N946CA

Service difficulty reports not matched to an aircraft · 78

They name N946CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N946CA' AND registry_match IS NULL
  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.

SDR COMA0160914Beam · crackedVERTICAL BEAM AT F.S. 409+128 RBL 27 CRACKED. VERTIDCAL BEAM AT F.S. 49+128 RBL 18 CRACKED. VERTICAL BEAM AT 409+128 LBL 27 CRACKED. NOTE: ALL BEAMS WERE CRACKED AT THE BOTTOM RIVET REF MAINT LOG PAGES #390153,#390154,#390155.VERTICAL BEAMS WERE REPAIRED I/ANov 22, 2001 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160913Beam · crackedENGINE SUPPORT BEAM AT F.S. 625 L/H WEB CRACKED, R/H SIDE WEB REPAIR INSTALLED PER CUSTOMER REQUEST. ALSO CENTER BEAM, UPPER AND LOWER WEBS CRACKED.PERFORMED A MAJOR REPAIR TO F.S. 625 ENGINE SUPPORT BEAM L/H AND R/H LOWER WEBS IAW REO 601R-53-61-366 REV C. RENov 21, 2001 · N946CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160660WindowFLIGHT #6015. DURING TAXI OUT RECEIVED A LEFT WINDOW AND LEFT WINDSHIELD OVERHEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE GATE.COOLED SUN HEATED WINDOWS WITH COLD WATER.Aug 29, 2001 · N946CA · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR COMA0160578LightFLOOR EMERGENCY LIGHTING FOR ROWS 9 THROUGH 12 FOUND INOPERATIVE.CLEANED CONNECTOR CONTACTS FOR AFFECTED LIGHTING, OPERATIONAL CHEECK WAS SATISFACTORY.Aug 8, 2001 · N946CA · Cndair CL6002B19 · Emergency LightingSDR COMA0160399Flap · chafedLEFT INBOARD FLAP, INTERIOR SKIN CHAFFED AT OUTBOARD ACTUATOR BONDING STRAP ATTACH POINT.REPLACED LEFT INBOARD FLAP WITH A SERVICEABLE PART S/N:SB/RJ/027.Jun 20, 2001 · N946CA · Cndair CL6002B19 · Leading Edge Slat Control SystemSDR COMA0160394Flap · chafedRIGHT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S/B 601R-57-022.Jun 20, 2001 · N946CA · Cndair CL6002B19 · Leading Edge Slat Control SystemSDR COMA0160282Stall Warning · activatedSTALL FAIL CAUTION DURING T/O. RESET THE STALL COMPUTER.Feb 21, 2001 · N946CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0160113Drag Brace · failedGEAR DISAGREE WARNING, NLG DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.Jan 14, 2001 · N946CA · Cndair CL6002B19 · Nose/Tail Landing GearSDR COMA0160066Computer · malfunctionedSTALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.Jan 5, 2001 · N946CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0160028Pseu · malfunctionedN.L.G. DID NOT RETRACT. REPLACED THE PSEU.Dec 29, 2000 · N946CA · Cndair CL6002B19 · Central WarningSDR COMA0061003Computer · malfunctionedSTALL FAIL CAUTION DURING TAKE OFF. RESET THE STALL COMPUTER.Dec 5, 2000 · N946CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060788Engine · failedLEFT ENGINE FAILED DURING CLIMB. TURBINE SEIZED. REMOVED AND REPLACED LEFT ENGINE.Oct 4, 2000 · N946CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060715Seal · tornLOUD SQUEAL FROM CABIN DOOR. REPLACED DOOR SEAL.Sep 2, 2000 · N946CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060562Light · inoperativeOVERHEAD EMERGENCY LIGHT AT ROW 4 IS INOPERABLE. DEFERRED MAINT PER MEL.Jul 9, 2000 · N946CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060496Floorbeam · corrodedTOP OF FLOORBEAM CAPS LBL 27, LBL 9, RBL 27, RBL 9 AT FS 280 TO 409 CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM CAPS (P/N 601R31113-67) FROM FS 280 TO FS 409 IAW REO 601R-53-00-027 REV N/C DATED 4 NOV 97.Jun 8, 2000 · N946CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0060495Angle · crackedVERTICAL J-ANGLE INSIDE CBP1 FS 280 LEFT HAND SIDE IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW WVAC EO 601R-53-1363.Jun 8, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060488Angle · corrodedTHE PASSENGER DOOR THRESHOLD ANGLE IS CORRODED AS WELL AS THE ANGLES FORWARD AND AFT OF THE MAIN ANGLE. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED ANGLES BETWEEN FS 310 - FS 349 LBL 42 IAW WVAC EO 601R-53-1361.Jun 7, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060493Skin · dentedTHE FUSELAGE SKIN HAS MULTIPLE DENTS BETWEEN FS 574.0 - FS 621.0 BETWEEN STR 29-23 LHS. PERFORMED A MAJOR REPAIR TO DENTED SKIN BETWEEN FS 574.0 - FS 621.0 STRI 20-23 LHS IAW WVAC EO 601R-53-1357.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0060487Clip · crackedBOTH CLIPS AT FS 280 - LBL 9 ARE CRACKED. REMOVED AND REPLACED CLIPS IAW WVAC EO 601R-53-1364.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060486Clip · crackedFOUND CLIPS AT FS 280 RBL 9 (P/N 601R31113-58) TO BE CRACKED. INSTALLED NEW CLIPS IAW WVAC EO 601R-53-1364.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060485Floorbeam · crackedFOUND FLOOR MEMBER (P/N 600-34017-17) AT FS 280.0 TO BE CRACKED L/1 - .75 INCH TO THE RIGHT OF FLOOR SUPPORT RBL 9.0. REPAIRED FLOOR MEMBER AT FS 280.0 AND RBL 9.0 IAW WVAC EO 601R-53-1366.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0060484Channel · corrodedFWD J-CHANNEL (P/N 600-34017-351) AT FS 280 CORRODED. REMOVED AND REPLACED FWD J-CHANNEL AT FS 280 IAW WVAC EO 601R-53-1367.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060483Angle · corrodedSERVICE DOOR ANGLE IS CORRODED (P/N 601R38303-105). REMOVED AND REPLACED CORRODED THRESHOLD ANGLE IAW WVAC EO 601R-53-1360.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060482Angle · crackedANGLE STIFFENER LOCATED AT THE FORWARD SIDE OF FS 280 AT LBL 9.0 WAS FOUND CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW WVAC EO 601R-53-1363.Jun 6, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060475Plate · corrodedFOUND TOP PLATES AT FS 349.00 TO BE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED TOP PLATES IAW WVAC EO 601R-53-1362 A.Jun 5, 2000 · N946CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060474Seal Bracket · dentedSEAL STRIKER ON PASSENGER DOOR AT FS 310.00 AND 349.00 DAMAGED CONTACT WITH DOOR PINS. REPAIRED IAW REO 601R-52-11-008 REPAIR A.Jun 5, 2000 · N946CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060130Drag Brace · failedGEAR DISAGREE WARNING DURING TAKEOFF. REPLACED THE NLG DRAG BRACE ASSY.Feb 3, 2000 · N946CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA9960711Controller · failedLEFT HAND PITOT, STATIC AND AOA HEAT CAUTION MESSAGE. REPLACED THE LEFT ADSHC.Nov 26, 1999 · N946CA · Cndair CL6002B19 · Pitot/Static Anti-Ice SystemSDR COMA9960562Windshield · crackedRIGHT WINDSHIELD CRACKED DURING FLIGHT AT 31,000 FEET, DESTINATION IAW. AIRCRAFT DIVERTED TO LIT. REPLACED RIGHT WINDSHIELD.Sep 27, 1999 · N946CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA9960491Warning · activatedCABIN DOOR LATCH MESSAGE ON EICAS. DEFERRED DOOR WARNING SYSTEM PER MEL.Sep 6, 1999 · N946CA · Cndair CL6002B19 · Door Warning SystemSDR COMA9960479Exhaust Frame · crackedRIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME.Aug 29, 1999 · N946CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR COMA9960467Smoke Detector · damagedCARGO SMOKE WARNING. REPLACED DAMAGED SMOKE DETECTOR IN CARGO COMPARTMENT.Aug 23, 1999 · N946CA · Cndair CL6002B19 · Smoke DetectionSDR COMA9960391Sensor Loop · chafedA 14TH STAGE BLEED AIR DUCT LEAK MESSAGE IFSD. REPLACED