N518AE

Service difficulty reports · 160

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 = 'N518AE' 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 VNAA202210281112None · crackedL WINDOW CRACKED IN FLIGHT ALONG WITH ARCING AT LOWER EDGE / REMOVED AND REPLACED L/H CAPT WINDOW IAW CRJ 700 AMM 56-12-01-000/400-801-A01-PSA REV D UP TO PG 7 STEP 28. PERFORMED RESISTANCE CHECK BETWEEN TEMPERATURE SENSORS PRIOR TO INSTALL. (S1-S2)-299OHMS, (Oct 20, 2022 · N518AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA202208051111Hand Rail · corrodedEXFOLIATION CORROSION FOUND ON RH UPPER DOOR HANDRAIL MOUNT / PERFORMED LPI OF ALL CUT LINES AND EDGES PER REO 670-52-11-848 STEP 2 IAW CRJ NDT 51-20-008-230. NO DEFECTS NOTED. COMPLIED WITH REO 670-52-11-848, REPAIR TO PAX DOOR (PHASE IV) STAIR FWD & AFT SIDAug 2, 2022 · N518AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202103021111Unknown · odorCREW REPORTED AN NOXIOUS FUMES/ODOR IN THE CABIN WHEN SHUTTING DOWN THE ENGINE AND STARTING THE APU. MAINTENANCE NOTIFIED AND STATION PERSONNEL ALSO REPORTED SMELLING A STRANGE ODOR ON THE AIRCRAFT. MAINTENANCE HAS BEEN NOTIFIED AND WILL INSPECT THE AIRCRAFT IFeb 27, 2021 · N518AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202011051111Windshield · crackedON APPROACH INTO CLT THE RT SIDE WINDSHIELD CRACKED. REMOVED AND REPLACED RT SIDE WINDSHIELD, IAW CRJ700 AMM 56-11-01-400-801. OPERATIONS CHECK AND LEAK CHECK GOOD.Nov 24, 2020 · N518AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2020082711102Wire Harness · failedWHILE ARRIVING IN CLT FLIGHT 5334 RECEIVED A NOSE STEERING INOP CAUTION MESSAGE. CREW DECLARED EMERGENCY AND LANDED SAFELY IN CLT. CREW THEN DID A SYSTEM RESET WITH MX AND WAS ABLE TO TAXI TO THE GATE WITH NO FURTHER ISSUES. R&R STEERING WIRING HARNESS ASSY, OAug 23, 2020 · N518AE · Cndair CL6002C10 · Landing Gear System WiringSDR VNAA2020082011104Warning Message · false activationSTEERING INOP CAUTION MSG ON FINAL, FULLY CONFIGURED FOR LANDING. PERFORMED OPERATION TEST OF NWS. OPS CHECK GOOD AT THIS TIMEAug 19, 2020 · N518AE · Cndair CL6002C10 · Central WarningSDR VNAA2020070211103Battery Pack · dischargedCURVED EXIT SIGN ON RT SIDE OF CABIN OVER THE MOUSTACHE CURTAIN WILL NOT ILLUMINATE. MX REMOVED AND REPLACED NR 2 EPSU BATTERY PACK IAW AMM. OPS CHECKS GOOD AT THIS TIME.Jul 1, 2020 · N518AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019111899903Stringer · corrodedSTR 26R BETWEEN FS 1031 AND FS 1047 IS CORRODED. EVALUATED AREA FS 1031-FS 1047 STR STRINGER FOUND TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-61-03-101-003-A01. STR 26 REQUIRES REPAIR IAW CRJ 700 SRM 53-00-03-201-001-A01. 2. REPAIRED STRINGER 26R IAW CRJ 700 SRMNov 18, 2019 · N518AE · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR VNAA2019071111101Windshield · crackedON APPROACH INTO PHL, AT FL060 CA'S WINSHIELD SHATTERED. UNKOWN CAUSE. EMERGENCY DECLARED AND TRUCKS ROLLED. CABIN DID NOT BRACE. FLIGHT LANDED ON RWY 27R WITHOUT FURTHER INCIDENT AND WAS ABLE TO TAXI TO THE GATE UNDER OWN POWER. MX REPLACED CAPT WINDSHIELD. Jul 11, 2019 · N518AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2019050211101Light · inoperativeEMERGENCY FLOOD LIGHT ABOVE ROWS 13 & 14 INOP. R/R EMERG CEILING FLOOD LIGHT IAW AMM 33-51-09-000/400-801. OPS CK GOOD.May 2, 2019 · N518AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2018122211101Warning Message · illuminatedAFTER T/O, CREW REPORTED A GEAR DISAGREE, LANDED WITHOUT ISSUE. ORF REPLACED THE GEAR SELECTOR VALVE.Dec 22, 2018 · N518AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2018112611101Fitting · looseDURING APPROACH THE CREW RECEIVED A NOSE WHEEL STEERING MSG. AS A PRECAUTION THEY DECLARED AN EMERGENCY WITH CLT ATC. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND WAS ABLE TO TAXI TO THE GATE ON ITS OWN POWER. SYS 3 LINE LEAKING. TIGHTENED FITTING.Nov 26, 2018 · N518AE · Cndair CL6002C10 · Hydraulic System, MainSDR VNAA2018112011101Strut · lowAFTER TAKEOFF THE NLG WOULD NOT RETRACT / GEAR DISAGREE. THE AIRCRAFT RETURNED TO FIELD AND MAINTENANCE COMPLETED A FULL SERVICE OF NLG STRUT. OPS CHECK GOOD.Nov 20, 2018 · N518AE · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR VNAA2018111311102Pseu · faultyAFTER TAKEOFF THE NLG WILL NOT RETRACT. THE AIRCRAFT RETURNED TO FIELD AND MAINTENANCE REPLACED THE PSEU OPS GOOD.Nov 13, 2018 · N518AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2018060699906Floor Support · corrodedPAX DOOR LOWER FLOOR SUPPORT WAS CORRODED. DRILLED, AND LOCATED A NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01.Jun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018060699905Strap · chafedINNER UPPER FRAME STRAP AT BS 349, STRINGER 3L WAS CHAFED. .025 INCH DEEP AT THE TOP AFT FASTENER. THE LOCK FASTENER HEAD IS ALSO CHAFED. REMOVED DAMAGED INNER UPPER FRAME STRAP IAW SEM 51-42-21-001-001-A01, LOCATED, DRILLED, AND INSTALLED A NEW STRAP IAJun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2018060699904Frame · corrodedFRAME WAS CORRODED AT BS 645, BETWEEN STRINGER 26L AND 26R. COMPLIED WITH REO 670-53-31-437.Jun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2018060699903Angle · crackedBS 280 FLOORBEAM LBL 9 - RBL 9 OTBD ANGLE WAS CRACKED. PERFORMED SB 670BA-53-041.Jun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018060699902Angle · corrodedBS 280 FLOORBEAM FWD SUPPORT ANGLE WAS CORRODED. PERFORMED SB 670BA-53-041.Jun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2018060699901Crossbeam · corrodedBS 280 CROSSBEAM WAS CORRODED AND CRACKED, BETWEEN LBL 12 AND RBL 12. PERFORMED SB 670BA-53-041.Jun 6, 2018 · N518AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2018032111102Warning System · false activationDURING APPROACH THE CREW RECEIVED AN IB FLT SPLRS/IB SPLRONS CAUTION MSG. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. TRUCKS ROLLED. A/C TAXIED TO GATE WHERE MX MET THEM FOR A SUCCESSFUL SYSTEM RESET.Mar 21, 2018 · N518AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2017021400023Selector · inoperativeGEAR DISAGREE WARNING MESSAGE. REMOVED AND REPLACED THE LANDING GEAR SELECTOR.Feb 14, 2017 · N518AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2017021400021Electronic Unit · faultedGEAR DISAGREE WARNING MESSAGE. REMOVED AND REPLACED THE PROXIMITY SENSOR ELECTRONICS UNIT.Feb 14, 2017 · N518AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2017021100014Warning Message · illuminatedGEAR DISAGREE MESSAGE IN FLIGHT.Feb 11, 2017 · N518AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2017020600011Warning Message · illuminatedGEAR DISAGREE WARNING MESSAGE ON CLIMB OUT.Feb 6, 2017 · N518AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2017020100001Selector Valve · malfunctionedGEAR DISAGREE WARNING WITH NOSEWHEEL THUMPING. REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE.Feb 1, 2017 · N518AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2017011700023Baffle · unsecureFOUR INCHES OF TRANS COWL BAFFLE HANGING OUT OF THE LEFT ENGINE COWLING. REMOVED BAFFLING AND PERFORMED REO 670-54-21-1044.Jan 17, 2017 · N518AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA2017011500018Sensor · out of adjustSERVICE DOOR CAUTION MESSAGE DURING CLIMB OUT. ADJUSTED SENSOR PX38.Jan 15, 2017 · N518AE · Cndair CL6002C10 · Service DoorsSDR VNAA2016121000014Cover · loosePLASTIC FLOOR SEAT TRACK COVER ON SEAT 15 AC WILL NOT STAY SECURED. RESECURED SEAT TRACK.Dec 10, 2016 · N518AE · Cndair CL6002C10 · Passenger Compartment EquipmentSDR VNAA2016091300013Light · inoperativeFORWARD AND AFT OVERHEAD EMERGENCY LIGHTS INOPERABLE. MAINTENANCE INSPECTED, RELAMPED FORWARD AND AFT OVERHEAD EMERGENCY LIGHTS AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Sep 13, 2016 · N518AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2016080600006Floorbeam · corrodedRIGHT HAND FLOORBEAM ANGLE AT FS 280 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAM ANGLE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 6, 2016 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2016080300004Skin · chafedMAINTENANCE DISCOVERED OUTER SKIN AT FS 985 WAS CHAFED FROM CONTACT WITH BELLY FAIRING. THE SKIN WAS REPAIRED IAW REO 670-53-00290, REVISION D.Aug 5, 2016 · N518AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2016072500028Web · corrodedFS 280 RT AND LT WEBS CORRODED. MAINTENANCE REPAIRED FS 280 RT AND LT WEBS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.Jul 25, 2016 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016072500027Crossbeam · corrodedFS 280 CROSSBEAM HAS CORROSION. MAINTENANCE R & R FS 280, RT AND LT CROSSBEAM IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Jul 25, 2016 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016072400025Angle · corrodedFS 280 FORWARD J-ANGLE CORRODED AROUND CAMLOCK RECEPTACLE. MAINTENANCE R & R FS 280.00 FORWARD J-ANGLE IAW THE AMM. THE ACFT CONTINUES HEAVY CHECK MAINTENANCE.Jul 24, 2016 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016072400024Frame · corrodedBS 280 RIGHT AND LEFT FLIGHT DECK CUTOUTS CORRODED. MAINTENANCE REPLACED GUSSETS, ANGLES AND REMOVED SURFACE CORROSION IAW THE AMM. TJul 24, 2016 · N518AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016012600026Controller · malfunctionedCREW REPORTED RT PACK CAUTION MESSAGE ILLUMINATED IN FLIGHT, CREW RETURNED TO FIELD. MAINTENANCE TROUBLESHOT, SWAPPED AIR-CONDITIONING SYS CONTROLLERS AND PERFORMED CHECKS IAW THE AMM. ACFT RELEASED FOR SERVICE.Jan 26, 2016 · N518AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2015122400015Position Sensor · failedCREW REPORTED OVERSPEED WARNING AT 230 KTS WITH SLATS AND FLAPS AT ZERO DEGREES. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT SLAT BRAKE POSITION SENSOR UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Dec 24, 2015 · N518AE · Cndair CL6002C10 · Leading Edge Slat Position Indicating SystemSDR SIMA20150806005Stringer · corrodedMAIN AVIONICS COMPARTMENT STRINGER 26R IS CORRODED, BETWEEN FS 333 & 349. COMPLETED INSTALLATION OF LT FS 280.00 CROSSBEAM IAW SRM 53-11-41.Aug 6, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150803007Stringer · corrodedMAIN AVIONICS COMPARTMENT UNDERFLOOR, STRINGER 25RT IS CORRODED, BETWEEN FS 319.70 & FS 333.00. R & R MAIN AVIONICS COMPARTMENT UNDERFLOOR, STRINGER 25RT IAW SRM 51-42-06.Aug 3, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150803006Stringer · corrodedMAIN AVIONICS COMPARTMENT UNDERFLOOR STRINGER 26RT IS CORRODED, BETWEEN FS 319.70 & FS 333.00. COMPLIED WITH R & R STRINGER 26R IAW SRM 51-42--06.Aug 3, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150802004Structure · crackedRIGHT LOWER TRANS COWL OTBD JOINT EXTRUSION IS CRACKED. R & R RT LOWER TRANS COWL OTBD JOINT EXTRUSION IAW ETN-CR-54-015R1.Aug 2, 2015 · N518AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20150802003Fairing · crackedWHEEL BIN FAIRING IN FORWARD SECTION OF THE LEFT MAIN LANDING GEAR WHEEL WELL IS CRACKED 1 INCH. R & R FAIRING LOCATED IN THE LEFT MAIN LANDING GEAR WHEEL WELL IAW AMM 53-83-85.Aug 2, 2015 · N518AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20150802002Fairing · crackedWHEEL BIN FAIRING IN FORWARD SECTION OF RIGHT MAIN LANDING GEAR WHEEL WELL IS CRACKED 3/8 OF AN INCH & ATTACHING NUTPLATE IS LOOSE. R & R FAIRING IN THE RIGHT MAIN LANDING GEAR WHEEL WELL IAW AMM 53-83-85.Aug 2, 2015 · N518AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20150801004Attach Angle · crackedATTACH ANGLE ON THE FWD SIDE OF THE LT COCKPIT BULKHEAD ATTACHING TO THE FLOORBEAM AT FS 280.00 IS CRACKED, APPROX .500 INCHES, LOCATED BETWEEN LBL 18.00 & 27.00. INSTALLED NEW ATTACH ANGLE ON FWD SIDE OF BULKHEAD AT FS 280.00, BETWEEN LBL 18.00 & 27.00 IAW SAug 1, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20150730009Floorbeam · crackedFLOORBEAM AT FS 280.00 IS CRACKED, APPROX 1" ON UPPER FLANGE, OTBD OF RBL 9.00. COMPLETED INSTALLATION OF RT FS 280.00 CROSSBEAM IAW SRM 51-42-21.Jul 30, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20150730008Floorbeam · crackedFLOORBEAM AT FS 280.00 IS CRACKED, APPROX 2 " ON UPPER FLANGE OTBD OF LBL 9.00. COMPLETED INSTALLATION OF LT FS 280.00 CROSSBEAM IAW SRM 51-42-21.Jul 30, 2015 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20150712003Light · inoperativeLEFT AFT EXTERIOR EMER LIGHT INOPERATIVE. LT AFT EXTERIOR EMER LIGHT DEFERRED. REPLACED LAMP IN LT AFT EXTERIOR EMER LIGHT ASSEMBLY IAW AMM 33-51-15. OPERATIONS CHECKED OK. MEL RESTORED.Jul 12, 2015 · N518AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20150712004Light · inoperativeLEFT FWD EXTERIOR EMER LIGHT INOPERATIVE. LT FWD EXTERIOR EMER LIGHT DEFERRED. REPLACED LAMP IN LT FWD EXTERIOR EMER LIGHT ASSEMBLY IAW AMM 33-51-15. OPERATIONS CHECKED OK. MEL RESTORED.Jul 12, 2015 · N518AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20150610001Unknown · odorDURING PUSH, NR 2 FLIGHT ATTENDANT REPORTED BURNING AROMA ROWS 10 - 11. ODOR EXPANDED TO ROWS 8 - 12 THEN WAS ONLY NOTICEABLE AROUND ROW 10 BY RTG TIME. PERFORMED FIM TASK 21-22-00 & OPERATIONS CHECK OF AIR CONDITIONER SYS IAW AMM 21-51-00. REPLACED CEILINJun 10, 2015 · N518AE · Cndair CL6002C10 · Air Distribution System
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