# N101DA: 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 2990004, 4 seats)
- Engine: [Thielert TAE-125-01](https://openairdocs.org/engine/thielert-tae-125-01) (registry code 59300)
- Data sheets: [TCDS A57CE](https://openairdocs.org/tcds/A57CE) (Diamond Aircraft Industries GmbH), [TCDS E00069EN](https://openairdocs.org/tcds/E00069EN) (Continental Aerospace Technologies GmbH) (OpenAirDocs)
- Serial number: 42.125
- Year built: 2006
- Type: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: May 8, 2006
- Certificate issued: April 4, 2024
- Expires: April 30, 2031
- Mode S code: A008B7
- Registered owner: [Flying High Again LLC](https://openairdocs.org/faa-owner/FLYING%20HIGH%20AGAIN%20LLC)
- Location: [Mount Juliet, TN](https://openairdocs.org/faa-place/TN/Mount%20Juliet)
- Owner type: LLC
- Owner's area on the map: 36.1825° N, 86.4909° W: Placed by OpenAirDocs at the center of ZIP code 37122, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=101DA
- Page: https://openairdocs.org/aircraft/N101DA

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): 26 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 (Thielert TAE-125-01)

- [AD 2015-02-01](https://openairdocs.org/ad/2015-02-01): Clutch assemblies · Technify Motors TAE 125-01 and TAE 125-02-99. Effective Feb 13, 2015
- [AD 2013-24-06](https://openairdocs.org/ad/2013-24-06): Engine clutch housing (crankcase assembly) · Technify Motors TAE 125-01. Effective Dec 30, 2013
- [AD 2012-26-13](https://openairdocs.org/ad/2012-26-13): Software mapping · Thielert Aircraft Engines TAE 125-01, TAE 125-02-114 and TAE 125-02-99. Effective Feb 13, 2013
- [AD 2010-11-09 R1](https://openairdocs.org/ad/2010-11-09-R1): Proportional pressure reducing valves (PPRVs) · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Apr 11, 2012
- [AD 2010-06-12 R1](https://openairdocs.org/ad/2010-06-12-R1): Rail pressure control valve · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Feb 3, 2012
- [AD 2010-14-21](https://openairdocs.org/ad/2010-14-21): Engine power · Thielert Aircraft Engines TAE 125-01. Effective Aug 17, 2010
- [AD 2010-04-06](https://openairdocs.org/ad/2010-04-06): Reduced control of aircraft · Thielert Aircraft Engines TAE 125-01. Effective Mar 30, 2010
- [AD 2009-24-10](https://openairdocs.org/ad/2009-24-10): Broken piston cooling oil nozzles · Thielert Aircraft Engines TAE 125-01. Effective Jan 4, 2010

### 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 2011-23-01](https://openairdocs.org/ad/2011-23-01) (historical): Clutch assemblies · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Nov 22, 2011
- [AD 2011-07-09](https://openairdocs.org/ad/2011-07-09) (historical): Full- authority digital electronic control (FADEC) software · Thielert Aircraft Engines TAE 125-01, TAE 125-02-114 and TAE 125-02-99. Effective May 5, 2011
- [AD 2010-18-02](https://openairdocs.org/ad/2010-18-02) (historical): Disc springs · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Sep 9, 2010
- [AD 2010-11-09](https://openairdocs.org/ad/2010-11-09) (historical): Proportional Pressure Reducing Valve (PPRV) · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Jul 13, 2010
- [AD 2010-06-12](https://openairdocs.org/ad/2010-06-12) (historical): Rail Pressure Control Valve · Thielert Aircraft Engines TAE 125-01 and TAE 125-02-99. Effective Apr 20, 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 N101DA.

## FAA accident and incident reports

None matched to N101DA.

## Reports on N101DA not matched to an aircraft (2)

They name N101DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19901210062419I](https://openairdocs.org/incident/19901210062419I), Dec 10, 1990: Boeing 767232 (N101DA), Covington - Cin, OH. Eicas message nose air-ground disagree on nose gear. Declared emergency. Landed without incident.
- [Incident 19900520037319I](https://openairdocs.org/incident/19900520037319I), May 20, 1990: Boeing 767232 (N101DA), Ontario, CA. NR1 engine stalled on takeoff climb. Shut down and landed. Vsv feedback cable broke. Caused compressor stall.

