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Aircraft record

N1372VCessna U206F

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jun 1986)2 ADs may apply4 service difficulty reports

Registration
Valid
expires May 31, 2030
Based in
Anchorage, AK
owner city / state
Engine
IO 520 SERIES · 285 hp
Cont Motor
Owners
1
since 2023
NTSB events
1
substantial, 1986
ADs may apply
2
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Individual owner
City, state
Anchorage, AK
Certificate issued
May 3, 2023
Expires
May 31, 2030
Airworthiness
Standard · Normal
Airworthiness date
Nov 4, 1974

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
U206F
Serial number
U20602588
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
A097E4

Engine

Make and model
Cont Motor Io 520 Series
Type
Reciprocating
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. 2023 – nowIndividual ownerAnchorage, AK · current
  2. 1948 – 1955Individual ownerDerwood, MD · different airframe: Boeing N2s-5 S/N 75-5358

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 (1)

Accident · substantial damage

Jun 21, 1986 · Ft. Myers, FL

THE PRIVATE PILOT HAD JUST COMPLETED A SHORT NO-RADIO NIGHT FLIGHT AND DURING THE LANDING ROLL THE NOSE GEAR WHEEL ASSEMBLY SEPARATED FROM THE AIRCRAFT. EXAMINATION REVEALED THAT THE WRONG NUTS HAD BEEN INSTALLED ON THE WHEEL ASSEMBLY AT THE LAST ANNUAL INSPECTION. THE LAST ANNUAL INSPECTION WAS CONDUCTED EIGHTEEN MONTHS BEFORE THE DATE OF THE ACCIDENT.

Damage
Substantial
Injuries
None
Report
MIA86LA186

From NTSB records; matched by serial number.Read NTSB report (search CAROL for MIA86LA186)

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 (U206F)
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 (4)

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.

  • Wings · hinge bracket · crackedApr 14, 2007

    FOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INSPECTION. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · hinge bracket · crackedApr 14, 2007

    FOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INSPECTION. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · corrodedApr 14, 2006

    FOUND PART TO SEVERLY CORRODED AND HAD SEPARATED, TO 2 RIBS. PROBABLE CAUSE: PAINT STRIPPER, RECOMMEND THROUGH CLEANING AFTER STRIPPING AN AIRCRAFT FOR PAINT. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Fuselage · bulkhead · crackedJan 5, 1996

    DURING ROUTINE ANNUAL INSP, DISCOVERED FWD CABIN DOORPOST BULKHEAD CRACKED ON LT AND RT SIDES AT WING LIFT STRUT ATTACH FITTINGS. INSP WAS DONE IAW CESSNA SEB 93-5 R1. PREVIOUS INSP OF THIS AREA DURING ANNUAL AND WHEN C/W CESSNA SEB 93-5, FAILED TO FIND THIS DAMAGE. DAMAGE WAS ONLY VISIBLE BY…

    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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