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Aircraft record

N1331C1982 Construcciones Aeronauticas Sa C-212-CC

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply13 service difficulty reports

Registration
Valid
expires Dec 31, 2027
Based in
Anchorage, AK
owner city / state
Engine
TPE331-10R · 940 hp
Honeywell
Owners
1
since 2020
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
13
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Ryan Air INC
Owner type
Corporation
City, state
Anchorage, AK
Certificate issued
Dec 16, 2020
Expires
Dec 31, 2027
Airworthiness
Standard · Transport
Airworthiness date
Mar 6, 2020

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
C-212-CC
Year
1982
Serial number
265
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
A088D4

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. 2020 – 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 (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 (13)

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 · damagedSep 16, 2026

    FS 27 LOWER BEAM & LOWER SKINS DAMAGED. REMOVED F27 LOWER BEAM. PREVIOUSLY REPAIRED RT LOWER SKIN SECTION, LT & RT FS27 TO C CHANNEL BRACKETS/CVR BOX MOUNTING STRUCTURE. CUT MIDDLE/LH LOWER SKINS JUST AHEAD OF F28 FLANGE REMOVING FWD ~13" OF BOTH SKINS. FAB'D NEW F27 LOWER BEAM. FAB'D NEW RH LWR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine oil · oil cooler · failedApr 6, 2026

    LEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · puncturedFeb 14, 2025

    FOUND A SMALL PUNCTURE IN THE AFT SIDE OF THE RH WEB OF FRAME 11, 2 INCHES ABOVE FLOOR LEVEL. REPAIRED PER CASA ENGINEERING DOC 252EA-00020 REV A. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED MATERIAL. DAMAGED AREA INSPECTED BY HFEC, NO INDICATIONS OF CRACKING FOUND, SEE AIX REPORT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · web · crushedFeb 14, 2025

    LH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~ 5.5" X 9.5". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICE PLATE 9.75" X 2.25" FROM 2024T3…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · web · crushedFeb 14, 2025

    RH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~4.5 X 9". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICE PLATE 9.75" X 2.25" FROM 2024T3 0.025".…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedJan 23, 2024

    WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.070" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, HE SITUATION REPORTED, AND A REPAIR SCHEME REQUESTED. THE OEM REPLIED WITH A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · gougedMar 24, 2022

    A FORKLIFT LOADING THE AIRCRAFT SLIPPED ON ICE, AND HIT THE AFT UPPER CARGO DOOR AS WELL AS THE AIRCRAFT STRUCTURE DIRECTLY AFT OF THE DOOR, CAUSING GOUGING, AS WELL AS BUCKLING OF THE ASSOCIATED FRAMES. DAMAGE WAS REPAIRED IAW THE SRM, AND A FAA FORM 337 WAS FILLED OUT, SIGNED AND FORWARDED AS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Propellers · governor · inoperativeApr 1, 2021

    ON T/O ROLL OUT OF OOK AT V1 SPEED, #1 ENGINE BETA LIGHT CAME ON. PILOTS ELECTED TO TAKE OFF. TORQUE DROPPED 40%, AND PROPELLER SPEED INCREASED ON THE SAME ENGINE. #1 ENGINE FEATHERED DUE TO DRAG AND OVERSPEED OF THE PROP. ENGINE WAS DOWN TO 20%TQ, AND NP PEAKED AT 103.7% MOMENTARILY. AIRCRAFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorbeam · corrodedDec 17, 2020

    INTERGRANULAR CORROSION FOUND ON UPPER FLOOR BEAM "T" CAP ANGLE AT FRAME 1F. THE SECTION OF EXTRUDED T-ANGLE WAS CUT, REMOVED AND REPLACED WITH A PIECE OF 2024T3511 OF SIMILAR SIZE AND LENGTH. IT WAS ETCHED, ALODINED AND PAINTED AS REQUIRED, AND INSTALLED USING MS20470E5 RIVETS AND HL21PB5…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · firewall · crackedDec 13, 2020

    NR 1 AND 2 ENGINE AFT SIDE OF FIREWALL LOWER DOUBLERS FOUND CRACKED NEAR OUTER EDGE OF BOTH LEFT AND RIGHT LOWER MOUNT FITTINGS. REPAIRED BOTH LT AND RT CRACKED DOUBLERS ON BOTH ENGINE FIREWALLS BY INSERTION OF NEW DOUBLER SECTIONS OF SIMILAR THICKNESS AND SIZE, USING MONEL RIVETS OF SIMILAR SIZE…

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

Showing the 10 most recent of 13 reports.

Related aircraft

Show all 8 related aircraft
All 12 registered Construcciones Aeronauticas Sa C-212-CC aircraft

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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