N512AE

Service difficulty reports · 159

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 = 'N512AE' 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 VNAA20260511037Seat Track · corrodedRBL 9 SEAT RAIL IS CORRODED BETWEEN FS 349 AND FS 485. INSTALLED RBL 9 SEAT RAIL BETWEEN FS 349 AND FS 485 IAW AMM 53-00-49-400-801-A03.Nov 14, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511029Seat Track · corrodedRIGHT SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 485 AND FS 573. INSTALLED SERVICEABLE R/H SIDE SEAT RAIL PN SH670-32234-3 BETWEEN FS 485.00 AND FS 573.00 IAW CRJ 700 AMM 53-00-49-400-801-A03.Nov 14, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511002Bracket · corrodedDURING CLEAN-UP OF HARDWARE (FWD FITTING MOUNT) FOUND LWR K-FRAME BRACKET HAS PITTED CORROSION. : REMOVED & REPLACED CORRODED LH LWR K-FRAME BRACKET WITH NEW SERVICEABLE BRACKET (PN CN624-4278-002) IAW CRJ700 AMM 78-36-01-000-801-A01 & 78-36-01-400-801-A01. Nov 14, 2025 · N512AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA20260511001Door Sill · corrodedAFT CARGO DOOR LOWER SILL IS CORRODED. REPAIRED AFT CARGO DOOR LOWER SILL IAW SRM 53-61-23-201-001-A01.Nov 14, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260511039Seat Track · corrodedLBL 9 SEAT RAIL IS CORRODED BETWEEN FS 485 AND FS 581. INSTALLED SERVICEABLE SEAT RAIL PN SH-670-33426-1 FOR LBL 9 FS 485 TO 581 IAW CRJ 700 AMM 53-00-49-400-801-A03.Nov 13, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511035Seat Track · corrodedRIGHT SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 708 AND FS 761. REMOVED UNSERVICEABLE SIDE SEAT RAIL AT FS 708 TO FS 761 IAW CRJ 700 AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICEABLE SIDE SEAT RAIL (P/N SH670-37509-1) RT STGR 15R FS 708 TO FS 761 Nov 13, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511034Seat Track · corrodedRIGHT SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 677 AND FS 708. INSTALLED NEW SERVICEABLE RH SIDE SEAT RAIL PN SH670-36255-3 AT STGR 15R BETWEEN FS 677 AND FS 708 IAW AMM 53-00-49-400-801-A03.Nov 13, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511033Seat Track · corrodedLEFT SIDE SEAT RAIL AT STGR 15L IS CORRODED BETWEEN FS 863 AND FS 969. INSTALLED NEW SERVICEABLE LH SIDE SEAT RAIL, P/N SH670-37543-3, BETWEEN FS 863 AND FS 969 IAW CRJ 700 AMM 53-00-49-400-801-A03.Nov 13, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511028Seat Track · corrodedRIGHT SIDE SEAT RAIL AT STGR 15R IS CORRODED BETWEEN FS 379 AND FS 485. INSTALLED SERVICEABLE R/H SIDE SEAT RAIL PN SH670-32233-3 BETWEEN FS 379.00 AND 485.00 IAW AMM 53-00-49-400-801-A03.Nov 13, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260511027Door Sill · corrodedGALLEY SERVICE DOOR LOWER SILL ANGLE IS CORRODED. DRILLED UP AND INSTALLED NEW SERVICEABLE GALLEY SERVICE DOOR LOWER SILL ANGLE IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Nov 6, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20260511023Skin · dentedTHE FUSELAGE SKIN HAS TWO DENTS BETWEEN FS 265 AND FS 280, STGR 27 AND 26L. REPAIRED DENTS IAW REO 670-53-11-2251 REV -- DATED 2026-01-19Oct 30, 2025 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20260511020Hinge · gouged53-21-23-201-007-A01 (PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT) REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007-A01. REMOVED AND REPLACED PAX