N523AE

Service difficulty reports · 124

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 = 'N523AE' 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 VNAA2026083123801Wire Harness · faultedGEAR DISAGREE WARNING MSG IN FLIGHT. REMOVED & REPLACED LT DRAG BRACE HARNESS ASSY IAW AMM 32-61-05-000/400-804-A01.Aug 27, 2026 · N523AE · Cndair CL6002C10 · Landing Gear System WiringSDR VNAA2026082723601Actuator · faultedGEAR DISAGREE/NLG UNCOMMANDED MOVEMENT/CABIN ALT INCREASED RAPIDLY. PERFORMED A HEALTH STATUS CHECK OF THE PROXIMITY SENSOR IN THE MDC IAW 32-61-00-710-801 HEALTH CHECK GOOD NO DEFECT NOTED. TROUBLESHOOT NLG IAW SDS 32-30-00-001 AND SSM 32-30-00. SUSPECTED LAug 24, 2026 · N523AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR 1Q2R2026081520119Pressure Blkhd · corrodedAT BS 235 PRESSURE BULKHEAD HAS CORROSION NEAR ELECT CONNECTOR J107. PERFORMED PERMANENT REPAIR IAW RFTS-129742, REV. 0, REO 670-53-11-2338, REV--, REO 670-53-11-2339, REV -.Aug 11, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR 1Q2R2026081020192Skin · dentedDURING OK TO INSTALL OF PAX DOOR, DENT WAS FOUND ON AFT SIDE OF PAX DOOR HINGE ON FUSELAGE SIDE. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130175 REV. 0, DATED AUGUST 06, 2026, AND REO 670-53-21-2944, REV-.Aug 6, 2026 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR 1Q2R2026080220138Fitting · gougedHORIZONTAL STAB FITTING HAS GOUGE DAMAGE ON UPPER OUTBOARD LEFT-HAND FITTING AND UPPER INBOARD LEFT-HAND FITTING.Aug 2, 2026 · N523AE · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous StructureSDR 1Q2R2026072950069Rib · crackedDURING NDT INSPECTION, CRACK INDICATION NOTED ON THE L/H SIDE AT WS178.00, FLAP HINGE BOX ATTACHMENT FITTING ON THE I/B FWD HOLE ON THE INTERNAL RIB SIDE. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-129840 REV. 0, DATED JULY 28, 2026, AND MHI RJ REO 670Jul 28, 2026 · N523AE · Cndair CL6002C10 · Wing, Rib/BulkheadSDR 1Q2R2026081620178Skin · chafedEXTERIOR SKIN AT 2 INCHES FWD OF BS 985, STR 27L HAS CHAFE DAMAGE. PERFORMED PERMANENT REPAIR IAW RFTS-129909, REV 0, AND REO 670-53-51-401, REV-.Jul 22, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR 1Q2R2026080950071Skin · dentedDENT DAMAGE TO FUSELAGE SKIN BETWEEN BS 319.70 - 333, S20R-S21R. PERFORMED PERMANENT REPAIR IAW RFTS-129715 REV. 0, AND REO 670-53-21-2933 REV. --,Jul 21, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR 1Q2R2026072920097Stringer · corrodedAT BS 295, STGR 19 LT FOUND TO BE POSSIBLE CORROSION ON BRACKET. PERFORMED PERMANENT REPAIR IAW RFTS-129854 REV. 0, AND REO 670-53-21-2936, REV--.Jul 14, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR 1Q2R2026071920133Hinge Fitting · gougedAFT SIDE OF RUDDER, CENTER SECTION, CENTER HINGE IS GOUGED.Jul 8, 2026 · N523AE · Cndair CL6002C10 · Rudder StructureSDR 1Q2R2026071920132Hinge Fitting · gougedAFT SIDE OF RUDDER, CENTER SECTION, UPPER HINGE IS GOUGED.Jul 8, 2026 · N523AE · Cndair CL6002C10 · Rudder StructureSDR 1Q2R2026072090002Skin · dentedDAMAGE AT FS501, STGR17 R/H FUSELAGE. DENT/GOUGE.Jun 26, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR 1Q2R2026071620115Fitting · damagedLEFT INBD PCU FITTING ELEVATOR SIDE LUG HAS DAMAGE ON LOWER CORNER.Jun 16, 2026 · N523AE · Cndair CL6002C10 · Elevator StructureSDR 1Q2R2026072950088Fitting · gougedLEFT ELEVATOR PCU 2 FITTING GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW REO 670-55-21-113 REV--, AND EA 57-2025-1480, REV C.Jun 15, 2026 · N523AE · Cndair