N511AE

Service difficulty reports · 137

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 = 'N511AE' 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 VNAA202501090016Seat Track · gougedTHE SEAT TRACK LOCATED ON RBL 9 BETWEEN F.S 834 - F.S 974 HAS DENTS AND DEEP GOUGES. THIS SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090015Seat Track · gougedTHE SEAT TRACK LOCATED ON LBL9 BETWEEN F.S 687 - F.S 581 HAS DEEP GOUGES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090014Seat Track · gougedRIGHT SIDE SEAT TRACK BETWEEN F.S 865 - F.S 969 HAS GOUGING AND PITTING. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090013Seat Track · gougedRIGHT SIDE SEAT TRACK BETWEEN F.S 483 - F.S 570 HAS GOUGES AND SCRATCHES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090012Seat Track · gougedLH SIDE SEAT TRACK BETWEEN F.S 674 - F.S 712 HAS MULTIPLE GOUGES AND SCRATCHES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090011Seat Track · gougedLEFT SIDE SEAT TRACK BETWEEN F.S 712 - F.S 761 HAS MULTIPLE GOUGES.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202501090010Fitting · gougedRIGHT FLAP FITTING (AFT) AT WS 264.00 HAS GOUGED ON LUG EAR.Jan 9, 2026 · N511AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA202601090009Skin · gougedFUSELAGE SKIN UNDER FWD DRAIN MAST IS GOUGEDJan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202601090008Skin · corrodedFUSELAGE EXTERNAL SKIN UNDER LOWER BEACON LIGHT IS GOUGED AND CORRODED IN MULTIPLE AREA SH670-33202 SKIN UNDER LWR. BEACONJan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202601090007Torque Tube · corrodedPASSENGER DOOR PULL-IN LEVER TORQUE TUBE PN 601R31863-1 HAS CORROSIONJan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202601090006Washer · crackedREQUEST, SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR , HR00572741 SO# 400416899 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7Jan 9, 2026 · N511AE · Cndair CL6002C10 · Wing Main, Frame StructureSDR VNAA202601090005Washer · crackedSUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00572740, SO 400416898 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7) RETENTION WASHERJan 9, 2026 · N511AE · Cndair CL6002C10 · Wing Main, Frame StructureSDR VNAA202601090004Skin · crackedWHILE DRILLING TO EXTRACT SCREWS ON RH OVER WING INSPECTION LIGHT DRILL BIT WALKED FROM CENTER AND DAMAGED SURROUNDING HOLE. DWG SH670-33162 FUSELAGE SKIN PANELJan 9, 2026 · N511AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA202601090003Skin · crackedPAX DOOR SURROUND STRUCTURE SKIN AT FS310.00 AND STGR17L IS CRACKED DUE TO PAX DOOR HINGE BEING MISALIGNED ONE LUG FWD SH670-31187-9 SKINJan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202601090002Angle · corrodedPASSENGER DOOR ANGLE AT FS338-963 TRACE DATUM 6 HAS MINOR SURFACE CORROSION PN 600-31902-269. (INSIDE PAX DOOR)Jan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202601090001Lug · gougedFOUND R/H UPPER THRUST EVERSER CENTER HINGE BRACKET IS GOUGED LOWER EDGE OF LUG. CN624-1404-212 HINGE BEAM LUGJan 9, 2026 · N511AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA2024121311101Skin · damaged#3 VHF ANTENNA MOUNTING AREA UNDER ANTENNA FUSELAGE