N943CA

Service difficulty reports not matched to an aircraft · 68

They name N943CA, 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 = 'N943CA' 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 COMA0160959Skin · dentedFUSELAGE SKIN FWD OF PAX DOOR FS 310.00 DENTED APPROXIMATELY .020 DEEP. FABBED REPAIR PARTS AND INSTALLED IAW CANADAIR REO 601R-53-21-180.Dec 12, 2001 · N943CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0160873Web · crackedENGINE SUPPORT BEAM CRACKED AT THE LEFT AND RIGHT LOWER WEB ACCESS PANEL.CUT OUT DAMAGE AND INSTALLED REPAIR TO LEFT AND RIGHT LOWER WEB I/A/W REO 601R-53-61-366.Nov 4, 2001 · N943CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160872Web · crackedENGINE SUPPORT BEAM CRACKED ON UPPER WEB.CUT OUT DAMAGE SECTION AND INSTALLED TEMPORARY REPAIR TO UPPER AND LOWER WEB. I/A/W REO 601R-53-61-345.Nov 4, 2001 · N943CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160870Plank · faultyFLAW INDICATION WERE NOTED BY EDDY CURRENT METHOD AT LOWER WING SURFACE ACCESS OPENINGS AT 640 EB W/S 116.366, 640 CB W.S. 76.161 AND 640 EB W.S. 116.366, 540 AB W.S. 56.68.BLENDED DAMAGE AT 4 ACCESS PANEL CUT OUTS I/A/W 601R-57-21-030.Nov 4, 2001 · N943CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0160871Skin · crackedOVERWING SKIN CRACKED ON FUSELAGE AT STA F.S.520.00 TO F.S. 528.7.REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLERS I/A/W REO 601R-53-51-069.Oct 29, 2001 · N943CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0160856Lamp · inoperativeFLIGHT #5800 - EMERGENCY FLOOR PATH LIGHTING, ROWS 9 AFT, ARE INOPERABLE.REPLACED DAMAGED FLOOR PATH LIGHTING STIRP.Oct 25, 2001 · N943CA · Cndair CL6002B19 · Emergency LightingSDR COMA0160645LightFLIGHT #5780. DURING PRE-FLIGHT INSPECTION DISCOVERED THE FLOOR EMERGENCY LIGHTING BETWEEN ROWS 9 AND 13 TO BE INOPERATIVE.RE-CONNECTED AFFECTED FLOOR EMERGENCY LIGHTING STRIP.Aug 28, 2001 · N943CA · Cndair CL6002B19 · Emergency LightingSDR COMA0160652Radome · burnedFLIGHT #5628. DURING CRUSIE FLIGHT AIRCRAFT ENCOUNTERED A LIGHTNING STRIKE, CREW REPORTED SMOKE/BURNING SMELL IN CABIN AND GALLEY AREA. AIRCRAFT CONTINUED FLIGHT TO IAD AND LANDED SAFELY.REPLACED THE RADOME.Aug 26, 2001 · N943CA · Cndair CL6002B19 · Aerodynamic FairingsSDR COMA0160533Switch · malfunctionedWING OVERHEAT MESSAGE.REPLACED THE BACKUP OVERHEAT SWITCH.Jul 28, 2001 · N943CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA0160501Control Unit · failedON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE MOTOR CONTROL UNIT.Jul 26, 2001 · N943CA · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0160500Control Unit · failedON FINAL APPROACH INTO CVG THE PITCH TRIM CAUTION MESSAGE ACTIVATED.REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT.Jul 26, 2001 · N943CA · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0160354Beam · crackedVERTICAL BEAM AT RBL 27 AND LBL 27 FS 409.0 + 128 INBOARD LOWER FASTENERS CRACKED. REPAIRED BOTH BEAMS IAW WVAC EO 601R-53-2336C.Mar 28, 2001 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160352Post · crackedINBOARD AND OUTBOARD POSTS AT RBL 9 AND LBL 9 AT FS 559 ARE CRACKED AT APPROXIMATELY WL 45. CAUSE UNKNOWN. DAMAGED AREAS REMOVED AND REPAIRED IAW WVAC EO 601R-53-2335B.Mar 26, 2001 · N943CA · Cndair CL6002B19 · Fuselage Fixed PartitionsSDR COMA0160341Angle · crackedTHE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT ANGLES AT RBL 27 AND LBL 27 INTERCOSTALS AT BL/36 (LEFT AND RIGHT) AT FS 484 I/A/W WVAC EO 601R-53-2334A.Mar 26, 2001 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160340Angle · crackedVERTICAL J-ANGLE CLIP INSIDE CBP1 AT LBL 9 IS CRACKED. REPAIRED IAW WVAC EO 601R-53-2337A.Mar 26, 2001 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160339Angle · crackedTHE ANGLES AT RBL 27 AND LBL 27 AND INTERCOSTALS AT BL 36 (LT AND RT) AT FS 484 ARE CRACKED. REPAIRED LEFT AND RIGHT ANGLES AT RBL 27 AND LBL 27 INTERCOSTAL AT BL/36 (LEFT AND RIGHT) AT FS 484 IAW WVAC EO 601R-53-2334B.Mar 26, 2001 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0160136Unknown · odorSTRONG ODOR OF FUEL IN CABIN WITH APU OPERATING. COULD NOT DUPLCIATE. INSPECTED APU. NO LEAKS OR DEFECTS NOTED.Jan 19, 2001 · N943CA · Cndair CL6002B19 · Air Distribution SystemSDR COMA0160071Windshield · failedPILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.Jan 3, 2001 · N943CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA0160023Skin · dentedTEMPORARY REPAIR ON FUSELAGE AFT AND BELOW CARGO DOOR.REPAIRED FOUR DENTS BETWEEN FS625 - 654.4 LT SIDE I/A/W W.V.A.C. E.O. 601R-53-2058.Dec 31, 2000 · N943CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0160011Computer · malfunctionedSTALL FAIL CAUTION MESSAGE DURING T/O. RESET THE STALL COMPUTER.Dec 24, 2000 · N943CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0060947Computer · malfunctionedSTALL FAIL MESSAGE DURING T/O. RESET STALL COMPUTER.Nov 20, 2000 · N943CA · Cndair CL6002B19 · Navigation SystemSDR COMA0060734Latch · out of adjDOOR HANDLE CAUTION MESSAGE. ADJUSTED DOOR LATCH MECHANISM.Sep 9, 2000 · N943CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060641Strap · damagedCAPPING STRAP ON RBL 9 AT FS 409 AND 16 WAS CUT TO TRANSVERSE BEAM NOT TO S/B 601R-53-037 SPECIFICATIONS. STRAP SHOULD NOT HAVE BEEN CUT. REPAIRED CAPPING STRIP ON RBL 9 AT FS 409 AND + 16 IAW WVAC EO 601R-53-1574.Aug 9, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060640Splice · misdrilledWHILE PERFORMING S/B 601R-53-037 P/N 601R31030-77 FS 409 SPLICE PLATE WAS DRILLED UPSIDE DOWN NOT TO WVAC EO 601R-53-1563 SPECIFICATIONS LBL 9. DRILLED AND INSTALLED NEW SERVICEABLE SPLICE PLATE IAW WVAC EO 601R-53-1563.Aug 9, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060635Strap · mismanufacturedWHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A CAPPING STRAP P/N 601R31030-77/S WAS MANUFACTURED INCORRECTLY AT RBL 9. REPAIRED 601R3103-77 CAPPING STRAP, RBL 9 IAW WVAC EO 601R-53-1563.Aug 7, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060634Strap · mismanufacturedWHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND CAPPING