N496CA

Service difficulty reports · 163

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 = 'N496CA' 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.

SDR SWIA202156422Angle · cracked* OUTBOARD CLIP AT RBL9 COMMON TO FS280 IS CRACKED. (C-CHECK) RO 2/25/2021 REPLACED OUTBOARD CLIP AT RBL9 COMMON TO FS280 PN: 601R-53-11-171-5 IAW REO 601R-53-11-171 REV -D DATED 13-FEB-07. COMPLETED 51-900-1003-SKYJan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156421Angle · cracked* INBOARD CLIP AT RBL9 COMMON TO FS280 IS CRACKED. (C-CHECK) RO 2/25/2021 REPLACED INBOARD CLIP AT RBL9 COMMON TO FS280, PN: 601R-31113-58 IAW REO 601R-53-11-171 REV -D DATED 13-FEB-07. COMPLETED 51-900-1003-SKYJan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156420Angle · cracked* OUTBOARD CLIP AT LBL9 COMMON TO FS280 IS CRACKED. (C-CHECK) RO 2/25/2021 REPLACED OUTBOARD CLIP AT LBL9 COMMON TO FS280, PN: 601R-53-11-171-2 IAW REO 601R-53-11-171 REV -D DATED 13-FEB-07. COMPLETED 51-900-1003-SKY.Jan 15, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156419Skin · chafedLEFT WING AFT SPAR - AFT LOWER WING PLANK, DIRECTLY BELOW LEFT REAR LOWER SPLICE JOINT @ BL 45, SHOWS EVIDENCE OF CHAFFING AND IMPACT DAMAGE AS MARKED (C-CHECK) RO 2/25/2021 REMOVED CHAFING ON LEFT WING AFT SPAR -AFT LOWER WING PLANK, DIRECTLY BELOW LEFT RJan 15, 2021 · N496CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202156469Spoiler · chafedL/H WING (INBD) GROUND SPOILER (UNDERSIDE SURFACE) "CHAFED" ALONG THE LEADING EDGE FROM MECHANICAL CONTACT WITH STAINLESS CLOSE OUT STRIP ATTACHED TO UPPER WING SKIN (MARKED). (C-CHECK) RO 2/25/2021 REMOVED CHAFING DAMAGE ON UNDERSIDE LE OF LH WING GROUND Jan 14, 2021 · N496CA · Cndair CL6002B19 · SpoilersSDR SWIA202156461Spoileron · corrodedCORROSION DETECTED ON HARDWARE, L/H WING SPOILERON, AT "BOTH" OTBD & INBD HINGE ATTACH POINTS. THE "NUTS" ON THE HINGE BOLTS AND THE ANTI-MIGRATION FITTINGS ATTACHING BOLTS (FLAGGED). (C-CHECK) RO 2/25/2021. INSTALLED WITH NEW FROM STOCK (2EA) NUTS AND WASHJan 14, 2021 · N496CA · Cndair CL6002B19 · SpoilersSDR SWIA202156460Flap System · corrodedCORROSION DETECTED DURING DETAILED INSP OF L/H OTBD FLAP HINGE BOXES, ON L/H OTBD FLAP (CENTER) HINGE BOX BUTE DOOR "SPRING" ACUTATOR , ON THE SPRING COILS (FLAGGED). (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED L/H OTBD FLAP HINGE BOX SPRING WITH A NEW HINGJan 14, 2021 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156459Flap System · corrodedRH IB FLAP #2 HINGE BOX TO HINGE ARM MOUNTING HARDWARE CORRODED. (C-CHECK) RO 2/25/2021.Jan 13, 2021 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156458Flap System · corrodedRH OB FLAP #3 HINGE BOX SPRING CORRODED. (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED R/H OB FLAP #3 HINGE BOX SPRING WITH A NEW HINGE BOX SPRING REF CRJ200 AMM 27-54-25-000-801 AND CRJ200 AMM 27-54-25-400-801.Jan 13, 2021 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156457Flap System · corrodedRH OB FLAP #4 HINGE BOX AFT MOUNTING HARDWARE CORRODED. (C-CHECK) RO 2/25/2021.Jan 13, 2021 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156418Spar · chafedRIGHT WING AFT SPAR - AFT LOWER WING PLANK, DIRECTLY BELOW REAR LOWER SPLICE JOINT @ BL 45, SHOWS EVIDENCE OF CHAFFING AND IMPACT DAMAGE AS MARKED / 57-610-600 (C-CHECK) RO 2/25/2021 REMOVED CHAFING DAMAGE TO WING PLANK TO A SMOOTH FINISH.C/W NDT INSPECTIOJan 13, 2021 · N496CA · Cndair CL6002B19 · Wing SparSDR SWIA202156417Stringer · cracked*STGR3L CRACKED AT FS379.00 AT THE ATTACH POINT WITH THE LONGERON. (C-CHECK) RO 2/25/2021 COMPLIED WITH REPAIR AT STGR3L FS379.00 REF REO 601R-53-21-3391 REV--, DATED 2021-01-26. