURE GAUGE INOPERATIVE. MAINTENANCE REPLACED TRANSMITTER. (M)
- [SDR RAIA990636](https://openairdocs.org/sdr/RAIA990636), Jun 24, 1999: TRANSMITTER. FAILED. FLT 7482 - STL - RIGHT FUEL FLOW METER AND TOTALIZER INOPERATIVE. MAINTENANCE REPLACED RT FUEL FLOW TRANSMITTER. (M)
- [SDR RAIA990625](https://openairdocs.org/sdr/RAIA990625), Jun 18, 1999: DOUBLER. FAILED. STL - DAMAGE TO AFT FUSELAGE RESULTED FROM THE TRESTLE NOT BEING REMOVED PRIOR TO LOWERING A/C OFF OF JACKS. MAINTENANCE REPAIRED DAMAGE IAW EO NR J3200-53-014-
- [SDR RAIA990531](https://openairdocs.org/sdr/RAIA990531), May 14, 1999: HANDLE. WORN. FLT 7439 - CMI - PAX DOOR CAP LIGHT ILLUMINATED. MAINTENANCE REPLACED MOUNT BOLT FOR PAX DOOR HANDLE. (M)
- [SDR RAIA990509](https://openairdocs.org/sdr/RAIA990509), May 4, 1999: VALVE. FAILED. FLT 7042 - COU - TORQUE DROPPED ON RIGHT ENGINE, TURNED TTL OFF, TORQUE CAME BACK UP. MAINTENANCE REPLACED FUEL BYPASS VALVE ON RIGHT ENGINE. (M)
- [SDR RAIA990343](https://openairdocs.org/sdr/RAIA990343), Mar 26, 1999: GYRO. LOOSE. FLT 7096 - STL - NR 1 COMPASS IS 30 DEGREE OFF. MAINTENANCE REPLACED MOUNTING SCREWS FOR DIRECTIONAL GYRO. (M)
- [SDR RAIA990311](https://openairdocs.org/sdr/RAIA990311), Mar 9, 1999: HYDRAULIC LINE. FAILED. FLT 7034 - STL - LOST ALL HYDRAULIC PRESSURE. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR RADIUS ROD HYDRAULIC LINE. (M)
- [SDR RAIA990227](https://openairdocs.org/sdr/RAIA990227), Feb 21, 1999: CIRCUIT BREAKER. FAILED. FLT 7332 - STL - MAIN INVERTER CIRCUIT BREAKER BROKE DURING OPS CHECK. MAINTENANCE REPLACE MAIN INVERTER CIRCUIT BREAKER. (M)
- [SDR RAIA990213](https://openairdocs.org/sdr/RAIA990213), Feb 10, 1999: ENGINE. FAILED. FLT 7364 - STL - LEFT ENGINE WILL NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE. (M)
- [SDR RAIA981112](https://openairdocs.org/sdr/RAIA981112), Nov 12, 1998: BOLTS. OUT OF ADJUST. FLT 7414 - STL - PASSENGER DOOR LIGHT CAME ON IN FLIGHT. MAINTENANCE ADJUSTED SHOOT BOLTS. (M)
- [SDR RAIA981110](https://openairdocs.org/sdr/RAIA981110), Nov 9, 1998: FUEL CONTROL. FAILED. FLT 7426 - STL - RIGHT ENGINE TORQUE FLUCTUATING 3 PERCENT. MAINTENANCE REPLACED THE FUEL CONTROL ON RIGHT ENGINE. (M)
- [SDR RAIA980604](https://openairdocs.org/sdr/RAIA980604), Jun 8, 1998: RT UNIT. FAILED. FLT 7067 - STL - WEATHER RADAR INDICATION IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED WEATHER RADAR RECEIVER TRANSMITTER. (M)
- [SDR RAIA980318](https://openairdocs.org/sdr/RAIA980318), Mar 27, 1998: BYPASS VALVE. FAILED. FLT 7468 - BRL - AIRCRAFT DIVERTED TO BRL, RIGHT ENGINE TORQUE FLUCTUATED IN FLIGHT. MAINTENANCE REPLACED RIGHT ENGINE FUEL BYPASS VALVE. (M)
