- Registered owner
- Jager Maarten O
- Location
- Houston, TX
- Owner type
- Individual
- Serial number
- 0760
- Year built
- 2026
- Type
- Fixed wing single engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, normal
- Airworthiness date
- April 15, 2026
- Certificate issued
- April 27, 2026
- Expires
- April 30, 2033
- Mode S code
- ABDEC7
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 N864MAMatched 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 N864MAMatched 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 N864MAGeneral 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 N864MA not matched to an aircraft · 4
They name N864MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR MK9A2013FA0000403Attach Fitting · failedEXAMINED UPPER STRUT ATTACH FITTING ON ACFT, AND FOUND FRACTURE OF THE FITTING WAS DUE TO FATIGUE. CLOSE EXAMINATION SHOWED THAT THE CRACKING INITIATED BY FRETTING FATIGUE.SDR MK9A20130710Fitting · brokenDURING A ROUTINE INSPECTION OF THE RT UPPER WING LIFT STRUT, THE AFT UPPER WING LIFT STRUT FITTING, PN 2622246-202 WAS DISCOVERED TO BE BROKEN THROUGH THE BOLT HOLD THAT ATTACHES THE WING LIFT STRUT TO THE WING. WE HAVE EXAMINED THE UPPER STRUT ATTACH FITTINGSDR MK9A2013070800001Fitting · brokenDURING A ROUTINE INSPECTION, OF RT UPPER WING LIFT STRUT, AFT UPPER WING LIFT STRUT FITTING WAS DISCOVERED TO BE BROKEN THROUGH THE BOLT HOLE THAT ATTACHES THE WING LIFT STRUT TO THE WING.
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.
Earlier aircraft with this N-number · 2
These aircraft carried N864MA before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.