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Aircraft record

N255MG2011 Costruzioni Aeronautiche Tecna P2006T

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched7 service difficulty reports

Registration
Valid
expires Jan 31, 2032
Based in
Hanford, CA
owner city / state
Engine
912S · 100 hp
Rotax
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Central Valley Flight School LLC
Owner type
LLC
City, state
Hanford, CA
Certificate issued
Jan 10, 2025
Expires
Jan 31, 2032
Airworthiness
Standard · Normal
Airworthiness date
Jan 20, 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
Costruzioni Aeronautiche Tecna
Model
P2006T
Year
2011
Serial number
087/US
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
A26B2B

Engine

Make and model
Rotax 912s
Type
4 Cycle
Power
100 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. 2025 – nowCentral Valley Flight School LLCHanford, CA · 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 (7)

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.

  • Electrical power · bracket · damagedNov 28, 2020

    SUGGEST EMERGENCY AD. DURING 100 HOUR INSPECTION, LEFT ENGINE ALTERNATOR AND BELT WAS LOOSE ON ITS MOUNT WITH ALL HARDWARE TIGHT AND SECURE. REMOVAL REVEALED THE INTERNAL ALTERNATOR MOUNTING LUG HAD WORN TO EGG SHAPE AND MOUNTING BRACKET HOLES SYMMETRICALLY LONG-TERM. UPON INSTALLATION OF FACTORY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · bracket · looseNov 28, 2020

    SUGGEST EMERGENCY AD. DURING 100 HOUR INSPECTION, LEFT ENGINE ALTERNATOR AND BELT WAS LOOSE ON ITS MOUNT WITH ALL HARDWARE TIGHT AND SECURE. REMOVAL REVEALED THE INTERNAL ALTERNATOR MOUNTING LUG HAD WORN TO EGG SHAPE AND MOUNTING BRACKET HOLES SYMMETRICALLY LONG-TERM. UPON INSTALLATION OF FACTORY…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · nose rib · crackedJun 11, 2014

    DURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARD SPAR. 2 OF THE SAME RIBS ON THE LEFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Wings · nose rib · crackedJun 11, 2014

    DURING 100HR INSPECTION OF AIRCRAFT, THREE LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARD SPAR. 2 OF THE SAME RIBS ON THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · nose rib · crackedJun 11, 2014

    DURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARD SPAR. 2 OF THE SAME RIBS ON THE LEFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · nose rib · crackedJun 11, 2014

    DURING 100HR INSPECTION OF AIRCRAFT 3 LEADING EDGE RIBS, ONE AT 83", ONE AT 97" AND ONE AT 110" FROM FUSELAGE CENTER (NO WING STATION GIVEN IN M/M) JUST OUTBOARD OF EACH ENGINE NACELLE WERE FOUND CRACKED AROUND LOWER AFT RIVET WHERE THEY CONNECT TO THE FORWARD SPAR. 2 OF THE SAME RIBS ON THE LEFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · flex hose · chafedJul 16, 2012

    LOWER ENGINE COOLANT HOSE AND EXHAUST SCAT HOSE ARE IN CONSTANT CONTACT DUE TO INSTALLATION DESIGN. CHAFING CAUSED WIRE FROM SCAT HOSE TO PUNCTURE LOWER COOLANT HOSE. SUBSEQUENT LOSS OF ALL COOLANT CAUSED ENGINE OVERHEATING. WHILE PILOT WAS DETERMINING CAUSE OF HIGH CHT INDICATION, CHT GAUGE WENT…

    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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