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Aircraft record

N6439N1978 Cessna T210N

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:1 NTSB accident (substantial damage, Jul 1996)6 ADs may apply1 service difficulty report

Registration
Valid
expires Mar 31, 2028
Based in
Las Vegas, NV
owner city / state
Engine
TSIO-520 SER · 300 hp
Cont Motor
Owners
1
since 2021
NTSB events
1
substantial, 1996
ADs may apply
6
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Spectraq LLC
Owner type
LLC
City, state
Las Vegas, NV
Certificate issued
Mar 11, 2021
Expires
Mar 31, 2028
Airworthiness
Standard · Normal
Airworthiness date
Nov 8, 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
T210N
Year
1978
Serial number
21063015
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
6
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A87400

Engine

Make and model
Cont Motor Tsio-520 Ser
Type
Reciprocating
Power
300 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 – nowSpectraq LLCLas Vegas, NV · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Jul 22, 1996 · Sunnyside, WA

inadequate preflight by the pilot, and subsequent fuel exhaustion. Factors relating to the accident were: darkness, and high vegetation (brush and small trees) in the emergency landing area.

Damage
Substantial
Injuries
Minor
Report
SEA96LA161

From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA96LA161)

Accident history for this model

ADs published since 1998 that may apply (6)

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
2023-02-17Fuselage Main, StructureMar 20, 2023Airframe (T210N)
2012-10-04WingsJun 5, 2012Airframe (T210N)Certain serial numbers: 210G 21058819–21058936; T210G T210-0198–T210-0307; 210H 21058937–21059061; T210H T210-0308–T210-0392; 210J 21059062–21059199; T210J 21058140; …
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (T210N)
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (TSIO-520 SER)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.
2008-10-02Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…May 12, 2008Airframe (T210N)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007.
Show all 6 ADs
ADSubjectEffectiveApplies to
98-05-14 R1Cessna Aircraft Company Models T210N, P210N, and P210R AirplanesSep 22, 1998Airframe (T210N)Certain serial numbers: T210N 21063641–21064897; P210N P21000386–P21000834

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

Service Difficulty Reports (1)

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.

  • Engine fuel and control · cover assy · misinstalledMar 27, 1995

    SHORTLY AFTER REINSTALLATION OF ENGINE, PILOT REPORTED FUEL PRESSURE COULD NOT BE MAINTAINED AS ACFT GAINED ALTITUDE. FUEL PRESSURE BEGAN TO DROP ABOVE 3,500 FEET MSL, AND BOOST PUMP NEEDED TO MAINTAIN ADEQUATE FUEL FLOWS AS ACFT CLIMBED ABOVE 7,000 FEET MLS. AT 100 HOURS SMOH, FUEL PUMP REMOVED…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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