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Aircraft record

N2009X1978 Beechcraft 76

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply6 service difficulty reports

Registration
Valid
expires Dec 31, 2029
Based in
Griffith, IN
owner city / state
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Griffith Aviation INC
Owner type
Corporation
City, state
Griffith, IN
Certificate issued
Dec 3, 2019
Expires
Dec 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Sep 1, 1978

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
76
Year
1978
Serial number
ME-66
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A195AC

Engine

Make and model
Lycoming O&Vo-360 Ser
Type
Reciprocating
Power
180 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. 2019 – nowGriffith Aviation INCGriffith, IN · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (2)

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
2021-08-06Textron Aviation Inc. AirplanesMay 25, 2021Airframe (76)Certain serial numbers: 76 ME-1–ME-437. Only with: Excludes airplanes with MLG "A" frame assemblies P/N 105-810023-0083 (left) and P/N 105-810023-0084 (right) installed.
99-05-13Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55…Apr 19, 1999Airframe (76)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798

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

Service Difficulty Reports (6)

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.

  • Power plant · mount · brokenJul 7, 2006

    BOTH LT AND RT ENGINE MOUNT TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · attach angle · brokenJul 7, 2006

    BOTH LT AND RT ENGINE MOUNTS TO FIREWALL ATTACH POINTS BROKE OUT AFT OF THE FIREWALL IN THE UPPER OB POINT. THIS BREAKAGE IS DIFFICULT TO DETECT DUE TO VISIBILITY ACCESS. THESE BRACKETS BROKE BECAUSE OF FLIGHT THROUGH TURBULENCE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · rib · crackedJan 13, 1998

    FOLLOWING A WINDSTORM THAT BROKE THE GUSTLOCK, AN INVESTIGATION OF THE FLIGHT CONTROLS REVEALED CRACKS ON BOTH THE INBD AND OTBD WING RIBS AT THE AILERON BRACKET RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Wings · rib · crackedJan 13, 1998

    FOLLOWING A WINDSTORM THAT BROKE THE GUSTLOCK, AN INVESTIGATION OF THE FLIGHT CONTROLS REVEALED CRACKS ON BOTH THE INBD AND OTBD WING RIBS AT THE AILERON BRACKET RIVETS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · mount · mismanufacturedDec 19, 1997

    UPON ARRIVAL OF A NEW ENGINE MOUNT, DISCOVERED TWO OF THE WELD JOINTS WERE DEFECTIVE. THE GUSSET PLATES ON BOTH UPPER BRACE ARMS WERE NOT WELDED DOWN, ONLY TACK-WELDED TO THE BRACE ARMS. THE MANUFACTURER SAID THAT ALTHOUGH IT WAS NOT CORRECT, SEVERAL UNITS HAD BEEN SHIPPED WITH THIS CONDITION.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · bolts · looseSep 8, 1997

    DURING 100-HOUR INSPECTION, THE CENTER SECTION WING BOLTS THAT ATTACH THE LOWER WING SPAR PLATE TO THE WING SPAR (I.E., 20 WING BOLTS) WERE ALL FOUND UNDERTORQUED BY ONE-HALF TO ONE FULL TURN. THE NAS464P5 BOLTS SHOULD BE TORQUED 100-140 INCH/POUND.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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