DOOR FUSELAGE HINGE IAW CRJ-700 SRM'S 53-21-23-201-00Sep 26, 2025 · N512AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2024082811102Warning Message · false indicationIB FLT SPLRS AND IB SPLRNS C MSG IN FLIGHT. / PERFORMED SPOST 1 AND SPOST 2 IAW CRJ 700 AMM 27-61-05-740-801-A03. THIS CLEARED THE FAULT AND HAS NOT RETURNED AT THIS TIME. AIRCRAFT OK FOR RETURN TO SERVICE.Aug 4, 2024 · N512AE · Cndair CL6002C10 · Central WarningSDR VNAA202201111112Acm · smokeSMOKE COMING FROM AIR VENTS WHEN RUNNING LEFT PACK. WHEN L PACK IS ON OUTPUT TEMP INCREASES RAPIDLY AND PRODUCED L PACK AUTOFAIL MESSAGE. / DEFFERED LH PACK AIR CONDITIONING SYSTEM PER MEL 21-51-01-2 CAT- C. OPTION-2- PLACARD INSTALLED. OPTION 2-) / R/R LH AJan 7, 2022 · N512AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA202008209995Seat Track · corrodedRH INBOARD INTERIOR SEAT RAIL BEAM AT FRAME FS549.00 HAS CORROSION. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH CRJ700 SRM 53-00-00-101-001. FABRICATED AND REPAIRED RH INBOARD INTERIOR SEAT RAIL BEAM AT FS549.00Aug 20, 2020 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202008209994Frame · corrodedFUSELAGE FRAME 517.00 CORRODED IN BELLY JUST FORWARD OF FORWARD CARGO DOOR CUTOUT. DETERMINED SUB-FRAME SECTION TO BE CORRODED OUT OF LIMITS PER SRM 53-31-06-101-003.Aug 20, 2020 · N512AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202008209993Intercostal · corrodedPASSENGER ENTRY DOOR CORRODED IN MULTIPLE LOCATIONS OF DOOR STRUCTURE. REPAIRED WITH NEW INTERCOSTALS.Aug 20, 2020 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202008209992Seat Track · corrodedRH OUTBOARD #6 SEAT RAIL HAS NUMEROUS SCRATCHES, GOUGES AND AREA OF CORROSION. EVALUATED RH OUTBOARD #6 SEAT RAIL AND FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH CRJ700 SRM 53-41-49-101-001. REMOVED AND REPLACED RH OUTBOARD #6 SEAT RAIL IN ACCORDANCE WITH CRJAug 20, 2020 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202008209991Seat Track · corrodedLH OUTBOARD #5 SEAT TAIL HAS NUMEROUS SCRATCHES, GOUGES AND AREA OF CORROSION. LH OUTBOARD #5 SEAT TRACK WAS FOUND OUT OF LIMITS.Aug 20, 2020 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2020021531101Relief Valve · failedCREW RECEIVED A L ENG BLEED CAUTION MESSAGE. THIS CAUSED THE CREW TO LOSE A/I ABILITY. THEY WERE INSTRUCTED TO HOLD FOR THE PHL GDP BUT COULD NOT DUE TO ICING CONDITIONS AT THE HOLD POINT. THE CREW DECLARED AN EMERGENCY IN ORDER TO AVOID THE HOLD AND LAND IN PFeb 13, 2020 · N512AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2018111411101Windshield · crackedWHILE AT FL370 THE CA WINDSHIELD CRACKED/SHATTERED. EMERGENCY DECLARED AND DIVERTED IMMEDIATELY TO STL. EMERGENCY EQUIPMENT WERE STANDING BY BUT DID NOT RESPOND. EMERGENCY WAS CANCELED AFTER EXITING THE RUNWAY AND TAXIED TO THE GATE UNDER ITS OWN POWER WITH Nov 14, 2018 · N512AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2018041611101Controller · faultyCREW REPORTED L BLEED DUCT WARNING MESSAGE. FOLLOWED QRH. BOTH BLEED VALVES CLOSED. COMPLIED WITH A RAPID DESCENT. OXYGEN MASKS DEPLOYED. DECLARED EMERGENCY. MAINTENANCE R & R THE AILC. OPS CHECKED GOOD.Apr 16, 2018 · N512AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR VNAA2018040599904Intercostal · corrodedFOUND INTERCOSTAL BS 319 - 333 CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01.Apr 5, 2018 