N494CA

Service difficulty reports · 209

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 = 'N494CA' 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 SWIA202053346Seat Track · chafedTHE PILOT SEATS INBOARD AND OUTBOARD FLOOR SEAT RAILS ARE CHAFED AND HAVE MISSING FASTENER HEADS. C-CHECK RO 10/13/2020. REMOVED AND INSTALLED BOTH PILOT SEATS INBOARD AND OUTBOARD FLOOR SEAT RAILS WITH NEW PART 601R41082-11, REF REO AND CRJ200 SRM. RESTORESep 6, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202053307Windshield · crackedTHE RT WINDSHIELD SIDE POSTS LOWER AFT FITTING IS CRACKED, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT WINDSHIELD SIDE POST LOWER AFT FITTING, REF CRJ200 SRM DWG.Sep 6, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053306Windshield · crackedTHE LT WINDSHIELD SIDE POSTS LOWER AFT FITTING IS CRACKED, MARKED WITH ORANGE FLAG TAPE. C-CHECK RO 10/13/2020. REMOVED AND REPLACED LT WINDSHIELD SIDE POST LOWER AFT FITTING, REF CRJ200 SRM DWG.Sep 6, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202053345Hinge Arm · chafedRT OUTBOARD FLAP CENTER HINGE ARM, FAIRING GUIDE PLATES ARE CHAFED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED RT OUTBOARD FLAP CENTER HINGE ARM, FAIRING GUIDE PLATES (OUTBOARD AND INBOARD), REF CRJ-200 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS.Sep 4, 2020 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053305Handle · crackedCARGO DOOR HANDLE HOUSING IS CRACKED AT THE AFT EDGE OF THE HANDLE POCKET. C-CHECK RO 10/13/2020. REPLACED CRACKED CARGO DOOR HANDLE HOUSING WITH NEW HOUSING, REF CRJ 200 SRM AND DRAWING.Sep 4, 2020 · N494CA · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202053347Fairing · gougedRT FLAP STUB FAIRING HAS GOUGE ALONG BOTTOM LENGTH OF FAIRING AND FORWARD HINGE HALF HAS BROKEN NUTPLATE. C-CHECK RO 10/13/2020. REPLACED WITH NEW RT FLAP STUB FAIRING ASSEMBLY, REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.Sep 2, 2020 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202053304Skin · chafedRT AILERON ALONG THE TOP UPPER LEADING EDGE, MULTIPLE AREA'S OF CHAFING, FLAGGED. C-CHECK RO 10/13/2020. REMOVED AND REPLACED WITH NEW RT AILERON UPPER LEDING EDGE SKIN, REF CRJ 200 SRM AND BOMBARDIER DRAWING.Sep 1, 2020 · N494CA · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA202053303Hinge · gougedPASSENGER DOOR HINGE LAND 27 IS GOUGED BY THE HINGE PIN. C-CHECK RO 10/13/2020. BLENDED OUT GOUGE FROM ROLL PIN IN HINGE LAND AREA, REF REO. FOUND TO BE OUT OF LIMITS, REF DWG. REPLACED FUSELAGE SIDE HALF HINGE, REF CRJ-200 SRM AND DWG. SEE CONTINUATION Aug 31, 2020 · N494CA · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA202053302Skin · dentedADM N494CA-6376 SKIN DEVIATION, RIGHT SIDE, AFT OF RADOME BETWEEN STRINGERS 15-16 AT STA 173. EVALUATION AND REPAIR AS REQUIRED. C-CHECK RO 10/13/2020. DENT NR 1 ON RT SKIN AT APPROXIMATELY FS 170.5 AND WL 86.5 MEASURES .70" WIDTH BY 2.0" LENGTH AND .010" DAug 28, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202053301Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYINJul 14, 2020 · N494CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019073046103Switch · inoperativeCAPTAIN SIDE PITCH TRIM SWITCH INOPERATIVE AFTER TAKEOFF. FLT 3888. REMOVED AND REPLACED THE CAPTAIN PITCH TRIM SWITCH IAW AMM. PERFORMED OPERATIONAL CHECK OF THE HORIZONTAL STABILIZER TRIM SYSTEM. OPS CHECKED GOOD AT THIS TIME.Jul 30, 2019 · N494CA · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA2019071246038Uplock Roller · defectiveGEAR DISAGREE WARNING. RAN QRH PROCEDURE. THE GEAR ALL CAME DOWN. LANDED WITHOUT INCIDENT. (FLT#3689) FO: 07/10/2019 CLOSED REMOVED AND REPLACED LH MLG UPLOCK ROLLER IAW CMM. OPS CHECK GOOD.Jul 10, 2019 · N494CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2019051545892Actuator · malfunctionedGEAR DISAGREE WARNING ON LEFT MAIN LANDING GEAR. RAN QRH AFTER CYCLING GEAR 1 TIME GEAR SHOWED DOWN 3 GREEN. LANDING AND TAXI IN NORMAL. (FLT#4799) FO: 05/15/2019 