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.Jan 13, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202156416Spar · chafedLEFT PYLON FRONT SPAR LOWER SURFACE HAS EVIDENCE OF CHAFING AND IS MISSING SEALANT PAD. (C-CHECK) RO 2/25/2021 REMOVED CHAFE DAMAGE FROM L/H PYLON FRONT SPAR LOWER SURFACE, ENSURED CHAFE DAMAGE WAS BLENDED TO A SMOOTH CONTOUR, NDT INSPECTED NO DEFECTS NOTEJan 8, 2021 · N496CA · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR SWIA202156456Riser · corrodedPAX DOOR FORWARD RISER IS CORRODED AT THE TOP STEP, MARKED. (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED FWD RISER W. NEW REF CRJ 200 SRM 51-42-06.Jan 2, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202156453Angle · crackedPAX DOOR AFT RISER DRAG ANGLE REPAIR SPLICE IS CRACKED, MARKED. (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE P/N 601R31772-5. REF: CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-42-13.Jan 2, 2021 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA202053467Landing Gear · obstructedRT F GEAR DISAGREE ON TAKEOFF. RT MAIN GEAR WOULD NOT COME UP. QRC HAD US PULL MANUAL GEAR EXTENSION. ALL GEAR CAME DOWN. NORMAL LANDING. NO OVERWEIGHT LANDING. PSEU WAS FLAGGING THE RT MLG UPLOCK. VERIFIED THE RT MLG UPLOCK GAP WAS WITHIN LIMITS, IN REOct 20, 2020 · N496CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2020082151949Striker · crackedBROKEN/CRACKED SEAL STRIKER BY FORWARD UPPER PAX DOOR FITTING. COMPLIED WITH REO. REPAIRED THE PASSENGER DOOR SEAL STRIKER.Aug 20, 2020 · N496CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2019071646060Unknown · malfunctionedRIGHT MAIN LANDING GEAR DISAGREE. QRH COMPLIED WITH. LANDING GEAR CYCLED BEFORE RIGHT MAIN GEAR SHOWED DOWN AND LOCKED. (FLT#3726) CLOSED DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL.Jul 16, 2019 · N496CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019030545609Attach Fitting · damagedRT WINDSHIELD CENTER POST ATTACH CLIP WL 110.00 DEFECT NOTED. (C-CHECK) RO: 03/04/2019 REMOVED AND REPLACED DAMAGED RT WINDSHIELD CENTER POST ATTACH CLIP IAW SRM.Feb 10, 2019 · N496CA · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2019030545608Plate · corrodedPASSENGER DOOR SURROUND. WARDROBE PLATFORM LT FS310.00 TO FS280.00 HAS CORROSION AROUND THE WARDROBE MOUNT HOLES. (C-CHECK) RO: 03/04/2019 BLENDED OUT CORROSION DAMAGES AT 2EA LOCATIONS OF WARDOBE PLATFORM AROUND MOUNT HOLES IAW SRM. REPLACED WARDROBE PLATFORMFeb 4, 2019 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019030545607Skin · dentedDENT ON THE UNDERSIDE OF THE RT HORIZONTAL STAB LEADING EDGE APPROX 36" FROM VERTICAL STAB. (C-CHECK) HAND-DRESSED DENT IN RT HORIZONTAL STAB L/E BACK TO ORIGINAL CONTOUR (WITHIN AERODYNAMIC LIMITS) REF REO 601R-51-00-309 REV (A) 2017-08-23 AND 601R-55-12-645 Jan 28, 2019 · N496CA · Cndair CL6002B19 · Horizontal Stabilizer, Plate/SkinSDR SWIA2019030545606Skin · dentedDENTS ON THE RT INBOARD FLAP LOWER SURFACE. (C-CHECK) RO: 03/04/2019 REPAIRED DENTS TO RT INBD FLAP LOWER SURFACE IAW REO.Jan 28, 2019 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2017120544005Unknown · odorSMELL/FUME IN COCKPIT. (FLT 4664) CLOSED PERFORMED OPS CHECK OF PACK SYS IAW