N247JS, cancelled May 14, 2022

Service difficulty reports · 79

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 = 'N247JS' AND deregistration_id = 'N247JS-2022-05-14'
  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 VNAA2020012711103Control Lever · failedFLAPS FAIL IN FLIGHT, RETURNED TO FIELD, DEFERRED THE SYSTEM. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL LEVER.Jan 27, 2020 · N247JS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA2019120651102Unknown · odorSMELL SMOKE IN CABIN JUST PRIOR TO PUSH BACK. PERFORMED OPS TEST OF THE AIR CONDITIONING SYS IAW CRJ 200 AMM 21-51-00-710-801 NO SMELL OF SMOKE DETECTED AT THIS TIMEDec 5, 2019 · N247JS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA2019051099913Bulkhead · crackedFS 621 REAR PRESSURE BULKHEAD FWD FACE BLO.00 WL127.5-WL113.5 INDICATIONS NOTED APPROX 6" LONG 50% FULL SCREEN HEIGHT, LBL9.5 WL76.50 INDICATION NOTED .6" LONG AND 100% FULL SCREEN HEIGHT FAILING NDT, RBL36 WL74.30 INDICATION NOTED 1.1" LONG AND 100% FULL SCRMay 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2019051099912Seat Track · corrodedLBL 9 FLOOR SEAT TRACK FROM FS 399- FS 399 +128 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019051099911Seat Track · corrodedRBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019051099910Angle · corrodedPAX DOOR LOWER SILL MID ANGLE IS CORRODED BEYOND LIMITS. C/A: REMOVED AND REPLACED MID ANGLE IAW SRM 51-42-06 AND 51-42-21.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2019051099909Bracket · crackedHYD SYS NR 3 PRESSURE TRANSDUCER BRACKET CRACKED IN LT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019051099908Bracket · crackedHYD SYS NR 3 TRANSDUCER BRACKET CRACKED IN RT MLG CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019051099907Bracket · crackedHYD SYS NR 3 PRESSURE TRANSDUCER Z-BRACKET CRACKED IN RT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED Z-BRACKET IAW SRM 51-42-06 AND 51-42-04.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2019051099906Seat Track · corrodedLBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019051099905Seat Track · corrodedRBL 9 FLOOR SEAT TRACK FROM FS399- FS409+128 SEGMENT IS CORRODED. C/A: REMOVED AND REPLACED RBL9 FLOOR SEAT TRACK FS399-FS409+128 SEGMENT IAW SRM 51-40-11, AMM 53-01-11-400-802, AND REO 601R-53-00-485.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019051099904Floorbeam · corrodedRBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 591 TO FS 621 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT RBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019051099903Floorbeam · corrodedLBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 595 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT LBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019051099902Floorbeam · corrodedRBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED RBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02. .May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019051099901Floorbeam · corrodedLBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED LBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02.May 10, 2019 · N247JS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2019030811101Light · inoperativeSUPPLEMENTAL INFORMATION:L/H FWD EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED L/H FWD EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000/400-801. OPS CHECK GOOD AT THIS TIMEMar 8, 2019 · N247JS · Cndair CL6002B19 · Emergency LightingSDR VNAA20181112101None · noneON TAKEOFF ABOUT 600 FEET THE CREW OBSERVED A LARGE BIRD GO PAST AND HEARD A "THUMP" AND BEGAN TO RECEIVE ENGINE INDICATIONS THAT THE BIRD MADE IMPACT WITH THE RIGHT HAND ENGINE. THE AIRCRAFT RETURNED TO FIELD AND CURRENTLY UNDER MAINTENANCE INSPECTION. THE AIOct 29, 2018 · N247JS · Cndair CL6002B19 · Turbine Engine Combustion SectionSDR VNAA2017062911101Bracket · bentAFTER TAKEOFF, THE CREW SELECTED GEAR UP AND THE GEAR DID NOT RETRACT. 