- Registered owners
- Middle Tennessee State UniversityDepartment Of Aerospace
- Location
- Murfreesboro, TN
- Owner type
- Government
- Serial number
- FA-117
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 10, 1987
- Certificate issued
- November 17, 2022
- Expires
- November 30, 2029
- Mode S code
- AADFB5
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 35
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 1 |
|---|---|
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 2 |
| 1994 | 2 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 7 |
| 1999 | 1 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 5 |
| 2008 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 39 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N80BZMatched 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 300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N80BZMatched 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 300 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2010FA0000704Stringer · crackedDURING COMPLIANCE WITH AD 2005-01-18/ SB 53-2472 R4 INSPECTION OF THE AFT STRINGER CRACKED. RT AND LT SIDE STRINGERS NR 8, 9 AND 10 WERE CRACKED. ORDERED KITS 101-4064-1S, 101-4064-2S, 101-4064-3S, 101-4064-4S, 101-4064-5S, AND 101-4064-11S TO MODIFY STRINGESDR 2009FA0000710Bearing · failedFROM MFG: AN ELECTRICAL CURRENT FROM THE STARTER GEN OUT PUT SHAFT DISCHARGED INTO THE ENG ACCESSORY DRIVETRAIN CAUSE AN IN-FLIGHT SHUTDOWN. THE ELECTRICAL DISCHARGE PITTED THE DRIVE GEARS AND NR 1 BRG. THE PITTING OF THE BEARING LEF TO FATIGUE FAILURE OF TSDR 2008FA0000064Starter Gen · failedTHE NR 1 BEARING FAILED RESULTING IN A CATASTROPHIC FAILURE AND AN IN FLIGHT SHUTDOWN. THE ENGINE WAS REMOVED AND SENT FOR REPAIR. DURING THE FAILURE INVESTIGATION, ELECTRICAL ARCING WAS FOUND ON THE NR 1 BEARING, INPUT SHAFT, AND STARTER/GENERATOR DRIVE GEA
STCs that may be installed · 322
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 300
STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light ControllerSTC SA02658LAReplacement of the original Pratt and Whitney PT6A-60A engines and propellers with Pratt and Whitney PT6A-67A engines and MT Propeller MTV-27-1-N-C-F-R(P)/CFR260-65b propellers