N514AE

Service difficulty reports · 135

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 = 'N514AE' 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 VNAA20250525015Skin · dentedDENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40. DENT ON LOWER SKIN OF LH INBOARD FLAP BTW FLS92.80 TO FLS101.40 WAS REPAIRED PER REO 670-57-52- 605. REV. - -.Mar 29, 2025 · N514AE · Bombdr CL6002D15 · Trailing Edge FlapsSDR VNAA20250525014Skin · dentedDENTS (6EAS) ON FUSELAGE SKIN LOCATED BTW FS349/ FS421 AND STGR18R / STGR19R. PREVIOUS BLEND OUT ON AREA (1 EA) BTW FS 364 TO FS349 STGR 18R TO STGR 19R AND AREAS (3 EAS) BTW FS379 TO FS 394 STGR18R TO STGR 19R WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53Mar 28, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA20250525012Skin · wornPROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R. PROTUBERANCE ON FUSELAGE SKIN LOCATED BTW FS1000 / FS1015 AND STGR1R / STGR2R WAS REPAIRED PER REO 670-51-00-085 REV - A AND PER REO 670-53-61-2496 REV. - .Mar 28, 2025 · N514AE · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR VNAA2024121311102Windshield · smokeCLIMBING THROUGH 1000FT, RECEIVED A LH WINDSHIELD HEAT CAUTION MSG AND BEGAN TO SMELL FUMES. A LITTLE BIT OF SMOKE PUFFED FROM THE LH WINDSHIELD TERMINAL BLOCK. SMOKE AND FUMES WENT AWAY AFTER THE HEAT WAS TURNED OFF. THE LOCATION OF THE FUMES WAS THE COCKPIT Nov 25, 2024 · N514AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2024110511103Filter · dirtyBURNING SMELL IN COCKPIT DURING FLIGHT. TURNED OFF UNNECESSARY LIGHTING, SMELL DISSIPATED. / INVESTIGATED SMOKE SMELL IN COCKPIT IAW CRJ 700 FIM 21-21-00-810-806. COULD NOT REPLICATE. FOUND DIRTY FLIGHT COMPARTMENT DISPLAY COOLING AIR FILTER. REMOVED AND REPLNov 2, 2024 · N514AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2024010611101Unknown · unknownAFTER LANDING AND STARTING THE APU, VERY STRONG FUEL SMELL IN COCKPIT AND PAX CABIN / REMOVED AND REPLACED APU IAW CRJ 700 AMM 49-10-00-000/400-801-A02-PSA. OPS CHECK GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME, NO FUEL SMELL PRESENT IN AIRCRAFT AT THIS TIDec 31, 2023 · N514AE · Cndair CL6002C10 · APU Engine Fuel and ControlSDR VNAA2023101111101Unknown · unknownAFTER LANDING TOWER OBSERVED SIGNIFICANT SMOKE COMING FROM RIGHT ENGINE. FIRE TRUCK ALSO SAW FUEL LEAKING FROM DRAIN TUBE LEAVING LARGE SPOT. INSPECTED AND FOUND RH ENGINE SCVGA ROD END HOSE LOOSE AND LEAKING. RETORQUED AND PERFORMED WET MOTOR AND ENGINE EXTEROct 8, 2023 · N514AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA202210061112None · unserviceableSTEERING INOP IN FLIGHT (AFTER GEAR EXTENSION). TROUBLESHOOT B1 CODE 006931 IAW CRJ 700 FIM 32-51-01-810-802-A01 FOUND PILOT HANDWHEEL CONTROLLER TO BE FAULTY. REMOVED AND REPLACED PILOT HANDWHEEL CONTROLLER IAW CRJ 700 AMM 32-51-01-000/400-801-A01. OP CHECKEOct 4, 2022 · N514AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA202206191111Elevator System · out of adjustDURING CLIMBOUT OUT OF SGF THE ELEVATOR SPLIT CAUTION MSG OCCURRED AT APPROXIMATELY 9,000 TO 10,000 FT. THE CREW RAN THE QRH AND HELD TO BURN FUEL BEFORE LANDING FOR STRUCTURAL CONCERNS. THE A/C DID NOT LAND OVERWEIGHT AND THE PAX DID NOT BRACE FOR LANDING. EMJun 15, 2022 · N514AE · Cndair CL6002C10 · Elevator Tab Control SystemSDR VNAA202201241111Warning Message · false activationCREW RECEIVED A SLATS FAIL CAUTION MESSAGE. THEY DECIDED TO GO AROUND AND CONSULT THE QRH. UPON LANDING THE FLAPS DEPLOYED BUT THE SLATS DID NOT. SLATS FAIL CAUTION MESSAGE WHEN