N424CA
Service difficulty reports · 31
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N424CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N424CA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UATA2420714265701Rib · buckledLEFT 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.SDR UATA2420127265305Floorbeam · 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 OUT THE WEB ON FRAME 15. FABRICATED A DOUBLER FROM 2024 T3, 0.032" THICK MEASURING 38.5" LONG X 3 1/4SDR UATA2420127265304Floorbeam · corrodedF16 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 MSSDR UATA2420127265303Floorbeam · buckledF12 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 PARTSSDR UATA2420127265302Floorbeam · corrodedF11 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 WESDR UATA2026012765301Fitting · corrodedL 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 & ASDR UATA2420127265701Hinge Bracket · corrodedRT 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/SDR UATA2021122242416Skin · corrodedLOWER 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 2.26SDR UATA2021100542413Stringer · crackedINSPECTION 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.SDR UATA2020050400001Skin · puncturedFOUND 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 UATA2020050400000Floorbeam · corrodedFOUND 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.SDR UATA2421209495701Profile · crackedIN COMPLYING WITH AD98-12-28, FOUND ONE FALSE SPAR PROFILE TO BE CRACKED. REPLACED PROFILE WITH A NEW FABRICATED PROFILE.SDR UATA2019101427213Control Cable · frayedPILOT'S SIDE FORWARD INBOARD AILERON CABLE FRAYED. REPLACED CABLE ASSEMBLY WITH NEW.SDR UATA2019101454201Bracket · cracked#1 ENGINE FORWARD COWL SUPPORT BRACKET IS CRACKED IN THE 12:00 POSITION. FABRICATED A NEW BRACKET PER AC43.13-1B, SECTION 4SDR UATA2019101424202Hinge Bracket · crackedUPPER LH CARGO DOOR HINGE BRACKET AT FRAME 27 IS CRACKED. REPLACED HINGE BRACKET WITH NEW.SDR UATA2019101453201Intercostal · crackedFOUND A CRACK IN AN INTERCOSTAL AT FRAME 19 RH BOTTOM, FORWARD OF RAMP ACTUATOR. REPAIRED PER SRM.SDR UATA2019101424201Rib · crackedLH OUTBOARD WING LEADING EDGE HAS A CRACKED NOSE RIB A WING STATION 8160 AND CRACKS IN THE SKIN. REPAIRED PER SRM.SDR UATA2019101424211Support · corrodedLH ELEVATOR SHAFT QUADRANT SUPPORT ASSEMBLY HAD CORROSION IN BOTH LOWER ATTACHMENT FEET. REPLACED SUPPORT ASSEMBLY WITH A NEW UNIT.SDR UATA201910144206Control Cable · frayedPILOTS FWD ELEVATOR UP CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.SDR UATA2019101424205Control Cable · frayedPILOTS OUTBOARD FORWARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA2019101400204Control Cable · frayedCOPILOT'S FWD INBOARD AILERON CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA2019101400203Control Cable · frayedCOPILOT'S OUTBOARD FWD AILERON CABLE IS FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA2019101400002Control Cable · frayedFOUND RH FWD RUDDER CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE WITH NEW.SDR UATA201910140001Control Cable · frayedFOUND RUDDER CABLE FRAYED WITH BROKEN STRANDS. REPLACED CABLE ASSEMBLY WITH NEW.SDR 2019FA0000201Stop Fitting · damagedELEVATOR TRIM STOPS FOUND DAMAGED. ONE STOP BENT AND ANOTHER BROKEN IN HALF.SDR KGBR2010051110002Regulator · leakingFLIGHT CREW DESCRIBED THAT THE OXYGEN SYSTEM EMPTIED TO QUICKLY. UPON FURTHER INSPECTION, DETERMINED THAT THE PRESSURE REGULATOR WAS LEAKING UNDER THE CAP / KNOB USED TO TURN THE REGULATOR ON AND OFF. THIS AREA WAS UNABLE TO GAIN ACCESS USING LEAK DETECTION SDR KGBR2010051110001Skin Panel · damagedCORROSION / 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 AND RIGHT. REPAIRED REF CASA TECHNICAL INSTRUCTION LETTER 17 REV 1.SDR 97ZZZX812Valve · failedTHE 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 ENG VALVE DISK WAS FROZEN ON SHAFT. NR 2 ENG VALVE DISK WAS PREVENTED FROM SEATING DUE MILD CORROSSDR 95ZZZX6332Attach Fitting · corrodedCORROSION 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. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.SDR 95ZZZX6330Attach Fitting · corrodedCORROSION 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. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.SDR 95ZZZX6329Attach Fitting · corrodedCORROSION 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. OPERATORS SHOULD PERFORM CLOSE INSPECTION AT 1,600 FLIGHTS.
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