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 SIMA20170606004Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. BATTERY DEAD. R & R EPSU BATTERY PACKS 3 AND 4 IAW MM 33-51-17. OPS CHECKED GOOD.Jun 6, 2017 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170606005Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. BATTERY DEAD. REMOVED AND REPLACED EPSU BATTERY PACKS 1 AND 2 IAW MM 33-51-17. OPS CHECKED GOOD.Jun 6, 2017 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170604001Light · inoperativeRIGHT SIDE AFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE RT AFT EMERGENCY EXTERIOR LIGHT IAW STANDARD MAINTENANCE PRACTICES. OPS CHECKED GOOD IAW AMM 35-51-15.Jun 4, 2017 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170325003Connector · disconnectedONE CABIN EMERGENCY LIGHT INOPERATIVE. FOUND AN ELECTRICAL CONNECTOR DISCONNECTED. CONNECTED THE ELECTRICAL CONNECTOR IAW AMM 25-26-05. OPS CHECKED GOOD.Mar 25, 2017 · N523AE · Cndair CL6002C10 · Light System WiringSDR SIMA20170125004Tee Fitting · crackedRIGHT TEE BRACKET AT BS 280 IS CRACKED. FABRICATED AND INSTALLED A NEW TEE BRACKET IAW SRM 53-11-41, 51-42-06, AND 51-42-21.Jan 25, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SIMA20170125003Tee Fitting · crackedLEFT TEE BRACKET UNDER CROSSMEMBER AT BS 280 IN LEFT INBOARD FLOOR SUPPORT IS CRACKED. FABRICATED AND INSTALLED NEW TEE BRACKET IAW SRM 53-11-41, 51-42-06, 51-42-21.Jan 25, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SIMA20170124001Attach Angle · crackedPASSENGER DOOR AFT STEP SKIN ATTACH ANGLE CRACKED BY PULLEY BRACKET. REPAIRED PAX AFT DRAG ANGLE IAW SRM 52-11-04.Jan 24, 2017 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170123006Bulkhead Web · corrodedRIGHT LOWER BULKHEAD WEB AT BS 280 IS CORRODED JUST ABOVE CROSSBEAM. REPAIRED IAW EO CR-53MR-174.Jan 23, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20170118005Frame · corrodedFRAME AT BS 319.70 IS CORRODED BETWEEN STRINGERS 26-27L. COMPLETED INSTALLATION OF SPLICE PLATE, INSTALLED ATTACHMENT BRACKETS AND COMPLETED INSTALLATION OF STRINGER CLEATS IAW ERS-CR-53MR-2561.Jan 18, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20170118004Floorbeam · corrodedFLOORBEAM AT BS 280 IS CORRODED AND HAS A ONE INCH CRACK. INSTALLED A NEW FLOORBEAM IAW SRM 51-42-06.Jan 18, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20170118003Structure · crackedFORWARD EQUIPMENT BAY FLOOR HAS A 1/8" CRACK BY LOWER AFT CUTOUT FOR 211AL. REPAIRED FWD EQUIPMENT BAY FLOOR IAW ETN CR-53-099.Jan 18, 2017 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20170118002Bulkhead · corrodedLEFT BULKHEAD AFT SIDE HAS CORROSION JUST ABOVE FS280.00. INSTALLED NEW FABRICATED LT LOWER WEB IAW CRH SRM CH 53-11-10.Jan 18, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20170114001Frame · corrodedFRAME AT BS 265 IS CORRODED BETWEEN STRINGERS 26L-26R. REMOVED AND REPLACED FRAME STIFFENER IAW SRM 51-42-06.Jan 14, 2017 · N523AE · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20170114002Support · corrodedNOSE JACK FITTING SUPPORT BETWEEN BS 265 - 280 IS CORRODED. REMOVED AND REPLACED RT NOSE JACK FITTING SUPPORT IAW SRM 51-42-06 AND SRM 51-42-21.Jan 14, 2017 