## 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 N101DA not matched to an aircraft (42)

They name N101DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DL767050678](https://openairdocs.org/sdr/DL767050678), Nov 3, 2005: LINE. FAILED. ON TOUCHDOWN LOST CTR HYD SYSTEM. FOUND DISCONNECT ON ADP PRESSURE LINE FAILED. REPLACED SAME.
- [SDR DL767050669](https://openairdocs.org/sdr/DL767050669), Oct 28, 2005: FAN. SEIZED. FUMES REPORTED IN MID CABIN OVERHEAD AREA, DIVERSION RDU. FOUND GASPER FAN AT FAULT. REPLACED SAME.
- [SDR DL767050481](https://openairdocs.org/sdr/DL767050481), Aug 23, 2005: POWER SUPPLY. INOPERATIVE. EMERGENCY LIGHTS INOP THROUGHOUT CABIN. REPLACED M9008 POWER SUPPLY, CHECKS OK.
- [SDR DL767050317](https://openairdocs.org/sdr/DL767050317), Jun 3, 2005: SKIN. CORRODED. REPAIR OF CORROSION WAS FOUND AT SEVERAL LOCATIONS ALONG STRINGER 38R AND 39R AF FS 434. THE DAMAGE TO THE BUTT SPLICE STRIP WAS BLENDED AND HFEC INSPECTED. SKI
- [SDR DL767041075](https://openairdocs.org/sdr/DL767041075), Dec 1, 2004: BOLT. MISINSTALLED. FOUND BY FAA INSPECTOR, RIGHT MLG WING DOOR LOWER AFT MOUNT BOLT INSTALLED INCORRECTLY. BOLT IS DAMAGED AND CENTER SHIMS ARE MISSING. INSTALLED NEW BOLT AND HAR
- [SDR DL767031124](https://openairdocs.org/sdr/DL767031124), Dec 19, 2003: PANEL. GOUGED. THE GORE PANEL ON THE AFT P-DOME WAS FOUND WITH A GOUGE NEAR STIFFENER 11R. THE GOUGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER
- [SDR DL767031122](https://openairdocs.org/sdr/DL767031122), Dec 19, 2003: PANEL. CRACKED. INSPECTION OF THE AFT P-DOME GORE PANELS PER AD 88-19-03 REVEALED A CRACK AT A FASTENER LOCATION COMMON TO THE STIFFENER 13R LAP JOINT. THE CRACK WAS REMOVED WI
- [SDR DL767031121](https://openairdocs.org/sdr/DL767031121), Dec 19, 2003: LAP JOINT. CRACKED. DURING INSPECTION OF THE AFT P-DOME AT FS 1582 A CRACK WAS FOUND AT A FASTENER COMMON TO THE STIFFENER 5L WEB LAP JOINT. THE CRACK WAS REMOVED BY TRIMMING OUT T
- [SDR DL767030640](https://openairdocs.org/sdr/DL767030640), Jul 13, 2003: WIRE HARNESS. CHAFED. FOUND LEFT AFT CHILLER WIRE HARNESS BURNT THROUGH DUE CHAFFING ON CHILLER RACK FRAME. SECURED HARNESS ASSY AND PULLED C/B'S. VERIFIED NO POWER TO HARNESS ASSY. 
- [SDR DL767030598](https://openairdocs.org/sdr/DL767030598), Jun 29, 2003: SKIN. DENTED. SKIN DENT REPAIR THE FUSELAGE SKIN WAS DENTED AT FS 1263 NEAR STRINGER 37L, DUE TO CONTACT WITH GROUND EQUIPMENT. THE DENT WAS REMOVED WITH A CUTOUT IN THE SKIN
- [SDR DL767030281](https://openairdocs.org/sdr/DL767030281), Mar 27, 2003: WEDGE. DEBONDED. SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 422819-14.
- [SDR DL767021220](https://openairdocs.org/sdr/DL767021220), Oct 22, 2002: WIRE HARNESS. DAMAGED. EMERGENCY PATH LIGHT AT SEAT 31AB INOP. REPLACED UNDERSEAT HARNESS. LIGHT OPERATES NORMALLY.
- [SDR DL767021090](https://openairdocs.org/sdr/DL767021090), Sep 16, 2002: LIGHT. INOPERATIVE. THE 1R EXTERIOR EMERGENCY LIGHT INOP. REPLAMPED SAME.
- [SDR DL767020785](https://openairdocs.org/sdr/DL767020785), Jul 10, 2002: LINE. SPLIT. ON CLIMBOUT, 'C' SYS HYD QTY MSG ACTIVATED. 'C' SYS QTY CK'D AT 0.31 FOUND BROKEN LINE IN RT UPPER OUTBD W/W. RPLD SAME
