N676CA

Service difficulty reports · 269

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 = 'N676CA' 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 REXA2026050400422Buttstrap · corrodedCORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN. CORROSION ON JOIN APPROX BS 280 BTW RBL25-LBL25 AT PASSENGER CABIN WAS REPAIRED PER REO 690-53-21-2118 REV. - -Apr 11, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080501493Fitting · corrodedCORROSION ON FITTING PN: CDSP2019-7C-760 IN FRONT ACCESS 107 (1EA) AND FITTING PN: CDSP2019-7C-620 AFT IN ACCESS 108 (1EA) ON GALLEY SUMMARY OF NRC 290:FITTING (1 EA) AND DOUBLER (1 EA) IN FRONT ACCESS 107 AND FITTING (1 EA) AFT IN ACCESS 108 (1 EA) ON GALLEY Mar 13, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080501492Fitting · corrodedCORROSION ON FITTING IN FRONT ACCESS 107 (1EA) AND FITTING PN: CDSP2019-7C-620 AFT IN ACCESS 108 (1EA) ON GALLEY FITTING (1 EA) AND DOUBLER (1 EA) IN FRONT ACCESS 107 AND FITTING (1 EA) AFT IN ACCESS 108 (1 EA) ON GALLEY WERE REPLACED IAW CMM 25-33-67.Mar 13, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026080501496Hinge Fitting · corrodedAFTER BUSHING AND BEARINGS REMOVAL FOUND CORROSION IN LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON LUG L2 & L5 AT CENTER HINGE FITTING OF FRONT SPAR IN LT AILERON WERE REPAIRED PER REO 670-57-61-107 REV. -B.Mar 12, 2026 · N676CA · Cndair CL6002D24 · AileronsSDR REXA2026080501491Hinge Fitting · corrodedCORROSION IN LUG R2 & R5 AT CENTER HINGE FITTING OF FRONT SPAR IN RH AILERON CORROSION AT CENTER FITTING IN LUGS R2 & R5 WERE REMOVED PER REO 670-57-61-107 REV.-B, REO 690-57-61-504 REV-- AND CRJ 900 SRM 51-26-00-001-001-A01 CLEANING, DEFERRAL NUMBERS WO W907Mar 12, 2026 · N676CA · Cndair CL6002D24 · AileronsSDR REXA2026080501499Transcowl · crackedAFTER REMOVAL OF Z STIFFENER ON LH ENGINE UPPER / LOWER TRANSCOWL, CRACKS WERE FOUND ON ACCOUSTIC PANEL PERFORATED SKIN ACUSTIC PANEL OF TRANSCOWL UPPER LH WAS REPAIRED PER EA CRJ954-21830 REV.IR ACUSTIC PANEL OF TRANSCOWL LOWER LH WAS REPAIRED PER EA CRJ954-2Mar 11, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026080501498Transcowl · crackedAFTER REMOVAL OF Z STIFFENER ON LT ENGINE UPPER / LOWER TRANSCOWL, CRACKS WERE FOUND ON ACCOUSTIC PANEL PERFORATED SKIN ACUSTIC PANEL OF TRANSCOWL UPPER LT WAS REPAIRED PER EA CRJ954-21830 REV.IR ACUSTIC PANEL OF TRANSCOWL LOWER LT WAS REPAIRED PER EA CRJ954-2Mar 11, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026050400421Stringer · corrodedCORROSION ON STRINGER 18R AND STRINGER 19R BTW STA=453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW STA= 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPHMar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026050400419Stringer · corrodedCORROSION ON STRINGER 19R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400418Stringer · corrodedCORROSION ON STRINGER 18R BTW BS 453-437 AT PASSENGER CABIN. STRINGER 18R AND STRINGER 19R BTW BS 349 TO 469 AT PASSENGER CABIN WERE REPLACED PER SRM 51-42-06-001-001-A01 PARAGRAPH 6.C. AND CRJ-900 SRM 51-42-20-001-001-A01 PARAGRAPH 6.C.Mar 10, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026050400443Fitting · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026050400442Doubler · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400441Fitting · corrodedWEAR AND CORROSION ON FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL 38(1EA) RBL17(1EA), FS310 LBL20(1EA) AND DAMAGE ANCHORD NUT ON FLOOR FITTING BTW 349 TO FS364 RBL36 (1EA). FLOOR FITTINGS AT FLOOR SUPPORT STRUCTURE BTW FS280 TO FS295 LBL Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026050400440Bracket · corrodedINITIAL INSPECTION: CORROSSION AND WEAR ON SENTLEMENT AREA OF WHEEL BIN LH (3 LOCATIONS) AND RH (5 LOCATIONS). NEW WHEEL BEAM STABILIZER