# N424CA: 1981 Construcciones Aeronauticas CASA-212-200

- Status: Valid registration
- Airframe: [Construcciones Aeronauticas CASA-212-200](https://openairdocs.org/model/construcciones-aeronauticas-casa-212-200) (registry code 2410304, 19 seats)
- Engine: [Garrett TPE331-10](https://openairdocs.org/engine/garrett-tpe331-10) (registry code 29053)
- Data sheets: [TCDS E4WE](https://openairdocs.org/tcds/E4WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 242
- Year built: 1981
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 27, 1982
- Certificate issued: October 2, 2026
- Expires: October 31, 2033
- Mode S code: A50AAE
- Registered owner: [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=424CA
- Page: https://openairdocs.org/aircraft/N424CA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 21 in force

### Matched by airframe (Construcciones Aeronauticas CASA-212-200)

None in force.

### Matched by engine (Garrett TPE331-10)

- [AD 2018-22-01](https://openairdocs.org/ad/2018-22-01): Turbine Section · Honeywell International TPE331-10, TPE331-10N, TPE331-10R and 8 more. Effective Dec 10, 2018
- [AD 2018-17-15](https://openairdocs.org/ad/2018-17-15): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 39 more. Effective Oct 22, 2018
- [AD 2018-13-05](https://openairdocs.org/ad/2018-13-05): Turbine Engine Reduction Gear · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 18 more. Effective Jul 26, 2018
- [AD 2016-21-07](https://openairdocs.org/ad/2016-21-07): Fuel control drive · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Nov 28, 2016
- [AD 2016-18-17](https://openairdocs.org/ad/2016-18-17): Compressor impeller · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 22 more. Effective Nov 4, 2016
- [AD 2015-18-03](https://openairdocs.org/ad/2015-18-03): Engine propeller shaft coupling failures · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 8 more. Effective Nov 13, 2015
- [AD 2012-02-06](https://openairdocs.org/ad/2012-02-06): First stage turbine disks · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 12 more. Effective Mar 15, 2012
- [AD 2011-18-51 R1](https://openairdocs.org/ad/2011-18-51-R1): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more. Effective Oct 19, 2011
- [AD 2009-17-05](https://openairdocs.org/ad/2009-17-05): First stage turbine disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Sep 1, 2009
- [AD 2006-14-03](https://openairdocs.org/ad/2006-14-03): New flight cycle counting method for first, second, and third-stage turbine rotors · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 48 more. Effective Aug 9, 2006
- [AD 2004-09-29](https://openairdocs.org/ad/2004-09-29): First Stage Turbine Disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Jun 15, 2004
- [AD 2002-25-02](https://openairdocs.org/ad/2002-25-02): First stage compressors implellers · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 35 more. Effective Jan 21, 2003
- [AD 98-12-09](https://openairdocs.org/ad/98-12-09): Fuel Manifold · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more. Effective Aug 7, 1998
- [AD 97-15-10](https://openairdocs.org/ad/97-15-10): Engine Inlet Ice Protection · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 39 more. Effective Sep 22, 1997
- [AD 95-16-08](https://openairdocs.org/ad/95-16-08): Life Limited Turbine Components · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 62 more. Effective Sep 5, 1995
- [AD 94-26-07](https://openairdocs.org/ad/94-26-07): Fuel Control Governor Drive · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 32 more. Effective Apr 18, 1995
- [AD 93-15-11](https://openairdocs.org/ad/93-15-11): Propeller Pitch Control (PPC) Gasket · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 58 more. Effective Sep 7, 1993
- [AD 93-02-01](https://openairdocs.org/ad/93-02-01): Stratoflex Fuel Manifold Assemblies · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 21 more. Effective Mar 18, 1993
- [AD 89-07-07 R1](https://openairdocs.org/ad/89-07-07-R1): Oil Scavenge Pump Assembly · Honeywell International TPE331-1, TPE331-10, TPE331-10R and 26 more. Effective Oct 30, 1989
- [AD 84-10-06 R1](https://openairdocs.org/ad/84-10-06-R1): Fuel Pump Assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10B and 45 more. Effective Dec 26, 1984
- [AD 79-12-04](https://openairdocs.org/ad/79-12-04): Forged Third Stage Turbine Wheel Blade · Honeywell International TPE331-10. Effective May 10, 1979

### Historical (superseded or no longer in force)

- [AD 2018-02-14](https://openairdocs.org/ad/2018-02-14) (historical): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 38 more. Effective Feb 28, 2018
- [AD 2015-12-04](https://openairdocs.org/ad/2015-12-04) (historical): Fuel control unit (FCU) · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Jul 22, 2015
- [AD 2011-18-51](https://openairdocs.org/ad/2011-18-51) (historical): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more
- [AD 2006-15-08](https://openairdocs.org/ad/2006-15-08) (historical): Woodward fuel control unit (FCU) assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Aug 24, 2006
- [AD 88-12-10](https://openairdocs.org/ad/88-12-10) (historical): Turbine Rotor · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 6 more. Effective Jun 6, 1988
- [AD 92-02-19 PL](https://openairdocs.org/ad/92-02-19-PL) (historical): Fuel Manifold Assembly Leak · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more