SKIN IS DAMAGED. / C/W INTELSAT EA9596-REVB FUSELAGE / FS 629-645 / SCRATCHES UNDER VHF-3 ANTENNA, DELTA ENGINEERING 8100-9 # ST04797NY-011. IAW EA9596-REVC INSTRUCTIONS.Dec 10, 2024 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2024041711102Door · damagedAFTER TAKE OFF THE FA'S COULD SEE LIGHT THROUGH THE PAX DOOR / REMOVED AND REPLACED PAX DOOR SEAL IAW CRJ700 AMM 52-11-07-000/400-804(A02)PSA. LEAK CHECK GOOD.Apr 16, 2024 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2024010911101Unknown · unknownANTI-DUCT WARNING AND ANTI-ICE CAUTION MSG IN FLIGHT / INTERROGATED MAC FOUND EVENT LOC HISTORY AT SS14. REMOVED CONNECTOR MT168P2 IAW CRJ700 AMM 36-21-09-000-801. FOUND OLD STYLE INSERT. R&R CERAMIC INSERT IAW CRJ700 ESPM 20-26-00. RECONNECTED MT168P2 IAW CRJJan 6, 2024 · N511AE · Cndair CL6002C10 · Ice/Rain Protection System WiringSDR VNAA202308292Plate · corrodedPAX DOOR CUTOUT, ATTACHMENT PLATE CORRODED AT STGR 18L, FS295.00 AND FS364.00Aug 29, 2023 · N511AE · Cndair CL6002C10 · DoorsSDR VNAA20230829001Skin · corrodedDISCREPANCY: FUSELAGE SKIN IS CORRODED UNDER FOOTPRINT OF PANEL 196DR AT STR 27.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2023082903Unknown · damagedSERVICE DOOR STABILIZATION BRACKET IS CRACKED.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Service DoorsSDR VNAA2023082904Skin · damagedLEADING EDGE 522AL HAS ONE DAMAGED FASTENER COUNTERSINK ON THE LOWER LEADING EDGE AT WS 178.00.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Wing, Plate/SkinSDR VNAA2023082905Angle · corrodedCLIP CORRODED AT FRAME AT FS295 AND STRG21R.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA2023082907Stringer · corrodedSTINGER 21R CORRODED BETWEEN FS319 AND FS333.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2023082908Doubler · corrodedDOUBLER FOR AFT POTABLE WATER LINES CORRODED BETWEEN FS 1031.00 AND FS 1047.00 STR 26R.Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202207011113Fuel Sys · odorSTRONG FUEL SMELL IN AFT CABIN AND LAV / OPENED PAX DOOR, SERVICE DOOR & REMOVED OVER-WING DOORS, CABIN FLOOR PANELS 272 GRF & 271 ALF, & AFT CARGO BAY FLOOR PANELS 281 HLF & 281 BLF TO ALLOW FOR AIR VENTILATION & TO SEARCH FOR SOURCE OF ODOR. REMOVED & DEFERJun 30, 2022 · N511AE · Cndair CL6002C10 · Fuel Transfer ValveSDR VNAA202207011112B-Nut · looseSTRONG FUEL SMELL IN PAX CABIN. PERFORMED DVI OF BELLY OF AIRCRAFT IN AFT CARGO BAY AND FOUND B-NUT ON APU FUEL-FEED DRAIN LINE T-FITTING TO BE LOOSE. INSULATION IN THE SURROUNDING AREA AT FS1000 WAS SOAKED IN FUEL. TIGHTENED B-NUT I.A.W. CRJ700 AMM 28-24-23-4Jun 29, 2022 · N511AE · Cndair CL6002C10 · Fuel Transfer ValveSDR VNAA202207011111Cabin Air Sys · odorSTRONG FUEL SMELL IN PAX CABIN. MAINTENANCE VENTED A/C FOR SEVERAL HOURS AS REQUIRED. "Jun 29, 2022 · N511AE · Cndair CL6002C10 · Aircraft Fuel SystemSDR VNAA202110271111Instrument Panel · abnormalFO LOST ALL INSTRUMENTATION RAN QRH. ADC2 SWITCHED WORKED LOST AGAIN. PITCH FEEL STATUS, FADEC FAULT STATUS, YAW DAMPER 2 FAULT STATUS MESSAGES / PERFORMED OPS TEST OF ADC IAW CRJ700 AMM 34-13-01-740-801( A01) OPS TEST GOOD. PERFORMED OPS TEST OF AHRS IAW CRJ7Oct 23, 2021 · N511AE · Cndair CL6002C10 · Instrument PanelSDR