N948CA

Service difficulty reports not matched to an aircraft · 67

They name N948CA, 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 = 'N948CA' 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 COMA0160879Web · chafedTHE AFT PRESSURE BULKHEAD HAS A HOLE WORN IN THE WEB STRUCTURE FROM A FASTENER THAT PROTRUDED BEYOND THE CARGO LINER INSTALLATION.PERFORMED A MAJOR REPAIR TO 621 BULKHEAD I/A/W WVAC EO 601R-53-2820A.Nov 7, 2001 · N948CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0160878Web · crackedL/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKEDPERFORMED A MAJOR REPAIR TO L/H ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-366 REV C AND WVAC EO 601R-33-2822.Nov 7, 2001 · N948CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160876Web · crackedR/H ENGINE SUPPORT BEAM I/B FORWARD CORNER CRACKED.PERFORMED A MAJOR REPAIR TO R/II ENGINE SUPPORT BEAM I/A/W CRJ REO 601R-53-61-366 REV C.Nov 7, 2001 · N948CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160810Actuator · faultyFLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY.REPLACED RIGHT INBOARD FLAP, INBOARD ACTUATOR.Oct 13, 2001 · N948CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0160809Actuator · faultyFLIGHT 5555. DURING APPROACH INTO CRW, RECEIVED A FLAP FAIL CAUTION WITH FLAP POSITION AT 26 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED SAFELY.REPLACED LEFT INBOARD FLAP, INBOARD ACTUATOR.Oct 13, 2001 · N948CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0160789Bpsu · malfunctionedFLIGHT #5431. FLAPS FAILED AT 39 DEGREES.REPLACED THE L/H BPSU.Oct 8, 2001 · N948CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160787Flap · failedFLIGHT 5234 - FLAPS FAILED AT 30 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01. A/C CONTINUED SERVICE.Oct 7, 2001 · N948CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160697Angle · crackedINTERCOSTAL FLANGES AT BL36 AND ANGLES AT BL27 LEFT AND RIGHT SIDES ARE CRACKED.REPAIRED ANGLE AND INTERCOSTAL AT FS484 I/A/W WVAC EO 601R-53-2701.Sep 8, 2001 · N948CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160696Angle · crackedPERFORMED A MAJOR REPAIR TO THE L/H AND R/H VERTICAL J-ANGLES AT F.S. 280, BL 9.0 L/H AND R/H BY REMOVING THE CRACKED ANGLES AND INSTALLING FABRICATED ANGLES I/A/W WVAC EO 601R-53-2705.Sep 8, 2001 · N948CA · Cndair CL6002B19 · Fuselage Structure (General)SDR COMA0160170Computer · malfunctionedSTALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.Jan 26, 2001 · N948CA · Cndair CL6002B19 · Stall Warning SystemSDR COMA0160008Control Unit · malfunctionedCONFIG SPOILERS WARNING DURING REJECTED T/O.COULD NOT DUPLICATE, SPOILER SYSTEM FUNCTION CHECK WAS NORMAL.Dec 21, 2000 · N948CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0061038Plate · wornCABIN DOOR WARNING. REPLACED THE INNER DOOR HANDLE CAM PLATE.Dec 11, 2000 · N948CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0061022Latch · out of adjCABIN DOOR LATCH CAUTION MESSAGE. ADJUSTED DOOR LATCH MECHANISM.Dec 8, 2000 · N948CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0060944Computer · malfunctionedSTALL FAIL MESSAGE DURING T/O. RESET STALL COMPUTER.Nov 20, 2000 · N948CA · Cndair CL6002B19 · Navigation SystemSDR COMA0060919Sensor · malfunctionedLANDING GEAR DISAGREE MESSAGE. NOSE LANDING GEAR PROXIMITY SENSOR WAS DAMAGED BY GROUND HANDLING TECHNIQUE. ADJUSTED THE NLG PROXIMITY SENSOR.Nov 13, 2000 · N948CA · Cndair CL6002B19 · Nose/Tail Landing GearSDR COMA0060891Idg · lowRT IDG CAUTION MESSAGE. SERVICED IDG WITH OIL TO PROPER LEVEL.Nov 6, 2000 · N948CA · Cndair CL6002B19 · AC Generation SystemSDR COMA0060769Light · inoperativeFWD FLOOR LEVEL EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT STRIP.Sep 28, 2000 · N948CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060746Plate · mismanufacturedTWO SPLICE PLATES (P/N 601R31030-77) FABRICATED INCORRECTLY BY THE MANUFACTURER. FABRICATED A NEW DOUBLER PLATE IAW WVAC EO 601R-53-1698.Sep 17, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060630Light · inoperativeEMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 THRU 5 IS INOPERABLE. SECURED ELECTRICAL CONNECTION, SYSTEM TEST NORMAL.Aug 8, 2000 · N948CA · Cndair CL6002B19 · Emergency LightingSDR COMA0060373Transponder · failedNR 2 TRANSPONDER FAILED. DEFERRED THE NR 2 TRANSPONDER PER MEL.Apr 24, 2000 · N948CA · Cndair CL6002B19 · Dependent Position Determining SystemSDR COMA0060358Warning System · activatedFLIGHT SPOILER FAULT MESSAGE. RESET THE SECU CIRCUIT BREAKERS. SYSTEM TEST NORMAL. COULD NOT DUPLICATE.Apr 20, 2000 · N948CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0060286Harness · defectiveRIGHT HAND ENGINE N1 FLUCTUATES. REPLACED THE ENGINE BROWN WIRE HARNESS.Mar 24, 2000 · N948CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA0060265Warning System · activatedANTI-SKID CAUTION MESSAGE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. AIRCRAFT RETURNED TO SERVICE.Mar 14, 2000 · N948CA · Cndair CL6002B19 · Brake Anti-Skid SectionSDR COMA0060232Eec · malfunctionedRIGHT ENGINE N1 DROPPED FROM 87 PERCENT TO 78 PERCENT. DEFERRED THE ENGINE ELECTRONIC CONTROL SYSTEM PER MEL.Mar 2, 2000 · N948CA · Cndair CL6002B19 · Fuel Controlling SystemSDR COMA0060231Wire · brokenEMERGENCY EXIT LIGHT AT ROW 5 IS INOPERABLE. REPLACED POWER WIRE.Mar 2, 2000 · N948CA · Cndair CL6002B19 · Light System WiringSDR COMA0060207Skin Panel · cracked5 LEFT LOWER WING ACCESS HOLES CRACKED, 540-EB - WS 116.366, 540 FB - WS 136.676, 550AB - WS 163.000, 550DB-WS 280.415, AND 550 GB - WS 294.048. REPAIRED DAMAGE IAW REO 601R-57-21-030.Feb 26, 2000 · N948CA · Cndair CL6002B19 · Wing, Plate/SkinSDR COMA0060090Actuator · malfunctionedGEAR DISAGREE, LEFT MLG DID NOT RETRACT. COULD NOT DUPLICATE, REPLACED THE SIDE STAY ACTUATOR.Jan 24, 2000 · N948CA · Cndair CL6002B19 · Landing Gear ActuatorSDR COMA0060079Angle · crackedANGLE AT FS 280 AT LBL9 OUTBOARD SIDE IS CRACKED P/N 601R31113-57. INSTALLED NEW CLIP P/N 601R31113-57 IAW CRJ SRM 51-42-21 AND WVAC EO 601R-53-0868.Jan 20, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060077Web · damagedWEB ASSY AT FS 349.00 TO 364 HAS DAMAGED ON LBL 9. FABRICATED NEW WEB FROM 2024T3 .032, INSTALLED NEW WEB IAW WVAC EO 601R-53-0862.Jan 20, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060075Skin · damagedWHILE COMPLYING WITH S/B 601R-53-050 INSTALLATION OF AN EXTERNAL REINFORCING STRAP FOUND FOUR HOLES BIRLLED THROUGH THE SKIN AND FRAME AT FS 409 AND 128 BETWEEN STRINGER 24L AND 24R ARE OBLONG AND REQUIRES OVERSIZING TO COMPLETE THE REPAIR. OVERSIZED 4 DISCREJan 20, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0060074Sill · corrodedINTERCOSTAL AT RBL 42 BETWEEN 349 - FS 360 IS CORRODED. REMOVED CORROSION ON INTERCOSTAL AND INSTALLED REINFORCING ANBLE IAW WVAC EO601R-53-0880A.Jan 20, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060073Frame · crackedFRAME 280 IS CRACKED OUTBOARD OF RBL 9, APROXIMATELY .25 CRACK. FLOOR MEMBER P/N 600-34017-17 AT FS 280 REPAIRED IAW WVAC EO NO 601R-53-0869.Jan 20, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0060080Frame · damagedWHILE ACCOMPLISHING CANADAIR SERVICE BULLETIN 601R-53-030, FOUR FASTENER HOLES DRILLED THROUGH THE SKIN AND FRAME AT FS 409 AND 128, BETWEEN STRINGER 24L AND 24R WERE DISCOVERED TO BE OBLONG AND REQUIRED OVERSIZING TO COMPLETE THE