STRAP LBL 9 P/N 601R31030-77S IS MANUFACTURED INCORRECTLY. REPAIRED 601R31030-77 CAPPING STRAP LBL 9 IAW WVAC EO 601R-53-1563.Aug 7, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060633Angle · misinstalledWHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND LBL 9 ATTACH BRACKETS FOR TRANSVERSE BEAMS REQUIRE SHIMMING TO MAINTAIN SUFFICIENT EDGE DISTANCE ON WEBS. FABRICATED SHIMS FOR ANGLES 601R311011-61S/62S/80S/81S/82S IAW EO 601R-52-1564.Aug 7, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060632Angle · misrepairedWHILE PERFORMING TITANIUM FLOORBEAM S/B 601R-53-037 REV A FOUND RBL 9 TO HAVE SHORT EO ON ANGLE BRACKETS AT THREE POSITIONS FS 280, 349 AND 364 TO A/C CONFIGURATION. FABRICATED AND INSTALLED NEW ANGLE BRACKETS IAW WVAC EO 601R-53-1561.Aug 7, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060636Threshold · corrodedPASSENGER DOOR SUPPORT THRESHOLD P/N 601R31527-221 AT FS 310.0 TO FS 349.0 LHS FS CORRODED. PERFORMED A MAJOR REPAIR BY REPLACING CORRODED THRESHOLD P/N 601R31527-221 AT FS 310.00 TO FS 349.0 LHS IAW WVAC EO 601R-53-1560.Aug 6, 2000 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060455Light · inoperativeAFT SECTION OF EMERGENCY FLOOR LIGHTS IS INOPERABLE. SECURED LOOSE CONNECTION IN LIGHT STRIP. SYSTEM OPERATIONAL.May 25, 2000 · N943CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060355Windshield · failedCO-PILOTS SIDE WINDOW SHATTERED. REPLACED WINDOW.Apr 18, 2000 · N943CA · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA9960632Skiin · cracked2 CRACKS DETECTED IN THE LOWER HORIZONTAL SURFACE LT LOWER WING ACCESS HOLE AT 540AB. BLENDED OUT DAMAGED AREAS, ROTO-PEENED, ALODINED IAW BOMBARDIER REO 601R-57-21-030.Oct 16, 1999 · N943CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA9960631Skin · crackedCRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF LT LOWER WING ACCESS HOLE AT 540EB. BLENDED OUT DAMAGED AREA, ROTO-PEENED AND ALODINED IAW BOMBARDIER REO 601R-57-21-030.Oct 16, 1999 · N943CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA9960630Skin · crackedCRACK DETECTED IN THE LOWER HORIZONTAL SURFACE OF RT LOWER WING ACCESS HOLE AT 640EB. BLENDED OUT DAMAGE AREA, ROTO-PEENED ALODINED IAW BOMBARDIER REO 601R-57-21-030.Oct 16, 1999 · N943CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA9960526Bulb · failedELECTRICAL ODOR IN THE AREA OF CABIN SEATING ROWS 2 AND 3 DURING FLIGHT. AIRCRAFT RETURNED TO CVG. REPLACED CEILING LIGHT BULBS ABOVE SEATS 2 AND 3.Sep 14, 1999 · N943CA · Cndair CL6002B19 · Passenger Compartment LightingSDR COMA9960507Angle · chafedPANEL 411AL CHAFED BY FASTENER MID FRAME OUTBOARD EDGE LEFT HAND ENGINE PYLON. PERFORMED MAJOR REPAIR SMOOTHED CHAFE ON (P/N 601-37004-133) AND FABED NEW SUPPORT ANGLE 601-37004-57 AS PER SAMPLE USING 2024-T3.040 PO NR 4206/1 AND INSTALLED IAW WVAC EO NR 601RSep 12, 1999 · N943CA · Cndair CL6002B19 · Nacelle/Pylon StructureSDR COMA9960506Frame · crackedFRAME AT FS 718.00 RHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 2 ABOVE STRINGER II IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING BETWEEN THE FIRST AND SECOND FASTENER HOLE BELOW STRINGER II. ALSO, THESep 12, 1999 · N943CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA9960502Frame · crackedFRAME AT FS 718.00 LHS HAS TWO CRACKS. ONE CRACK IS IN THE RADIUS EXTENDING APPROXIMATELY 4 ABOVE STRINGER II IN THE FLANGE ATTACHING TO THE SKIN AND THE OTHER IS IN THE FLANGE EXTENDING TO THE SECOND FASTENER HOLE BELOW STRINGER II. ALSO, DOUBLER ON THE AFTSep 12, 1999 · N943CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA9960422Deploy Sys · malfunctionedADG DEPLOYED DURING FLIGHT. DEFERRED THE ADG AUTO DEPLOY SYSTEM.Aug 7, 1999 · N943CA · Cndair CL6002B19 · DC Generating SystemSDR COMA9960360Wire Harness · looseAFTER TAKEOFF, RIGHT ENGINE ROLLED BACK AND THEN SURGED 10 PERCENT. SECURED LOOSE WIRING HARNESS AT FUEL CONTROL UNIT.Jul 11, 1999 · N943CA · Cndair CL6002B19 · Engine Fuel System WiringSDR COMA9960289Cowl · crackedDURING MAINTENANCE SEVERAL CRACKS WERE FOUND ON INLET COWL AFT BULKHEAD OF RIGHT ENGINE. ENGINE INLET COWL WAS REPLACED.Jun 21, 1999 · N943CA · Cndair CL6002B19 · Engine Cowling SystemSDR COMA9960056Striker Seal · crackedPASSENGER DOOR STRIKER SEAL DAMAGED BY BOTTOM AFT LATCH PIN. REPAIRED DAMAGE TO PAX DOOR STRIKER SEAL PER REO 601R-52-11-008.Feb 3, 1999 · N943CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA9960034Fuel Control · malfunctionNR 1 ENGINE LAGS NR 2 DURING TAKEOFF. REPLACED THE LEFT ENGINE FUEL CONTROL.Jan 15, 1999 · N943CA · Cndair CL6002B19 · Fuel Control/Turbine EnginesSDR COMA9860021Tcas · malfunctionedAIRCRAFT SUSTAINED NEGATIVE 'GS' FOR 5 SECONDS DUE TO TCAS RA COMMAND, (FALSE WARNING). COMPLIED WITH TURBULANCE AND HARD LANDING INSPECTIONS. NO DAGMAGE NOTES.Jan 22, 1998 · N943CA · Cndair CL6002B19 · Air Collision Avoidance SystemSDR COMA9860007Transformer · out of adjustUPON GEAR EXTENSION, RECEIVED STEERING CAUTION MESSAGE. ADJUSTED THE ROTARY VARIABLE DIFFERENTIAL TRANSFORMER.Jan 11, 1998 · N943CA · Cndair CL6002B19 · Landing Gear Steering SystemSDR COMA9760251Steering · malfunctionedSTEERING INOP MESSAGE WHEN LANDING GEAR LOWERED. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK OF NWS SYSTEM WAS NORMAL.Dec 17, 1997 · N943CA · Cndair CL6002B19 · Landing Gear Steering SystemSDR COMA9760219Fuse · blownSERVICE DOOR EMERGENCY LIGHT IS INOP. REPLACED POWER SUPPLY FUSE F2.Nov 6, 1997 · N943CA · Cndair CL6002B19 · Emergency LightingSDR COMA9760216Lamp · failedLEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REPLACED BULB.Nov 5, 1997 · N943CA · Cndair CL6002B19 · Emergency LightingSDR COMA976020Flap Lever · malfunctionFLAPS FAILED AT 20 DEGREES AFTER TAKEOFF. REPLACED THE FLAP CONTROL HANDLE.Oct 22, 1997 · N943CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9760177Retract Mech · malfunctionedFLAPS FAILED AT 20 DEGREES. COULD NOT DUPLICATE DISCREPANCY. OPERATONAL CHECK OF FLAP SYSTEM NORMAL, NO FAULTS FOUND.Sep 19, 1997 · N943CA · Cndair CL6002B19 · Trailing Edge Flap Control System
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