- Registered owner
- At Aero LLC
- Location
- Wilmington, DE
- Owner type
- LLC
- Serial number
- BB-863
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- November 10, 1983
- Certificate issued
- June 1, 2020
- Expires
- June 30, 2027
- Mode S code
- AAE184
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 56 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N80WMMatched 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 Beech 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N80WMMatched 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 Beech 200 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2013FA0000588Nut · wornMLG ACTUATOR NUT FOUND SEVERLY WORN DURING 30 MONTH INSPECT AND LUBRICATION REQUIREMENT. THE ACTUATOR IN QUESTION HAD BEEN O/H APPROXIMATELY 17 MONTHS PRIOR. THE 1000 CYCLE LIMIT WAS THE REASON FOR INSPECTION.SDR 20001218SH026Nut · separatedTHREADED INSERT SEPARATED FROM LANDING GEAR ACTUATOR ROD CAUSING AN UNSAFE LANDING GEAR INDICATION IN COCKPIT. THE ACTUATOR NUT WAS INSTALLED NEW IN THE LANDING GEAR ACTUATOR. POSSIBLE CAUSE: MANUFACTURING DEFECT. (X)
STCs that may be installed · 409
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller