# Service difficulty reports: N348CA A list on [N348CA](https://openairdocs.org/aircraft/N348CA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR UATA1750227265701](https://openairdocs.org/sdr/UATA1750227265701.md): Skin · cracked · Feb 27, 2026 · N348CA · Casa C212CC · Wing, Plate/Skin > TWO CRACKS FOUND IN TRAILING EDGE OF LT LOWER INNER FLAP COVE AT APPROXIMATE WS 1800 & 2800. REMOVED 6 1/4 X 2 3/8 SECTION FROM OTBD CRACKED AREA & 4 1/4 X 2 3/8 SECTION FROM INBD CRACKED AREA. REMOVED RIVETS AS REQUIRED FROM UPPER FLAP COVE SKIN FOR ACCESS. - [SDR UATA1750815255701](https://openairdocs.org/sdr/UATA1750815255701.md): Hinge · cracked · Aug 13, 2025 · N348CA · Casa C212CC · Ailerons > LH AILERON CENTER HINGE STRUCTURE, A PREVIOUS REPAIR PATCH IS CRACKED. REPAIR WAS ACCOMPLISHED AS FOLLOWS: REMOVED THE PREVIOUS CRACKED REPAIR ANGLE. USING THE ORIGINAL ANGLE AS A PATTERN A NEW ANGLE WAS FABRICATED FROM 301 STAINLESS STEEL 0.040 THICK AND INST - [SDR UATA1750702255301](https://openairdocs.org/sdr/UATA1750702255301.md): Channel · damaged · Jul 2, 2025 · N348CA · Casa C212CC · Fuselage Miscellaneous Structure > IMPACT DAMAGE FOUND IN C CHANNEL AFT OF F19. REMOVED DAMAGED C CHANNEL AND INTERCOSTALS AT F18 AND F19 THAT WERE MODIFIED TO ACCEPT A PREVIOUS REPAIR TO OLD C CHANNEL. FABRICATED NEW INTERCOSTALS FOR F18 AND F19. ALL NEW PARTS WERE ACID ETCHED, ALODINED AND P - [SDR UATA20205095701](https://openairdocs.org/sdr/UATA20205095701.md): Skin · corroded · May 8, 2025 · N348CA · Casa C212CC · Wing, Plate/Skin > CORROSION FOUND ON LOWER SURFACE OF LH WING AT W.S. 3450. REMOVED BRACE STRUT AT APPROXIMATE W.S. 3200 AND SPLICE PLATE AT APPROX. W.S. 3060 FOR ACCESS TO REPAIR AREA. REMOVED DAMAGED SKIN, REMOVED SEALANT FROM PREVIOUS INSTALLATION. FABRICATED NEW SKIN FROM 0 - [SDR UATA2025031915701](https://openairdocs.org/sdr/UATA2025031915701.md): Stiffener · cracked · Mar 11, 2025 · N348CA · Casa C212CC · Wing Miscellaneous Structure > CRACKED U CHANNEL IN AFT LH CENTER WING SECTION STATION 2380, AS FLAGGED. REPLACED CRACKED STIFFENER WITH NEW. SEE 337 DATED 03/11/2025 FOR FURTHER INFO. FAA FORM 337 STATES: FOUND CRACK IN STIFFENER ON THE LEFT CENTER WING AFT BEAM AT W.S. 2380. CRACKED STIFF - [SDR UATA202403183483](https://openairdocs.org/sdr/UATA202403183483.md): Skin · cracked · Feb 9, 2024 · N348CA · Casa C212CC · Fuselage Main, Plate/Skin > WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.5" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, THE SITUATION REPORTED, AND A REPAIR SCHEME WAS PROV - [SDR UATA202312013483](https://openairdocs.org/sdr/UATA202312013483.md): Skin · corroded · Nov 22, 2023 · N348CA · Casa C212CC · Wing, Plate/Skin > DURING MAINTENANCE, SEVERE CORROSION WAS FOUND IN THE UPPER SKIN OF THE R/H WING BETWEEN STA. 2380 AND STA. 2900, CENTERED OVER STRINGER #1. UNDER THE ENGINE NACELLE FAIRING/SCALLOP. - [SDR UATA202306013481](https://openairdocs.org/sdr/UATA202306013481.md): Fairing · loose · Mar 23, 2023 · N348CA · Casa C212CC · Trailing Edge Flaps > UPON SCHEDULED MAINTENANCE INSPECTION, FOUND FIBERGLASS FLAP HINGE FAIRING LOOSENED, AND SUBSEQUENTLY CHAFED THE FLAP ATTACH PYLON BEYOND LIMITS. - [SDR