- Serial number
- 650-0081
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- November 12, 2025
- Expires
- November 30, 2032
- Mode S code
- AC96FC
- Registered owner
- Abotan Air LLC
- Location
- Fort Lauderdale, FL
- Owner type
- LLC
From the FAA registry file of October 20, 2026.
On this page
Airworthiness directives that may apply · 27
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.
| 1985 | 2 |
|---|---|
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1993 | 2 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 2002 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2008 | 1 |
| 2010 | 1 |
| 2013 | 1 |
| 2015 | 1 |
| 2023 | 1 |
| 2026 | 1 |
See all 28 ADs
Information bulletins that may apply · 4
Advisory, not mandatory. Matched the same way as ADs.
Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N910DFMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 650 aircraft
FAA incident reports
No FAA accident or incident reports matched to N910DFMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 650 aircraft
Service difficulty reports · 4
SDR 2016FA0000458Relay · failedON APPROACH, FLAPS FAILED AT 7 DEGREES, DIVERTED . TROUBLESHOT SYSTEM, FOUND FAULT CODE NR 4 ON FLAP CONTROLLER.REPLACED HIGH SPEED RELAY WITH NEW PART. OPS CHECKED GOOD, WORK PERFORMED IAW MM 27-54-01. AIRCRAFT RETURNED TO SERVICE.SDR 2014FA0000379Connector · brokenPILOTS REPORT UPON PLACING LANDING GEAR HANDLE IN DOWN POSITION ON APPROACH, GEAR AND WARNING LIGHTS TWO CIRCUIT BREAKERS TRIPPED AND ALL GEAR INDICATION AND FUNCTION WAS LOST. EMERGENCY GEAR SYSTEM WAS DEPLOYED. ACFT LANDED WITHOUT INCIDENT. TRACED WIRING SDR 2014FA0000311Line · chafedWHILE TAXING INTO RAMP AREA, FOLLOWING AN UNSCHEDULED ENGINE CHANGE RUN-UP. THE AUXILIARY HYDRAULIC PUMP WAS ACTIVATED TO SET THE PARKING BRAKE. THIS PRESSURIZED THE BACKUP PRESSURE SUPPLY TO THE RT ROLL SPOILER. A CLOUD OF HYDRAULIC FLUID WAS OBSERVED BY TSDR FCPA20110816Chip Detector · contaminatedAFTER DEPARTURE DURING CLIMBOUT, THE RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. AIRCRAFT FLIGHT MANUAL INDICATES TO SHUT DOWN ENGINE (WHEN PRACTICAL) AND LAND AS SOON AS POSSIBLE. THE FLIGHT CREW SHUT DOWN THE ENGINE AND RETURNED TO THE POINT OF DEPARTURE