- Registered owner
- East Texas Air One LLC
- Location
- Nashville, TN
- Owner type
- LLC
- Serial number
- 0018
- Year built
- 1997
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- February 4, 1999
- Certificate issued
- March 28, 2018
- Expires
- March 31, 2028
- Mode S code
- ACA5FD
Eurocopter Deutschland EC135P1TCDS H88EUAirframe · Eurocopter Deutschland EC135P1TCDS E42NEEngine · Pratt & Whitney Canada PW206A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 57
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1999 | 1 |
|---|---|
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 5 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 6 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC135P1
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N914ETMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter Deutschland EC135P1 aircraft
FAA incident reports
No FAA accident or incident reports matched to N914ETMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter Deutschland EC135P1 aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HDNA2023053010003Unknown · unknownCREW MEMBERS AND PASSENGER SMELLED FUEL IN THE CABIN. PILOT DID NOT SMELL FUEL BUT LANDED FOR MX INSPECTION FOR GOOD MEASURE. IT WAS DETERMINED TO BE ERRONEOUS AND THERE WAS ZERO FUEL LEAKAGE FROM THE AIRCRAFT OR ANY COMPONENTS.SDR HDNA2022061610008Bypass Valve · malfunctioned#2 ENGINE OIL TEMP HIGH READING IN "RED"SDR HDNA2020021503018Deck Plate · crackedMAIN ROTOR TRANSMISSION DECK P.N. L533M1017293 HAS CRACKS THAT MEASURE 8.50 INCHES AND 1.0 INCHES IN LENGTH.SDR HDNA202002153018Angle · crackedROOF ANGLE P.N. L533M1017266 HAS A APPORX. 3.0 INCH CRACK TO THE RIGHT OUTBOARD PROTION.SDR HDNA2020020218Skin · crackedTAIL CONE SKIN CRACKED WITH APPROXIMATELY 3.3 INCH CRACK TO RIGHT TAILCONE SKIN P.N. L533M1022216.SDR HDNA202002150118Frame · crackedLEFT HAND AND RIGHT HAND FUSELAGE FRAME 5 STRUCTURE P.N. L533M1105219 (RIGHT) AND P.N. L533M1088219 (LEFT) HAVE CRACKS TO THE INSIDE RADIUS OF THE FRAME DOUBLERS.SDR HDNA2020021118Deck Plate · crackedTHE RIGHT HAND ENGINE DECK P.N. L533M1018246 HAS A 4.5" AND A 5.5 INCH CRACK 4 INCHES AND 1 INCH AFT OF THE INBOARD ENGINE MOUNT.SDR HDNA202002110018Angle · corrodedTHE LOWER ANGLE P.N. L533M1052318 FOR THE ATTACHMENT OF THE MAIN ROTOR CONTROL ROD CENTER POST CORRODED BEYOND SERVICEABLE LIMITS REQUIRING REPLACEMENT.SDR HDNA2019111800381Engine · crackedWHILE ON FINAL APPROX 200-250 FEET WHEN THE NUMBER 1 ENGINE CHIP AND OIL PRESSURE LIGHT CAME ON CONFORMATION OF THESE INDICATIONS CONFIRMED WITH OIL PRESSURE INDICATION AT 0 PSI. THE #1 ENGINE WAS SECURED, AN EMERGENCY WAS DECLARED WITH A RUN ON LANDING PERFORSDR HDNA20150513003Display · faultyCOCKPIT DISPLAY SYS, CDS INTERMITTENTLY DISPLAYS INACCURATE INFORMATION WHEN AMBIENT AIR TEMP IS ABOVE 85 DEGREES. THIS COMPONENT WAS INSTALLED LESS THAN A YEAR AGO & 476 HRS AGO. THIS WAS AN 0.0 TSO PART & SHOULD NOT BE FAULTY THIS SOON.SDR 99ZZZX1422Mount · leakingFLUID LEAKED OUT-PIN RETRACTED.SDR 99ZZZX1421Transmission · making metalMETAL CONTAMINATION OF OIL SYSTEM.SDR 99ZZZX1420Shaft · wornDRIVE SPLINES WERE DOWN AND WOULD NOT TURN BLOWER.SDR 98ZZZX1699Engine · malfunctionedTWO MINUTES AFTER TAKEOFF, POWER DECREASED TO 20 - 40 PERCENT OF NORMAL ON NR 1 ENGINE. RETURNED FOR PRECAUTIONARY LANDING. ENGINE APPEARED TO FUNCTION NORMALLY BELOW 50 PERCENT TORQUE, ABOVE 50 PERCENT, TORQUE WOULD DECREASE. NO FURTHER INCIDENT OCCURRED.
STCs that may be installed · 69
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.