## Information bulletins (advisory) (2 in force)

- [SAIB NE-16-19](https://openairdocs.org/saib/NE-16-19): Turbine Engine Compressor Section  Stator Nozzle Distress. Issued Jul 22, 2016
- [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever  Loss of Power Control. Issued Jul 11, 2016

## NTSB investigations

None matched to N424CA.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20210713012919I](https://openairdocs.org/incident/20210713012919I), Jul 13, 2021: Construcciones Aeronauticas Sa CASA-212-200 (N424CA), Bethel, AK, Minor damage. The crew reported that during final approach decent at approximately 1000 feet into Bethel, Alaska (pabe) on 07/13/2021, a seagull flew up towards the aircraft…
- [Incident 19831207071719I](https://openairdocs.org/incident/19831207071719I), Dec 7, 1983: Casa C212 (N424CA), Boston, MA, Minor damage. Strong gust of wind caused right wing tip to strike the ground. Taxiing to gate. ATC reported gust of 50 knots.

## Service difficulty reports (31)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UATA2420714265701](https://openairdocs.org/sdr/UATA2420714265701), Jul 8, 2026: RIB. BUCKLED. 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 A
- [SDR UATA2420127265305](https://openairdocs.org/sdr/UATA2420127265305), Jan 27, 2026: FLOORBEAM. COLLAPSED. - 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 O
- [SDR UATA2420127265304](https://openairdocs.org/sdr/UATA2420127265304), Jan 27, 2026: FLOORBEAM. CORRODED. 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
- [SDR UATA2420127265303](https://openairdocs.org/sdr/UATA2420127265303), Jan 27, 2026: FLOORBEAM. BUCKLED. 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, DESIG
- [SDR UATA2420127265302](https://openairdocs.org/sdr/UATA2420127265302), Jan 27, 2026: FLOORBEAM. CORRODED. 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
- [SDR UATA2026012765301](https://openairdocs.org/sdr/UATA2026012765301), Jan 27, 2026: FITTING. CORRODED. 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. 
- [SDR UATA2420127265701](https://openairdocs.org/sdr/UATA2420127265701), Jan 27, 2026: HINGE BRACKET. CORRODED. 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. AN
- [SDR UATA2021122242416](https://openairdocs.org/sdr/UATA2021122242416), Nov 15, 2021: SKIN. CORRODED. 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 A
- [SDR UATA2021100542413](https://openairdocs.org/sdr/UATA2021100542413), Sep 13, 2021: STRINGER. CRACKED. 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 UNLOADI
- [SDR UATA2020050400001](https://openairdocs.org/sdr/UATA2020050400001), May 4, 2020: SKIN. PUNCTURED. FOUND HOLE IN BELLY SKIN BETWEEN FRAME 2/F AND 3F. CLEANED HOLE TO 1/2 INCH ROUND AND INSTALLED A FLUSH PLUG PATCH PER CASA 212 SRM.
- [SDR UATA2020050400000](https://openairdocs.org/sdr/UATA2020050400000), May 4, 2020: FLOORBEAM. CORRODED. 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 S
- [SDR UATA2421209495701](https://openairdocs.org/sdr/UATA2421209495701), Dec 4, 2019: PROFILE. CRACKED. IN COMPLYING WITH AD98-12-28, FOUND ONE FALSE SPAR PROFILE TO BE CRACKED. REPLACED PROFILE WITH A NEW FABRICATED PROFILE.
- [SDR UATA2019101427213](https://openairdocs.org/sdr/UATA2019101427213), Sep 18, 2019: CONTROL CABLE. FRAYED. PILOT'S SIDE FORWARD INBOARD AILERON CABLE FRAYED. REPLACED CABLE ASSEMBLY WITH NEW.
- [SDR UATA2019101454201](https://openairdocs.org/sdr/UATA2019101454201), Sep 18, 2019: BRACKET. CRACKED. #1 ENGINE FORWARD COWL SUPPORT BRACKET IS CRACKED IN THE 12:00 POSITION. FABRICATED A NEW BRACKET PER AC43.13-1B, SECTION 4
- [SDR UATA2019101424202](https://openairdocs.org/sdr/UATA2019101424202), Sep 18, 2019: HINGE BRACKET. CRACKED. UPPER LH CARGO DOOR HINGE BRACKET AT FRAME 27 IS CRACKED. REPLACED HINGE BRACKET WITH NEW.
- [SDR UATA2019101453201](https://openairdocs.org/sdr/UATA2019101453201), Sep 18, 2019: INTERCOSTAL. CRACKED. FOUND A CRACK IN AN INTERCOSTAL AT FRAME 19 RH BOTTOM, FORWARD OF RAMP ACTUATOR. REPAIRED PER SRM.