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018040599905Stringer · corrodedSTRINGER 21R BETWEEN BS 349 AND 364 CORRODED. REPLACED THE STRINGER.Apr 5, 2018 · N512AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2018040599903Floorbeam · corrodedBS 280 FLOORBEAM FWD ANGLE IS CORRODED. LOCATED AND DRILLED A NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED THE REPLACEMENT ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01Apr 5, 2018 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018040599902Floorbeam · crackedBS 280 FLOORBEAM ANGLE, RBL 9 CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21-001-001-A01.Apr 5, 2018 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018040599901Floorbeam · crackedBS 280 FLOORBEAM LBL 9 CRACKED. REMOVED THE FITTINGS IAW SRM 51-42-21-001-001-A01.Apr 5, 2018 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018030111101Warning Message · false activationTHE CREW RECEIVED A BLEED DUCT WARNING MESSAGE DURING FLIGHT AND DIVERTED AND DECLARED AN EMERGENCY. MAINTENANCE PERFORMED OPS TEST OF BLEED-AIR DETECTION AND WARNING SYSTEM NO DEFECTS NOTED. PERFORMED LEAK TEST OF BLEED-AIR DISTRIBUTION NO DEFECTS NOTED.Mar 1, 2018 · N512AE · Cndair CL6002C10 · Engine Bleed Air SystemSDR VNAA2017070811102Detector · malfunctionedCREW DECLARED EMERGENCY DUE TO FLAPS FAIL AT 0 WHEN SELECTING FLAPS DURING APPROACH. REPLACED LEFT OUTBOARD AND LEFT INBOARD & OUTBOARD SKEW DETECTOR.Jul 8, 2017 · N512AE · Cndair CL6002C10 · Trailing Flap Position Indicating SystemSDR VNAA2017062711101Control Unit · failedAT FLIGHT LEVEL 190 AND SPEED OF 280 KNOTS GOING INTO CLT THE CREW RECEIVED A FLAP FAIL MESSAGE. THE FLAP LEVER WAS SELECTED AT "0" DEGREES AND THE CREW RAN THE QRH BUT IT DID NOT FIX THE ISSUE. THE CREW DECLARED AN EMERGENCY AT THIS TIME AND THEY LANDED WITH Jun 27, 2017 · N512AE · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR VNAA2016110300005Pseu · faultyGEAR DISAGREE WARNING ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Nov 3, 2016 · N512AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2016100600011Warning Message · false activationAUTO PRESSURIZATION CAUTION MESSAGE DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS IAW THE AMM. OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 6, 2016 · N512AE · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA2016090800002Skin Panel · damagedELONGATED HOLES IN PASSENGER DOOR INNER SKIN PANEL. MAINTENANCE PERFORMED A MAJOR REPAIR BY FABRICATING AND INSTALLING A PASSENGER DOOR INNER SKIN AND PERFORMING CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.Sep 8, 2016 · N512AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2016082800035Doubler · chafedFS 987.0, STR 27 HAS CHAFTED REPAIR DOUBLER. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE CHAFED REPAIR DOUBLER AT FS 987.0, STR 27 AND PERFORMED CHECKS IAW REO 670-53-00-466, REV DATED 8-19-16 AND REO 670-53-00-290, REV D DATED 9-10-15. THE AIRCRAFT WAS RELEAug 28, 2016 · N512AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2016082400028Floorbeam · crackedBS 280 FLOORBEAM LEFT AND RIGHT SIDES CRACKED AT RBL 11 AND LBL 11. MAINTENANCE PERFORMED A MAJOR REPAIR IAW AMM.