- [SDR RAIA980123](https://openairdocs.org/sdr/RAIA980123), Jan 22, 1998: SEAL. LEAKING. STL - FLT 7446 - HYDRAULIC PRESSURE DROPPED IN FLIGHT. REPLACE SEAL ON FITTING OF PRESSURE TRANSMITTER. (M)
- [SDR RAIA970603](https://openairdocs.org/sdr/RAIA970603), Jun 3, 1997: PRESSURE SWITCH. FAILED. STL - FLT 7468 - RIGHT AIR OFF CAPTION ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED RIGHT AIR OFF PRESSURE SWITCH. (X)
- [SDR RAIA961282](https://openairdocs.org/sdr/RAIA961282), Dec 25, 1996: STARTER/GEN. FAILED. STL - FLT 7466 - RIGHT GENERATOR WARNING ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED THE RIGHT STARTER/GENERATOR. (M)
- [SDR RAIA961214](https://openairdocs.org/sdr/RAIA961214), Dec 19, 1996: AIRSPEED IND. STUCK. PAH - FLT 7367 - FIRST OFFICERS AIRSPEED INDICATOR STAYED AT ZERO. MAINTENANCE REPLACED THE FLIGHT OFFICERS AIRSPEED INDICATOR. (M)
- [SDR RAIA960924](https://openairdocs.org/sdr/RAIA960924), Sep 22, 1996: T2 CONNECTOR. SHORTED. STL - FLT 7029 - RIGHT ENGINE EGT FLUCTUATES. MAINTENANCE REPLACED THE RIGHT T2 CANNON PLUG. (M)
- [SDR RAIA960914](https://openairdocs.org/sdr/RAIA960914), Sep 17, 1996: EGT CONNECTOR. DIRTY. BMI - FLT 7327 - RIGHT EGT FLUCTUATES WITH SRL ON, SRL OFF EGT STABILIZES. MAINTENANCE CLEANED T2 CANNON PLUG AND PERFORMED TROUBLE SHOOTING, COULD NOT DUPLICAT
- [SDR RAIA960504](https://openairdocs.org/sdr/RAIA960504), May 3, 1996: EGT HARNESS. INOPERATIVE. STL - FLT 7532 - NR 1 ENGINE EGT FLUCTUATION. REPLACED EGT HARNESS. (M)
- [SDR RAIA960238](https://openairdocs.org/sdr/RAIA960238), Feb 25, 1996: EGT COMPENSATOR. FAILED. STL - FLT NR 7054 - RIGHT ENGINE DOES NOT MAKE TARGET TORQUE FOR TAKEOFF. MAINTENANCE REPLACED EGT COMPENSATOR, GROUND RUN GOOD. (M)
- [SDR RAIA960227](https://openairdocs.org/sdr/RAIA960227), Feb 19, 1996: FLAP HANDLE. FAILED. STL - FLT NR 7334 - FLAPS STUCK AT 10 DEGREES WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED FLAP CONTROL HANDLE OPERATIONAL CHECK GOOD. (M)
- [SDR RAIA960117](https://openairdocs.org/sdr/RAIA960117), Jan 11, 1996: LIFT TRANSDUCER. FAILED. STL - FLT 7300 - DURING TAXI OUT, STICK SHAKER ACTIVATED. MAINTENANCE REPLACED RIGHT LIFT TRANSDUCER. SYSTEM OPERATIONAL CHECK GOOD. (X)
- [SDR RAIA951136](https://openairdocs.org/sdr/RAIA951136), Nov 30, 1995: O-RINGS. LEAKING. EVV - FLT NR 7423 - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR O-RINGS (P/N 173M165 AND 134M33206A). GEAR SWINGS REVEALED NORMAL OP
- [SDR RAIA951124](https://openairdocs.org/sdr/RAIA951124), Nov 17, 1995: TRANSMITTER. FAILED. STL - FLT 7073 - RIGHT OIL PRESSURE WENT TO 140. REPLACED OIL PRESSURE TRANSMITTER. (M)
