N605LR

Service difficulty reports · 115

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 = 'N605LR' 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 REXA2026052800854Web · crackedINITIAL INSPECTION': CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. WAS REPAIRED PER CRJ-900Nov 11, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800862Intercostal · corrodedCORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 DUE TO EXCESIVE CORROSION ON INTERCOSTAL AT STGR 20RH BTW FS333.00 TO FS 349.00 WAS REPLACED PER CRJ900 SRM 53-21-23-101-002-A02, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01Oct 30, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052800855Stringer · corrodedCORROSION ON STRINGER 26RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) CORROSION ON STRINGER 26RH IN STA. FS= 295 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRSep 24, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800848Intercostal · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTAL AT STGR 20LH BTW FS333.00 TO FS 349.00 INTERCOSTAL AT STGR 20LH BTW FS333.00 TO FS 349.00 WAS EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER CRJ900 SRM 51-21-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42Sep 23, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800850Rub Strip · wornOUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB STSep 21, 2025 · N605LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2026052800849Rub Strip · wornOUT OF SCOPE': WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE/LH ENGINE WEAR ON RUB STRIPS OF LOWER AND UPPER FORWARD CORE COWL AT RH ENGINE AND UPPER FORWARD CORE COWL LH ENGINE WERE REPLACED PER CRJ-900 SRM 54-23-00-201-006-A01, RUB STRSep 21, 2025 · N605LR · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR REXA2026052800863Stringer · corrodedIN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052800861Hinge · corrodedCORROSION ON BOTH HINGES OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (2 EAS) SUMMARY: BOTH HINGES OF AFT LAVATORY WASTE SERVICE ACCESS PANEL 196ER (2 EAS) WERE REMOVED PER CRJ900 AMM 52-45-01 AND INSTALLED PER CRJ900 AMM 52-45-01 AND FABRICATED HINGE OF Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026052800860Frame · corrodedCORROSION ON FRAME FS 847.00+32 BTWN STGR 25LH TO 25RH CORROSION ON FRAME FS 847.00+32 BTWN STGR 25LH TO 25RH WAS REPAIRED PER REO 690-53-51-526 REV --Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052800859Stringer · corrodedIN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2026052800858Stringer · corrodedIN REFERENCE TO NRC 00604: CORROSION ON STRINGER 19RH, 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT. (E/E) SUMMARY OF NRC 677 CORROSION ON STRINGER 20RH AND 21RH IN STA. FS= 437 TO FS= 453 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED OSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800857Hinge · crackedCRACKED FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT REPLACED IAW SRM 51-42-06-001-001-A01 (FWD & AFT HINGES) WERE MANUFACTURED PER EA NO. CRJ953-20605 REV IR Sep 19, 2025 · N605LR · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026052800856Hinge · crackedCRACKED FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT FWD / MID & AFT HINGES OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 (FWD & AFT HINGES) WERE MANUFACTURED PER EA NO. CRJ953-20605Sep 19, 2025 · N605LR · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2026052800853Bracket · corrodedCORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. WAS REMOVED PER CRJ900 SRSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800852Fitting · corrodedINITIAL INSPECTION: CORROSION ON CLOSING FITTINGS (2EAS) BTW FS 314.00 AND FS 342.00 AND STGR 18L. CORROSION ON CLOSING FITTINGS (2EAS) BTW FS 314.00 AND FS 342.00 AND STGR 18L WERE REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, CLOSING FITTINGS FWD WAS EVALUATSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800851Frame · corrodedINITIAL INSPECTION: CORROSION ON FRAME FS= 310.00 BETWEEN STRG 24LH TO 24RH AT MAIN AVIONIC COMPARTMENT DUE TO EXCESIVE CORROSION ON FRAME IN STA. FS= 310 BETWEEN STRG 25RH TO STRG 24LH AT MAIN AVIONIC COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-21-06-101-0Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2026052800845Drag Angle · crackedINITIAL INSPECTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026052800844Angle · corrodedCORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. CORROSION ON WEB FLOOR PROTECTOR THEIR ANGLES (8 EAS) AT SERVICE DOOR SURROUND STRUCTURE BTW FS 319.70 TO FS 349.00. WAS REMOVED PER CRJ900 SRSep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800843Angle · corrodedCORROSION ON FWD, MID AND AFT ANGLE CAP (3 EAS) AT PASSENGER DOOR SURROUND STRUCTURE BTW FS 310.00 TO FS 349.00 OVER STGR 18L. DUE TO EXCESSIVE CORROSION ON MID AND AFT ANGLE CAP WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 51-21-06-001-00Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800842Angle · corrodedCORROSION ON FWD, MID AND AFT ANGLE CAP (3 EAS) AT PASSENGER DOOR SURROUND STRUCTURE BTW FS 310.00 TO FS 349.00 OVER STGR 18L. DUE TO EXCESSIVE CORROSION ON MID AND AFT ANGLE CAP WERE EVALUATED OUT LIMITS THEREFORE WERE REPLACED PER CRJ-900 SRM 51-21-06-001-00Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800840Drag Angle · crackedINITIAL INSPECTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL 0.00) CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67Sep 19, 2025 · N605LR · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026052800841Bracket · corrodedINITIAL INSPECTION: CORROSION ON BRACKET OF THE AFT LAV WASTE LEVEL INDICATOR LIGHT (PRESS-TO-TEST INDICATOR). CORROSION ON BRACKET OF THE AFT LAV WASTE LEVEL INDICATOR LIGHT (PRESS-TO-TEST INDICATOR) WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01, EVALUATESep 16, 2025 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026052800846Door Frame · crackedCRACK ON UPPER FRAME AT AFT RH/LH & FWD RH OVERWING EMERGENCY EXIT DOOR. UPPER FRAME AT AFT RH/LH & FWD RH OVERWING EMERGENCY EXIT DOOR WERE REPAIRED PER REO 670-52-21-103 REV. - -Sep 12, 2025 · N605LR · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2024090600686Battery Pack · inoperativeCENTER CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CENTER CEILING EMERGENCY LIGHT BATTERY PACK AND CHARGER IAW AMM 33-51-17. OPS CHECK GOOD. (PS 36). BATTERY PACK P/N: 2013-1ASMISep 3, 2024 · N605LR · Cndair CL6002D24 · Emergency LightingSDR REXA2022120202667Floor Support · corrodedR/H FLOOR SILL IS CORRODED BETWEEN F.S. 280 TO F.S. 333. REMOVED AND REPLACED RH FLOOR SILL PN:SH670-32172-11 IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.Nov 30, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022120202666Support Angle · corrodedGALLEY DOOR STEP PLATE AFT TWO SUPPORT ANGLES ARE CORRODED. REMOVED AND REPLACED THE TWO SUPPORT ANGLES IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.Nov 30, 2022 · N605LR · Cndair CL6002D24 · Galley DoorsSDR REXA2022113002633Angle · corrodedPASSENGER DOOR AFT DOOR ANGLE IS CRACKED MIDDLE POINT OF DOOR. COMPLIED WITH SRM 52-11-01-201-002-A01.Nov 28, 2022 · N605LR · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022113002604Door Sill · corrodedGALLEY DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED CORRODED LOWER SILL ANGLE WITH NEW IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Nov 28, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022113002605Angle · corrodedPAX DOOR UPPER SILL ANGLE IS CORRODED. REMOVED UPPER SILL (KICK PLATE) AT PAX DOOR IAW CRJ-900 SRM 51-41-02-001-001-A01. INSTALLED NEW PAX DOOR UPPER SILL ANGLE IAW SRM 51-42-06-001-001-A01Nov 27, 2022 · N605LR · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022052601036Light · missingFOUND FLOOR LIGHTING MISSING AT 13 D/C INSTALLED FLOOR LIGHTING IAW CMM 33-51-07May 22, 2022 · N605LR · Cndair CL6002D24 · Emergency LightingSDR REXA2020103000733Trunnion · damagedLT MLG TRUNNION HAS TOOLING GOUGES ON INNER SURFACE BETWEEN HOLES 5 AND 11. SIX DISCREPANT AREAS, LARGEST APPROXIMATELY .250L Z .010D. C/W MHIRJ REO 690-57-21-3672, REV- DATED 10/22/20.Oct 25, 2020 · N605LR · Cndair CL6002D24 · Wing, Landing Gear Attach FittingsSDR REXA2019021000150Seat Track · corrodedCORROSION ON SIDE SEAT RAILS IN SECTIONS [FS=785 TO FS= 847+16, STR 15L] [FS=847+16 TO FS=913, STR 15L] AT PAX CABIN. SEAT RAILS WERE REPLACED PER AMM 53-00-49.Feb 10, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019020500145Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 25L AND 25R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. CORROSION ON STRINGER SPLICE WAS REMOVED PER SRM 51-21-06-001-001-A01 ITEM 5. REWORKED AREA ON STRINGER SPLICE 25L WAS MEASURE AND ORIGINAL THICFeb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019020500143Stringer · corrodedCORROSION ON STRINGER 26L AND 26R IN STA FS= 295 TO FS= 327 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. STRINGER REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019020500142Stringer · corrodedCORROSION ON STRINGER 26L AND 26R IN STA FS= 339 TO FS= 364 AT MAIN AVIONIC COMPARTMENT. CORROSION LEVEL 2. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 ITEM 5. STRINGER 26R WAS MEASURE ORIGINAL THICKNESS IS 0.050" AND MAXIMUM DEPTH REMOVED IS 0.012" THFeb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019020500141Stringer · corrodedCORROSION ON STRINGER 24R IN STA FS= 295 TO FS=333 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. STRINGER WAS REPLACED PER SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.Feb 5, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019013000146Stringer Splice · corrodedCORROSION ON STRINGER SPLICE 26L AND 26R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2. CORROSION ON STRINGER SPLICE WAS REMOVED PER SRM 51-21-06-001-001-A01 PAR 5D, REWORKED AREAS ON STRINGER SPLICE, MEASURE AND MAXIMUM DEPTH REMOVJan 30, 2019 · N605LR · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR REXA2019012700149Seat Track · corrodedFLOOR SEAT RAILS IN SECTIONS [FS= 485 TO FS= 581, 9RBL] [FS=581 TO FS=661+32, 9RBL] [FS=661+32 TO FS=693, 9 RBL] [FS=693 TO FS=830, 9LBL/9RBL] AT PAX CABIN. FLOOR SEAT RAILS WERE REPLACED PER AMM 53-00-49.Jan 27, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2019012500148Seat Track · corrodedCORROSION ON SIDE SEAT RAILS IN SECTIONS [FS= 485 TO FS= 572, STR 15L/R] [FS= 572 TO FS= 661+16, STR 15L/R] [FS= 661+16 TO FS= 661+90, STR 15L] AT PAX CABIN. SIDE SEAT RAILS AT PAX CABIN WERE REPLACED FOR A NEW ONES PER AMM 53-00-49.Jan 25, 2019 · N605LR · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2018080300668Light · inoperativeRT OVERWING EXTERIOR EMERGENCY LIGHT (FWD) INOP. R&R RT FWD OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-15. OPS CHECK GOOD.Aug 1, 2018 · N605LR · Cndair CL6002D24 · Emergency LightingSDR REXA2018070600612Knob · missingMEGAPHONE VOLUME KNOB MISSING. REMOVED AND REPLACED MEGAPHONE IAW AMM 25-61-14. PERFORMED OPS TEST. OPS TEST GOOD. A/C OK FOR SVC.Jul 6, 2018 · N605LR · Cndair CL6002D24 · Emergency EquipmentSDR REXA2018052700423Battery · dischargedDURING LINE CHECK FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY ASSY IAW AMM 33-51-17 OPS CHECK GOOD LIGHTS WORK P/N ON 2013-1A S/N ON 119621, P/N OFF AD-2013-1A S/N OFF 105626.May 27, 2018 · N605LR · Cndair CL6002D24 · Emergency LightingSDR REXA2018012100042Light · missingEMERGENCY LIGHT STRIP MISSING, NEXT TO 1A SEAT. REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-51-01.Jan 21, 2018 · N605LR · Cndair CL6002D24 · Emergency LightingSDR REXA2018010300006Seal · brokenEMK KIT SEAL BROKEN. REMOVED AND REPLACED EMK KIT IAW AMM 25-61-04.Jan 3, 2018 · N605LR · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017082000896Seal · missingSEAL MISSING ON FWD FA PBE. INSTALLED A NEW SEAL ON FWD FA PBE.Aug 20, 2017 · N605LR · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017073100844Pbe · unserviceableFLIGHT DECK PBE OTS SOFT TO THE TOUCH HAS LOST VACCUM SEAL. R&R CAPT PBE IAW AMM 35-31-06.Jul 31, 2017 · N605LR · Cndair CL6002D24 · Portable Oxygen SystemSDR REXA2017052600643Flashlight · inoperativeAFT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW CMM 25-60-02, OPS CHECKED GOOD. "May 26, 2017 · N605LR · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017031200405Light · burned outINTERMITTENT FUMES IN FLIGHTDECK ONLY. CAN ONLY DESCRIBE IT AS HOT ELECTRICAL APPLIANCE SMELL, ON FINAL CRUISE INTO DESCENT. COMPLIED WITH FIM 21-21-00. RAN ENGINES AS WELL 21-00-00. NO SMELL REPORTED. ALL INDICATIONS REPORTED NORMAL. A/C OK FOR SVC. CONFIRMEDMar 12, 2017 · N605LR · Cndair CL6002D24 · Flight Compartment LightingSDR REXA2017011700047Flashlight Assy · inoperativeCOPILOT`S FLASHLIGHT INOPERATIVE. R & R THE FLASHLIGHT AND HOLDER IAW AMM 25-61-02. OP CHECKED GOOD IAW AMM 25-61-00.Jan 17, 2017 · N605LR · Cndair CL6002D24 · Emergency EquipmentSDR REXA2017010600010Lamp · inoperativeFORWARD LEFT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-15. OPSCHECKED GOOD.Jan 6, 2017 · N605LR · Cndair CL6002D24 · Emergency Lighting
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