REPAIR. PERFORMED A MAJOR REPJan 19, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0060067Angle · corrodedSERVICE DOOR ANGLE IS CORRODED AT FS 317 TO FS 342.0 P/N 601R38303-105. REMOVED CORRODED ANGLE AND REPLACED WITH NEW ANGLE IAW WVAC EO 601R-53-0865.Jan 18, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060066Floorbeam · corrodedTOP OF FLOORBEAM CAPS LBL9 AT FS 280 TO FS 409.0 RBL9 AT FS 280 TO FS 409.0 AND RBL 27 AT FS 280 TO FS 349 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM CAPS.Jan 18, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA0060065Plate · corrodedTOP PLATES OUTBOARD OF LBL 27, LBL9, RBL 9 AND RBL 27FS 349.0 CORRODED. REMOVED AND INSTALLED NEW TOP PLATES IAW WVAC EO 601R-53-0866.Jan 18, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060064Web · damagedWEB ASSY AT FS 349.0 TO 364.0 HAS DAMAGED HOLE ON LBL.9. INSTALLED NEW WEBW WVAC EO 601R-53-0862.Jan 18, 2000 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0060062Frame · crackedFRAME FS 718.00 STR 11-12 CRACKED IN RADIUS LHS. REPAIRED PER CANADAIR REO 601R-53-61-193A.Jan 17, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, StructureSDR COMA0060061Frame · crackedAFT DOUBLER OF FRAME FS 718.00 STR 11-12 RHS CRACKED. REPLACED PER CANADAIR REO 601R-53-61-193A.Jan 17, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0060060Frame · crackedFRAME FS 718.00 STR 11-12 RHS CRACKED IN RADIUS. REPAIRED PER CANADAIR REO 601R-53-61-192A.Jan 17, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0060059Frame · crackedAFT DOUBLER OF FRAME FS 718.00, STR 11-12 LHS CRACKED. REPLACED PER CANADAIR REO 601R-53-61-193A.Jan 17, 2000 · N948CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA9960764Filter · cloggedRIGHT HAND ENGINE OIL PRESSURE AT 130 PSI. REPLACED CLOGGED OIL FILTER, AND CLEANED THE OIL PUMP SCAVENGE SCREENS.Dec 14, 1999 · N948CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COMA9960759Window Heat · inoperativeLEFT WINDOW HEAT INOPERABLE. SWITCHED WIRE TERMINALS TO THE BACK UP TERMINAL BLOCK, OPERATIONAL CHECK NORMAL.Dec 10, 1999 · N948CA · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR COMA9960548Intercostal · misdrilledHOLES FOR A CANNON PLUG MOUNTING BRACKET WERE INCORRECTLY LOCATED ON THE INTERCOSTAL BETWEEN FS 217.75 AND FS 226 AT RBL 12 DURING ACCOMPLISHMENT OF COMAIR EO 601R-31-023 FOR MOD PART A & B. REPAIRED INTERCOSTAL BETWEEN FS 217.75 AND FS 226 IAW WVAC EO 601R-5Sep 19, 1999 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA9960547Doubler · crackedDOUBLER PLATE (P/N 600-31068-19) AT RBL 9 AT 461.00 CRACKED. REPLACED DOUBLER PLATE FOR RBL 9 AT FS 461.00 IAW WVAC EO 601R-53-0342.Sep 18, 1999 · N948CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA9960362Smoke Detector · malfunctionedCARGO SMOKE WARNING. REPLACED THE CARGO SMOKE DETECTOR.Jul 12, 1999 · N948CA · Cndair CL6002B19 · Smoke DetectionSDR COMA9960148Connector · defectiveEMERGENCY FLOOR LIGHTING, AFT SECTION, IS INOPERABLE. REPLACED WIRE CONNECTOR.Apr 7, 1999 · N948CA · Cndair CL6002B19 · Emergency LightingSDR COMA9860337Tr Unit · malfunctionedLEFT THRUST REVERSER MESSAGE DURING TAKEOFF. DEFERRED LEFT HAND THRUST REVERSER.Nov 8, 1998 · N948CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA9860289Pump · failedRIGHT HAND HYDRAULIC PUMP FAILED. REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP.Oct 1, 1998 · N948CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA9860208Light · inoperativeSEVERAL SECTIONS OF EMERGENCY FLOOR LIGHTING ARE INOPERABLE. REPLACED TWO SECTIONS OF FLOOR TRACK LIGHTING.Jul 29, 1998 · N948CA · Cndair CL6002B19 · Emergency Lighting
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