- Registered owner
- Metro Aviation Inc
- Location
- Shreveport, LA
- Owner type
- Corporation
- Serial number
- 0485
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- May 2, 2014
- Expires
- May 31, 2027
- Mode S code
- ACF952
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2000 | 1 |
|---|---|
| 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 EC 135 P2
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 N935MCMatched 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 P2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N935MCMatched 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 P2 aircraft
Reports on N935MC not matched to an aircraft · 1
They name N935MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HDNA2014F00129Static Inverter · malfunctionedIN CRUISE FLIGHT, THE ACFT ROLLED RT AND LT UN-COMMANDED ABOUT 5 PERCENT. THE INVERTER CAUTION LIGHT ALSO ILLUMINATED. PILOT MADE A PRECAUTIONARY LANDING. SYSTEM AFFECTED WAS THE ROLL SAS BECAUSE OF THE INVERTER FAILURE.SDR 2007F00041Blade · crackedVISUAL INSPECTION REVEALED CRACK IN M/R BLADE APPROX. 103 INCHES FROM BLADE ROOT. CRACK RUN FROM AFT OF SPAR TO THE TRAILING EDGE.
STCs that may be installed · 72
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.