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20161103002Flashlight · inoperativeAFT ATTENDANT FLASHLIGHT INOP. REMOVED AND REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT IAW EEL.Nov 3, 2016 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20161017001Light · odorGALLEY LIGHTS BURNING ODOR REPORTED BY FLIGHT ATTENDANTS. OPC GALLEY LIGHTS IAW AMM 33-26-00. OPERATED GALLEY LIGHTS FOR SEVERAL HOURS WITH OUT HAVING ODORS IN GALLEY FROM LIGHTS. OPS CHECKED GOOD.Oct 17, 2016 · N523AE · Cndair CL6002C10 · Passenger Compartment LightingSDR SIMA20160602006Engine · malfunctionedAFTER TAKEOFF CREW HEARD A BANGING NOISE ON ROTATION. CREW DECLARED EMERGENCY & RETURNED WITHOUT INCIDENT. SUSPECT, ENGINE COMPRESSOR STALL AFTER TAKEOFF ROTATION, LOUD BANDING NOISE ACFT SWAY TO LT AND RT. R & R LT ENGINE IAW WORK CARD 71-001 AND 71-002, OJun 2, 2016 · N523AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20160527001Roller · lack of lubeMAIN ENTRY DOOR HARD TO OPEN FROM INSIDE & OUTSIDE THE ACFT. PERFORMED MAIN CABIN DOOR ROLLER LUBE IAW AMM 52-11-00. OPERATIONS CHECKED OK.May 27, 2016 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160524001Handle · lack of lubePASSENGER DOOR HANDLE IS JAMMED, CANNOT OPEN DOOR FROM INSIDE. LUBED DOOR HANDLE IAW STANDARD PRACTICES. NO DEFECTS NOTED.May 24, 2016 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20151022008Stiffener · crackedFORWARD SIDE OF BULKHEAD AT FS 202.75, FOUND INDICATION ON TOP OF STIFFENER RBL 30.0, APPROX 1/8" LONG. STIFFENER FAILED NDT INSPECTION. REPAIRED IAW REO 670-53-11-1099 & NCR-CR-53-152.Oct 22, 2015 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151022001Stiffener · crackedFWD SIDE OF BULKHEAD AT FS 202.75, FOUND INDICATION ON TOP OF STIFFENER, RBL30.0, APPROX 1/8" LONG, STIFFENER FAILED NDT INSPECTION. REPAIRED IAW REO 670-53-11-1099 & NCR-CR-53-152.Oct 22, 2015 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WVER20151020001Post · crackedAT FS 847.00, LBL 18.00, VERTICAL POST HAS AN INDICATION NOTED IN THE RADIUS OF THE HORIZONTAL FLANGE, AT THE FWD FASTENER INBD SIDE, APPROX .250"L X 70% FSH. FAILED NDT INSPECTION.Oct 19, 2015 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WVER20151020002Post · crackedAT FS 847.00, LBL 27.00, VERTICAL POST HAS AN INDICATION NOTED IN THE RADIUS OF THE HORIZONTAL FLANGE, AT THE FWD FASTENER INBD SIDE, APPROX .250"L X 80% FSH. FAILED NDT INSPECTION.Oct 19, 2015 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150428002Flashlight · inoperativeFORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD.Apr 28, 2015 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20141223006Holder · defectiveFIRST OFFICER`S FLASHLIGHT HOLDER DOES NOT HOLD COCKPIT EMER FLASHLIGHT SECURELY, FALLS OUT. R & R FIRST OFFICER`S FLASHLIGHT HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.Dec 23, 2014 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140908003Compressor Blade · lack of lubeAT INITIAL CRUISE FLIGHT, NR 2 ENG FAN REACHED APPROX 3.5 VIBRATION. AOM VOL 1 PROCEDURE FOLLOWED. REDUCTION IN THRUST EVENTUALLY HELPED A BIT. FOLLOWED PROCEDURE IN AMM 22-21-02 & PERFORMED THE VIBRATION CHECK IAW 71-00-00. PERFORM BLADE LUBE WITHIN 50 F Sep 8, 2014 · N523AE · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SIMA20140709002Light · inoperativeEMERGENCY LIGHT IMMEDIATELY AFT OF PAX DOOR IS INOPERATIVE. R & R EMER LIGHT BULB LOCATED IMMEDIATELY AFT OF PAX DOOR IAW AMM 33-51-15.Jul 9, 2014 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140526003Strap · crackedAFT BELLY PANEL 196DR HAS A CRACKED SUPPORT STRAP. REPAIRED CRACKED SUPPORT FOR THE AFT FAIRING 196DR IAW SRM 53-82-83.May 26, 2014 · N523AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20140520005Diaphragm · crackedLEFT & RIGHT WW DIAPHRAGMS CRACKED. R & R LT & RT WW DIAPHRAGMS IAW AMM 53-83-85. DIAPHRAGM PN CC670-39205-5.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140520008Skin · crackedPASSENGER DOOR AFT SIDE SKIN HAS A 1 1/4 INCH CRACK BEHIND STIFFENER FOR GAS SPRING. REPAIRED PAX DOOR IAW ETN-CR-52-039.May 20, 2014 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140520011Bracket · crackedLEFT SIDE BRACKET AT BL 9.04 ON CROSSBEAM AT FS 280.00 HAS A 1/8 INCH CRACK. FABRICATED & INSTALLED NEW BRACKET & FILLER PIECE IAW SRM 53-11-41.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140520010Doubler · corrodedANTENNA DOUBLER BETWEEN FS 295.00 - 310.00 AT STRINGER 27 IS CORRODED. R & R THE ANTENNA DOUBLER BETWEEN FS 295.00 - 310.00 AT STRINGER 27 IAW SRM 51-42-06.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20140520009Aileron · crackedTRANSFERRED FROM AML PAGE 3419401 NR 1. RT AILERON HAS A LARGE CRACK ON THE OTBD EDGE, AFT CORNER. DEFERRED IAW ETN CR-57-037 AUTH 523570590. PERFORMED PERMANENT REPAIR DISBONDING OTBD EDGE RUBBING BLOCK ON RT AILERON IAW ETN-CR-57-053.May 20, 2014 · N523AE · Cndair CL6002C10 · AileronsSDR SIMA20140520012Angle · crackedSECOND FROM INBD BULKHEAD ANGLE AT 280 LT IS CRACKED. R & R OF ANGLE IAW SRM 51-42-06.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20140520007Plate · crackedFORWARD EQUIPMENT COMPARTMENT FLOOR IS CRACKED UNDER THE ADG PUMP. REPAIRED FWD EQUIPMENT COMPARTMENT FLOOR UNDER THE ADG PUMP IAW ETN-CR-53-099.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140520006Bracket · crackedRIGHT SIDE BRACKET AT BL 9.04 ON CROSSBEAM AT FS 280.00 HAS A 1/4 INCH CRACK. FABRICATED & INSTALLED BRACKET & FILLER PIECE IAW SRM 53-11-41.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140520004Crossbeam · corrodedCROSSBEAM AT FS 280.00 IS CORRODED. R & R CROSSBEAM AT FS 280.00 IAW SRM 51-42-06, SRM 51-42-13 & SRM 51-42-21.May 20, 2014 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140412003Power Unit · inoperativeFIRST OFFICER`S FLASHLIGHT DOES NOT WORK, INDICATES CHARGING IN HOLDER BUT DOES NOT HOLD CHARGE. R & R POWER UNIT FOR FIRST OFFICER`S FLASHLIGHT IAW CMM 25-60-11. OPERATIONS CHECKED IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.Apr 12, 2014 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140331001Cradle · inoperativeFIRST OFFICER'S FLASHLIGHT NOT CHARGING IN HOLDER. R & R FIRST OFFICER`S FLASHLIGHT HOLDER IAW AMM 25-61-02.Mar 31, 2014 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140207005Light · inoperativeAFT EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-00, ALL CHECKED GOOD.Feb 7, 2014 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140118001Sensor · failedGOING THROUGH 13,000 FT, GOT WING OVERHEAT WARNING. REMAINED ON ABOUT 20 SECONDS, WENT OUT, THEN CAME RIGHT BACK ON, OCCURRED NUMEROUS TIMES. DECLARED EMERGENCY. RETURNED LGA. WING ANTI-ICE WAS NOT ON & ALL AOM PROCEDURES COMPLIED WITH. R & R THE OTBD TEMPJan 18, 2014 · N523AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR SIMA20140109006Pin · out of positionMAIN DOOR WILL NOT CLOSE. DOOR HANDLE PINS IN WRONG POSITION. PUT PINS IN CORRECT LOCATION. OPERATIONS CHECKED GOOD IAW AMM 52-10-00.Jan 9, 2014 · N523AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20130318005Flashlight · inoperativeON FLIGHT 3610 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW CRJ 700 AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SMar 18, 2013 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20130317005Flashlight Assy · brokenFLIGHT 3610, CREW REPORTED FIRST OFFICER’S FLASHLIGHT HOLDER CLIP BROKEN. REMOVED AND REPLACED FLASHLIGHT HOLDER IAW AMM 25-61-02. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.Mar 17, 2013 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20130309002Duct · defectiveON FLIGHT 3758 THE CREW REPORTED THAT ON CLIMBOUT FROM MSP IN ICING CONDITIONS THEY RECEIVED AN EICAS WARNING "ANTI ICE DUCT" WARNING MESSAGE. MESSAGE EXTINGUISHED WHEN WING ANTI ICE WAS TURNED OFF. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MSP. THE AIMar 9, 2013 · N523AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR SIMA20130304005Fitting · brokenDURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT HOLDER BOTTOMS CLIPS BROKEN. THE FLASHLIGHT WAS FOUND STOWED IN THE FORWARD ENTRY AREA STORAGE SPACE. DATE OF DISCOVERY 03/01/13. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED ANMar 4, 2013 · N523AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20121217002Light · inoperativeON FLIGHT 3634 THE CREW REPORTED 3 INOPERATIVE BULBS ON THE LEFT OVERWING EMERGENCY EXIT SIGN (VERTICAL SIGN, FORWARD OF EXIT). THE AIRCRAFT WAS REMOVED FROM SERVICE. RELAMPED AS REQUIRED. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICEDec 17, 2012 · N523AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20120605008Floorbeam · corrodedDURING C CHECK INSPECTION, FOUND CROSSBEAM AT FS280.00 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FS280.00 CROSSBEAM IAW BOMBARDIER STRUCTURAL REPAIR MANUAL 51-42-06, 51-42-11 AND 51-42-21. THE AIRCRAFT RETURN TO SERVICEJun 5, 2012 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20120605007Attach Angle · crackedDURING C-CHECK, FOUND LEFT FORWARD VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AFT END IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED ATTACH ANGLE IAW EO CR-55MR-053. THE AIRCRAFT WAS RETURNED TO SREVICE.Jun 5, 2012 · N523AE · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20120605006Attach Angle · crackedDURING C-CHECK, FOUND RIGHT AFT VERTICAL STAB TO FUSELAGE ATTACH ANGLE FORWARD END IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR OF RIGHT VERTICAL STAB TO FUSELAGE AFT ATTACH ANGLE IAW EO CR-53MR-164R1. THE AIRCRAFT WAS RETURNED TO SJun 5, 2012 · N523AE · Cndair CL6002C10 · Vertical Stabilizer, Attach Fittings
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