- [SDR UATA2019101424201](https://openairdocs.org/sdr/UATA2019101424201), Sep 18, 2019: RIB. CRACKED. LH OUTBOARD WING LEADING EDGE HAS A CRACKED NOSE RIB A WING STATION 8160 AND CRACKS IN THE SKIN. REPAIRED PER SRM.
- [SDR UATA2019101424211](https://openairdocs.org/sdr/UATA2019101424211), Sep 18, 2019: SUPPORT. CORRODED. LH ELEVATOR SHAFT QUADRANT SUPPORT ASSEMBLY HAD CORROSION IN BOTH LOWER ATTACHMENT FEET. REPLACED SUPPORT ASSEMBLY WITH A NEW UNIT.
- [SDR UATA201910144206](https://openairdocs.org/sdr/UATA201910144206), Sep 18, 2019: CONTROL CABLE. FRAYED. PILOTS FWD ELEVATOR UP CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.
- [SDR UATA2019101424205](https://openairdocs.org/sdr/UATA2019101424205), Sep 18, 2019: CONTROL CABLE. FRAYED. PILOTS OUTBOARD FORWARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.
- [SDR UATA2019101400204](https://openairdocs.org/sdr/UATA2019101400204), Sep 18, 2019: CONTROL CABLE. FRAYED. COPILOT'S FWD INBOARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.
- [SDR UATA2019101400203](https://openairdocs.org/sdr/UATA2019101400203), Sep 18, 2019: CONTROL CABLE. FRAYED. COPILOT'S OUTBOARD FWD AILERON CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.
- [SDR UATA2019101400002](https://openairdocs.org/sdr/UATA2019101400002), Sep 18, 2019: CONTROL CABLE. FRAYED. FOUND RH FWD RUDDER CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.
- [SDR UATA201910140001](https://openairdocs.org/sdr/UATA201910140001), Sep 18, 2019: CONTROL CABLE. FRAYED. FOUND RUDDER CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.
- [SDR 2019FA0000201](https://openairdocs.org/sdr/2019FA0000201), Jun 26, 2019: STOP FITTING. DAMAGED. ELEVATOR TRIM STOPS FOUND DAMAGED. ONE STOP BENT AND ANOTHER BROKEN IN HALF.
- [SDR KGBR2010051110002](https://openairdocs.org/sdr/KGBR2010051110002), May 11, 2010: REGULATOR. LEAKING. FLIGHT CREW DESCRIBED THAT THE OXYGEN SYSTEM EMPTIED TO QUICKLY. UPON FURTHER INSPECTION, DETERMINED THAT THE PRESSURE REGULATOR WAS LEAKING UNDER THE CAP / KNO
- [SDR KGBR2010051110001](https://openairdocs.org/sdr/KGBR2010051110001), May 11, 2010: SKIN PANEL. DAMAGED. CORROSION / EROSION ON CENTER WING LOWER AFT SKIN PANEL IN THE AREA OF THE EXHAUST TRAILS OF THE LEFT AND RIGHT ENGINES FROM APPROX CWS 2230MM TO 3070MM LEFT AN
- [SDR 97ZZZX812](https://openairdocs.org/sdr/97ZZZX812), Sep 10, 1996: VALVE. FAILED. THE PURPOSE OF THE TWO EXTINGUISHING VALVES IS TO LEAD BY MEANS OF ITS COORDINATE ACTION, THE DISCHARGE OF EXTINGUISHING AGENT TOWARDS THE DESIRED ENGINE. NR 1 
- [SDR 95ZZZX6332](https://openairdocs.org/sdr/95ZZZX6332), Oct 26, 1995: ATTACH FITTING. CORRODED. CORROSION FOUND ON C-212 51D AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG.
- [SDR 95ZZZX6330](https://openairdocs.org/sdr/95ZZZX6330), Oct 26, 1995: ATTACH FITTING. CORRODED. CORROSION FOUND ON C-212 5ID AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG.
- [SDR 95ZZZX6329](https://openairdocs.org/sdr/95ZZZX6329), Oct 20, 1995: ATTACH FITTING. CORRODED. CORROSION FOUND ON C-212 51D AT BEARING AREA. BEARING MATERIAL IS DISSIMILAR. SUBMITTER STATED THAT POSSIBLY A BEARING WAS INSTALLED DRY AT INSTALLATION BY MFG.

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Garrett TPE331-10)

- [STC SE00265AT](https://openairdocs.org/stc/SE00265AT): Install Ayres Fuel Manifold Purge Assembly Kit, P/N 21757-1 in accordance with "Installation Instructions - Ayres P/N 21757-1 Fuel Manifold Purge Assy-Kit" Dwg. No. 21757-1(1), Revision none, dated April 20, 1993, or later FAA approved revision. Thrush Aircraft Inc

## Related

- Other Construcciones Aeronauticas CASA-212-200 aircraft: https://openairdocs.org/model/construcciones-aeronauticas-casa-212-200/aircraft.md
- The Garrett TPE331-10 engine: https://openairdocs.org/engine/garrett-tpe331-10.md

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