Skip to content
KnownTail
Aircraft record

N392CA1989 Casa 300

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply31 service difficulty reports

Registration
Valid
expires Oct 31, 2033
Based in
Carson City, NV
owner city / state
Engine
TPE331-10R · 940 hp
Honeywell
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
31
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
International Air Services INC Trustee
Owner type
Corporation
City, state
Carson City, NV
Certificate issued
Oct 6, 2026
Expires
Oct 31, 2033
Airworthiness
Standard · Transport
Airworthiness date
Dec 19, 2024

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
Casa
Model
300
Year
1989
Serial number
398
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
19
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A48A6A

Engine

Make and model
Honeywell Tpe331-10r
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. 2026 – nowInternational Air Services INC TrusteeCarson City, 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 (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 (TPE331-10R)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 (TPE331-10R)Only with: Hydraulic torque sensor gear assemblies P/Ns 3101726-1, -2, or -3 installed.
2018-02-14Turbine Engine Combustion SectionFeb 28, 2018Engine (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)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 (TPE331-10R)
2002-21-15Honeywell International Inc. TPE331 Series Turboprop and TSE331-3U Series Turboshaft…Nov 26, 2002Engine (TPE331-10R)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 (31)

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.

  • Doors · panel · corrodedFeb 13, 2014

    DURING INSPECTION FOUND CORROSION IN AFT CARGO DOOR. REMOVED CORROSION DAMAGED PANELS. FABRICATED & INSTALLED TWO REPAIR PANELS. ALL REPAIRS PERFORMED IAW SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · profile · crackedJan 30, 2014

    DURING 1200 HR FALSE SPAR RECURRING INSPECTION, & AD INSPECTION AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE RT WING. REMOVED RT WING AUXILIARY SPAR PROFILE ANGLE. INSTALLED REINFORCED RT WING AUXILIARY SPAR PROFILE ANGLE. ALL REMOVAL AND REPLACEMENT OF PARTS WAS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · profile · crackedJan 30, 2014

    DURING 1200 HR FALSE SPAR RECURRING AD INSPECTION, IAW AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE LT WING. REMOVED LT WING AUXILIARY SPAR PROFILE ANGLE, WS 5700. INSTALLED REINFORCED LT WING AUXILIARY SPAR PROFILE ANGLE. ALL REMOVAL AND REPLACEMENT OF PARTS ACCOMPLISHED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Ice and rain protection · terminal block · burnedApr 12, 2013

    DURING FLIGHT LT WINDOW HEAT SHORTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · spar · corrodedApr 11, 2011

    RIGHT WING, REAR SPAR WEB HAS CORROSION, WS 5940 AFT SIDE AT BOTTOM SPAR CAP (MARKED).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrodedApr 11, 2011

    RIGHT FLOOR SEAT TRACK IS CORRODED FROM FS 3950 TO FS 7332.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · support fitting · corrodedApr 11, 2011

    LEVEL 2 CORROSION ON MAIN LEFT LANDING GEAR FWD INTERIOR SUPPORT FITTING AT FS 5744.3 BELOW FLOOR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · structure · corrodedApr 11, 2011

    LEFT WING, CENTER SECTION, AREAS OF TRAILING EDGE OVER FLAP REMOVED, WS 1963-2200 AND WS 3296-3497, SAME AREAS HAVE SEVERE CORROSION (LEVEL 2).

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · support · corrodedApr 11, 2011

    RIGHT OUTER FLAP INBOARD ACTUATOR BELLCRANK BOTTOM SUPPORT IS CORRODED ON INBOARD FWD CORNER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · mount · delaminatedApr 11, 2011

    RIGHT WING UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATED

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

Showing the 10 most recent of 31 reports.

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

Request owner name removalReport an error in this record

Claim this airplaneWatch