- [SDR DL767021295](https://openairdocs.org/sdr/DL767021295), May 10, 2002: CONNECTOR. SHORTED. NR 2 ENG INFLT SHUTDOWN RT OIL FILTER LIGHT CAME ON. FOUND SHORT BETWEEN D4254P AND D4258J. REPLACED PLUG D4258J. SYSTEM CHECKS NORMAL.
- [SDR DL767011700](https://openairdocs.org/sdr/DL767011700), Oct 22, 2001: RIB. DAMAGED. INBOARD AFT RT FLAP WAS FOUND WITH ELONGATED FASTENER HOLES IN THE LEADING EDGE RIBS. REPAIR PER ER/A 410559-14 AND NORDAM EWO E0034025, REV A.
- [SDR DL767010926](https://openairdocs.org/sdr/DL767010926), Jun 5, 2001: FRAME. CRACKED. ACCOMPLISHMENT OF PERMANENT REPAIR FOR CRACKED CHORD PER SB 767-53-0078.
- [SDR DL767010237](https://openairdocs.org/sdr/DL767010237), Feb 10, 2001: FAN. ODOR. AFTER ENG START ELECTRICAL ODOR IN COCKPIT AND BY L1 DOOR. FOUND EICAS MSG, FWD SUP FAN 1. SECURED C/B H18. RAN ENGS, PACKS, CKD E/E COMPARTMENT, FWD GALLEY. UN
- [SDR DL767010196](https://openairdocs.org/sdr/DL767010196), Feb 4, 2001: BATTERY PACK. DISCHARGED. COACH CLASS SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP ON BOTH LEFT AND RIGHT SIDE. REPLACED BOTH LEFT AND RIGHT BATTERY PACKS.
- [SDR DL767001427](https://openairdocs.org/sdr/DL767001427), Jul 29, 2000: SLIDE. MISINSTALLED. R1 CABIN DOOR SLIDE NOT PROPERLY ATTACHED TO DOOR. REPLACED R1 DOOR SLIDE PER M/M, OPS CHECKS NORMAL.
- [SDR DL767000859](https://openairdocs.org/sdr/DL767000859), Apr 28, 2000: BRACE. MISMANUFACTURED. NR 1 ENGINE DIAGIONAL BRACE REPLACED WITH NEW THREE PIECE DIAGONAL BRACE ASSY TO MEET AD 200-07-05 REQUIREMENTS. NEW DIAG BRACE ASSY 0.033 INCH TOO SHORT WITH M
- [SDR DL767000812](https://openairdocs.org/sdr/DL767000812), Apr 25, 2000: BULKHEAD. CORRODED. CORROSION DAMAGE FOUND ON THE AFT FACE AND FLANGES OF THE REAR SPAR BULKHEAD FITTINGS. THE CORROSION IS LOCATED JUST FWD OF THE FWD EDGE OF THE MLH W/W UPPER PR
- [SDR DL767992553](https://openairdocs.org/sdr/DL767992553), Nov 20, 1999: MODULE. CRACKED. ON TOUCHDOWN, LOST CTR HYD SYS AND INTERMITTENT BRAKE VLV LIGHT WITH ALT SELECTED. RES BRAKE VLV EICAS MSG. CTR HYD SYS SHOWS .09 RF. NO RES BRAKE OR OR STEERIN
- [SDR DL767991014](https://openairdocs.org/sdr/DL767991014), May 8, 1999: RELAY. FAILED. RELAY K459 SHORTED OUT IN P-33 PANEL, CAUSING ELECTRICAL SHORT. REMOVED P33 PANEL. REPLACED K459 RELAY. FOUND HEAT DAMAGE ON TB090. REPLACED ALL HIGH DENSITY BL
- [SDR DL767990986](https://openairdocs.org/sdr/DL767990986), May 6, 1999: ENGINE. FAILED. IN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE.
- [SDR DL767980499](https://openairdocs.org/sdr/DL767980499), Mar 2, 1998: WEDGE. DELAMINATED. THE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-1
- [SDR DL767972547](https://openairdocs.org/sdr/DL767972547), Dec 5, 1997: STRINGER. CORRODED. CORROSION DAMAGE BEYOND LIMITS FOUND ON STR 34R FROM STA 550 TO STA 654. REPAIRED PER ERA 331055-14.
- [SDR DL767972546](https://openairdocs.org/sdr/DL767972546), Dec 5, 1997: STRINGER. CORRODED. STR 30R CORRODED BEYOND LIMITS BETWEEN STA 1439 AND 1461. ALSO, STR 32R CORRODED BEYOND LIMITS BETWEEN STA 1417 AND 1439. REPAIRED PER ERA 331054-14.
- [SDR DL767972545](https://openairdocs.org/sdr/DL767972545), Dec 5, 1997: FLOORBEAM. CORRODED. CORROSION FOUND ON STA 287 FLOORBEAM UPPER CHORD FROM LBL 10 TO THE RT EOP. REPAIRED PER ERA 331029-14.