- [SDR RAIA950940](https://openairdocs.org/sdr/RAIA950940), Sep 28, 1995: TQ SIGNAL COND. OUT OF ADJUST. STL - FLT 7512 - RIGHT ENGINE LOW TORQUE. ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND RUNS CHECK NORMAL. (M)
- [SDR RAIA950928](https://openairdocs.org/sdr/RAIA950928), Sep 19, 1995: TQ SIGNAL COND. OUT OF ADJUST. DEC - FLT NR 7285 - RIGHT ENGINE DID NTO MAKE TARGET TORQUE. MAINTENANCE ADJUSTED RIGGING AND RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUNS GOOD. (M)
- [SDR RAIA950850](https://openairdocs.org/sdr/RAIA950850), Aug 29, 1995: BRAKE FLUID. LOW. STL - FLT 7431 - FIRST OFFICER'S LEFT BRAKE PEDAL VERY MUSHY, SHOWS NO PRESSURE WHERE FULLY DEPRESSED. MAINTENANCE REFILLED FIRST OFFICER'S BRAKE MASTER CYLINDE
- [SDR RAIA950849](https://openairdocs.org/sdr/RAIA950849), Aug 29, 1995: TQ SIGNAL COND. OUT OF ADJUST. CMI - FLT 7437 - RIGHT ENGINE WOULD NOT MAKE TAKEOFF TORQUE BY 5 PERCENT. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER PER GARRETT DSC SETTINGS AND ADJU
- [SDR RAIA950841](https://openairdocs.org/sdr/RAIA950841), Aug 23, 1995: BRAKE SYSTEM. REQ'D SERVICE. STL - FLIGHT OFFICERS LEFT BRAKE INOP, NO PRESSURE SHOWN ON GAUGE. MAINTENANCE SERVICED BOTH FLIGHT OFFICERS BRAKE MASTER CYLINDERS, P/N ACM26810. TAXI CHECK GO
- [SDR RAIA950716](https://openairdocs.org/sdr/RAIA950716), Jul 17, 1995: ALTIMETER. FAILED. STL - 7061 - NR 1 ALTIMETER STICKING. MAINTENANCE REPLACED NR 1 ALTIMETER. PITOT/STATIC LEAK CHECK GOOD. (M)
- [SDR RAIA950317](https://openairdocs.org/sdr/RAIA950317), Mar 13, 1995: GASKETS. WORN. STL - FLT 7088 - RT ENGINE ONLY ACHIEVED 82 PERCENT TORQUE. MAINTENANCE REPLACED BLEED AIR GASKETS ON THE RIGHT ENGINE. GROUND POWER RUNS REVEALED NORMAL OPERAT
- [SDR RAIA950316](https://openairdocs.org/sdr/RAIA950316), Mar 13, 1995: SIGNAL COND. OUT OF ADJUST. STL - FLT 7088 - THE LT ENGINE ONLY ACHIEVED 82 PERCENT TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER FOR LT ENGINE. GROUND POWER RUNS REVEALED NORMAL 
- [SDR RAIA950315](https://openairdocs.org/sdr/RAIA950315), Mar 13, 1995: SWITCH. OUT OF ADJUST. STL - FLT 7508 - THE PAX DOOR CAPTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED PAX DOOR MICRO-SWITCH. SYSTEM TEST GOOD. (W)

## STCs that may be installed (OpenAirDocs) (32)

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

### Approved for the engine (Austro E4 series)

- [STC SE03232CH](https://openairdocs.org/stc/SE03232CH): Installation of Engine Preheat Kit p/n TA2925-1 for 115 volt application. Hartzell Propeller Inc

## Related

- Other Diamond Aircraft Ind DA 42 aircraft: https://openairdocs.org/model/diamond-aircraft-ind-da-42/aircraft.md
- The Austro E4 series engine: https://openairdocs.org/engine/austro-e4-series.md

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