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Aircraft record

N756NG1977 Cessna U206G

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Aug 1994)2 ADs may apply

Registration
Valid
expires Mar 31, 2028
Based in
Bishop, TX
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
since 2021
NTSB events
2
substantial, 1994
ADs may apply
2
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Partnership
City, state
Bishop, TX
Certificate issued
Mar 16, 2021
Expires
Mar 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Jan 17, 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
Cessna
Model
U206G
Year
1977
Serial number
U20604219
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Type certificate data sheet
A4CE
Mode S code
AA3186

Engine

Make and model
Cont Motor Io 520 Series
Type
Turbo-shaft
Power
285 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. 2021 – nowPartnershipBishop, TX · 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 (2)

Accident · substantial damage

Aug 9, 1994 · Bethel, AK

THE PILOT MISJUDGED THE STRENGTH OF THE TAILWIND AND DID NOT PERFORM A GO-AROUND IN A TIMELY FASHION SO AS TO AVOID LANDING THE AIRPLANE HALFWAY DOWN THE STRIP. FACTORS IN THE ACCIDENT WERE THE WET LANDING STRIP AND THE TAILWIND.

Damage
Substantial
Injuries
Minor
Report
ANC94LA102

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC94LA102)

Accident · substantial damage

Sep 15, 1989 · Nondalton, AK

FAILURE OF THE PILOT TO ATTAIN THE PROPER TOUCHDOWN POINT FOR THE LANDING, HIS EXCESSIVE AIRSPEED, AND HIS MISJUDGEMENT OF RUNWAY DISTANCE REMAINING. FACTORS RELATED TO THE ACCIDENT WERE: LOOSE/WET GRAVEL ON THE RUNWAY AND THE LOCATION OF THE PARKED AIRCRAFT NEAR THE END OF THE RUNWAY.

Damage
Substantial
Injuries
None
Report
ANC89LA165

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC89LA165)

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
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (U206G)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.

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

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

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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