- Registered owner
- Compassion Medflight LLC
- Location
- Pikeville, KY
- Owner type
- LLC
- Serial number
- 0765
- Year built
- 2026
- Type
- Fixed wing single engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- April 30, 2026
- Certificate issued
- July 31, 2026
- Expires
- July 31, 2033
- Mode S code
- A954BC
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2019 | 1 |
|---|---|
| 2020 | 1 |
| 2023 | 1 |
Airframe · Cirrus Design SF50
AD 2023-04-20Auto Flight SystemAD 2020-03-50CommunicationsEmergency ADAD 2019-08-51Flight ControlsEmergency ADInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N700BWMatched 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 Cirrus Design SF50 aircraft
FAA incident reports
No FAA accident or incident reports matched to N700BWMatched 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 Cirrus Design SF50 aircraft
Service difficulty reports
No reports matched to N700BWGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Cirrus Design SF50 aircraft
Reports on N700BW not matched to an aircraft · 3
They name N700BW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX2055Valve · leakingMASTER REFUEL VALVE LEAKED DURING REFUELING OF AIRCRAFT USING SINGLE POINT REFUEL SYSTEM. THE VALVE IS LOCATED IN THE MAIN GEAR WHEELWELL AND THE LEAKING FUEL TRAVELS ALONG THE WIRE BUNDLE FOR THE LOWER ROTATING BEACON AND INSIDE THE BEACON CAUSING BEACON FAISDR 99ZZZX1166Indicator · malfunctionedAT FLIGHT LEVEL 8,000 FEET, NR 1 ENGINE PRECAUTIONARY SHUT DOWN. PASSING THROUGH 8,000 FEET TO 6,000 FEET, NR 1 ENGINE ITT CLIMBED TO 1,160 DEGREES CELSIUS. PILOT REDUCED POWER TO IDLE, NOTIFIED ATC OF SITUATION, PROCEEDED TO INITIATE A PRECAUTIONARY ENGINE SDR 98ZZZX2246Drain · deterioratedFOUND PITOT LEAK ON COPILOT SIDE AND STATIC SYSTEM OPEN. TROUBLESHOOTING FOUND PITOT AND STATIC DRAINS WERE SOURCE OF LEAKS DUE TO DETERIORATION OF DRAIN CORES.
STCs that may be installed · 3
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.