VNAA202109021112Warning Message · false activationCOMING INTO CLT AROUND FL120, THE CREW EXPERIENCED ICING CONDITIONS AND TURNED ON THE A/I SYSTEM. SHORTLY AFTER, THEY RECEIVED A A/I DUCT WARNING MESSAGE THAT THEN WENT TO AMBER. THE QRH SAID TO TURN OFF THE ANTI-ICE SYSTEM AND LEAVE ICING CONDITIONS. THE CREWAug 31, 2021 · N511AE · Cndair CL6002C10 · Central WarningSDR VNAA2021051311101Proximity Switch · failedAIRCRAFT HAS A DOOR INDICATOR MEL. CREW WAS TOLD TO EXPECT DOOR CAUTION MESSAGE. NEAR CRUISE, RECEIVED A DOOR WARNING MSG. NO PRESSURIZATION ISSUES THOUGH. CREW RAN THE QRH, AND DETERMINED TO RETURN TO SYR. CREW DID DECLARE AN EMERGENCY. ONCE FLIGHT DESCENDED May 9, 2021 · N511AE · Cndair CL6002C10 · Door Warning SystemSDR VNAA2020081611101Controller · failedCREW THE BROUGHT AIRCRAFT INTO FNT LAST NIGHT HAD NO ISSUES. UPON ARRIVING FOR OUTBOUND FLIGHT, FOUND A WRITE-UP FOR A BURNING ELECTRICAL SMELL IN AFT OF AIRCRAFT. CREW ALSO FOUND MULTIPLE BREAKERS POPPED. UPON START-UP CREW ALSO FOUND MULTIPLE LRU INOP, ACSC Aug 16, 2020 · N511AE · Cndair CL6002C10 · Navigation SystemSDR VNAA202008161111Computer · failedCREW THE BROUGHT AIRCRAFT INTO FNT LAST NIGHT HAD NO ISSUES. UPON ARRIVING FOR OUTBOUND FLIGHT, FOUND A WRITE-UP FOR A BURNING ELECTRICAL SMELL IN AFT OF AIRCRAFT. CREW ALSO FOUND MULTIPLE BREAKERS POPPED. UPON START-UP CREW ALSO FOUND MULTIPLE LRU INOP, ACSC Aug 16, 2020 · N511AE · Cndair CL6002C10 · Navigation SystemSDR VNAA2020071711101Power Supply · failedSEVERAL EMERGENCY LIGHTS INOP. R&R #2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.Jul 17, 2020 · N511AE · Cndair CL6002C10 · Emergency LightingSDR VNAA202005119991Hinge · wornPAX DOOR HINGE HAS EXCESSIVE PLAY ON FWD SIDE. PERFORMED DETAILED INSPECTION OF THE PASSENGER DOOR PIANO HINGE LUGS FUSELAGE SIDE AND PASSENGER DOOR SIDE AND FOUND FUSELAGE SIDE LUGS AND PASSENGER DOOR SIDE LUGS OUT OF LIMITS. PASSENGER DOOR FUSELAGE SIDE HINGMay 11, 2020 · N511AE · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2020012301102Battery Pack · inoperativeMULTIPLE PORTIONS OF EMERGENCY LIGHT SYSTEM INOP. REMOVED AND REPLACED POWER SUPPLY BATTERY IAW CRJ 700 AMM. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (P/N: 2013-1A S/N: 122248)Jan 20, 2020 · N511AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2020011499907Stiffener · crackedPAX DOOR POWER ASSIST MOTOR STIFFENER FOUND TO BE CRACKED. REMOVED PAX DOOR POWER ASSIST MOTOR FOR ACCESS IAW AMM 52-11-08-000-801-A02. REINSTALLED PAX DOOR POWER ASSIST MOTOR IAW AMM 52-11-08-400-801-A02. REMOVED PAX DOOR POWER ASSIST MOTOR CABLE GUARD FOR ACJan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020011419906Stiffener · crackedPAX DOOR POWER ASSIST MOTOR STIFFENER FOUND TO BE CRACKED. REMOVED UNSERVICEABLE PAX DOOR AFT WEB STIFFENER IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT WEB STIFFENER IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLEJan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020011409906Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE WITHIN 1000 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES. REMOVED PREVIOUS AFT DRAG ANGLE REPAIR IAW SRM 51-42-13-001-001-A01. INSTALLED NEW