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Aircraft record

N117CC1979 Swearingen SA226-T(B)

Registration validUnclaimedSource: FAA, updated Oct 16, 2026

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply1 service difficulty report

Registration
Valid
expires Aug 31, 2029
Based in
Scottsdale, AZ
owner city / state
Engine
TPE331-10U · 940 hp
Honeywell
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Registered owner
Ev Advisors LLC
Owner type
LLC
City, state
Scottsdale, AZ
Certificate issued
Aug 12, 2022
Expires
Aug 31, 2029
Airworthiness
Standard · Normal
Airworthiness date
Sep 14, 2010

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
Swearingen
Model
SA226-T(B)
Year
1979
Serial number
T-325
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
11
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A04669

Engine

Make and model
Honeywell Tpe331-10u
Type
Turbo-prop
Power
940 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. 2022 – nowEv Advisors LLCScottsdale, AZ · current
  2. 1988 – 1991Grand Rapids AviationSparta, MI · different airframe: Cessna 310q S/N 310q0696

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 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 (11)

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
2018-22-01Turbine SectionDec 10, 2018Engine (TPE331-10U)Only with: Second stage turbine rotor assemblies P/N 3102106-1, -6, -8 or P/N 3101514-1, -10, -12 installed.
2018-13-05Turbine Engine Reduction GearJul 26, 2018Engine (TPE331-10U)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed.
2018-02-14Turbine Engine Combustion SectionFeb 28, 2018Engine (TPE331-10U)Only with: Combustion chamber case assemblies P/Ns 869728-x, 893973-x, 3101668-x, or 3102613-x (any dash number) installed.
2016-21-07Honeywell International Inc. Turboprop EnginesNov 28, 2016Engine (TPE331-10U)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) of the AD installed.
2016-18-17Honeywell International Inc. Turboprop and Turboshaft EnginesNov 4, 2016Engine (TPE331-10U)Only with: With 2nd stage compressor impeller P/N 893482-1 through -5 inclusive, or P/N 3107056-1 or 3107056-2, installed.
Show all 11 ADs
ADSubjectEffectiveApplies to
2015-18-03Honeywell International Inc. Turboprop Engines (Type Certificate Previously Held by…Nov 13, 2015Engine (TPE331-10U)Only with: Engine propeller shaft coupling P/N 3107065-1, 865888-3, 865888-6, or 865888-8 installed.
2014-12-04Honeywell International Inc. Turboprop EnginesJul 22, 2015Engine (TPE331-10U)Only with: Woodward fuel control unit (FCU) assemblies with Honeywell P/Ns listed in Table 1 to paragraph (c) (P/N 869199, 893561, 897770, 897375, 897780 dash numbers) installed.
2012-02-06Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop EnginesMar 15, 2012Engine (TPE331-10U)Serial numbers per Table 2 of Honeywell International Inc. Alert Service Bulletin TPE331-72-A2156, dated December 2, 2008. Only with: First stage turbine disk P/N 3101520-1 or 3107079-1 with S/N listed in the ASB installed.
2009-17-05Honeywell International Inc. TPE331-10 and TPE331-11 Series Turboprop EnginesSep 1, 2009Engine (TPE331-10U)Only with: First stage turbine disk P/N 3101520-1 or 3107079-1, S/N 2-03501-2299, 2-03501-2300, 2-03501-2301, 2-03501-2302, or 2-03501-2304 installed.
2002-25-02Honeywell International Inc. TPE331-3, -5, -6, -8, -10, and -11 Series Turboprop and…Jan 21, 2003Engine (TPE331-10U)
2002-21-15Honeywell International Inc. TPE331 Series Turboprop and TSE331-3U Series Turboshaft…Nov 26, 2002Engine (TPE331-10U)Only with: Engines with second stage turbine stator assemblies P/N 894528-1, -2, -3, -5, -6, -10, or -11 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 (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.

  • Landing gear · valve · failedJul 8, 2002

    OVERHAULED VALVE FAILED SHOP GROUND TEST. VALVE (SN 493A), FAILED ON FIRST LANDING, CAUSING AN UNCONTROLABLE SHIMMY IN STEERING OF AIRCRAFT, VIOLANT SHAKING.

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

Sources

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

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