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2016082400027Bulkhead · corrodedFS 280 BULKHEAD RT AND LT WEBS ARE CORRODED. MAINTENANCE PERFORMED A MAJOR REPAIR TO LT AND RT BULKHEAD WEBS AT FS 280 IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2016082400026Support Angle · corrodedRIGHT NLG JACK FITTING SUPPORT ANGLE CORRODED. MAINTENANCE R & R THE RT NLG JACK FITTING SUPPORT ANGLE AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016081400026Support Angle · corrodedRIGHT NLG JACK FITTING SUPPORT ANGLE CORRODED. MAINTENANCE R & R THE RT NLG JACK FITTING SUPPORT ANGLE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016082400025Support Angle · corrodedLEFT NLG JACK FITTING SUPPORT ANGLE CORRODED. MAINTENANCE R & R THE LT NLG JACK FITTING SUPPORT ANGLE AND PERFORMED CHECKS IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016082400024Seat Track · corrodedRIGHT SIDE SEAT TRACK FROM FS 863.00 TO FS 969.00 IS CORRODED. MAINTENANCE REPLACED SEAT TRACK FROM FS 863.00 TO 969.00 IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Aug 24, 2016 · N512AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2016081800014Door Sill · corrodedSERVICE DOOR LOWER SILL ANGLE CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOOR SILL ASSEMBLY AND PERFORMED CHECKS IAW THE AMM.Aug 18, 2016 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016070200003Pcu · faultyON APPROACH, AILERONS REQUIRED EXCESSIVE ROLL. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT AILERON NR 1 POWER CONTROL UNIT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASEDJul 2, 2016 · N512AE · Cndair CL6002C10 · Aileron Control SystemSDR VNAA2016052600028Spoiler Sys · warning lightOTBD FLIGHT SPOILERS AND OTBD SPOILERONS AMBER MESSAGE APPEARED IN FLIGHT. MAINTENANCE TROUBLESHOT, CYCLED SYSTEM CIRCUIT BREAKERS, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.May 26, 2016 · N512AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20151005003Web · crackedLEFT FWD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED APPROX 1/4". REPAIRED LT FWD EQUIPMENT COMPARTMENT FLOOR WEB IAW ETN-CR-53-099.Oct 5, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151005002Support Bracket · crackedFORWARD EQUIPMENT COMPARTMENT JB6 SUPPORT BRACKET IS CRACKED APPROX 3/8". R & R FWD EQUIPMENT COMPARTMENT JB6 SUPPORT BRACKET IAW SRM 51-42-06.Oct 5, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151005001Web · crackedRIGHT FWD EQUIPMENT COMPARTMENT FLOOR WEB IS CRACKED APPROX 1/2". COMPLIED WITH REPAIR OF RT FWD EQUIPMENT BAY FLOOR IAW ETN CR-53-099.Oct 5, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150930006Duct · crackedRIGHT INBD FLAP SLAT, TELESCOPIC DUCT CRACKED ON INBD SIDE AT WELD FOR CLOSING PLATE BRACKET. R & R TELESCOPIC DUCT IAW AMM 30-11-10-400-801.Sep 30, 2015 · N512AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR SIMA20150930005Bracket · crackedLEFT TEE BRACKET AT BL 9.04 ATTACHED TO CROSSBEAM FS 280.00 IS CRACKED. R & R LT TEE BRACKET AT BL 9.04 ATTACHED TO CROSSBEAM FS 280.00 IAW SRM 53-11-41.Sep 30, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150930004Bracket · crackedRIGHT TEE BRACKET AT BL 9.04 ATTACHED TO CROSSBEAM FS 280 IS CRACKED. R & R TEE BRACKET AT BL 9.04 ATTACHED TO CROSSBEAM FS 280.00 IAW SRM 53-11-41.Sep 30, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150924006Structure · corrodedFS 295 IS CORRODED, BETWEEN STRINGER 27 & 26R. REPAIRED FS 295, BETWEEN STRINGER 27 - 26R IAW SRM 51-21-06.Sep 24, 2015 · N512AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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