N941CA, cancelled Apr 18, 2018

Service difficulty reports · 102

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 = 'N941CA' AND deregistration_id = 'N941CA-2018-04-18'
  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 COMA20111850009Sensing Element · failedON CLIMBOUT FROM JAX TO DCA RECEIVED RIGHT ANTI-ICE DUCT WARNING MSG. IN ICING CONDITIONS. EMERGENCY DECLARED, A/C DIVERTED TO GSO LANDED SAFELY. REMOVED AND REPLACED RIGHT FUSELAGE SENSING ELEMENT A40WK.Jan 17, 2011 · N941CA · Cndair CL6002B19 · Pneumatic Indicating SystemSDR COMA2010060450124Floorbeam · corrodedCORROSION ON FLOORBEAM RBL 27 FS 618 AROUND NUT PLATE EXCEEDS DAMAGE LIMITATIONS. REMOVED CORROSION AND REPAIRED FLOORBEAM AT FS 618 RBL 27 IAW EA 10-5361-02977.Jun 4, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR COMA2010060150120Bulkhead · crackedBULKHEAD WEB CRACKED AROUND LINTEL ATTACH FITTING AT FS 621, LBL 36.2. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-61-1230 REV D.May 30, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2010060150200Bulkhead · crackedBULKHEAD WEB CRACKED FS 621.00, LBL 18, JUST ABOVE WL 73.0. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLERS IAW REO 601R-53-61-1285.May 30, 2010 · N941CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA2009120250222Connector · shortedDURING CLIMBOUT FROM CVG RECEIVED AN ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. REPLACED SHORTED CONNECTOR (P58WK).Dec 2, 2009 · N941CA · Cndair CL6002B19 · Ice/Rain Protection System WiringSDR COMA2009052750145Angle · crackedLT 559 CAP ANGLE CRACKED AT FS 559.00, LBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.May 24, 2009 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA2009052750144Angle · crackedRT 559 CAP ANGLE CRACKED AT FS 559.00, RBL 18.00. PERFORMED PERMANENT REPAIR IAW REO 601R-53-41-260.May 24, 2009 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0860257Skin · damagedFUSELAGE SKIN HAS DAMAGE FROM DOOR PIN AT FWD LOWER POSITION AT FS 310.00. TRIMMED OUT DAMAGE AND INSTALLED REPAIR PARTS PER REO 601R53-21-180 AND SR 99-5140-0001.May 23, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0860252Fitting · crackedWHILE PERFORMING TASK CARD CRJ-2-122006, SPECIAL DETAILED INSP OF THE WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 202.75, FOUND LOWER RT POST FITTING TO BE CRACKED. REPLACED FITTING IAW CRJ SRM 51-42-21 PGS 1-21.May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0860251Door Frame · crackedPAX DOOR FRAME FS 338.9 IS CRACKED AT UPPER END. REPAIRED IAW REO 601R-52-11-402.May 21, 2008 · N941CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0860250Frame · crackedCARGO COMPARTMENT UNDERFLOOR FRAME SECTOR AT FS 605 IS CRACKED. REMOVED AND REPLACED WITH SERV FRAME IAW CRJ SRM 51-42-06 AND COMAIR SR99-5140-0001.May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0860249Bulkhead · crackedTEMP REPAIR PREVIOUSLY APPLIED TO FS 559.0 BULKHEAD. REMOVED TEMP REPAIR AND PERFORMED PERMANENT REPAIR IAW COMAIR SR10-53-41-0001 REV A SECTION II.May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0860248Pressure Panel · crackedWHILE PERFORMING TASK CARD CRJ-2-162011, PRESSURE FLOOR SKIN DETAILED INSPECTION FOUND 2 CRACKS IN THE PRESSURE FLOOR SKIN BETWEEN RBL 9 AND LBL 9. CRACKS MEASURED 2.50" IN LENGTH. THE FLOOR SKIN WAS REPAIRED IAW BOMBARDIER REO 601R-53-41-103 REV D. May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0860247Frame · corrodedDURING A 72/48 MO INSPECTION, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE AND CRACKED ON LOWER EDGE. PERFORMED PERMANENT REPAIR IAW REO 601R-53-11-136.May 21, 2008 · N941CA · Cndair CL6002B19 · Fuselage Main, FrameSDR COMA0860244Sill · corrodedSEVERE CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED SECTION OF FLOOR SILL IAW EA 10-5320-02217.May 14, 2008 · N941CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0860051Unknown · unknownFLIGHT 5262 - ON DESCENT INTO JFK RECEIVED PROX SYSTEM CAUTION MESSAGE. EMERGENCY DECLARED, MESSAGE WENT OUT BELOW 200 KTS AND BEFORE GEAR EXTENSION. ALL INDICATIONS WERE NORMAL DURING