- [SDR DL767972544](https://openairdocs.org/sdr/DL767972544), Dec 5, 1997: FLOORBEAM. CRACKED. FS 246 FLOORBEAM UPPER WEB FOUND WITH TYP CRACK AT RBL 20 UNDERNEATH THE RBL 20 STIFFENER. ALSO, STIFFENER CRACKED. ADDITIONALLY, CORROSION FOUND ON WEB AND MID
- [SDR DL767972543](https://openairdocs.org/sdr/DL767972543), Dec 5, 1997: SKIN. CORRODED. ADDITIONAL CORROSION DAMAGE FOUND NEAR EXISTING REPAIRED CORROSION DAMAGE (REF ERA208585-14). REPAIR IS REMOVED AND A LARGER REPAIR INSTALLED. REPAIR PER ERA 20
- [SDR DL767972513](https://openairdocs.org/sdr/DL767972513), Dec 1, 1997: SKIN. CORRODED. THE FUSELAGE SKIN AT BS 1202, STR 39R WAS FOUND CORRODED. THE CUTOUT IS APPROX 5.5 X 1.75 IN THE SKIN. REPAIRED PER ERA 331052-14.
- [SDR DL767971804](https://openairdocs.org/sdr/DL767971804), Sep 15, 1997: POWER SUPPLY. INOPERATIVE. TWO SECTIONS OF EMERGENCY FLOOR TRACK LIGHTS IN REAR SECTION OF AIRCRAFT INOP. REPLACED BATTERY PACKS AND RACKS M9009 AMD M9010. EMERGENCY FLOOR TRACK LIGHTS OP
- [SDR DL767971379](https://openairdocs.org/sdr/DL767971379), Jul 14, 1997: POWER SUPPLY. INOPERATIVE. AFT SECTION OVERHEAD AISLE EMERGENCY LIGHTS AND R-4 DOOR EXIT LIGHT INOP. REPLACED POWER SUPPLY. SYSTEM CHECKS NORMAL.
- [SDR DL767971332](https://openairdocs.org/sdr/DL767971332), Jul 8, 1997: SLAT. DELAMINATED. THE NR 9 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE A 4 INCH INBOARD/OUTBOARD X 2 FWD/AFT SECTION OF THE UPPER SKIN DELAMINATED. THE DAMAGE IS LOCA
- [SDR DL767970299](https://openairdocs.org/sdr/DL767970299), Jan 18, 1997: SKIN. CRACKED. DURING A LAYOVER VISIT, SKIN WAS FOUND CRACKED AND CORRODED AT STRINGER 32R AND 34R BETWEEN FS 1461 AND FS 1480. BOTH WERE REPAIRED PER SRM.
- [SDR DL767962074](https://openairdocs.org/sdr/DL767962074), Sep 7, 1996: SWITCH. MALFUNCTIONED. ALL EXTERIOR EMERGENCY LIGHTS REPORTED ON. RETURNED TO GATE. ASSOCIATED WITH RT AFT ENT DOOR LIGHT CYCLING ON AND OFF. REPLACED PROX SWITCH AT RT AFT DOOR, SYST
- [SDR DL767961965](https://openairdocs.org/sdr/DL767961965), Aug 25, 1996: COFFEE MAKER. FAULTY. THE F/C NR 2 COFFEE MAKER STARTED SMOKING WHEN BREW BUTTON WAS PRESSED. SMOKE STOPPED AFTER CIRCUIT BREAKER PULLED. REPLACED COFFEE MAKER. SYSTEM CHECK GOOD.
- [SDR DL767961519](https://openairdocs.org/sdr/DL767961519), Jun 24, 1996: WIRE. BROKEN. AFT GALLEY EMERGENCY TRACK LIGHTS ARE OUT. REPAIRED BROKEN WIRE ON TRACK, CHECKS GOOD.
- [SDR DL767960638](https://openairdocs.org/sdr/DL767960638), Mar 22, 1996: COFFEE MAKER. FAILED. SMOKE AND HOT SMELL IN AFT GALLEY. HOT WATER COMING OUT OF COLD WATER FAUCET UNDER LT SIDE COFFEE MAKERS. FOUND NR 3 COFFEE MAKER OVERHEATING. PULLED AND COLLAR
- [SDR DL767954424](https://openairdocs.org/sdr/DL767954424), Nov 18, 1995: HYD LINE. CHAFED. LT HYD SYS PRES MESSAGE, HYD QTY APPEARED TO STOP DECREASING AFTER TURNING OFF LEFT HYD SYSTEM. FOUND LEFT ENG HYD LINE FROM ENG PUMP CHAFING. REPLACED HYD LINE
- [SDR DL767953201](https://openairdocs.org/sdr/DL767953201), Jul 25, 1995: WINDOW. SHATTERED. DURING CRUISE, FIRST OFFICER'S NR 1 WINDSHIELD SHATTERED, LANDED MCO. REPLACED WINDOW AND CONTROLLER, GROUND OPERATION NORMAL.

## 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 Thielert TAE-125-01 engine: https://openairdocs.org/engine/thielert-tae-125-01.md

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