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Aircraft record

N500PJ1974 Mitsubishi MU-2B-36

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched9 service difficulty reports

Registration
Valid
expires May 31, 2033
Based in
Ooltewah, TN
owner city / state
Engine
TPE331-6 · 750 hp
Alliedsign
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
9
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
FLY2MELLC
Owner type
LLC
City, state
Ooltewah, TN
Certificate issued
May 9, 2026
Expires
May 31, 2033
Airworthiness
Experimental · Research and Development
Airworthiness date
Sep 13, 2012

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
Mitsubishi
Model
MU-2B-36
Year
1974
Serial number
668
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A63B3E

Engine

Make and model
Alliedsign Tpe331-6
Type
Turbo-prop
Power
750 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. 2026 – nowFLY2MELLCOoltewah, 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 (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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

Service Difficulty Reports (9)

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.

  • Landing gear · tire · failedAug 1, 2003

    UPON LANDING, THE TIRE DISINTEGRATED. ASSURE THE TIRE WAS FLAT ON LANDING, DUE TO RUNWAY FOD ON TAKEOFF.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · valve · damagedMay 25, 1999

    HIGH PRESSURE RELIEF VALVE BODY, P/N 867927-1, WAS STILL IN FUEL PUMP HOUSING, BUT THE WRENCHING FLATS AND CAP OF RELIEF VALVE WERE FOUND HANGING FROM SAFETY WIRE CAUSING FUEL TO BE SPRAYED ON ENGINE. FUEL COULD ONLY BE STOPPED BY SHUTTING OFF AIRFRAME SUPPLY TO ENGINE. FOUND DURING GROUND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · wheel · failedJun 26, 1998

    INNER WHEEL HALF EXPERIENCED A BEARING FAILURE. FAILURE RESULTED IN BRAKE DISC RUBBING INTO BRAKE ASSEMBLY REQUIRING BRAKE ASSEMBLY REPLACEMENT. INNER WHEEL HALF ALSO REQUIRED REPLACEMENT DUE TO CRACKING AROUND BEARING AREA.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Landing gear · tire · separationApr 30, 1997

    LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE OF 3 SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS RETURNED TO MFG FOR EVALUATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · tire · separatedApr 30, 1997

    LEFT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE FOR APPROXIMATELY 10 INCHES. OCCURRED ON LANDING. TIRE REMAINED INFLATED. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT MU-2'S. TIRE WAS RETURNED TO MFG FOR EVALUATION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · tire · separationApr 2, 1997

    RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STAYED ATTACHED AROUND OUTBOARD EDGE CIRCUMFERENCE. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT AIRCRAFT (BOTH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · tire · separatedApr 2, 1997

    RIGHT HAND MAIN GEAR TIRE TREAD SEPARATED FROM CASING ALONG INBOARD EDGE COMPLETELY AROUND CIRCUMFERENCE. OCCURRED ON LANDING. TIRE REMAINED INFLATED. TREAD STAYED ATTACHED AROUND OUTBOARD EDGE CIRCUMFERENCE. THIS WAS ONE OF THREE SIMILAR OCCURRENCES WITHIN 30 DAYS ON TWO DIFFERENT AIRCRAFT (BOTH…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedNov 27, 1995

    FRAME 4610, LEFT, CRACKED THROUGH SCREW HOLES APPROXMATELY 31MM BELOW LOWER HOLE. ALL 6 STATIONS HAD TO BE SHIMMED PER SB 209A.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · window · crackedApr 11, 1995

    DURING A POST-INSPECTION WALK-AROUND, A CRACK WAS NOTED EXTENDING APPROXIMATELY 1 INCH INTO THE VISIBLE AREA OF THE OUTER WINDOW IN THE CREW EMERGENCY ESCAPE DOOR. WHEN WINDOW RETAINERS WERE REMOVED, A CRACK 16 INCHES LONG CONNECTING 11 BOLT HOLES ACROSS THE TOP EDGE OF THE WINDOW WAS FOUND. THE…

    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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