- Registered owners
- Carolinas Healthcare System DBAMedcenter Air
- Location
- Charlotte, NC
- Owner type
- Corporation
- Serial number
- 0755
- Year built
- 2009
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- June 9, 2009
- Certificate issued
- September 22, 2009
- Expires
- May 31, 2028
- Mode S code
- A52E81
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 N433CMMatched 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 N433CMMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2019123119100Frame · crackedCRACK FOUND AT FRAME 5A RIGHT TOP MOST HOLE EMANATING FROM RIVET HOLE TO EDGE OF DOUBLER APPROX .25 IN LENGTH.
WILL REPAIR CRACK AT FRAME 5A IAW EA 23-5310-EA-1480 REV. DATED 06/23/2016 FRAME PROCEDURE ON FAA FORM 337.SDR QMLA2018052918062Angle · crackedDURING A 1000 HOUR AIRFRAME INSPECTION, THE MECHANIC FOUND A CRACK OF APPROXIMATELY 2.25 INCHES IN LENGTH ON THE RT FORWARD MAIN TRANSMISSION DECK AT THE TRANSITION TO THE CABIN ROOF ABOVE THE NR 4 BULKHEAD. THE CRACK IS LOCATED IN THE RADIUS OF THE DOUBLER THSDR QMLA2013071613100Pivot · corrodedTHE PILOT REPORTED THAT ON FINAL APPROACH, THE LT TAIL ROTOR PEDAL BECAME STUCK, AND THE ACFT BEGAN FLYING TO THE RIGHT. DECIDED TO ABORT APPROACH, COULD NOT GAIN CONTROL TO LAND AT DESTINATION. DECLARED AN EMERGENCY, AND AFTER 20 SECONDS, PEDAL MOVEMENT RSDR QMLA2012073012121Circuit Card · failedDURING TAKEOFF, THE PILOT AND MEDICAL CREW ALL DETECTED AN ODOR OF BURNING METAL AND RUBBER. PILOT IMMEDIATELY RETURNED TO THE AIRPORT AND SHUTDOWN AIRCRAFT. FOUND THAT THE Z300 CARD IN THE BATTERY MASTER BOX HAD FAILED. OPEN
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.