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Aircraft record

N424CA1981 Construcciones Aeronauticas Sa CASA-212-200

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched31 service difficulty reports

Registration
Valid
expires Oct 31, 2033
Based in
Anchorage, AK
owner city / state
Engine
TPE331-10 · 940 hp
Garrett
Owners
1
since 2026
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
31
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Ryan Air INC
Owner type
Corporation
City, state
Anchorage, AK
Certificate issued
Oct 2, 2026
Expires
Oct 31, 2033
Airworthiness
Standard · Transport
Airworthiness date
Jul 27, 1982

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
Construcciones Aeronauticas Sa
Model
CASA-212-200
Year
1981
Serial number
242
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
A50AAE

Engine

Make and model
Garrett 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. 2026 – nowRyan Air INCAnchorage, AK · current

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 (0)

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

Accident history for this model

ADs published since 1998 that may apply (0)

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.

No ADs published since 1998 matched this airframe or engine model.

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.

  • Wings · rib · buckledJul 8, 2026

    LEFT WING HAS BUCKLED RIB AND WRINKLED SKIN AT WING STATION 6500. CAUSE/TIMEFRAME OF DAMAGE UNKNOWN. WING APPEARS TO HAVE ENDURED IMPACT ON BOTTOM OF WING TIP AREA. SFP APPROVED BY ANC FSDO FOR RELOCATION TO GREYBULL, WY FOR REPAIRS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · corrodedJan 27, 2026

    L F11 REAR UNDER FLOOR FITTING CORRODED BEYOND LIMITS, F11 & F6 UNDERFLOOR FITTING HAVE CORROSION AT NUT PLATES. F6 & F11 JUNCTION BAR FITTINGS FOUND CORRODED. JUNCTION BAR FITTINGS. REMOVED ALL JUNCTION BAR FITTINGS FROM F6 & F11. REMOVED CORROSION UNDER & AROUND FITTING TO WEB INTERFACE. FITTED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedJan 27, 2026

    F11 CAP CORRODED BETWEEN SEAT RAILS. FL 1 UNDERFLOOR T ANGLE CENTER CAP - REMOVED FRAME 11 CAP SPLICE SECTION. FABRICATED NEW CAP SPLICE SECTION FROM 2024T351 0.125" X 1 5/8" X 1" ALUMINUM TO SAME SIZE, DESIGN, AND HOLE PATERN AS PREVIOUSLY INSTALLED. PARTS WERE ACID ETCHED, ALODINED, AND PRIMED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · floorbeam · buckledJan 27, 2026

    F12 BUCKLED UNDER FLOOR. F12 UNDERFLOOR T ANGLE CENTER CAP - REMOVED DAMAGED T ANGLE. FABRICATED NEW T ANGLE FROM 2024T3 .085" X 1 5/8" X 1" TO SAME SIZE, DESIGN, AND HOLE PATTERN AS PREVIOUSLY INSTALLED. FABRICATED REPAIR DOUBLER 4 1/2"X 39 1/2" ALL NEW PARTS ACID ETCHED, ALODINED, AND PRIMED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedJan 27, 2026

    F16 TOP CAP CORRODED AT NUT PLATES. REMOVED FRAME 16 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.100 THICK. ETCHED AND ALODINED THE "T" ANGLE AND PRIMED WITH SUPER KOROPON EPOXY PRIMER. INSTALLED THE "T" ANGLE USING MS20470AD-4 AND MS2470AD-5 RIVETS IAW AC43.13-1B, PARA.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · collapsedJan 27, 2026

    - F15 WEB SAGGING UNDERFLOOR - REMOVED FRAME15 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.084 THICK, 38.5 INCHES LONG. STRAIGHTENED OUT THE WEB ON FRAME 15. FABRICATED A DOUBLER FROM 2024 T3, 0.032" THICK MEASURING 38.5" LONG X 3 1/4" TALL WITH A 1/4" FLANGE ALONG THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · hinge bracket · corrodedJan 27, 2026

    RT INBD. FLAP, THE OUTBD. PYLON AIRFRAME SIDE, BOTH OF THE HINGE PLATES HAVE PITTING CORROSION THAT IS BEYOND LIMITS. DRILLED BOTH HINGE PLATES AND THE INBD. AND OUTBD. PYLON SIDE SKINS OFF. FITTED AND INSTALLED NEW SIDE SKINS P/N 212-13202-05-1 (INBD.) AND P/N 212-13202-05-2 (OUTBD.) USING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedNov 15, 2021

    LOWER WING SKIN SECTION @ WING STATION 2800 UNDER FLAP PYLON WAS FOUND TO HAVE SEVERE PITTING CORROSION. FABRICATED NEW SKIN AS PER ORIGINAL, AND REPLACED PER AC43.13-1B, PAR 4-53, 4-55, 4-57 AND CASA 212 SRM SECT. II, FIG 2.26

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · stringer · crackedSep 13, 2021

    INSPECTION FOUND A BENT AND CRACKED STRINGER BETWEEN FR18 AND FR19 ON R/H SIDE. POSSIBLE CAUSE SEEMS TO BE LOADING DAMAGE CAUSED BY CARELESS LOADING AND UNLOADING.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedMay 4, 2020

    FOUND INTERGRANULAR CORROSION WHERE NUT PLATES WERE ATTACHED ON THE BOTTOM OF THE CAP STRIP OF FLOOR FRAME #11. SPLICED IN A NEW SECTION OF FRAME CAP PER CASA SRM.

    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 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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