LANDING. INSPECTED PSEU NO FAULT CODES STORED. PERFORMED SYSTEM SELF TEJan 4, 2008 · N941CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0760199Flap · malfunctionedFLIGHT 5138 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3 (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.Feb 19, 2007 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0760010Warning Light · false activationFLIGHT 5662 - DURING CLIMB THRU APPROX FL 180 LEFT REV UNLOCK MESSAGE CAME ON. FOLLOWED QRH AND RETURNED BACK TO PHF AND LANDED SAFELY. INSPECTED LEFT T/R AND STOW, DEPLOY AND THROTTLE LOCKOUT SWITCHES. ALL CHECKED GOOD. OPS CHECKED T/R, OPS CHECK GOOD.Jan 6, 2007 · N941CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0660584Pump · faultyFLIGHT 5395 - HYD NR 3 LOW PRESSURE CAUTION MESSAGE AT FLIGHT LEVEL 290, QTY ZERO, PRESSURE 1400 PSI. FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 3A ACMP.Oct 20, 2006 · N941CA · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR COMA0660526Switch · malfunctionedFLIGHT 5542 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM MHT TO CVG, FLIGHT DIVERTED TO MDT AND LANDED WITHOUT INCIDENT. FOUND RIGHT THRUST REVERSER STOW SWITCH OUT OF RIG. RE-ADJUSTED STOW SWITCH, OPS CHECK GOOD.Sep 2, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0660521Warning Light · false activationFLIGHT 5664 - RIGHT REV UNLOCK MESSAGE IN FLIGHT FROM CVG TO MSP. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. TRANSFERRED TO DMI LIST PER MEL 78-30-01.Sep 1, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0660517Thrust Reverser · malfunctionedFLIGHT 9463- EN ROUTE PIT-CVG RECEIVED A RIGHT ENGINE THRUST REVERSER CAUTION, FLIGHT DIVERTED TO CMH. DEFERRED THE RIGHT THRUST REVERSER PER MEL 78-30-01.Aug 30, 2006 · N941CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA0660442Light · inoperativeFLIGHT 5233 - FIRST 5 ROWS OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. REPLACED THE FIRST SECTION OF FLOOR TRACK LIGHTING STRIP.Jul 19, 2006 · N941CA · Cndair CL6002B19 · Emergency LightingSDR COMA0660441Light · inoperativeFLIGHT 5233 - SECTION OF FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE. DEFERRED INOPERATIVE SECTION OF FLOOR TRACK LIGHTING PER MEL 33-51-01.Jul 19, 2006 · N941CA · Cndair CL6002B19 · Emergency LightingSDR COMA0560506Actuator · faultyFLIGHT 5321 - DURING CLIMBOUT OF CVG THE NR 2 HYDRAULIC C/B TRIPPED. REPLACED THE NR 2 HYDRAULIC SOV ACTUATOR.Sep 17, 2005 · N941CA · Cndair CL6002B19 · Hydraulic System, MainSDR COMA0560491Warning Light · illuminatedFLIGHT 5089- FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Sep 7, 2005 · N941CA · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA0560414Outflow Valve · malfunctionedFLIGHT 5553 - CABIN ALTITUDE CAUTION MESSAGE. REPLACED THE PRIMARY OUTFLOW VALVE.Jul 27, 2005 · N941CA · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR COMA0560318Warning Light · false activationFLIGHT 5568 CARGO DOOR CAUTION MESSAGE. COULD NOT DUPLICATE. FOUND NO DEFECTS IN CARGO DOOR OR WARNING SYSTEM.May 22, 2005 · N941CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0560246Fcu · faultyFLIGHT 5142 RECEIVED A FLAP FAIL CAUTION WHILE PARKED AT THE GATE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.Apr 7, 2005 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560118Warning Light · illuminatedFLIGHT 5130 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. C/W EXTENSION AND RETRACTION CHECKS, NO DEFECTS FOUND.Feb 4, 2005 · N941CA · Cndair CL6002B19 · Landing Gear Position and WarningSDR COMA0560037Overheat Loop · malfunctionedFLIGHT 9487 ANTI ICE DUCT WARNING. REPLACED THE RIGHT WHEEL WELL SENSING LOOP.Jan 6, 2005 · N941CA · Cndair CL6002B19 · Overheat DetectionSDR COMA0560036Anti-Ice System · false indicationFLIGHT 4959 ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED AND OPERATIONAL CHECKS WERE NORMAL.Jan 6, 2005 · N941CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA0460599Skin · corrodedFLIGHT DURING HEAVY MAINTENANCE CHECK (PAX DOOR DETAILED INSPECTION) THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED IN ACCORDANCE WITH COMAIR ENGINEERING AUTHORIZATION EA 10-5210-00499. OK FOR RETURN TO SERVICNov 10, 2004 · N941CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA0460228Bulkhead · crackedCRACKS IN FORWARD PRESSURE BULKHEAD AT PARKING BRAKE CABLE PASS THROUGH. REPAIRED IN ACCORDANCE WITH REO 601R-53-11-539.Mar 29, 2004 · N941CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR COMA0460197Duct · blownFLIGHT 5200 RIGHT 14TH STAGE DUCT LEAK WARNING. FOUND 14TH STAGE BLEED DUCT BLOWN APART. REPLACED DUCT.Mar 12, 2004 · N941CA · Cndair CL6002B19 · Pneumatic Distribution SystemSDR COMA0460141Pcu · brokenFLIGHT 5110 GROUND SPOILER DEPLOY MESSAGE DURING APPROACH. LEFT OUTBOARD SPOILER PCU BROKEN. REPLACED PCU.Feb 10, 2004 · N941CA · Cndair CL6002B19 · Drag Control SystemSDR COMA0460018Warning Light · illuminatedFLIGHT 5833 ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE. SYSTEM OPERATION NORMAL.Jan 4, 2004 · N941CA · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR COMA0360135AcmFLIGHT 5892 AFTER T/O - BURNING ODOR IN COCKPIT AND CABIN.INSPECTED AIRCRAFT, NO DEFECTS NOTED, FLIGHT CHECK SATISFACTORY.Mar 9, 2003 · N941CA · Cndair CL6002B19 · Cabin Cooling SystemSDR COMA0360060ApuFLIGHT 5729 APU LOW OIL PRESSURE WARNING.ADDED 2.5 QUARTS OF OIL TO APU.Jan 29, 2003 · N941CA · Cndair CL6002B19 · APU Oil SystemSDR COMA0360029Apu · unwantedFLIGHT 5807 STRONG FUEL SMELL WHEN APU STARTED.REPLACED APU.Jan 14, 2003 · N941CA · Cndair CL6002B19 · Airborne Auxiliary Power Unit (APU) SystemSDR COMA0360010Priority Valve · unreliableFLIGHT 5495 LANDING GEAR DISAGREE WARNING.REPLACED THE NLG PRIORITY VALVE.Jan 1, 2003 · N941CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA0260580Lamp · inoperativeEMERGENCY LIGHTS ROWS 2 THUR 5 ARE INOPERABLE.REPLACED FLEXIBLE LAMP ASSEMBLY.Oct 10, 2002 · N941CA · Cndair CL6002B19 · Emergency LightingSDR COMA0160843Web · crackedDURING INSPECTION DISCOVERED A CRACK IN THE ENGINE SUPPORT BOX BEAM.PERFORMED TEMPORARY REPAIR TO UPPER AND LOWER WEBS F.S. 630 IN ACCORDANCE WITH CANADAIR REO 601R-53-61-345.Oct 22, 2001 · N941CA · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR COMA0160820Skin · chafedFLIGHT N/A, DURING REPAIR OF ENGINE BOX BEAM DISCOVERED A CHAFED AREA ABOVE THE BOX BEAM AT Z-MEMBER. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-448.Oct 16, 2001 · N941CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0160640Switch · faultyFLIGHT #5612. DURING CLIMB OUT OF LIT AT 9000 FT. RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED D117 PROXIMITY SWITCH IN MAIN CABIN DOOR.Aug 24, 2001 · N941CA · Cndair CL6002B19 · Door Warning SystemSDR COMA0160455Flap · failedFLAP CAUTION MESSAGE AFTER TAKE-OFF FROM GSP, AIRCRAFT RETURNED TO THE FIELD.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIREST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3 (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGE.Jul 10, 2001 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160462Bpsu · wornFLAP CAUTION MESSAGE DURING APPROACH INTO CVG, AN EMERGENCY WAS DECLARED, AIRCRAFT LANDED SAFETLY.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "SECOND EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 3 (D AND E)4. REPLACED THE RIGHT BRAKE POSITIONING SENSING UNIT.Jul 10, 2001 · N941CA · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0160355Bushing · wornRIGHT VERT STAB BUSHING AT HORZ STAB PIVOT POINT WORN. REMOVED AND REPLACED BUSHING P/N 601R-55-31-001-5 IAW CRJ AMM 20-26-00-910-803. MACHINED BUSHING IAW WVAC EO 601R-55-2345. BORE WITHIN TOLERANCE IAW CRJ DRAWING 600-21058. REAMED BUSHING IAW CRJ DRAWINMar 28, 2001 · N941CA · Cndair CL6002B19 · Vertical Stabilizer, Attach FittingsSDR COMA0160322Warning System · malfunctionedT/O CONFIG MESSAGE DURING T/O. COULD NOT DUPLICATE. OPERATIONAL CHECK OF SYSTEM NORMAL.Mar 15, 2001 · N941CA · Cndair CL6002B19 · Central WarningSDR COMA0061059Computer · malfunctionedSTALL FAIL MESSAGE DURING T/O. RESET THE STALL COMPUTER.Dec 17, 2000 · N941CA · Cndair CL6002B19 · Stall Warning System
Back to N941CA, cancelled Apr 18, 2018