LOWERING FLAPS TO 8 DEGREES MSG DID NOT GO AWAY DURING QRH PROCEDURE HAPPENDED DURJan 20, 2022 · N514AE · Cndair CL6002C10 · Leading Edge Slat Control SystemSDR VNAA2020052111101Charger · failedLH OVERWING EMERGENCY EXIT SIGN FWD OF DOOR INOP. MX REMOVED AND REPLACED #3 EPSU BATTERY CHARGER IAW CRJ700 AMM. OPS CHECK GOOD AT THIS TIME.May 19, 2020 · N514AE · Cndair CL6002C10 · Emergency LightingSDR VNAA202004069994Intercostal · corroded3 INTERCOSTALS BETWEEN FS.349 AND FS.364 BETWEEN STGR 25L AND STGR 26R ARE CORRODEDApr 6, 2020 · N514AE · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA202004069993Frame · corrodedFUSELAGE FRAME FS.333 BETWEEN STGR26R AND STGR 26L IS CORRODED.Apr 6, 2020 · N514AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202004069992Stringer · corrodedSTRINGER 26R IS CORRODED AT RIVETS BETWEEN RS295 AND FS310Apr 6, 2020 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA202004069991Stringer · corrodedSTRINGER 25R IS CORRODED AT RIVSTS BETWEEN FS 319.70 AND FS.333Apr 6, 2020 · N514AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA202004059991Angle · crackedPNL 196DR AT STRUCTURAL ANGLE IS CRACKED.REMOVED AND REPLACED DAMAGED AFT STRUCTURAL SUPPORT ANGLE AND STRAP IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-40-11-001-001-A01.Feb 5, 2020 · N514AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202004059992Intercostal · corrodedREMOVED LEFT AND RIGHT JACK PAD INTERCOSTALS IAW CRJ700 SRM 51-42-21-001-001-A01. INSTALLED NEW INTERCOSTALS CC670-32179-1, CC670-32179-2 IAW CRJ700 SRM 51-42-21-001-001-A01.Feb 5, 2020 · N514AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019040651102Access Panel · detachedON CLIMBOUT OUT, #3 HYDRAULIC ACCESS PANEL 195AB DEPARTED THE A/C. THE A/C CONTINUED TO DESTINATION WHERE THE CREW DISCOVERED THE PANEL WAS MISSING. THE A/C FERRIED WHERE MX PERFORMED A DETAILED INSPECTION. MX REWORKED DAMAGED AREA AND REPLACED MISSING PANELApr 5, 2019 · N514AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2017020200004Guide · loosePASSENGER DOOR WILL NOT OPEN. REMOVED AND INSTALLED PASSENGER DOOR AFT ANCHOR FITTING GUIDE SHAFT AND SWIVEL LEVER.Feb 2, 2017 · N514AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2017012600035Manifold · defectiveSTEERING INOPERATIVE CAUTION MESSAGE. REMOVED AND REPLACED THE STEERING MANIFOLD.Jan 26, 2017 · N514AE · Cndair CL6002C10 · Steering UnitSDR VNAA2017012000027Door Frame · corrodedPASSENGER DOOR FORWARD FORMER AT BS 311.75 IS CORRODED UNDER PANEL 832FL. REMOVED AND REPLACED FORWARD FORMER.Jan 20, 2017 · N514AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2017012000026Skin · corrodedPASSENGER DOOR IS CORRODED ON THE INNER SKIN UNDER PANELS 832EL, 832BL, 832FL, 832HL, AND 832DL INNER SKIN HAS MULTIPLE AREAS OF CORROSION ON OUTER AND INNER SURFACES. REMOVED, FABRICATED AND INSTALLED INNER SKIN.Jan 20, 2017 · N514AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2017011600020Attach Angle · corrodedSERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACH ANGLES ARE CORRODED. REMOVED AND REPLACED THE ATTACH ANGLES.Jan 16, 2017 · N514AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2017011300012Door Sill · corrodedCARGO DOOR SILL IS CORRODED BETWEEN BS 1000 AND 1047. REMOVED AND REPLACE CARGO DOOR SILL.Jan 13, 2017 · N514AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2017011200011Attach Angle · corrodedSERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACHMENT ANGLES CORRODED. REMOVED AND REPLACED SERVICE DOOR STEP PLATE SUPPORT