N507AE

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 = 'N507AE' 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 VNAA2021113099912Stringer · corrodedSTINGER 20R CORRODED BETWEEN FS 379 AND FS 394.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2021113099911Stringer · corrodedSTRINGER 19R CORRODED BETWEEN FS 394 AND FS 409.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2021113099910Seat Track · corrodedSEAT TRACK AT RBL27 BEGINNING AT APPROX FS923.00  CORRODEDNov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202111309999Seat Track · corrodedSEAT TRACK AT RBL9 BEGINNING AT APPROX FS830.00Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202111309998Seat Track · corrodedSEAT TRACK AT LBL9 BEGINNING AT APPROX FS830.00 CORRODEDNov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202111309997Angle · bentFS280.00 BULKHEAD RH AFT FACE 2ND, 4TH, 5TH, AND 7TH FROM TOP REINFORCEMENT ANGLES BENT.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202111309996Angle · bentFS280.00 BULKHEAD LH AFT FACE TOP, 5TH AND 6TH FROM TOP, AND BOTTOM REINFORCEMENT ANGLES BENT.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202111309995Seat Track · corrodedRH FLOOR SEAT TRACK CORRODED AT RBL 9 BETWEEN FS 677- FS 830. RH FLOOR SEAT TRACK CORRODED BETWEEN FS 830-FS 969 AT RBL 9. LH FLOOR SEAT TRACK AT LBL 9 CORRODED BETWEEN FS 830-FS 969.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202111309994Stringer · corrodedSTRINGER 20R CORRODED BETWEEN FS 421 AND FS 453.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202111309993Stringer · corrodedCORROSION AT FS 549.00 FROM STGR 26L TO STGR 26R (FRAME)Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202111309992Door Sill · corrodedR/H FLOOR SILL UPPER SURFACE RBL 45.0 FS 287.00 HAS AREA OF MINOR CORROSION.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202111309991Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED BETWEEN FS 1000 AND FS 1047.Nov 30, 2021 · N507AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202104271114Proximity Switch · failedON APPROACH INTO TYS, THE CREW RECEIVED A PAIR OF SPOILER WARNINGS (INBOUND GROUND AND GROUND SPOILER DEPLOY). THEY RAN THE QRH, AND THE DEPLOY WARNING REQUIRED THEM TO LAND WITH FLAPS 20. THE CAPTAIN DECLARED A MAINTENANCE EMERGENCY AT FL050 FOR PRECAUTIONARYApr 26, 2021 · N507AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA202101241111Controller · failedLH WINDSHIELD CRACKED/ARCING WITH HEAT ON. LH WINDSHIELD CRACKED IN DESCENT, SUBSEQUENT WINDSHIELD HEAT CAUTION MESSAGE. REMOVED AND REPLACED LH WINDSHIELD IAW AMM 56-11-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED LH WINDSHIELD HEAT Jan 21, 2021 · N507AE · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR VNAA202101201111Adc · failedDURING CLIMB, RECEIVED ADC 2 FAIL MESSAGE. FLIGHT RETURNED TO CLT. NO EMERGENCY DECLARED. FLIGHT LANDED ON RWY 18R AND RETURNED TO GATE 31 WITHOUT FURTHER INCIDENT. PERFORMED BIT TEST OF ADC2, IAW CRJ-700 AMM 34-13-01-740-801, TEST GOOD. FOUND S2 DRAIN ASJan 16, 2021 · N507AE · Cndair CL6002C10 · Pitot/Static SystemSDR VNAA202101181112Adc · failedSHORTLY AFTER TAKEOFF, CREW ENCOUNTERED ISSUES WITH THE ADC ON THE FO SIDE. EFIS COMP MON, IAS, AND ALT ALL FLAGGED IMMEDIATELY. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. R & R ADC2 (RT), IAW CRJ 700 AMM 34-13-01-000/400-801. OPERATIONS CHECKED, IAW Jan 15, 2021 · N507AE · Cndair CL6002C10 · Pitot/Static SystemSDR VNAA202101181111Adc · failedSHORTLY AFTER TAKEOFF, CREW ENCOUNTERED ISSUES WITH THE ADC ON THE FO SIDE. EFIS COMP MON, IAS, AND ALT ALL FLAGGED IMMEDIATELY. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. R & R ADC2 (RT), IAW CRJ 700 AMM 34-13-01-000/400-801. OPERATIONS CHECKED, IAW CJan 15, 2021 · N507AE · Cndair CL6002C10 · Pitot/Static SystemSDR VNAA2020110499911Former · corrodedTHE PAX DDOR FWD FORMER IS CORRODED AROUND THE LOWER TENSION TIE FITTING. REMOVED AND REPLACED THE FWD FORMER, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020110499910Floorbeam · crackedRT SIDE FS 280 FLOORBEAM IS CRACKED. REMOVED AND REPLACED RT SIDE FS 280 FLOOR BEAM, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202011049999Stringer · corrodedSTR 25R IS CORRODED FROM FS 280 TO FS 333. REMOVED AND REPLACED STR 25R, IAW CRJ 700 SRM 51-42-06-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202011049998Former · corrodedTHE PAX DOOR FWD FORMER IS CORRODED AROUND THE LOWER TENSION TIE FITTING. REMOVED AND REPLACED THE FWD FORMER, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202011049997Stringer · corrodedSTR 27 IS CORRODED FROM FS 280 TO FS 300. REMOVED AND REPLACED STR 27, IAW CRJ 700 SRM 51-42-06-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202011049996Angle · wornREINFORCING ANGLE, FUSELAGE FS 310 HAS AN ELONGATED HOLE AT STR 26L. PERFORMED A MAJOR REPAIR TO THE REINFORCING ANGLE, FUSELAGE FS 210 AT STR 26L, IAW STS EA 20-2020-107 REV IR DATED 10-27-2020.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202011049995Doubler · corrodedANTENNA DOUBLER BETWEEN FS 295 AND FS 310 AT STGR 27 IS CORRODED. REMOVED CORRODED DOUBLER BETWEEN FS 295 AND FS 310 AT STGR 27 AND INSTALLED NEW SERVICEABLE DOUBLER P/N SH670-32364-7, IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202011049994Former · corrodedTHE PAX DOOR FWD FORMER IS CORRODED AROUND THE LOWER TENSION TIE FITTING. C/A: REMOVED AND REPLACED THE FWD FORMER, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202011049993Skin · corrodedPAX DOOR INNER SKIN IS CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED DOOR SKIN, IAW APPLICABLE CRJ 700 SRM’S.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202011049992Intercostal · corrodedLT AND RT LATCH PIN INTERCOSTALS BETWEEN FS 349 AND FS 364 HAVE AREAS OF CORROSION. REMOVED AND REPLACED INTERCOSTALS, IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202011049991Frame · corrodedFS 310 HAS CORROSION ON ATTACH FLANGE AND WEB BETWEEN STR 26L & 26R. REPAIRED IAW REO 670-53-21-799 REV A.Nov 4, 2020 · N507AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020071111101Idg · failedON CLIMB OUT, THE RT ENGINE GENERATOR FAILED AT HIGH POWER. THIS CAUSED A FAILURE OF THE GENERATOR CONTROL, AS WELL AS A DEPRESSURIZATION OF HYD SYSTEM 3 AMONG OTHER THINGS. AN EMERGENCY WAS DECLARED BY ATC. MX REMOVED AND REPLACED THE NR 2 IDG AND OPS TESTED Jul 8, 2020 · N507AE · Cndair CL6002C10 · AC Generator-AlternatorSDR VNAA2020040311102Warning System · false activationCREW AIR RETURNED FOR MAINTENANCE ISSUE IN FLIGHT. ANTI-SKID CAUTION MESSAGE ILLUMINATED CREW DECIDED TO AIR RETURN TO CLT FOR MAINTENANCE. DEFERRED ANTI-SKID SYSTEM. SUPPLEMENTAL INFORMATION: PERFORMED TROUBLESHOOTING OF THE ANTI SKID SUBSYSTEM. INTERROGATED Apr 2, 2020 · N507AE · Cndair CL6002C10 · Brake Anti-Skid SectionSDR SIMA201808298002Skin · damagedEXTERIOR SKIN DAMAGED BETWEEN BS 969 - 985 AT STRINGER 27L. REPAIRED IAW ERS-CR-53MR-3390.Aug 28, 2018 · N507AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20180828001Tee Fitting · crackedATTACH ANGLE ON THE AFT SIDE OF FLOORBEAM AT BS 280, LBL 9 WAS CRACKED .250 INCHES. INSTALLED A NEW FABRICATED TEE BRACKET ATTACH ANGLE IAW SRM 51-21-26 AND 51-42-21.Aug 28, 2018 · N507AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA201808021002Relay · failedEMERGENCY LIGHTS CYCLE ON AND OFF UNCOMMANDED. REMOVED AND REPLACED RELAY K135 REF ESPM 20-42-00. OPC GOOD REF AMM 33-24-07.Aug 1, 2018 · N507AE · Cndair CL6002C10 · Emergency LightingSDR SIMA2018042380008Computer · malfunctionedLEFT AHRS SPINNING 30* LT, EXCESSIVE EFIS COMP MOM MESSAGES ON TAXI, CLIMB, LEVEL, ONCE W BOUND NO ERRORS. REMOVED AND REPLACED THE LT AHRS COMPUTER IAW AMM 34-21-01. OPS CHECKED GOOD. PERFORMED TAXI IAW GHC. NO MESSAGES NOTED. OPS CHECKED GOOD. IAW NRWC 507Apr 20, 2018 · N507AE · Cndair CL6002C10 · Attitude and Direction Data SystemSDR SIMA201804238009Computer · malfunctionedLOST MAG INFO ON THE PFD & MFD. REGAINED INFO THEN LOST IT AGAIN. RED NAV FLAG ON THE CAPTAIN`S SIDE. FOUND THE NR 1 AHC WAS BACK ONLINE. RETRIEVED MDC FAULT 005922. R & R THEN NR 1AHC CHECKS GOOD IAW AMM 34-21-01.Apr 20, 2018 · N507AE · Cndair CL6002C10 · Attitude and Direction Data SystemSDR SIMA201804193002Windshield · arcedAT FL230 THE LT WINDSHIELD HEAT MESSAGE WITH ARCING ON THE CAPTAIN`S SIDE. DONNED OXYGEN MASKS & DECLARED AN EMERGENCY. INIATED DESCENT AND AT 16,000 FT, THE WINDSHIELD SHATTERED. NRWC 507-CMH-03091 FOR WORK ACCOMPLISHED. REMOVED AND REPLACED THE CAPTAIN'S Apr 17, 2018 · N507AE · Cndair CL6002C10 · Flight Compartment WindowsSDR SIMA20180131004Manifold · failedSTEERING INOPERATIVE CAUTION MESSAGE POSTED. PERFORMED NEUISANCE MESSAGE PROCEDURE, CAUTION CLEARED FOR A FEW SECONDS AND REPOSTED. REMOVED AND REPLACED STEERING MANIFOLD IAW AMM 32-51-50. PERFORMED BITE TEST OF STEERING MANIFOLD IAW AMM 32-50-00-740-801. Jan 31, 2018 · N507AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA20171224001None · noneAFTER CLIMBING THRU 1000 FT AGL, CAPTAIN AND FIRST OFFICER BEGAN SMELLING FUMES AND WITHIN SECONDS A MASTER WARNING SMOKE AFT