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Aircraft record

N80BZBeechcraft 300

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply3 service difficulty reports

Registration
Valid
expires Nov 30, 2029
Based in
Murfreesboro, TN
owner city / state
Engine
PT6A-60A · 1050 hp
P&W Canada
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Middle Tennessee State University
Owner type
Government
City, state
Murfreesboro, TN
Certificate issued
Nov 17, 2022
Expires
Nov 30, 2029
Airworthiness
Standard · Normal
Airworthiness date
Apr 10, 1987

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Beechcraft
Model
300
Serial number
FA-117
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
19
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
AADFB5

Engine

Make and model
P&W Canada Pt6a-60a
Type
Turbo-prop
Power
1050 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2022 – nowMiddle Tennessee State UniversityMurfreesboro, TN · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (6)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2022-03-23Rudder Control SystemFeb 22, 2022Airframe (300)Only with: Equipped with a Garmin G1000 integrated avionics system installed per STC SA01535WI-D with GSA 9000 yaw servo software version 2.13 or earlier.
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (300)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; …
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.
98-04-24Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes…Mar 13, 1998Airframe (300)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (300)
Show all 6 ADs
ADSubjectEffectiveApplies to
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (300)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; …

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuselage · stringer · crackedJul 7, 2010

    DURING 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 STRINGERS NR 5 TO NR 11 ON BOTH SIDES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · bearing · failedMar 3, 2009

    FROM 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 THE BRG AND SUBSEUENT ENGINE FAILURE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · starter gen · failedNov 19, 2007

    THE 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 GEAR. SD ADVISORY NR AV-2007-05 ISSUED THAT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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