- Registered owner
- Eurotec Vertical Flight Solutions LLC
- Location
- Eudora, KS
- Owner type
- LLC
- Serial number
- 0138
- Year built
- 2000
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 26, 2000
- Certificate issued
- May 21, 2025
- Expires
- May 31, 2032
- Mode S code
- AC9A9E
Eurocopter Deutschland EC135T1TCDS H88EUAirframe · Eurocopter Deutschland EC135T1Engine modelAmateur-built UNKNOWN ENG
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 56
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 | 3 |
| 2004 | 1 |
| 2008 | 2 |
| 2009 | 1 |
| 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 EC135T1
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 N911CKMatched 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 EC135T1 aircraft
FAA incident reports
No FAA accident or incident reports matched to N911CKMatched 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 EC135T1 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CCHA20180608001Engine · failedPILOT HEARD A LOUD BANG COMING FROM THE NR 1 ENGINE AND FELT A SLIGHT YAW. THE NR 1 ENG CHIP, NR 1 ENG FAIL AND NR 1 ENG FIRE CAUTION LIGHTS ILLUMINATED. PILOT PERFORMED A SINGLE ENGINE EMERGENCY SHUTDOWN AND MADE A RUNNING LANDING.SDR CCHA093688Inverter · intermittentNR 2 AC INVERTER INTERMITTENT OPERATION. REPLACED AC INVERTER WITH NEW S/N 561.SDR CCHA088957Gearbox · seizedMETRO AVIATION VAPOR AIR CONDITIONING SYSTEM: 90 DEGREE GEARBOX SIEZED CAUSING INTERNAL SHAFT SHEER. ALSO FLEX DRIVESHAFT TO 90 DEGREE GEARBOX COUPLING SHEERED. REPLACED 90 DEGREE GEARBOX, FLEX DRIVESHAFT, AND COMPRESSOR.SDR CCHA745CGearbox · seizedUPON TAKEOFF OF AN INTER-FACILITY TRANSPORT, THE AIR CONDITIONING 90 DEGREE GEARBOX SEIZED CAUSING SHAFT TO SHEAR IN GEARBOX AND COUPLING TO SHEAR ON DRIVESHAFT. COUPLING SHEAR CAUSED SEVERE VIBRATIONS FORCING PILOT TO RETURN TO TAKEOFF POINT AND LANDED WITHOSDR CCHA088667Hmu · defectiveENGINE DEGRADE LIGHT IN FLIGHT RETURNING TO BASE. MEMORY FAULT CODES 117 & 118. (RESOLVER & FEDEC FAIL) FAULT CODES CLEARED UPON NEXT START, HOWEVER TOT DURING START REACHED 895 FOR ONE SECOND. REPLACED HMU WITH S/N 198B.SDR CCHA087897Transducer · defectiveMAIN ROTOR GEARBXO HAS INTERMITTANT GUAGE FLUCUATIONS.SDR CCHA087050Mount · failedARIS MOUNT FAILED INSPECTION. REPLACED ARIS MOUNT
STCs that may be installed · 67
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.