AMM. RAN BOTH ENGINES AT HIGH POWER AND BOTH PACKS WITH NO SMELLS NOTED.Nov 24, 2017 · N496CA · Cndair CL6002B19 · Air Distribution SystemSDR SWIA2017091143747Strut · underservicedAFTER TAKE OFF GEAR DISAGREE WARNING MESSAGE. NO EMERGENCY DECLARED. SERVICED THE NLG IAW AMM. PERFORMED GEAR SWINGS, OPS & LEAK CHECKED GOOD.Sep 11, 2017 · N496CA · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR SWIA201743023Vane · chafedRIGHT INBD FLAP MOST INBOARD VANE CAP CHAFED. REMOVED AND REPLACED THE INBD FLAP INBD VANE CAP IAW SRM.Jan 20, 2017 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743022Door Sill · corrodedFLOOR SUPPORT VERTICAL ANGLE AT PAX DOOR SILL BS 310 - 349 HAS EVIDENCE OF CORROSION AROUND NUT PLATE LOCATIONS FOR THE FOLDING STEP ATTACHMENT. INSTALLED A NEW PAX DOOR SILL VERTICAL ANGLE FROM FS310-FS349. PERFORMED OPS CHECKS, OPS CHECKS GOOD. PERFORMED BJan 19, 2017 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541328Pump · failedON CLIMBOUT, LT ENGINE OIL TEMP KEPT INCREASING AND WOULD NOT STABILIZE. REDUCED POWER AND RETURNED TO FIELD. R & R LT ENGINE SCAVENGER PUMP, LT ENG OIL TEMP BULB AND BYPASS CHECK VALVE IAW AMM.Jun 19, 2015 · N496CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA201541153Proximity Switch · failedCREW LOST CABIN PRESSURE AT 12,000 FEET AND RETURNED TO THE FIELD. R & R PAX DOOR D116 PROXIMITY SWITCH. OPS CHECKED GOOD.May 10, 2015 · N496CA · Cndair CL6002B19 · Door Warning SystemSDR SWIA201540628Nut · undertorquedTHERE IS AN AILERON CLICK WHEN MOVING THE CAPTAIN`S YOKE THROUGH FULL RANGE OF TRAVEL, TORQUED PILOT CONTROL COLUMN FORWARD NUT IAW REO.Jan 20, 2015 · N496CA · Cndair CL6002B19 · Control Column SectionSDR SWIA201540627Tube · tornSERVICE DOOR TUBING TORN, PERFORMED REPAIR TO SERVICE DOOR TUBING, IAW REO. OPS TEST GOOD.Jan 19, 2015 · N496CA · Cndair CL6002B19 · Service DoorsSDR SWIA201540626Stringer · corrodedSTRINGER 26L CORRODED BEYOND ALLOWABLE LIMITS AT BS 603. INSTALLED REPAIR DOUBLER IAW EA.Jan 14, 2015 · N496CA · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA201540614Frame · corrodedCORROSION ON FUSELAGE FRAME BS 605, BETWEEN STRINGERS 25L TO 25R. INSTALLED A NEW FRAME SECTION IAW SRM. MAJOR REPAIR.Jan 6, 2015 · N496CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201540613Floor Support · corrodedAFT CARGO BAY AT BS 605, LBL 27 FLOOR SUPPORT HAS CORROSION AT NUT PLATE LOCATIONS. R & R THE FLOOR SUPPORT CAP IAW REO & SRM.Jan 5, 2015 · N496CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201540612Hinge · chafedCHAFE ON SERVICE DOOR INNER HANDLE. PERFORMED BLENDOUT ON DAMAGE AREA ON SERVICE DOOR INNER DOOR HANDLE AT 2 SPOTS, SPOT A, REPORTED DEPTH IS 0.025", AFTER BLENDOUT REMAINING DEPTH IS 0.025", NO MATERIAL LOSS IN DEPTH. SPOT B, REPORTED DEPTH IS 0.015", AFTEJan 5, 2015 · N496CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201540611Hinge · chafedCHAFE ON SERVICE DOOR MAIN DOOR HINGE. PERFORMED A DETAIL VISUAL INSPECTION OF THE SERVICE DOOR MAIN DOOR HINGE AND THE SURROUNDING AREAS AND FOUND NO LOOSE, MISSING, OR DAMAGE FASTENERS. CHECKED DOOR AND FOUND THAT CHAFING WAS CAUSE BY EXCESS FORCE WHEN OPEJan 5, 2015 · N496CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201540610Hinge · gougedPASSENGER DOOR HINGE LUGS CHAFED AND GOUGED. BLENDED DAMAGED ON PAX DOOR HINGE LUGS AND WITHIN LIMITS IAW REO.Jan 5, 2015 · N496CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201540609Vent · dentedPASSENGER DOOR VENT FLAP DENTED ABOVE UPPER RIB, VISIBLE FROM EXTERIOR, MARKED, C-CHECK. EVALUATED DENT ON PAX DOOR VENT FLAP DOOR CAUSED BY BREAKER CABLE RUBBING INNER SURFACE. A DENT IS ACCEPTABLE IN THIS AREA. THE DENT HAS NO SHARP CREASES AND IS WITHIN LJan 5, 2015 · N496CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201540608Rib · chafedPASSENGER DOOR VENT FLAP CHAFED FROM CABLE ON UPPER RIB. HAND BLENDED CHAFE ON PAX DOOR VENT FLAP DOOR INNER RIB AND FOUND TO BE WITH-IN LIMITS IAW REO. ORIGINAL THICKNESS OF RIB STIFFENER IS .625? REMAINING AFTER BLEND IS .534?, LOSS OF .080?.Jan 5, 2015 · N496CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201540607Lever · chafedPASSENGER DOOR FWD PULL-IN LEVER CHAFED. HAND SANDED OUT SMALL CHAFE MARK ON PAX DOOR FWD PULL-IN LEVER AND REPAIR IS WITHIN LIMITS IAW REO. ORIGINAL THICKNESS AT THE CROSS SECTION OF THE PAX DOOR FWD PULL-IN LEVER IS 1.080", REMAINING THICKNESS AFTER BLEND OJan 5, 2015 · N496CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201540625Skin · chafedLEFT INBD FLAP VANE L/E IS CHAFED, OTBD SIDE. BLENDED OUT DAMAGE ON LT INBD FLAP L/E ON OTBD SIDE AND FOUND TO WITH IN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540624Skin · chafedLEFT INBD FLAP VANE L/E IS CHAFED, CENTER, BLENDED OUT DAMAGE ON LT INBD FLAP L/E ON CENTER SIDE AND FOUND TO WITH IN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540623Skin · chafedLEFT INBD FLAP VANE L/E IS CHAFED, INBD SIDE. BLENDED OUT DAMAGE ON LT INBD FLAP L/E ON INBD SIDE AND FOUND TO WITH IN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540622Skin · chafedRIGHT INBD FLAP VANE L/E IS CHAFED, OTBD SIDE. BLENDED OUT DAMAGE ON RT OTBD FLAP L/E ON CENTER SIDE AND FOUND TO WITH IN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540621Skin · chafedRIGHT INBD FLAP VANE L/E IS CHAFED, CENTER OF VANE. BLENDED OUT DAMAGE ON RT INBD FLAP L/E ON CENTER SIDE AND FOUND TO WITH IN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540620Skin · chafedRT INBD FLAP VANE L/E IS CHAFED, INBD SIDE. BLENDED OUT DAMAGE ON RT INBD FLAP L/E ON INBD SIDE AND FOUND TO WITHIN LIMITS IAW REO.Jan 4, 2015 · N496CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201540606Hinge · gougedLEFT NLG DOOR AFT HINGE FITTING IN WHEEL WELL GOUGED FROM F/O. MARKED, C-CHECK BLENDED GOUGE ON THE NLG DOOR AFT HINGE FITTING IAW STS EA. WITHIN LIMITS. OP CHECKS GOOD. ORIGINAL MATERIAL: .650", MATERIAL REMOVED: 025", REMAINING MATERIAL: .625".Jan 4, 2015 · N496CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA201540619Skin · damagedLEFT WING L/E INNER SHROUD DEBONDED, DISFIGURED, WARPED AND WAVY, AND A BROKEN RIVET AT OTBD AREA, LOWER FLANGE, REPAIRED L/E PANEL 530KL, REF REO.Jan 3, 2015 · N496CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201540617Nut · undertorquedCO-PILOTS CONTROL YOKE HAS A CLICKING NOISE, FELT AT FULL TRAVEL BOTH DIRECTIONS. TORQUED CONTROL WHEEL-SHAFT INTERFACE NUT IAW REO. OPS CHECKED GOOD. NO CLICKING HEARD AT THIS TIME.Jan 2, 2015 · N496CA · Cndair CL6002B19 · Control Column SectionSDR SWIA201438706Light · inoperativeBOARDING AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED FLOODLIGHT ASSY IAW AMM.Jul 11, 2014 · N496CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201436591Light · inoperativeNR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 2951 RELAMPED.Mar 3, 2014 · N496CA · Cndair CL6002B19 · Emergency Lighting
Back to N496CA