CL6002C10 · Elevator, Spar/RibSDR 1Q2R2026080550084Lock Tab · brokenLEFT AILERON PCU TENSION REGULATOR TO PCU LINK ASSY HAS BOTH LOCK TABS BROKEN OFF. PERFORMED PERMANENT REPAIR WITH REPLACEMENT OF TENSION REGULATOR TO PCU LINK ASSY IAW RFTS-126593, REV. 0, AND EA 2711-2026-0040, REV-.Jan 12, 2026 · N523AE · Cndair CL6002C10 · Aileron Control SystemSDR 1Q2R2026071650087Cap · damagedDURING LIGHTNING STRIKE INSPECTION FOUND MULTIPLE EXITS AT FS893.00 AND FS953.00, ALSO FOUND DAMAGE EXIT ON TOP OF SKULL CAP AND THE END CAP HAS 3 EXIT POINTS.Jan 11, 2026 · N523AE · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202505090012Attach Angle · corrodedRH LONGERON ATTACHMENT ANGLE (OVERWING FAIRING SUPPORT) IS CORRODED BETWEEN FS 693 AND FS 797. CORRECTIVE ACTION: REPAIRED CORRODED AREAS IAW MHIRJ REO 690-53-82-230 REV -- DATED 2025-04-14.May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202505090011Rivet · corrodedR/H F.S. 280 BEAN HAS TWO CORRODED RIVETS BETWEEN RBL 9 TO RBL 18. CORRECTIVE ACTION: REMOVED 2 EACH CORRODED FASTENERS IAW CRJ900 SRM 51-42-13-001-001-A01. INSTALLED 2 NEW FASTENERS. APPLIED TO FASTENERS. IAW CRJ900 SRM 51-42-13-001-001-A01, 51-25-16-001-001-May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202505090010Angle · corrodedUPON REMOVAL OF J-ANGLE FOUND L/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: REPLACED LH FS280 LWR WEB PN: 670-53-11-052-1 IAW BOMBARDIER REO 670-53-11-052 REV.-A DATED NOV-18-2004 REPAIR #2.May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202505090009Floorbeam · corrodedGALLEY 1 FWD INBRD SIDE FLOOR FITTING AT THE 280 IS CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED THREE CORRODED FLOOR FITTING AND DOUBLER PLATES AND INSTALLED THREE NEW FLOOR FITTINGS AND DOUBLER PLATES ON GALLEY 1 IAW CRJ 700 SRM TASK 51-41-0May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202505090008Hinge · chafedPAX DOOR HINGE (FUSELAGE SIDE) HAS CHAFING DAMAGE THE ENTIRE LENGTH BETWEEN THE LUGS. THE HINGE ALSO HAS A GOUGE BESIDE THE AFT LUG, APPROXIMATELY 0.5" LONG AND .025" DEEP. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR HINGE AT FUSELAGE SIDE P/N SH670-31876May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202505090007Angle · damagedFS 280 CROSSBEAM AND AFT J-ANGLE ARE CORRODED ALONG THE UPPER EDGE. CORRECTIVE ACTION: CORROSION FOUND ON MULTIPLE CROSS SECTIONS. REPLACE J-ANGLE WITH NEW. LOCATED AND DRILLED NEW "J" ANGLE CC670-34095-1 IAW CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW J-AMay 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202505090006Floorbeam · damagedWHILE REMOVED 280 FLOOR BEAM FOUND 5 EACH FASTENERS TO BE OVERSIZED ON LH FLOOR SILL GOING THROUGH BEAM CORRECTIVE ACTION: COMPLIED WITH ALL STEPS REO 670-53--21-2609 REV-- DATED 2025-04-16May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202505090005Angle · corrodedPAX DOOR LOWER MID ANGLE HAS MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR LOWER MID ANGLE PN: SH670-31875-3 IAW CRJ700 SRM TASKS 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.May 9, 2025 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202505090004Angle · corrodedPAX DOOR UPPER MID ANGLE HAVE MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.May 9, 2025 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202505090003Angle · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202505090002Angle · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6 .040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202505090001Web · corrodedUPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: LOCATED AND DRILLED NEW R/H CROSSBEAM PN# CC670-34094-2 IAW CRJ 700 SRM 51-40-11-001-001-A01. R/H LOWER WEB, R/H BUTTSTRAP & R/H CROSSBEAM INSTALLED PER SERVICE BULLETIN 67May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2025021911101Window · arcedCAPTAIN SIDE WINDOW ELECTRICAL ARCHING. / REMOVED AND REPLACED THE CAPTAIN SIDE FLIGHT COMPARTMENT SIDE WINDOW IAW AMM 56-12-01-000/400-801-A01-PSA. PERFORMED OPS TEST OF WINDSHIELD/SIDE WINDOW TEMP CONTROLLER IAW AMM 30-41-06-710-801. OPS TEST GOOD. PRESSURIZFeb 18, 2025 · N523AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2025020411101Lamp · inoperativeBURNING SMELL COMING FROM FWD CABIN ROW 1 CEILING LIGHT AREA. THERE WAS NO MEDICAL ATTENTION REPORTED FOR THIS EVENT. / FOUND LAMP CARRIER FOR CEILING LIGHTS ABOVE ROW 1 TO BE FAULTED INTERNALLY CAUSING BURNING SMELL. REMOVED AND REPLACED BOTH LAMP CARRIERS IAFeb 1, 2025 · N523AE · Cndair CL6002C10 · Passenger Compartment LightingSDR VNAA2024092311101Bpsu · faultedFLAPS FAIL CAUTION AFTER T/O. / UPON TROUBLESHOOTING FOUND LH FLAP BPSU DISCONNECTED. MANUALLY RIGGED LH BPSU IAW CRJ 700 AMM 27-52-03-801-A01. PRIOR TO CONNECTING OTBD FLAP TORQUE TUBE VERIFIED LH FLAP BPSU IS WITHIN RIG LIMITS. INSTALLED OTBD FLAP TORQUE TUBSep 19, 2024 · N523AE · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR VNAA2024090411102Display · failedMFD 2 FAIL IN FLIGHT DU #5 / RESET MFD 2 IAW CRJ 700 AMM 31-61-01-400-801. NO DEFECTS NOTED.Aug 31, 2024 · N523AE · Cndair CL6002C10 · Central DisplaySDR VNAA2024090411101Display · failedMFD 1 FAIL IN FLIGHT DU #5 / RESET MFD 1 IAW CRJ 700 AMM 31-61-01-400-801. NO DEFECTS NOTED.Aug 31, 2024 · N523AE · Cndair CL6002C10 · Central DisplaySDR VNAA202111051111Engine · odorFLIGHT 5359 WAS ALREADY DELAYED SEVERAL HOURS DUE TO SMOKE FILLING THE CABIN DURING AIR START. IT WAS DETERMINED THAT THE SMOKE WAS COMING FROM THE AIR START. FLIGHT FINALLY LEFT JAN AT 1731Z. DURING CLIMB, CREW BEGAN TO SMELL SMOKE. NONE WAS VISIBLE. CA BELIENov 3, 2021 · N523AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202108191112Seal · out of positionCABIN DOOR SEAL POPPED, DECLARED AN EMERGENCY AND DESCENDED TO FL120, THEN CANCELED EMERGENCY. MAIN PAX DOOR SEAL BROKEN IN FLIGHT / RE-SECURED PASSENGER DOOR SEAL IAW CRJ700 AMM 52-11-07-400-801-A02. LEAK CHECK GOOD AT THIS TIME. VISUALLY CHECK PASSENGER DOOAug 15, 2021 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020032011102Power Supply · dischargedEMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS OF BEING TURNED ON. REMOVED AND REPLACED ALL FOUR EMERGENCY POWER SUPPLY UNITS. OPS CHECK GOOD. #1 P/N 2013-1A S/N 99189, #2 P/N 2013-1A S/N 125186, #3 P/N 2013-1A S/N 122970, #4 P/N AD2013-1A S/N 97199.Mar 20, 2020 · N523AE · Cndair CL6002C10 · Emergency LightingSDR VNAA20191012105Warning Message · false activationRIGHT EMER DOOR CAUTION MSG DURING TAXI OUT. DEFERRED INDICATION. ON OCT 13 MAINTENANCE PERFORMED HEALTH CHECK OF RH EMERGENCY DOOR PROX SENSOR, OPS CHECK GOOD ON SENSOR AND ALSO DOOR INDICATION SYSTEM. CLEARED MELOct 11, 2019 · N523AE · Cndair CL6002C10 · Door Warning SystemSDR SIMA20190122002Angle · corrodedSERVICE DOOR FUSELAGE CUT OUT HAS CORROSION ON THE SILL ANGLE BETWEEN FS 319.70 AND FS 349.00 AT FLOOR LEVEL. REMOVED AND REPLACED SERVICE DOOR SILL ANGLE BETWEEN FS 319.70-349.00 IAW SRM 51-42-06.Jan 22, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA2019021019008Structure · corrodedBACK UP SILL BETWEEN FRAMES FS310.00 AND FS333.00 AT STRINGER 21L IS CORRODED-C/A-C/W INSTALLATION OF NEW BACK UP SILL IAW SRM 51-42-06.Jan 19, 2019 · N523AE · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20190119007Cleat · corrodedFRAME FS319.70 HAS A CORRODED SHEAR CLEAT AT 21L. EVALUATED FRAME FS319.70 AT STRINGER 21L, FOUND ONLY LIGHT SURFACE CORROSION. REPAIRED IAW SRM 51-21-06.Jan 19, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190111008Floor Support · corrodedLT OUTBD LONGITUDINAL FLOORBEAM IS CORRODED BETWEEN FS1000.00 AND FS1031.00. C/A-COMPLETE:REPAIRED IAW ERS-CR-5300-3632.Jan 11, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA2018091110001Sign · unsecureEMERGENCY EXIT SIGN OVER SERVICE DOOR FALLING DOWN. REMOVED AND REPLACED EXIT SIGN ASSY OVER SERVICE DOOR IAW AMM 33-51-05.Sep 10, 2018 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA201809076001Connector · dirtyBRAKE OVHT WARNING ENROUTE AT FL360. RAN CHECKLIST RESET SYSTEM WITH BTMS BUTTON NR 4 BRAKE INDICATED 14. CLEANED AND APPLIED STABILANT TO J616/P616 PIN 3 AND 4 IAW EEC SPM. OPERATIONAL CHECKS GOOD IAW AMM 32-46-00. NO FURTHER FRETTING OR DEFECTS NOTED.Sep 6, 2018 · N523AE · Cndair CL6002C10 · BrakeSDR SIMA2018083029002Lamp · inoperativeEMERGENCY LIGHT OUT AFT CABIN 2ND LIGHT FROM END OF AFT CABIN-C/A-DEFERRED EMERGENCY LIGHT IAW MEL 33-34. REMOVED AND REPLACED CEILING EMERGENCY-FLOOD-LIGHT LAMP IAW CRJ-700 AMM 33-51-09 OPS CHECK GOOD MEL ITEM RESTOREDAug 29, 2018 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA201808065002Thermocouple · failedBRAKE OVERHEAT INDICATION ON THE RIGHT OUTBOARD DURING CRUISE AT FL 300. RAN THE PROCEDURE, DECLARED EMERGENCY. LANDED IWTHOUT INCIDENT. INDICATIONS NORMAL AFTER PROCEDURE. REMOVED AND REPLACED THE THERMOCOUPLE SENSOR IAW AMM 32-46-01 OPS CHECKED GOOD.Aug 5, 2018 · N523AE · Cndair CL6002C10 · Landing Gear Brake SystemSDR SIMA2018043028001Warning Message · illuminatedDURING DECENT, DEPLOYED FLIGHT SPOILERS SLOWLY GOING THRU FL260 AFTER 10 SECONDS OF DEPLOYMENT, CAUTION MESSAGE FOR OTBD SPOILERONS & OTBD FLT SPOILERS DISPLAYED. INTERROGATED MDC, FOUND CORRELATED MESSAGE, LT OTBD MFS PCU BINDING. PERFORMED SPOST 1 RESETApr 28, 2018 · N523AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20171008002Rotor · shearedWHILE ACCOMPLISHING W/C 72-009 PG 5, BORESCOPE PROCEDURES, FOUND ONE STAGE 1 HP TURBINE ROTOR BLADE SHEARED. REMOVED AND REPLACED THE LT ENGINE IAW WORK CARDS 71-001 AND 71-002. OPS CHECKED GOOD. NO LEAKS NOTED.Oct 8, 2017 · N523AE · Cndair CL6002C10 · Turbine SectionSDR SIMA20170714003Lamp · inoperativeAFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-09.Jul 14, 2017 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170623001Spoiler Sys · malfunctionedWHEN USING THE FLIGHT SPOILER LEVER IN FLIGHT AT 27,000 FEET, A CAUTION MESSAGE FOR THE INBD FLT SPOILERS AND INBD SPOILERONS APPEARED. INTERROGATED MDC, FOUND THE RT INBD MFS PCU BINDING MDC MESSAGE. PERFORMED SPOST 1 RESET. PERFORMED OPS CHECK IAW ETN-CRJun 23, 2017 · N523AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20170614001Sensor · failedBTMS OVERHEAT WARNING DURING CLIMB OUT, RIGHT OTBD BRAKE. REMOVED AND REPLACED THE RT OTBD BRAKE TEMP SENSOR IAW AMM 32-46-01, OPS CHECKED GOOD. PERFORMED DVI OF BRAKE SYSTEM IAW AMM 05-51-09, NO DEFECTS NOTED.Jun 14, 2017 · N523AE · Cndair CL6002C10 · Landing Gear Brake System
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