- Registered owners
- Charlotte-Mecklenburg Hospital Authority DBAMedcenter Air
- Location
- Charlotte, NC
- Owner type
- Corporation
- Serial number
- 219
- Year built
- 2021
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- April 19, 2021
- Certificate issued
- September 21, 2021
- Expires
- September 30, 2028
- Mode S code
- A2C7F3
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 17
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2020 | 3 |
|---|---|
| 2021 | 5 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 3 |
See all 20 ADs
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N279AHMatched 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 Pilatus PC-24 aircraft
FAA incident reports
No FAA accident or incident reports matched to N279AHMatched 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 Pilatus PC-24 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 DBCA202608190001Gearbox · contaminatedRT EGINE ROLL BACK ON CLIMB OUT. EMERGENCY DECLARED BY CREW, AIRCRAFT RETURNED TO DEPARTURE AIRPORT (135 MED FLIGHT) PATIENT ALREADY DROPPED OFF, ONLY 2 FLIGHT NURSES AND 2 CREW ON BOARD. ONSITE INVESTIGATION BY HOME BASE MX TEAM FOLLOWING DAY REVEALED EXCESSSDR DBCA2024090410005Anti-Ice Valve · failed1) CREW RECEIVED AMBER WING ANTI-ICE FAIL AND AMBER WING ANTI-ICE VALVE CLOSED MESSAGES DURING OPERATION IN ICING CONDITIONS 2) CREW RETURNED TO HOME BASE 3) MTN TROUBLESHOT RH ANTI-ICE VALVE 4) MTN DEFERRED PER MEL 30-10-01 5) MTN REMOVED LH & RH WING ANTI-ICSDR DBCA2024010800001Transducer · failed1) DURING DESCENT ON FLIGHT TO ELM CREW RECEIVED RH ENG HIGH OIL NOTICE. 2) CREW PERFORMED ENG INFLIGHT SHUTDOWN ON RH ENGINE. 3) CREW DECLARED AN EMERGENCY AND LANDED AT ELM. 4) MTN COMPLIED WITH FHDB AND WI DOWNLOADS. 5) MTN REMOVED AND REPLACED RH OIL PRESSSDR DBCA2022AA060007Heater · failed1) CREW NOTED SMOKE IN COCKPIT/CABIN AFTER TAKE OFF. 2) CREW DECLARED AN EMERGENCY AND RETURNED TO SAT. 3) MTN FOUND RH FWD CABIN ELECTRIC HEATER/FAN PCB BURNED. 4) MTN REPLACED RH FWD CABIN ELECTRIC HEATER ASSY WITH NEW.SDR DBCA202207130006Nozzle · detachedMANUFACTURER INDICATES A FAILED BRAZE WELD ON THE #1 LPT NOZZLE GUIDE VANE WHICH ALLOWED THE NOZZLE TO FLEX AND CONTACT THE #1 LPT DISK. THIS DAMAGED THE DISK SENDING DEBRIS THROUGH THE REST OF THE TURBINE SECTION CAUSING DAMAGE THROUGHOUT. ENGINEERING IS INSDR DBCA202205120003Switch · out of adjust1) ON APPROACH WITH GEAR DOWN CREW NOTED "GEAR" ON MFD AND LH GEAR ANNUN FLICKER TO WHITE UNSAFE POSITION FOR A SECOND. IN THE FLARE AFTER RETARDING POWER HEARD AN AUDIBLE GEAR WARNING 2) MTN CHECKS SHOWED NO DEFECTS ON GROUND. 3) MTN PERFORMED CHECKS ON DOWNSDR DBCA20220105001None · none1) IN FLIGHT CREW NOTED 200 LB IMBALANCE, OBSERVED FUEL LEAKING FROM LH WINGTIP AREA 2)CREW DIVERTED TO BHM 3)LANDING WAS UNEVENTFUL 4) STERLING MTN WITH PILATUS TECH SUPPORT DETERMINED THE ISSUE WAS CAUSED BY EXCESSIVE PRESSURE DURING FUELI
STCs that may be installed · 10
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-24
STC SA01124DEInstallation of an Gogo Galileo HDXSTC SA11158SCDemonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS)STC SA11832CHInstallation of an Aircraft Medical ConversionSTC SA02658SEInstallation of Garmin GI 275 Multi-Function Display SystemSTC SA00076IBInstallation of Photo luminescent Safety SystemsSTC SA01072DEAirtext system installationSTC SA01082DEInstallation of Cabin Power OutletsSTC SA01003DEAvance L3 system installationSTC SA01905WITransmitting Portable Electronic Devices (T-PED) Aircraft Tolerance TestingSTC SA01025DEMedical Interior Installation