UATA202203243482](https://openairdocs.org/sdr/UATA202203243482.md): Attach Fitting · cracked · Feb 23, 2022 · N348CA · Casa C212CC · Wing, Attach Fittings > DURING SCHEDULED MAINTENANCE, FOUND A CRACK IN THE R/H WING LOWER OUTBOARD ATTACH FITTING USING X-RAY METHOD. - [SDR UATA2019101517501](https://openairdocs.org/sdr/UATA2019101517501.md): Attach Fitting · dislodged · Sep 9, 2019 · N348CA · Casa C212CC · Fuselage Main, Attach Fittings > LH UPPER ATTACH FITTING FOR THE CARGO RAMP ACTUATOR WAS DISLODGED, SHEARING FASTENERS. REPAIRED ATTACHMENT PER SRM. - [SDR 8EKA20140627001](https://openairdocs.org/sdr/8EKA20140627001.md): Attach Bracket · cracked · Jun 10, 2014 · N348CA · Casa C212CC · Ailerons > DURING 25 HOUR SERVICE CHECK FOUND RT OTBD AILERON & WING ATTACHMENT BRACKET CRACKED. TEMPORARY REPAIR ACCOMPLISHED IAW DERT 8110-3 TO ALLOW ACFT TO RELOCATE TO PERMANENT MAINTENANCE BASE WHERE FINAL REPAIR CAN TAKE PLACE. FORM 337 FILED & SENT TO FAA FOR TEM - [SDR 8EKA20140507](https://openairdocs.org/sdr/8EKA20140507.md): Fairing · broken · Apr 26, 2014 · N348CA · Casa C212CC · Trailing Edge Flaps > DURING POST FLIGHT CHECK, PILOT DISCOVERED A PIECE OF BROKEN FAIRING ON LT INBD FLAP OB PYLON. FIBERGLASS FAIRING PN 212-13223.1 CHAFED A HOLE THROUGH LT INBD FLAP LE PLATE OVER TIME. REPAIRS ARE CURRENTLY IN PROCESS, SUPPLEMENTAL INFORMATION WILL BE SUBMITT - [SDR 8EKA2014033100001](https://openairdocs.org/sdr/8EKA2014033100001.md): Hinge Bracket · cracked · Mar 19, 2014 · N348CA · Casa C212CC · Ailerons > DURING ROUTINE 25 HOUR INSPECTION, MAINTENANCE FOUND LT OTBD AILERON HINGE TO BE CRACKED. REMOVED & REPLACED HINGE BRACKET WITH SERVICEABLE BRACKET. MOC FLIGHT PERFORMED SATISFACTORY. - [SDR 8EKA20140205001](https://openairdocs.org/sdr/8EKA20140205001.md): Wheel · cracked · Jan 29, 2014 · N348CA · Casa C212CC · Wheel/Ski/Float > DURING POST FLIGHT INSPECTION MAINTENANCE CREW FOUND LT MLG OTBD WHEEL HALF TO BE CRACKED IN FOUR PLACES, CRACK LENGTH NOT EXCEEDING.25 INCHES. ACFT WAS GROUNDED IMMEDIATELY & A NEW WHEEL & TIRE ASSEMBLY WERE INSTALLED. - [SDR 8EKA20140206001](https://openairdocs.org/sdr/8EKA20140206001.md): Coupling · cracked · Jan 23, 2014 · N348CA · Casa C212CC · Engine Fireseals > DURING 400HR SCHEDULED INSPECTION MECHANIC FOUND NR 2 ENG FIRE SHIELD AUGMENTER FLANGE COUPLING ATTACHED TO FIREWALL CRACKED APPROXIMATELY 80% AROUND CIRCUMFERENCE. REMOVED & RE-INSTALLED ENG & PROPELLER TO FACILITATE REMOVAL & REPLACEMENT OF COUPLING WITH NE - [SDR 8EKA20140305001](https://openairdocs.org/sdr/8EKA20140305001.md): Mount · deformed · Jan 18, 2014 · N348CA · Casa C212CC · Engine Mount Section > DURING POST FLIGHT INSPECTION, FOUND ENG ISOLATOR MOUNT PAD TO BE DEFORMED AFTER 13.6 HOURS IN USE. THIS UNIT WAS REPLACED PREVIOUSLY ON 01/06/2013 DUE TO DE-BONDING FROM FUEL & OIL CONTAMINATION. - [SDR 8EKA20140121001](https://openairdocs.org/sdr/8EKA20140121001.md): Skin · dented · Jan 15, 2014 · N348CA · Casa C212CC · Fuselage Main, Plate/Skin > FOUND DENT IN UPPER SKIN OF FUSELAGE DURING INSPECTION, BETWEEN FRAMES 17 & 18. REPAIRED WITH PATCH IAW SRM. - [SDR 8EKA20140116001](https://openairdocs.org/sdr/8EKA20140116001.md): Cover · departed · Jan 12, 2014 · N348CA · Casa C212CC · Wheel/Ski/Float > DURING