P/N: CC670-39221-4 WAS FABRICATED PER DWG CC670-39221 REV NC & EA CRJ953-21866 REV IRMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400439Bracket · corrodedINITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LH/RH) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400438Bracket · corrodedINITIAL INSPECTION: CORROSION ON RH/LH MLG HYDRAULIC LINES AND HARNESS SUPPORTS PLATE 04 EA (IN BK, OUB BK, LG EXT, LG RET) ON WHEEL WELL AREA PLATE (BRACKET) (IN BK, OUB BK, LG EXT, LG RET) 2 EAS (LT/RT) ON WHEEL WELL AREA WERE REPLACED PER AMM 20-22-00-910-8Mar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400424Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026050400423Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026050400417Latch · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Accessory Compartment DoorsSDR REXA2026050400416Hinge · corrodedCORROSION ON HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR HINGES (2EAS) OF ACCESS DOOR 196ER AT FAIRING 196DR, ALSO DAMAGE 1 LATCH OF ACCESS DOOR 196ER AT FAIRING 196DR WERE EVALUATED OUT LIMITSMar 8, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026080501497Door Frame · wornWEAR ON LOWER FRAME COVET AT FWD LAVATORY DOOR. NEW TRIM LOWER. (1EA) AT FWD LAVATORY DOOR WAS REPLACED IAW CMM 25-40-76.Mar 7, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050400437Landing · crackedCRACK ON AFT LT DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 211AL)(2 LOCATIONS) AFT LT DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 211AL) WAS FABRICATED PER EA. CRJ953-21839 REV. IR AND REPLACED PER SRM 51-42-10-001-001-A01Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026050400434Drag Angle · crackedCRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-A01Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050400433Drag Angle · crackedCRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-00Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050400430Doubler · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG PUMP AREA) FS193.00 WAS REPAIRED PER SRM 53-11-43-201-001-A01 AND PER SRM 53-11-43-201-001-A01Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400429Bracket · crackedBROKEN WATER SPRAYER BRACKET BTW FS1144.00 TO FS1162.00 AND STGR 9 LH AT AFT EQUIPMENT COMPARTMENT REPLACED PER SRM 51-42-06-001-001-A01.Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026050400428Drag Angle · crackedCRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-AMar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050400427Drag Angle · crackedCRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LT FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED IAW SRM 55-31-00-201-001-Mar 6, 2026 · N676CA · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026050400425Doubler · wornWEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WEAR ON DOUBLER BTW FS913.00 AND STGR 26RH TO STGR 26LH WAS REPAIRED PER REO 670-53-00-290 REV FMar 5, 2026 · N676CA · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR REXA2026080501495Access Panel · corrodedCORROSION ON ACCESS PANEL 832AT, 832CT, 832FT CORROSION ON ACCESS PANEL 832CT WAS REMOVED PER SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER SRM 52-11-04-101-001-A01, ACCESS PANEL 832AT WAS REPLACED IAW SRM 51-41-02-001-001-A01 AND SRM 51-42-06-001-Mar 4, 2026 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026050400415Fairing · crackedCRACKED FAIRING BTW RH ENG. AND PYLON FS 1086 APROX. FAIRING BTW RT ENG. AND PYLON FS 1086 APROX WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.Mar 4, 2026 · N676CA · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2025121801047Rod · inoperativeUNABLE TO OPEN PAX DOOR REPLACED PAX DOOR VENT FLAP ROD ASSYDec 16, 2025 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2025071100718Lamp · inoperativeCEILING EMERGENCY LIGHT AT ROW 10 INOP RELAMPED CEILING EMER LIGHT IAW CRJ 900 AMM 33-51-09 OPS CHECK GOODJul 9, 2025 · N676CA · Cndair CL6002D24 · Emergency LightingSDR REXA2022110200946Lamp · inoperativeEMERGENCY EXIT SIGN LIGHT INOP, CABIN CEILING. R & R LAMP BULB IAW AMM 33-51-07, PN ON/OFF: 6100945Oct 30, 2023 · N676CA · Cndair CL6002D24 · Emergency LightingSDR REXA2022060600973Splice · corrodedPANEL 191AB SPLICE JOINT PLATE CORRODED IN MULTIPLE AREAS WITH A DEPTH OF .016". REMOVE AND REPLACE SPLICE JOINT.Apr 22, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600972Plate · crackedLH ENGINE LOWER TRANSCOWL BIFURCATION PANEL NYLON PLATE BROKEN MANUFACTURED NEW PLATE PER EA# CRJ954-13327.Apr 18, 2022 · N676CA · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2022060600971Stringer · corrodedSTR 26L HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS280-333 WITH UP TO 100% MATERIAL LOSS. REMOVE AND REPLACE STR 26L.Apr 15, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600970Stringer · corrodedSTR 24L CORRODED BETWEEN FS333-364. CORROSION MEASURES 7.0"X1.0"X.040" DEEP. REMOVE AND REPLACE STRINGER.Apr 13, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600969Intercostal · corrodedINTERCOSTAL BETWEEN FS349-364 JUST RIGHT OF STR27 LOWER FLANGE HAS EXFOLIATED CORROSION. REMOVE AND REPLACE INTERCOSTAL.Apr 10, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600968Cover · corrodedPAX DOOR UPPER, FWD AND AFT CORNER COVERS HAVE EXFOLIATED CORROSION. REPLACE CORNER COVERS. AFT P/N 600-31902-287 AND FWD P/N 600-31902-288Apr 8, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060600967Skin · corrodedFEED BAGGAGE DOOR SURROUND STRUCTURE BACKING SKIN CORRODED BETWEEN STR 24L-25L AND FS 517-565. MULTIPLE SPOTS OF CORROSION WITH A MAX DEPTH OF .007". REPAIRED CORROSION PER EA CRJ953-13302.Apr 8, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600966Angle · corrodedSUPPORT ANGLE AT STR 22R BETWEEN FS280-295 HAS MULTIPLE SPOTS OF EXFOLIATED CORROSION. REPLACE SUPPORT ANGLEApr 6, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600965None · corrodedFS280.00 BUTT STRAP HAS AREAS OF CORROSION FROM STR 26R-26L. DIMENSIONS AFTER BLEND AS FOLLOWS. STR26R-27 10.0"X6.0"X.005" MAX DEPTH, STR26L-27 10.0"X6.0"X.005" MAX DEPTH REPAIRED CORROSION PER EA CRJ953-13363Apr 4, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600964Stringer · corrodedSTR 23L HAS MULTIPLE AREAS OF CORROSION BETWEEN FS319-333 WITH UP TO 100% MATERIAL LOSS. REPLACED STR 23L IAW EA CRJ953-13351Apr 1, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060601022None · corrodedAVIONICS BAY DOOR SEAL RETAINER CORRODED. CORROSION MEASURES 10.0"X.200"X100% MATERIAL LOSS. REMOVE AND REPLACE SEAL RETAINER.Apr 1, 2022 · N676CA · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060600963Former · corrodedPAX DOOR AFT FORMER HAS EXFOLIATED CORROSION ON THE INNER SIDE. REPLACE AFT FORMER.Mar 29, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060600962Intercostal · corrodedPAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE WEB. 6TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.Mar 29, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060600961Intercostal · corrodedPAX DOOR INTERCOSTAL HAS EXFOLIATED CORROSION ON THE LOWER FLANGE. 4TH INTERCOSTAL DOWN ON THE AFT SIDE. REPLACE PAX DOOR INTERCOSTAL.Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060600960Intercostal · corrodedPAX DOOR SEVENTH INTERCOSTAL DOWN MIDDLE OF PAX DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060600959Intercostal · corrodedPAX DOOR THIRD INTERCOSTAL DOWN IN MIDDLE OF DOOR HAS EXFOLIATED CORROSION ON THE WEB. REPLACE INTERCOSTAL.Mar 28, 2022 · N676CA · Cndair CL6002D24 · Passenger/Crew Doors
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