CLOSED REMOVED AND REPLACED LT MLG SIDE STAY ACTUATOR IAW AMM. OPS CHECK GOOD AT THIS TIME. NO LEMay 14, 2019 · N494CA · Cndair CL6002B19 · Landing Gear ActuatorSDR SWIA2018061844792Shroud · gougedRIGHT AILERON. LOWER LEADING EDGE SHROUD GOUGED. REPLACED THE SHROUDS IAW SRM.May 27, 2018 · N494CA · Cndair CL6002B19 · AileronsSDR SWIA2018061844791Shroud · gougedLEFT AILERON LOWER LEADING EDGE SHROUD WAS GOUGED. REMOVED AND REPLACED THE SHROUD IAW SRM.May 27, 2018 · N494CA · Cndair CL6002B19 · AileronsSDR SWIA2018061844790Bulkhead Web · crackedBS 621 BULKHEAD WEB HAD TWO CRACKS, BL 0 AND TWO CRACKS AT RBL 18. INSTALLED A REPAIR IAW REO.May 26, 2018 · N494CA · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2018061844789Structure · damagedCARGO DOOR INTERIOR SURROUND STRUCTURE LOWER COAMING HAD DAMAGE. REMOVED AND REPLACED COAMING IAW SRM. ALL CHECKD GOOD.May 23, 2018 · N494CA · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2018061844788Vane · chafedRIGHT, INBD FLAP LEADING EDGE VANE HAD THREE CHAFES ON THE LEADING EDGE. INSTALLED A NEW FLAP VANE IAW SRM.May 23, 2018 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018061844787Skin · dentedLEFT WING LEADING EDGE PNL 530JL HAS DENT LOWER SIDE MIDDLE. REPAIRED IAW REO AND SRM.May 23, 2018 · N494CA · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201844786Hinge · corrodedLAVATORY SERVICING DOOR HINGE HAD CORROSION. REMOVED AND REPLACED THE HINGES IAW SRM.May 23, 2018 · N494CA · Cndair CL6002B19 · Fluid Service DoorsSDR SWIA2018061844785Skin · dentedDENT LOCATED AFT OF THE PAX DOOR AND APPROXIMATELY 3 FEET BELOW. REPAIRED BETWEEN BS 333 TO 379, STRINGER 21L TO 24L IAW REO. ALL CHECKED GOOD.May 22, 2018 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018061844784Skin · damagedTWO SCRATCHES AND ONE DENT BELOW CARGO DOOR. PERFORMED A REPAIR IAW REO.May 22, 2018 · N494CA · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201642280Cap · chafedRIGHT INBD FLAP, MID VANE CAP IS CHAFED. R & R DISCREPANT RT INBD FLAP VANE CAP, PN 601R14303-52 IAW SRM.Jun 6, 2016 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642279Cap · chafedLEFT INBD FLAP, MID VANE CAP CHAFED. R & R DISCREPANT LT INBD FLAP VANE CAP, PN 601R14303-51 IAW SRM.Jun 6, 2016 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642281Frame · corrodedFRAME AFT FACE CORRODED FS 333.00, STR 26L TO STR 26R. R & R FRAME AT FS333.0 AT PRODUCTION SPLICES 24L TO 24R IAW SRM. PRESSURIZATION CHECKED GOOD.Jun 5, 2016 · N494CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201642272Frame · corrodedFRAME FORWARD FACE CORRODED FS 349.00, STR 26L TO STR 26R. REMOVED AND INSTALLED NEW SERVICEABLE FRAME, PN 601R32005-69 AT FS 349.00 BETWEEN STR 23L AND STR 23R IAW SRM.Jun 5, 2016 · N494CA · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201642277Cap · chafedLEFT INBD FLAP, INBD VANE CAP IS CHAFED. R & R LT INBD FLAP, INBD VANE CAP IAW SRM.Jun 4, 2016 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642271Intercostal · crackedRT SIDE FUSELAGE, FS 484.0 OUTSIDE INTERCOSTAL ANGLE HAS CRACK AT HI-LIGHT LOCATION. REPAIRED DAMAGE TO RT SIDE FS 484.00 OUTSIDE INTERCOSTAL IAW STS EA.Jun 3, 2016 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642274Panel · chafedPANEL 599AB IS CHAFED. REPLACED PANEL 599AB WITH NEW PN CC670-13055-1 IAW SRM.Jun 2, 2016 · N494CA · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA201642273Panel · chafedPANEL 599BB IS CHAFED. REPLACED PANEL 599BB WITH NEW PN CC670-13056-3 IAW SRM.Jun 2, 2016 · N494CA · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA201438614Actuator · malfunctionedLEFT MAIN GEAR DISAGREE AFTER LONG PAUSE ON GEAR EXTENSION. ONE RECYCLE IAW QRH RECEIVED DOWN AND LOCKED INDICATION NORMALLY. R & R THE LT MLG SIDE STAY ACTUATOR, THE UPLOCK ASSY FOR THE LT MLG IAW AMM. SWUNG THE GEAR SEVERAL TIMES AND A FREE FALL CHECK AS WJul 7, 2014 · N494CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201438537Selector Valve · failedLEFT MAIN GEAR DID NOT COME DOWN. SECOND ATTEMPT IT CAME DOWN NORMALLY. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM.Jul 6, 2014 · N494CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201438509Bulb · inoperativeOVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB.Jun 30, 2014 · N494CA · Cndair CL6002B19 · Emergency LightingSDR SWIA201438528Light · inoperativeNR 6 EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R LIGHT IAW AMM.Jun 29, 2014 · N494CA · Cndair CL6002B19 · Emergency LightingSDR SWIA2014061738203Valve · faultyBRAKES REQUIRED EXCESSIVE, UNEVEN PRESSURE TO ENGAGE. FELT LIKE FOOT CONTROLS ARE BINDING. R & R UPPER AND LOWER BRAKE CONTROL VALVES IAW AMM.Jun 13, 2014 · N494CA · Cndair CL6002B19 · Landing Gear Brake SystemSDR SWIA201437874Floor Support · corrodedFLOOR SUPPORT CORRODED AT BS 349, RBL 40. C-CHECK, FOUND OUT OF LIMITS REF SRM. REPLACED WITH NEW FLOOR SUPPORT.May 22, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437875Floor Support · crackedFLOOR SUPPORT CRACKED. C-CHECK, INSTALLED NEW FLOOR SUPPORT IAW SRM.May 21, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437879Web · crackedTRU BAY WEB LT SIDE AT BS 193, LBL 29 IS CRACKED. C-CHECK, REPAIRED.May 15, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437878Floorbeam · crackedCOCKPIT FLOORBEAM CRACKED AT LBL 11 & RBL 11. C-CHECK, REPLACED COCKPIT FLOORBEAM IAW SRM.May 15, 2014 · N494CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201437877Floorbeam · crackedFS 280, FLOORBEAM ATTACH ANGLE AT LBL 9 AND RBL 9 INBD AND OTBD POSITIONS CRACKED. C-CHECK, REPLACED FLOORBEAM ANGLE IAW SRM.May 15, 2014 · N494CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201437876Web · crackedTRU BAY WEB LT SIDE AT BS 193, LBL 29 IS CRACKED. C-CHECK, REPAIRED REF EA, AND AMM.May 15, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437881Floorbeam · crackedFS 280, RBL 9 UPPER FLOORBEAM CRACKED. C-CHECK, CUT AND REMOVED CRACKED SECTION UPPER FLOORBEAM, NDT, NO DEFECTS FOUND AT CUT LINE, FABRICATED REPLACEMENT SECTION, DRILLED AND LOCATED REPAIR PARTS. INSTALLED REPAIR PARTS IAW REO.May 14, 2014 · N494CA · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201437880Carriage · chafedLEFT WING INBD FLAP, OTBD LAP VANE ACTUATOR CARRIAGE HAS CHAFE/ RUB DAMAGE ON OTBD TRACK AND 2 EA WEAR SPOTS ON INNER TRACK RACES AS MARKED, C-CHECK. CHAFED AREAS OF LT INBD VANE CRADLE FOUND WITHIN LIMITS AND REPAIRED REF REO.May 14, 2014 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437888Skin · chafedLEFT INBD FLAP CHAFED INBD SIDE AT L/E. C-CHECK, REPLACED LT INBD FLAP RIBLET, REF SRM.May 13, 2014 · N494CA · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201437887Structure · corrodedCORROSION AT AFT LOWER CORNER OF SERVICE DOOR SURROUND AT BS 349 ON FLOOR SUPPORT EDGE. C-CHECK REPAIRED IAW EA.May 13, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437886Structure · corrodedPAX DOOR SURROUND STRUCTURE LOWER AFT CORNER BS 349 HAS CORROSION ON EDGE OF FLOOR SUPPORT. C-CHECK, REPAIRED PAX DOOR SURROUND LOWER AFT CORNER REF STS EA.May 13, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437885Threshold · corrodedPAX DOOR LOWER THRESHOLD HAS CORROSION BETWEEN BS 310 - 349. C-CHECK, REPLACED PAX DOOR THRESHOLD IAW SRM.May 13, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201437884Step · corrodedPAX DOOR BOTTOM FOLDING STEP HAS CORROSION BELOW ANTI-SLIP STRIP. C-CHECK, REPLACED THE PAX DOOR BOTTOM FOLDING STEP WITH NEW PAX DOOR BOTTOM FOLDING STEP.May 13, 2014 · N494CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201437883Vent · chafedPAX DOOR VENT HAS INTERNAL CHAFING. C-CHECK, COMPLIED WITH REO BLENDED OUT DAMAGED AREA ON PAX DOOR VENT DOOR.May 13, 2014 · N494CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201437882Floor Support · corrodedCORROSION ON AFT FLOOR SUPPORT BS 621. C-CHECK, REPAIRED FLOOR SUPPORT.May 13, 2014 · N494CA · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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