- Registered owner
- Lta Group Holdings LLC
- Location
- Amarillo, TX
- Owner type
- LLC
- Serial number
- 0884
- Year built
- 2010
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 31, 2010
- Certificate issued
- October 10, 2025
- Expires
- October 31, 2032
- Mode S code
- AC2DC9
Eurocopter Deutschland EC 135 T2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 T2+TCDS E34NEEngine · Turbomeca ARRIUS-2B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2007 | 1 |
| 2008 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2019 | 3 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 3 |
| 2025 | 4 |
| 2026 | 6 |
Airframe · Eurocopter Deutschland EC 135 T2+
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 N884MEMatched 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 EC 135 T2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N884MEMatched 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 EC 135 T2+ aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR E3MA2019051000001Actuator · corrodedDURING COMPLIANCE WITH EASB EC135-67A-039 PITTING WAS DISCOVERED ON CONNECTING ROD OF THE LATERAL HYDRAULIC ACTUATOR.SDR E3MA20150821001Engine · leakingDURING FLIGHT THE PILOT HEARD A NOISE FROM THE ENG WITH AN ASSOCIATED ACFT YAW. THE TORQUE OF THE ENG FELL BELOW THE OPPOSING ENG FOLLOWED BY A CHIP CAUTION ON THE CAD. THE ENG THEN TORQUE INDICATION CAME BACK TO MATCH THE OPPOSING ENG. UPON POST FLIGHT WALSDR E3MA201210180001Bolt · wornDURING FLIGHT, THE PILOTS WERE COMPLAINING OF A VIBRATION IN THE MAIN ROTOR. THE MAIN ROTOR TRACK AND BALANCE WAS CHECKED AND NECESSARY ADJUSTMENTS WERE MADE TO BRING IT WITHIN ACCEPTABLE LIMITS. THE VIBRATION REMAINED DURING FLIGHT. AFTER FURTHER INSPECTIO
STCs that may be installed · 71
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.