LAV MESSAGE. RAN EPC AND APPRC CHECKLISTS. MESSAGE WENT AWAY AND RETURNED BRIEFLY AFTER COMPLETION OF CHECKLISTS. MESSAGE WENT AWAYDec 24, 2017 · N507AE · Cndair CL6002C10 · Standard Practices/StructuresSDR SIMA20171202004Bulb · inoperativeLH OVER WING EXT EMER LIGHT INOP-C/A-RAR LH OVER WING EXT EMER LIGHT BULB IAW AMM 33-51-15. OPC GOODDec 2, 2017 · N507AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170724001Battery · dischargedNR 2 EMERGENCY LIGHT BATTERY INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY PER AMM 33-51-17.Jul 24, 2017 · N507AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170724002Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK NR 1 IAW AMM 33-51-17 OPS CHECK GOOD.Jul 24, 2017 · N507AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170626002Tire · damagedFOUND A DENT ON THE INBD RT FLAP FROM THROWN TIRE TREAD. C/W ETN-GN-32-009 THROWN TIRE INSPECTION. REMOVED AND REPLACED RT INBD FLAP IAW AMM 27-52-21 OPS CHECK GOOD. INSPECTED TIRE AND FOUND BIG CHUNK OF TIRE MISSING REMOVED AND REPLACED NR 3 MLG WHEEL AND TIRJun 26, 2017 · N507AE · Cndair CL6002C10 · TireSDR SIMA20161128004Angle · crackedANGLE LOCATED ON FWD SIDE OF THE RIGHT BULKHEAD RBL 26 AT FLOOR LEVEL HAS A ONE INCH CRACK. INSTALLED A NEW ANGLE IAW SRM 51-42-06.Nov 28, 2016 · N507AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20161128003Floorbeam · crackedLEFT BS 280 CROSSBEAM TEE BRACKET IS CRACKED. INSTALLED A NEW TEE BRACKET IAW SRM 51-42-06 AND 51-42-20.Nov 28, 2016 · N507AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20161120004Bulkhead · corrodedRH COCKPIT BULKHEAD CORRODED ON THE AFT SIDE AT FLOOR LEVEL. COMPLETED INSTALL OF RT WEB IAW SRM 53-11-10.Nov 20, 2016 · N507AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20161118008Angle · corrodedFLOORBEAM AT BS 280 CORRODED. INSTALLED A NEW FLOORBEAM TO WEB ANGLE.IAW SREM 51-42-06.Nov 18, 2016 · N507AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20161118007Tee Fitting · crackedRIGHT TEE FITTING ON AFT SIDE OF CROSSBEAM BS 280 IS CRACKED. INSTALLED A NEW TEE FITTING IAW SRM 51-42-006 AND 51-42-20.Nov 18, 2016 · N507AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SIMA20161118005Door Sill · corrodedAFT CARGO DOOR SILL CORRODED. REPAIRED THE DOOR SILL IAW ETN-CR-53-104.Nov 18, 2016 · N507AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20160816001Acm · malfunctionedODOR OF SMOKE IN CABIN AND IN COCKPIT IN FLIGHT ON APPROACH TO LANDING, APU OFF. TRANSFERRED TO NRWC 507-ORD-02496. R & R RT ACM NR 2 IAW AMM 21-51-08. OPS CHECK AND LEAK CHECK GOOD. NO ABNORMAL ODOR NOTED. ALSO, GROUND RAN BOTH ENGINES IAW AMM 71-00-00.Aug 16, 2016 · N507AE · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20160725004Control Unit · failedFLAP FAIL ON APP AT SLATS 20 FLAPS LEFT 3 RIGHT . REMOVED AND REPLACED SFECU NR 1 IAW CRJ AMM 27-51-05. OPS CHECKS 27-50-00 AND 27-51-05 GOODJul 25, 2016 · N507AE · Cndair CL6002C10 · Trailing Edge Flap Control System
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