BRACKET ATTACHMENT ANGLES.Jan 12, 2017 · N514AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2017011200010Angle · corrodedSERVICE DOOR SILL LOWER MOUNTING ANGLE IS CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL LOWER MOUNTING ANGLE.Jan 12, 2017 · N514AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016091100009Bellows · leakingCLIMBING OUT OF 24500, THE CREW RECEIVED A RT RED BLEED DUCT CASS MESSAGE FOLLOWED BY AN AMBER RT DUCT BLEED MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LEAKING BELLOWS AND PERFORMED CHECKS IAW THE AMM. THSep 11, 2016 · N514AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2016081800021Sign · malfunctionedCABIN OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE INSPECTED, CYCLED SYSTEM SWITCH AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 18, 2016 · N514AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2016061100017Acm · odorLEFT PACK HIGH TEMP AND BURNING ELECTRICAL ODOR IN COCKPIT. MAINTENANCE TROUBLESHOT, DEFFERED THE LT PACK AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE. MAINTENANCE R&R LT ACM IAW AMM, OPS CHECK GOOD, LEAK CHECK GOOD. MEL CLEARED.Jun 11, 2016 · N514AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2015112900020Motor · failedAFTER TAKEOFF, CREW REPORTED CAPTAIN’S WINDSHIELD WIPER WOULD NOT STOP. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT WINDSHIELD WIPER MOTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Nov 29, 2015 · N514AE · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR VNAA2015112200010Controller · malfunctionedUPON CLIMB AT APPROXIMATELY 22,000 FT, CREW NOTICED SPARK ON RT WINDSHIELD AND SHORTLY AFTER GOT A RT WINDSHIELD HEAT MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMEDNov 22, 2015 · N514AE · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR VNAA2015112200009Windshield · sparksUPON CLIMB AT APPROXIMATELY 22,000 FT, CREW NOTICED SPARK ON RT WINDSHIELD AND SHORTLY AFTER GOT A RT WINDSHIELD HEAT MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RNov 22, 2015 · N514AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2015102600022Check Valve · brokenCREW REPORTED LT ENGINE DEGRADED MESSAGE FOLLOWED BY LT ENGINE FLAMEOUT AT FL 360. CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, R & R LT ENGINE 6TH STAGE BLEED AIR CHECK VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOROct 26, 2015 · N514AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SIMA20150822004Skin · gougedFUSELAGE EXTERIOR SKIN IS GOUGED, BETWEEN FS 969.00 - 985.00 ALONG STRINGER 27. REPAIRED FUSELAGE EXTERIOR SKIN GOUGE IAW ERS-CR-53MR-1599.Aug 22, 2015 · N514AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20150707002Ballast · faultyELECTRICAL BURN SMELL IN GALLEY. R & R GALLEY LIGHTING BALLAST PS88 & PS89 IAW AMM CH 33-26-03. OPERATIONS CHECKED GOOD.Jul 7, 2015 · N514AE · Cndair CL6002C10 · Passenger Compartment LightingSDR SIMA20150316001Flashlight · defectiveAFT FLIGHT ATTENDANT FLASHLIGHT WILL NOT STAY IN CRADLE. R & R AFT EMER FLASHLIGHT ASSEMBLY IAW AMM 25-61-02.Mar 16, 2015 · N514AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20150130001Unknown · malfunctionedAT FL 230 GOT CABIN A/T ON EO2 COMPLIED WITH POMI PROCEDURES DESCENDED TO FL 100 COULD NOT CONTROL. CABIN ALTITUDE CONTINUED FLIGHT UNPRESSURIZED. COMPLIED WITH PRESSURIZATION CHECK IAW AMM 21-31-00. NO DEFECTS NOTED. OPERATIONS CHECKED GOOD.Jan 30, 2015 · N514AE · Cndair CL6002C10 · Cabin Pressure Control SystemSDR SIMA20141109005Unknown · smokeON LANDING EXCESSIVE SMOKE REPORTED BY TOWER FROM LT MLG. INSPECTED MLG & DOOR IAW AMM CH 32-10-00, NO DEFECTS NOTED.Nov 9, 2014 · N514AE · Cndair CL6002C10 · Main Landing GearSDR SIMA20141001004Cradle · brokenFORWARD CABIN FLASHLIGHT CRADLE BROKEN. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.Oct 1, 2014 · N514AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140404001Ecu · failedSTEERING INOPERATIVE IN FLIGHT. R & R ECU IAW AMM 37-51-10. PERFORMED OPERATIONS CHECK OF RVDT RIGGING IAW AMM 32-50-00. OPERATIONS CHECKED GOOD. STEERING INOPERATIVE MSG CLEARED. .Apr 4, 2014 · N514AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA20140127006Warning System · false activationDECLARED EMERGENCY LG ISSUE FLIGHT CXL. DURING MAINTENANCE INSPECTION ON FLIGHT 3313 FOUND EICAS GEAR DISAGREE ON TAKEOFF. AIRCRAFT WAS REMOVED FROM SERVICE. COMPLY WITH THE EXTENSION AND RETRACTION OF THE LANDING GEAR. COULD NOT DUPLICATE FAULT. OPS CHECJan 27, 2014 · N514AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR SIMA20131122004Bracket · defectiveFIRST OFFICER`S FLASHLIGHT WILL NOT STAY IN CRADLE. R & R FIRST OFFICER`S FLASHLIGHT BRACKET IAW CRJ MM 25-61-02, OPERATIONS CHECKED GOOD.Nov 22, 2013 · N514AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20131010003Drag Angle · crackedRT VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE HAS 1 INCH CRACK ALONG L/E OF ANGLE. REPAIRED THE RT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IAW EO CR-53MR-164R1 PART B.Oct 10, 2013 · N514AE · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20131010002Drag Angle · crackedLEFT VERTICAL STABILIZER TO FUSELAGE FWD DRAG ANGLE HAS A 1.5 INCH CRACK ALONG T/E OF ANGLE. LT VERTICAL STAB TO FUSELAGE FWD DRAG ANGLE REPAIRED IAW EO CR-55MR-038.Oct 10, 2013 · N514AE · Cndair CL6002C10 · Vertical Stabilizer, Attach FittingsSDR SIMA20131007002Floorbeam · crackedFOUND FLOORBEAM AT FS 280 CRACKED ON LT AND RT SIDES. REPLACED FLOORBEAM IAW SRM 51-42-06. AIRCRAFT RETURNED TO SERVICE.Oct 7, 2013 · N514AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20131007003Angle · crackedLEFT INBD FLOORBEAM ANGLE AT FS 280 CRACKED. FABRICATED REPAIR IAW EO 53EP-115. AIRCRAFT RETURNED TO SERVICE.Oct 7, 2013 · N514AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20131001004Handle · tornRT OVERWING EMERGENCY EXIT CENTER HANDLE HAS A TEAR IN IT. R & R RT OVERWING EMERGENCY EXIT CENTER HANDLE IAW AMM 25-26-09.Oct 1, 2013 · N514AE · Cndair CL6002C10 · Emergency ExitsSDR SIMA20131001003Light · inoperativeLT AFT SECTON OF AISLE EMERGENCY FLOOR PROXIMITY STRIP IS CRACKED. R & R THE LT AFT SECTION OF AISLE EMERGENCY FLOOR PROXIMITY STRIP IAW AMM 33-51-01-400-801 AND ETN CR-33-004.Oct 1, 2013 · N514AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130817003Electrical Sys · overheatedFOUND STRONG ODOR OF ELECTRICAL SMOKE IN COCKPIT. OVERTEMP MESSAGE DISPLAYED ON ED 1 AND ED 2, CIRCUIT BREAKER C9 WAS FOUND TO BE TRIPPED. CIRCUIT BREAKER E-14 WAS ALSO TRIPPED. ACFT WAS SUSPECTED TO BE POWERED FOR 15 PLUS HOURS WITH NO AIR CONDITIONING PACK Aug 17, 2013 · N514AE · Cndair CL6002C10 · Electrical Power SystemSDR SIMA20130713004Control Unit · failedTHE CREW REPORTED THAT DURING THE CLIMB THEY RECEIVED A STALL FAIL AND SLATS FAIL CAUTION MESSAGE. THE CREW COMPLIED WITH AOM VOL 1 PROCDURES AND DECLARED AN EMERGENCY. THE CREW RETURNED TO ORD AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. Jul 13, 2013 · N514AE · Cndair CL6002C10 · Leading Edge Slat Control System
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