- Registered owner
- Med-Trans Corp
- Location
- Denton, TX
- Owner type
- Corporation
- Serial number
- 1083
- Year built
- 2012
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- March 15, 2013
- Certificate issued
- June 3, 2020
- Expires
- June 30, 2027
- Mode S code
- A08FC3
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
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 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 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 N135WLMatched 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 N135WLMatched 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
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M3XA20231216002Bypass Valve · unserviceablePILOT REPORTED #1 ENGINE OIL TEMPERATURE EXCEEDANCE OF 129.5. PLACED THE #1 ENGINE TO IDLE AND EXECUTED A SUCCESSFUL PRECAUTIONARY LANDING WITH A PATIENT ON BOARD TO KROA AIRPORT. THE PATIENT WAS TRANSPORTED BY GROUND. THE MECHANIC REPLACED THE #1 ENGINE OISDR M3XA20210506004Bypass Valve · malfunctionedPILOT REPORTED IN CRUISE FLIGHT THAT THE #1 ENGINE OIL TEMPERATURE WAS HIGH. MECHANIC REPLACED #1 ENGINE OIL BYPASS VALVE.SDR M3XA2017090507Gearbox · warning messagePILOT MADE A PL FOR TAIL ROTOR CHIP LIGHT INDICATION. PERFORMED INSPECTION IAW MSM 05-51-00, 6-13 AND AMM 65-40-00, 6-1 AND FIGURE 601. FOUND ONE SMALL FINE HAIR ON THE CHIP DETECTOR, DEFINED AS CAT A. CLEANED AND REINSTALLED CHIP DETECTOR AND PERFORMED
Reports on N135WL not matched to an aircraft · 3
They name N135WL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR RMXA1221200903292Support Beam · crackedDURING A SCHEDULED INSP, A CRACK WAS DISCOVERED IN A SUPPORT BEAM JUST BELOW FRAME 5 IN THE FUSELAGE TAILCONE. A REPAIR SCHEME REQUEST WAS SUBMITTED AND RECEIVED FROM THE MFG. THE CRACK WAS STOPPED DRILLED AND A REPAIR DOUBLER FROM 0.050" ALUMINUM WAS INSTALSDR RMXA1221200903291Frame · crackedDURING A SCHEDULED INSP, A CRACK WAS DISCOVERED IN THE FUSELAGE TAILCONE SUPPORT FRAME PN L533M1022205. REPAIR SCHEME REQUEST SUBMITTED TO MFG AND RECEIVED. REPAIR WILL CONSIST OF INSTALLED A SB DOUBLER ON THE FRAME. THIS HAD BEEN A ISSUE ON EARLIER SN ACFT, SDR RMXA0329121708Fairing · delaminatedDURING A SCHEDULED INSP, FOUND THE TAIL ROTOR DRIVESHAFT FAIRING HAS A DELAMINATED AREA ON THE TOP SURFACE. THE DELAMINATED AREA WAS 8 INCHES L X 2.25 INCHES W. REPAIR SCHEME WAS PROVIDED FROM THE MFG AND THE FAIRING WAS REPAIRED.
STCs that may be installed · 74
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.