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Aircraft record

N602AR1980 Eads Casa C-212-CC-15 AVIOCAR

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 4, 2022.

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply32 service difficulty reports

Registration
Deregistered
Last based in
North Salt Lake, UT
owner city / state
Engine
TPE331-10 · 940 hp
Honeywell
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
32
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Tvpx Aircraft Solutions INC Trustee
Owner type
Corporation
City, state
North Salt Lake, UT
Certificate issued
Oct 10, 2019
Canceled
Mar 4, 2022
Airworthiness
Standard · Transport
Airworthiness date
Sep 26, 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
Eads Casa
Model
C-212-CC-15 AVIOCAR
Year
1980
Serial number
161
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
28
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A7CEBD

Engine

Make and model
Honeywell Tpe331-10
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. 2019 – 2022Tvpx Aircraft Solutions INC TrusteeNorth Salt Lake, UT
  2. 1989 – 1996Aar Financial Services CorpElk Grove Village, IL · different airframe: Boeing 727-228 S/N 20075

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 (0)

No NTSB accidents or incidents found for this airframe since 1982.

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 (TPE331-10)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 (TPE331-10)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed.
2018-02-14Turbine Engine Combustion SectionFeb 28, 2018Engine (TPE331-10)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 (TPE331-10)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 (TPE331-10)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 (TPE331-10)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 (TPE331-10)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 (TPE331-10)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 (TPE331-10)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 (TPE331-10)
2002-21-15Honeywell International Inc. TPE331 Series Turboprop and TSE331-3U Series Turboshaft…Nov 26, 2002Engine (TPE331-10)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 (32)

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.

  • Fuselage · skin · puncturedJun 5, 2019

    DURING SCHEDULED INSPECTIONS, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE TAIL STAND MOUNT. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, OPEN

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · angle · corrodedMay 31, 2019

    DURING SCHEDULED INSPECTIONS, A T-ANGLE WAS FOUND TO BE CORRODED ON THE CARGO/RAMP DOOR. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedMay 31, 2019

    DURING SCHEDULED INSPECTIONS, THE FLOOR BEAM AT LANDING GEAR FRAME 9 WAS FOUND TO HAVE CORROSION AT A FLOORBOARD NUTPLATE. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. OPEN

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · fitting · wornOct 30, 2018

    DURING INSPECTION, DANAGE WAS NOTED TO THE RT INBD FLAP PIVOT CONTROL POINT. THE LT AND RT FITTING PLATES WERE FOUND WORN BEYOND LIMITS AT THE BOLT HOLES. REF SRM FIG 2-24 POS 7 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · channel · corrodedOct 30, 2018

    DURING REPAIR ACTIONS TO THE RT INBD FLAP PIVOT CONTROL POINT, THE CHANNEL ATTACHED TO THE SUPPORT BOX WAS FOUND TO BE CORRODED. REF SRM FIG 2-24 POS 3 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · blade · crackedOct 4, 2015

    DURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · unknown · fumesSep 2, 2015

    DURING CRUISE, WHEN HEATER VLV OPENED, THE FLIGHT CREW NOTICED FUMES IN BOTH THE FLIGHT DECK & CABIN. TESTED GEARBOX FOR POSITIVE PRESS & FOUND NORMAL NEGATIVE PRESS. HEATING SYS CHECKED GOOD ON GND IAW AMM 21-40-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · control quadrant · corrodedApr 30, 2015

    LEFT AILERON CABLE QUADRANT HAS AN AREA OF EXFOLIATION CORROSION APPROX 1.00 INCH BY .750 INCH BY .125 DEEP. REPLACED LT AILERON CABLE QUADRANT IAW AMM 27-11-02 P BLOCK 401.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · cap · corrodedMar 26, 2015

    RIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · bracket · crackedMar 26, 2015

    RIGHT WING OUTER FLAP INBD STANCHION CAREEN LE CHAFED & CRACKED. REPAIRED IAW EO 14022-300. OPERATIONAL & FUNCTIONAL CHECKS SATISFACTORY IAW 212-200 MM.

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

Showing the 10 most recent of 32 reports.

Related aircraft

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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