POST FLIGHT INSPECTION, PILOT DISCOVERED THE LT MLG WHEEL AXLE BEARING COVER DEPARTED ACFT DURING TRANSIT ON PREVIOUS FLIGHT. THERE WAS NO INDICATION OF MALFUNCTION DURING FLIGHT. COVER WAS REPLACED WITH NEW FROM KIT. - [SDR 8EKA20140124002](https://openairdocs.org/sdr/8EKA20140124002.md): Stringer · cracked · Nov 5, 2013 · N348CA · Casa C212CC · Cargo/Baggage Doors > CRACKS ON & IN THE VICINITY OF THE AFT UPPER DOOR WERE FOUND. ON 22-NOV-13 5 CRACKS WERE REPAIRED IAW THE SRM. THE ACFT WAS FLOWN UNTIL 27-NOV-13 WHEN THE DOM BECAME AWARE OF THE CRACKS, UPON READING THE E-MAIL & THEN PULLED THE ACFT OUT OF SERVICE. THIS E- - [SDR 8EKA20140124001](https://openairdocs.org/sdr/8EKA20140124001.md): Skin · cracked · Nov 5, 2013 · N348CA · Casa C212CC · Cargo/Baggage Doors > CRACKS ON & IN THE VICINITY OF THE AFT UPPER DOOR WERE FOUND. ON 22-NOV-13 5 CRACKS WERE REPAIRED IAW THE SRM. THE ACFT WAS FLOWN UNTIL 27-NOV-13 WHEN THE DOM BECAME AWARE OF THE CRACKS, UPON READING THE E-MAIL & THEN PULLED THE ACFT OUT OF SERVICE. THIS E- - [SDR EHAA20120824007](https://openairdocs.org/sdr/EHAA20120824007.md): Gearbox · inoperative · Aug 24, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop) > DURING CRUISE AT FL 85, THE NR 2 ENGINE RAPIDLY STARTED TO LOSE POWER AND DISPLAYED INDICATIONS OF FAILURE. THE COPILOT AND I NOTICED A CHANGE IN ACFT AND ENGINE PERFORMANCE, VERIFIED BY ENGINE TORQUE, RPM, FUEL FLOW, EGT AND SUBSEQUENT LOSS OF OIL PRESSURE D - [SDR EHAA20120731006](https://openairdocs.org/sdr/EHAA20120731006.md): Engine · power loss · Jul 31, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop) > DURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER. - [SDR 2012F00064](https://openairdocs.org/sdr/2012F00064.md): Connector · loose · Feb 27, 2012 · N348CA · Casa C212CC · Engine Indicating System Wiring > AFTER TAKEOFF, RT ENGINE LOST EGT INDICATION. ACFT RETURNED TO FIELD. LOOSE CONNECTOR PLUG FOUND. SAME REINSTALLED AND SYSTEM OPS CHECKED OK. - [SDR EIAA2010F00155](https://openairdocs.org/sdr/EIAA2010F00155.md): Fire Loop · chafed · Jul 10, 2010 · N348CA · Casa C212CC · Fire Detection > RT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. MANUAL POWER REDUCTION AND VISUAL CHECK DONE, WARNING LIGHT EXTINGUISHED. NO FIRE PRESENT. FIRE DETECTION LOOP WAS FOUND CHAFFED. REPLACED DETECTION LOOP, OPS CHECK GOOD. - [SDR 2010F00122](https://openairdocs.org/sdr/2010F00122.md): Diode · arced · Jun 2, 2010 · N348CA · Casa C212CC · Instrument Panel > PILOT REPORTED SMOKE SMELL IN THE COCKPIT. WHILE SEARCHING FOR THE CAUSE THEY FOUND THE INSTRUMENT LIGHTING CIRCUIT BREAKER POPPED. THE SMELL DISSIPATED, SO THEY CONTINUED. AFTER LANDING AT THE DESTINATION IT WAS DISCOVERED THAT A ZENER DIODE WAS INSTALLED INC - [SDR 97ZZZX3561](https://openairdocs.org/sdr/97ZZZX3561.md): Engine · failed · Jan 10, 1997 · N348CA · Casa C212CC · Engine (Turbine/Turboprop) > NR 2 ENGINE SHUT DOWN IN-FLIGHT DUE TO ZERO TORQUE AND DECREASING ENGINE RPM FUEL FLOW. ENGINE OIL OVER-SERVICE SUSPECTED DUE TO OIL TANK VENT VALVE OPEN. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N348CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N348CA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.