REPAIR TO PAX Jan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020011499905Floorbeam · corrodedAFT CARGO BAY FLOORBEAM AT LBL 9 HAS MULTIPLE AREAS OF CORROSION ON TOP OF THE BEAM BETWEEN FS 1007 AND FS 1064. IAW SRM 53-61-43-101-001-A01 NO DAMAGE ALLOWED TO FLOORBEAMS IN THIS LOCATION REQUIRES ENGINEERING REPAIR. BLENDED OUT DAMAGE IAW REO 670-53-61-162Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2020011499904Floorbeam · corrodedAFT CARGO BAY FLOOR BEAM AT LBL 27HAS MULTIPLE AREAS OF CORROSION ON TOP OF THE BEAM BETWEEN FS 992 TO FS 1033. COMPLIED WITH REO 670-53-61-1626.Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2020011499903Floorbeam · corrodedAFT CARGO RBL 9 AND RBL 27 FLOORBEAMS HAVE MULTIPLE AREAS OF CORROSION ON TOP OF BEAMS BETWEEN FS 1007 TO FS1064 ON RBL 9 AND FS 1060 TO FS 1075 ON RBL 27.0. IAW SRM 53-61-43-101-001-A01 NO DAMAGE ALLOWED TO FLOOR BEAMS IN THIS LOCATION REQUIRES ENGINEERING REJan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2020011499902Frame · corrodedFUSELAGE FRAME AT FS 310 IS CORRODED ON BOTH SIDES BETWEEN STGR 26L AND STGR 26R. CUT AND REMOVED DAMAGED SECTION OF FS 310.00 FRAME IAW SRM 53-00-06-201-006-A01. COMPLETED REPAIR OF DAMAGED SECTION OF FS 310.00 FRAME IAW SRM 53-00-06-201-006-A01. REPAIR INSTAJan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020011489901Frame · crackedFRAME BS 333, STGR 0 WAS CRACKED. REMOVED THE FRAME SECTION BETWEEN STRINGERS 0 AND 3 IAW EA 69-2019-308 REV.P1. INSTALLED FRAME SECTION IAW EA 69-2019-380 REV.P1. LOCATED AND DRILLED REPAIR FRAME SECTION IAW EA 69-2019-380 REV.P1. PERFORMED EDDY CURREJan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA201908021102Brake Sys · malfunctionedWHILE CLIMBING OUT OF DCA AIRPORT THE CREW RECEIVED A ANTI SKID FAULT STATUS MESSAGE. THE CREW RAN THE QRH. CREW ALSO RAN LANDING NUMBERS THROUGH ACARS FOR THE DESTINATION AIRPORT OF BDL. CREW DETERMINED IT WAS UNSAFE TO LAND THERE DUE TO RUNWAY LENGTH. THE CRAug 1, 2019 · N511AE · Cndair CL6002C10 · Landing Gear Brake SystemSDR VNAA2019070211101Drag Angle · crackedPLACED ON EA69-2019-136 DURING ROUTINE MAINTENANCE IN (CAK), MAINTENANCE NOTED THAT THE 601R31772-5 AFT DRAG ANGLE HAS A CRACK IN IT THAT MEASURES APPROXIMATELY 1.60Ï¿½, AND IS LOCATED IN THE RADIUS OF THE DRAG ANGLE.Jul 2, 2019 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2019042411102Battery · dischargedFLOOR LEVEL EMERGENCY EXIT SIGN ADJACENT TO SEAT 16F DOES NOT ILLUMINATE SWAPPED #3 AND #4 ESPU BATTERIES OPS CHECK GOOD.Apr 24, 2019 · N511AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2018051011101Manifold · malfunctionedIN FLIGHT WITH THE GEAR UP THE CREW RECEIVED A STEERING INOP CAS MESSAGE. THE MESSAGE RESET ON THE GROUND AND CAME BACK ON MULTIPLE TIMES. REMOVED AND REPLACED STEERING MANIFOLD. OPS AND RIG CHECK GOOD.May 10, 2018 · N511AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2017090311101Warning Light · illuminatedRETURNED TO FIELD IMMEDIATELY AFTER TAKEOFF FOR A SERVICE DOOR INDICATOR LIGHT. FLIGHT LANDED SAFELY WITH NO COMPLICATIONS, NO EMERGENCY WAS DECLARED.Sep 3, 2017 · N511AE · Cndair CL6002C10 · Door Warning System
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