N914ET1997 Eurocopter Deutschland Gmbh EC135P1
Safety record in brief:No NTSB accidents or incidents since 198217 ADs may apply13 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- East Texas Air One LLC
- Owner type
- LLC
- City, state
- Nashville, TN
- Certificate issued
- Mar 28, 2018
- Expires
- Mar 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Feb 4, 1999
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Eurocopter Deutschland Gmbh
- Model
- EC135P1
- Year
- 1997
- Serial number
- 0018
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 7
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H88EU
- Mode S code
- ACA5FD
Engine
- Make and model
- P&W Canada Pw206a
- Type
- Turbo-shaft
- Power
- 621 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2018 – nowEast Texas Air One LLCNashville, TN · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (17)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-05-06 R1 | Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by… | Jan 22, 2019 | Airframe (EC135P1)Certain serial numbers: EC135 P1 0005–00829; EC135 P2 0005–00829; EC135 P2+ 0005–00829; EC135 T1 0005–00829; EC135 T2 0005–00829; EC135 T2+ 0005–00829; …. Only with: EC135: tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117C-2: tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed. |
| 2018-07-01 | Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter… | May 3, 2018 | Airframe (EC135P1)Serial numbers per Table 1 of Airbus Helicopters Alert Service Bulletin EC135-63A-017, Revision 2, dated December 5, 2016. Only with: Main transmission FS108 housing upper part P/N 4649 301 034, 4649 301 067, or 4649 301 088 installed, with a serial number listed in Table 1 of ASB EC135-63A-017. |
| 2017-03-01 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters | Mar 31, 2017 | Airframe (EC135P1)Certain serial numbers: EC135 0005–00829; MBB-BK 117 C-2 9004–9310. Only with: EC135: with tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117 C-2: with tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed. |
| 2016-11-21 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Jul 11, 2016 | Airframe (EC135P1) |
| 2015-12-09 R1 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Feb 25, 2016 | Airframe (EC135P1) |
Show all 17 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-16-24 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus… | Sep 25, 2014 | Airframe (EC135P1)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed. |
| 2014-13-09 | Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter… | Jul 30, 2014 | Airframe (EC135P1)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 installed. |
| 2014-05-01 | Eurocopter Deutschland GmbH Helicopters | Apr 14, 2014 | Airframe (EC135P1)Only with: Main gearbox (MGB) P/N 4649 010 003, 4649 010 005, 4649 010 006, 4649 010 006X, 4649 010 008, 4649 010 008X, 4649 001 007, 4649 010 010, or 4649 010 013 installed. |
| 2013-21-06 | Eurocopter Deutschland GmbH Helicopters | Jan 31, 2014 | Airframe (EC135P1)Only with: Goodrich external mounted hoist with boom support assembly P/N 44301-500, 44307-500, or 44307-500-1 installed (EC135); boom P/N 44307-500 installed (MBB-BK 117 C-2). |
| 2013-21-05 | Eurocopter Deutschland GmbH Helicopters | Dec 5, 2013 | Airframe (EC135P1)Only with: With bearing P/N LN9367GE6N2, rod P/N L671M5040205, lever P/N L671M5040101, and floor P/N L533M1014101 through L533M1014106 installed. |
| 2013-18-05 | Eurocopter Deutschland GmbH Helicopters | Oct 18, 2013 | Airframe (EC135P1)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed. |
| 2013-11-15 | Eurocopter Deutschland GmbH Helicopters | Jul 26, 2013 | Airframe (EC135P1)Certain serial numbers: EC135 P1 0005–0699; EC135 P2 0005–0699; EC135 P2+ 0005–0699; EC135 T1 0005–0699; EC135 T2 0005–0699; EC135 T2+ 0005–0699; …. Only with: BO-105A/C/S/LS A-1 with cantilever assembly P/N 105-40132 or 105-40139; BO 105 LS A-3 with cantilever assembly P/N 105-40139; EC135 (excluding S/Ns 0076, 0093, 0098, 0099, 0102, 0104, 0106, 0108, 0110, 0111, 0113, 0114, 0116, 0117, 0119) with cyclic stick locking device P/N L670M1045101/-102/-104/-105/-106/-107 and pin P/N L311M1038205 or L311M1099205; MBB-BK117 A-1 through C-1 with cyclic stick holder assembly P/N 117-41140-01, 117-41230-01 or 117-41230-03; MBB-BK117 C-2 with cyclic stick locking device P/N B856M1011101 and pin P/N L311M1038205 or L311M1099205 installed. |
| 2009-03-05 | Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and… | Mar 27, 2009 | Engine (PW206A) |
| 2004-22-11 | Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters | Dec 7, 2004 | Airframe (EC135P1)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed. |
| 2004-17-03 | Pratt & Whitney Canada PW206A and PW206E Turboshaft Engines | Sep 24, 2004 | Engine (PW206A) |
| 2000-26-12 | Eurocopter Deutschland GmbH Model EC135 P1 and EC135 T1 Helicopters | Feb 6, 2001 | Airframe (EC135P1)Certain serial numbers: 0005–0094. Only with: Hydraulic line shielding hose DN 56, P/N L290M20X1 001, installed. |
| 99-22-01 | Eurocopter Deutschland GmbH Model EC135 P1 and T1 Helicopters | Dec 17, 1999 | Airframe (EC135P1)Certain serial numbers: 0005–0120 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (13)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuel · unknown · unknownMay 26, 2023
CREW 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.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine oil · bypass valve · malfunctionedJun 16, 2022
#2 ENGINE OIL TEMP HIGH READING IN "RED"
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedFeb 15, 2020
TAIL CONE SKIN CRACKED WITH APPROXIMATELY 3.3 INCH CRACK TO RIGHT TAILCONE SKIN P.N. L533M1022216.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · frame · crackedFeb 15, 2020
LEFT 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.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · crackedFeb 15, 2020
MAIN ROTOR TRANSMISSION DECK P.N. L533M1017293 HAS CRACKS THAT MEASURE 8.50 INCHES AND 1.0 INCHES IN LENGTH.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedFeb 15, 2020
ROOF ANGLE P.N. L533M1017266 HAS A APPORX. 3.0 INCH CRACK TO THE RIGHT OUTBOARD PROTION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · angle · corrodedFeb 11, 2020
THE LOWER ANGLE P.N. L533M1052318 FOR THE ATTACHMENT OF THE MAIN ROTOR CONTROL ROD CENTER POST CORRODED BEYOND SERVICEABLE LIMITS REQUIRING REPLACEMENT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · deck plate · crackedFeb 11, 2020
THE 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.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · engine · crackedNov 18, 2019
WHILE 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 PERFORMED SUCCESSFULLY. THE #1 ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Indicating and recording systems · display · faultyMay 11, 2015
COCKPIT 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.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 13 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026