6 SECONDS AFTER SELECTING THE HANDLE UP THE MAIN GEAR RETRACTED AND THE NOSE GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND MAINTENANCE FOUND THE CENTERING PROXIMITY SENSOR BJun 29, 2017 · N247JS · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR VNAA2017062999902Fitting · crackedCARGO DOOR UPPER FWD FITTING CRACKED. INSTALLED NEW SERVICEABLE CARGO DOOR UPPER FORWARD FITTING.Jun 29, 2017 · N247JS · Cndair CL6002B19 · Cargo/Baggage DoorsSDR VNAA2017062999901Bulkhead · crackedCRACK INDICATIONS AT LBL 36.20, LBL 18.0 AND RBL 18.0 AND WL 74. REPAIRED AREAS AT LBL 36.20 LBL 18.00 AND RBL 18.0 AT WL 74 IAW REO 601R-53-61-6070.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899912Channel · crackedBS 621 DOOR SUPPORTS CHANNEL, LOWER ANGLE CRACKED. REMOVED AND REPLACED THE CHANNEL.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017062899911Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 27.5, WL 80, APPROXIMATELY 2 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899910Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18, WL 74, APPROXIMATELY 2.5 INCHES LONG, 70% FSH. COMPLIED WITH REO 601R-53-61-6070.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899909Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT BL 0, WL 112, APPROXIMATELY 4.0 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899908Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 18, WL 74, APPROX 2 INCHES LONG, 90% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-6070, REV -.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899907Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT LBL 18.00, WL 106, APPROX 2.5 INCHES LONG, 50% FSH. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285, REV E.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899906Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION OF A CRACK NOTED AT LBL 36.20, WL 74, APPROX 2.5 INCHES LONG, 90% FSH. REPAIRED THE REAR PRESSURE BULHEAD IAW REO 601R-53-61-6070.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017062899905Skin · crackedNLG WHEEL CUTOUT HAS VISIBLE SIGNS OF POSSIBLE CRACK IN BOTH AFT CORNERS AT FS 235.00. REPAIRED IAW REO 601R-53-11-010Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2017062899904Floor Support · corrodedCORROSION ON RT SIDE PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 AND 529. REPAIRED PER REO 601R-53-41-666Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017062899903Floor Support · corrodedCORROSION ON LT PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 TO 529. REPAIRED IAW REO 601R-53-41-666Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017062899902Frame · crackedLEFT BS 718 FRAME CRACKED AT STRINGER 11L. REPLACED THE FRAME SECTION.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017062899901Frame · crackedRIGHT BS 718 FRAME CRACKED AT STRINGER 11R. REPLACED THE FRAME SECTION.Jun 28, 2017 · N247JS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017012400033Tire · failedLEFT NOSE TIRE BLEW ON TAKE OFF. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES.Jan 24, 2017 · N247JS · Cndair CL6002B19 · Nose/Tail Landing GearSDR VNAA2016062600028Light · brokenSEGMENT OF EMERGENCY LIGHTING GLOW STICK AND COVER, BROKEN AND MISSING AT SEAT 1D. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHT LAMP AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.Jun 26, 2016 · N247JS · Cndair CL6002B19 · Emergency LightingSDR VNAA2016053100034Apu · faultyAPU LOW OIL PRESSURE CAUTION MESSAGE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PROPERLY SERVICED THE APU AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.May 31, 2016 · N247JS · Cndair CL6002B19 · APU Oil SystemSDR VNAA2016011300010Seal · detachedCREW REPORTED TOP 8" OF SERVICE DOOR SEAL DETACHED IN FLIGHT. MADE A VERY LOUD NOISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REATTACHED SERVICE DOOR SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 13, 2016 · N247JS · Cndair CL6002B19 · Service DoorsSDR VNAA2015121600010Battery Pack · failedCREW REPORTED EMERGENCY LIGHT FLOOR STRIP NOT WORKING FROM ROW 9 TO THE AFT OF AIRCRAFT. MAINTENANCE INSPECTED, R & R NR 4 EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Dec 16, 2015 · N247JS · Cndair CL6002B19 · Emergency LightingSDR VNAA2015083000038Connector · disconnectedCREW REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 9 AND AFT. MAINTENANCE INSPECTED, FOUND RT AFT EMERGENCY LIGHT CONNECTOR DISCONNECTED, RECONNECTED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Aug 30, 2015 · N247JS · Cndair CL6002B19 · Light System WiringSDR VNAA2015081700018Skin · damagedLIGHTENING STRIKE DAMAGE TO RT AILERON UPPER SKIN AND T/E. REPAIRED THE AILERON IAW REO 601R-57-61-528, REV.Aug 17, 2015 · N247JS · Cndair CL6002B19 · AileronsSDR VNAA2015081700017Post · crackedFS 409+128, BL 0, VERTICAL POST LT AND RT SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250" LONG 60 PERCENT FSH FAILED NDT. R & R VERTICAL POST FS409+128, BLO.O IAW REO 601R-53-41-889, REV A.Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2015081700016Cargo Track · corrodedCARGO TRACK ON RBL 9BETWEEN BS 559+80 AND 559+96 AND CARGO TRACK HAD CORROSION. R & R CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2015081700014Mount · corrodedWARDROBE OTBD MOUNT PAD AT FS 310 HAS CORROSION AROUND BOLT HOLE. R & R 200 DWG 601R38670 AND SRM 51-40-11. INSTALLED NEW PAD IAW SRM 51-42-13 AND 51-21-16.Aug 17, 2015 · N247JS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2015041100014Wire · brokenCREW REPORTED MAIN CABIN DOOR EMERGENCY EXIT STRIP WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE ON EMERGENCY LIGHT, INSTALLED NEW WIRE SPLICE ON BROKEN WIRE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Apr 11, 2015 · N247JS · Cndair CL6002B19 · Light System WiringSDR VNAA2014090500001Wire Harness · damagedCREW REPORTED EMERGENCY FLOOR LEVEL LIGHTING AFT OF EMERGENCY EXIT ROW WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE TROUBLESHOT, R & R LIGHT WIRE HARNESS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.Sep 5, 2014 · N247JS · Cndair CL6002B19 · Light System WiringSDR VNAA2014060600005Connector · brokenCREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS ROW 9, AND AFT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND EMERGENCY LIGHT CONNECTOR PIN BROKEN AT END OF ROW BY LAVATORY. MAINTENANCE R & R SHORT CABLE, PIGTAIL AT LAVATORY ENTRANCE EMERGENCY FLOOR LIGHT AND PERFOJun 6, 2014 · N247JS · Cndair CL6002B19 · Light System WiringSDR VNAA2014040900008Warning Light · false activationCREW REPORTED AMBER STEERING INOPERATIVE MESSAGE ON TAKEOFF. LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF NOSEWHEEL STEERING (NWS) ELECTRONIC CONTROL UNIT (ECU) AND PERFORMED BITE TEST OF STEERING SYS IAW AMM. OPS CHECApr 9, 2014 · N247JS · Cndair CL6002B19 · Landing Gear Steering SystemSDR VNAA2013121400007Shutoff Valve · failedCREW REPORTED RED WING OVERHEAT MESSAGE DURING CLIMB. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MODULATING AND SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.Dec 14, 2013 · N247JS · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR VNAA2013101700007Pdu · failedCREW REPORTED LT THRUST REVERSER UNLOCK CAUTION MESSAGE IN DESCENT OUT OF FL200. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT, R & R LT THRUST REVERSER PDU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Oct 17, 2013 · N247JS · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA2013091600007Inverter · inoperativeCREW AND MX REPORTED ROWS 6 THROUGH 8 EMERGENCY LIGHT INOPERATIVE AND LOWER RT EMERGENCY LIGHT BY OVERWING EXIT INOPERATIVE. MX TROUBLESHOT, R & R NR 3 EMERGENCY LIGHT INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Sep 16, 2013 · N247JS · Cndair CL6002B19 · Emergency LightingSDR VNAA2013020500002Fuel Control · leakingCREW REPORTED SMOKE TOILET CAUTION MESSAGE ON DESCENT AFTER SWITCH TO APU BLEED. NO SMOKE IN CABIN, BUT FAIRLY STRONG SMELL WHEN BLEEDS WERE SWITCHED. MESSAGE WENT AWAY ON ITS OWN AFTER ONE MINUTE. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOFeb 5, 2013 · N247JS · Cndair CL6002B19 · APU Engine Fuel and Control
Back to N247JS, cancelled May 14, 2022