THE RT PYLON LEAK SENSOR LOOP.Jul 24, 1999 · N946CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA9960358Retract Mech · malfunctionedFLAPS FAILED. RESET FLAP SYSTEM, AIRCRAFT RETURNED TO SERVICE.Jul 10, 1999 · N946CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9960299Duct · wornAPU EXHAUST SUPPORT DUCT ASSY IS WORN ON INBOARD SIDE. REPLACED DUCT.Jun 13, 1999 · N946CA · Cndair CL6002B19 · APU Exhaust SystemSDR COMA9960298Clamp · brokenAPU EXHAUST FINGER CLAMP HAS BROKEN AND CHAFED FINGERS. REPLACED CLAMP.Jun 13, 1999 · N946CA · Cndair CL6002B19 · APU Exhaust SystemSDR COMA9960297Duct · brokenAPU EXHAUST DUCT HAS SEVERAL BROKEN TABS. REPLACED DUCT.Jun 13, 1999 · N946CA · Cndair CL6002B19 · APU Exhaust SystemSDR COMA9960296Cover · brokenFLOOR EMERGENCY LIGHT STRIP TOP COVER BROKEN. REPLACED COVER.Jun 13, 1999 · N946CA · Cndair CL6002B19 · Emergency LightingSDR COMA9960293Dampener · leakingLEFT INBOARD ELEVATOR FLUTTER DAMPENER LEAKING. REPLACED FLUTTER DAMPENER.Jun 13, 1999 · N946CA · Cndair CL6002B19 · Elevator Control SystemSDR COMA9960292Blanket · damagedUPPER APU EXHAUST HEAT BLANKET HAS HOLES. REPLACED HEAT BLANKET.Jun 13, 1999 · N946CA · Cndair CL6002B19 · APU Exhaust SystemSDR COMA9960291Blanket · damagedLOWER APU EXHAUST HEAT BRACKET HAS HOLES. REPLACED HEAT BLANKET.Jun 13, 1999 · N946CA · Cndair CL6002B19 · APU Exhaust SystemSDR COMA9960290Support · crackedCARGO DOOR SLIDE BRACKET SUPPORT CRACKED. REPLACED SUPPORT.Jun 13, 1999 · N946CA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR COMA9960279Frame · crackedFS 718 AND STR 11 (LHS) HAS A CRACK IN THE RADIUS EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE ABOVE STRINGER 11 IN THE FLANGE ATTACHING TO THE SKIN AND A CRACK IN THE DOUBLER ON THE AFT SIDE OF FRAME. FRAME FLANGE REPAIRED IAW WVAC EO 601R-53-0066. Jun 13, 1999 · N946CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA9960278Frame · crackedFS 718 AND STR 11 (RHS), DISCOVERED DURING 24 MONTH INSPECTION TO HAVE A CRACK IN THE RADIUS EXTENDING BETWEEN THE SECOND AND THIRD FASTENER HOLE ABOVE STR 11 IN THE FLANGE, A CRACK IN THE FLANGE EXTNEDING THROUGH THE FIRST FASTENER HOLE, AND A CRACK IN THE DOJun 13, 1999 · N946CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA9960295Bulkhead Angle · crackedANGLE BRACKET ON REAR PRESSURE BULKHEAD, LEFT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.Jun 12, 1999 · N946CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA9960294Bukkhead Angle · crackedANGLE BRACKET ON REAR PRESSURE BULKHEAD RIGHT AFT SIDE IS CRACKED. REPLACED ANGLE BRACKET.Jun 12, 1999 · N946CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA9960192Control Handle · failedAFTER LANDING RETRACTED FLAPS TO 30 DEGREES, FLAPS INDICATED 30 DEGREES BUT FLAP CAUTION MESSAGE APPEARED. COMPLIED WITH EO 27-045 AD EO 27-046 AD. REMOVED AND REPLACED FLAP HANDLE.May 9, 1999 · N946CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9960161Duct · detachedDURING TAXI, AFTER NR 1 ENGINE START, COCKPIT FILLED WITH SMOKE. AIR DUCT BETWEEN LEFT HAND ACM AND HEAT EXCHANGER CAME OFF. REINSTALLED DUCT.Apr 18, 1999 · N946CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA9960111Lever · malfunctionedFLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP SELECTOR HANDLE.Mar 13, 1999 · N946CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9960110Bpsu · malfunctionedFLAPS FAILED AFTER TAKEOFF. REPLACED THE LEFT HAND BPSU.Mar 12, 1999 · N946CA · Cndair CL6002B19 · Trailing Edge Flap Control System
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