N508JL

Service difficulty reports · 143

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 = 'N508JL' 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 YENA201612011067Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT -Y1162 FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472780.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011066Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT Y254, FRAMES 12 - 24. R & R THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53110984.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011065Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, -Y1219, FRAME 66. R & R THE FLOOR SUPPORT IAW SRM 51-72-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011064Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, - Y765, FRAME 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472780.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011063Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT BETWEEN Y1225, FRAMES 66+5 TO 67+15. R & R THE FLOOR SUPPORT IAW SRM A320 51-72-11, DRAWING D53472815, & D53472831Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011062Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT BETWEEN -Y1292 AT AFT GALLEY AREA FROM FRAMES 66+5 TO 67+15. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472831.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011061Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT. R & R FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472831.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011060Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT. R & R THE FLOOR SUPPORT IAW SRM A320 51-72-11 AND DRAWING D53472816.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011059Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y465 FRAME 66+5. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472816.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011058Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y1162 FRAME 68. R & R THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53472780.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011057Floor Support · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y512, FRAME 66. R & R THE FLOOR SUPPORT BETWEEN FRAMES 64 TO 67 IAW SRM 51-72-11 AND DRAWING D53472815.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011056Door Sill · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL FR 66 TO FR 68 STR 23L AT AFT GALLEY AREA. R&R LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23 LEFT HAND AT AFT GALLEY AREA IAW SRM A320-51-72-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011055Door Sill · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON LOWER SILL FR 66 TO FR 68 STR 23R AT AFT GALLEY AREA. R & R LOWER SILL LOCATED BETWEEN FR 66 TO FR 68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM A320-51-72-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011054Dummy Rail · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON RAIL DUMMY Y503-2 LOC FRAME 16 LEFT HAND SIDE AT FWD GALLEY AREA. R&R DUMMY RAIL Y503.2 LOC FRAME 12 TO FRAME 16 LEFT SIDE AFT FWD GALLEY AREA IAW SRM 51-72-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA201612011053Web · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON WEB BETWEEN FR 69 -FR 70 AND STR 23L AT AFT GALLEY AREA. R&R WEB BETWEEN FR69- FR70 AND STR 23L AT AFT GALLEY AREA IAW 31-22-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA201612011052Web · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON WEB BETWEEN FR69 - FR70 AT AFT GALLEY. R & R WEB BETWEEN FR69 -FR70 AND STR 23R AT AFT GALLEY AREA IAW 31-22-11.Dec 1, 2016 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA20140501088Actuator · failedACFT DIVERTED DUE TO ELAC 2 FAILED AFTER TAKEOFF, SUBSEQUENT LOSS OF AUTOPILOT. TSM 27-93-00-810-837, PERFORMED RESISTANCE CHECK OF PITCH TRIM ACT MOTOR 1 SPLY RELAY CHECKS OK. R & R PITCH TRIM ACT. FAULT CLEARED, OPS CHECK OK, REF AMM 27-44-57.May 1, 2014 · N508JL · Airbus A320232 · Elevator Control SystemSDR YENA20130813179Actuator · corrodedDURING HEAVY MX CHECK, INBD AND OTBD OF NR 3 SPOILER ACTUATOR HAS EVIDENCE OF CORROSION. R & R INBD AND OTBD NR 3 SPOILER ACTUATOR RIVETS IAW SRM 51-42-1. ACCOMPLISHED PERMANENT REPAIR IAW EC A13-329-01.Aug 13, 2013 · N508JL · Airbus A320232 · SpoilersSDR YENA20130417075Heat Exchanger · damagedFLT 272 FLL-LGA, AIRCRAFT DIVERTED TO JFK DUE TO "AIR L WING LEAK" FOLLOWED BY "AIR R WING LEAK" ECAMS. FORCED THE A/C IN UNPRESSURIZED CONDITION WITH "AIR PACK 1 & 2 FAULT" ECAM. FLIGHT CONTINUED AT 10,000 FT/DIVERSION. THE TECHNICIAN FOUND DAMAGED DUCTINGApr 17, 2013 · N508JL · Airbus A320232 · Cabin Cooling SystemSDR YENA20120820584Display · failedFLT 739 JFK-PSE, AIR RETURN DUE TO INTERMITTENT UPPER ECAM FAILURE DURING CLIMB. REMOVED AND REPLACED UPPER ECAM DU IAW AMM 31-63-22-04. OPS CHECK OK.Aug 20, 2012 · N508JL · Airbus A320232 · Central DisplaySDR YENA20110707295Outflow Valve · failedFLT 43 JFK-MCO, AIR RETURN TO JFK DUE TO AIRCRAFT UNABLE TO PRESSURIZE WITH VENT SKIN VALVE AND A/C BLOWER FAULT. TECHNICIAN REMOVED AND REPLACED SKIN AIR OUTLET VALVE (22HQ) IAW AMM CH 21-26-53 & ACTIVATED THE SKIN EXCHANGER ISOLATION VALVE (24HQ). PERFORMEJul 7, 2011 · N508JL · Airbus A320232 · Pressure Regulator/Outflow ValveSDR YENA20110705290Pump · failedFLT 1061 JFK-AUS, AIR RETURN TO JFK DUE TO HYD B ELEC PUMP OVHT ECAM ON CLIMBOUT. MESSAGE DID NOT CLEAR EVEN AFTER SHUTDOWN. TECHNICIAN REMOVED AND REPLACED HYD B ELECTRIC PUMP. OPS AND LEAK CHECK OK PER AMM 29-12-51-000-001.Jul 5, 2011 · N508JL · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR YENA20110204193Display · malfunctionedFLT 346 SRQ-JFK, HOT SMELL COMING FROM EYELET VENT NEAR FRONT GALLEY. ACCOMPLISHED TSM 24-00-00-810 AND INSPECTION PER 23-39-00-810-801 AND FOUND VDU AT 2E TO HAVE AN ELECTRICAL ODOR. REPLACED VDU OPS CHECK NORMAL.Feb 4, 2011 · N508JL · Airbus A320232 · Entertainment SystemSDR 2010FA0001209Plate · crackedCRACK AT FASTENER HOLE ON CONNECTION PLATE FOR RT MLG DOOR ACTUATOR MOUNT FITTING. R & R CONNECTION PLATE IAW SRM 51-72-11.Dec 1, 2010 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2010FA0001208Fitting · corrodedCORROSION ON AFT CARGO COMPARTMENT FITTING (FLOOR STRUCTURE). FITTING IS LISTED AS PRIMARY STRUCTURE. NO CORROSION REMOVAL LIMITS AVAILABLE. R & R FITTING IAW SRM 51-42-11.Dec 1, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001194Link · corrodedLT WING SHROUD BOX FWD INBD SUPPORT LINK CORRODED. NO CORROSION REMOVAL LIMITS AVAILABLE. SUPPORT LINK IS LISTED AS PRIMARY/ FATIGUE CRITICAL STRUCTURE.Nov 22, 2010 · N508JL · Airbus A320232 · Wing Main, Frame StructureSDR 2010FA0001166Plate · crackedCRACK AT FASTENER HOLES ON CONNECTION PLATE FOR LT MLG DOOR ACTUATOR MOUNT FITTING. CONNECTION PLATE IS LISTED AS PRIMARY STRUCTURE. R & R PLATE IAW SRM 51-72-11.Nov 11, 2010 · N508JL · Airbus A320232 · Fuselage, Landing Gear Attach FittingsSDR 2010FA0001161Floor Support · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT PROFILE FR 56, LBL24 - RBL12. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE IAW SRM 51-42-11.Nov 8, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001160Support · corrodedCORROSION ON FRAME SUPPORT FR 69-70 RBL 50. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. SUPPORT IS LISTED AS PRIMARY STRUCTURE. R & R FITTING IAW SRM 51-42-11.Nov 8, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001159Fitting · corrodedCORROSION ON AFT CARGO COMPARTMENT FLOOR SUPPORT FITTING FR 56 LBL 15. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. FITTING IS LISTED AS PRIMARY STRUCTURE. R & R FITTING IAW SRM 51-42-11.Nov 8, 2010 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2010FA0001145Floor Support · corrodedCORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT PROFILE FR 24 - 28, Y765. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE IAW SRM 51-42-11.Nov 1, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001129Fitting · crackedFITTING CRACKED ON AFT CABIN FLOORBEAM. R & R FITTING IAW SRM 51-42-11.Oct 22, 2010 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR 2010FA0001039Shear Plate · corrodedCORROSION ON CABIN FLOOR SIDE PANEL (SHEAR PLATE) FR 69 - FR 70 -Y1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. SHEAR PLATE IS LISTED AS PRIMARY STRUCTURE. R & R SHEAR PLATE IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001038Shear Plate · corrodedCORROSION ON CABIN SIDE PANEL (SHEAR PLATE) FR 69 - FR 70 Y1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. SHEAR PLATE IS LISTED AS PRIMARY STRUCTURE. R & R SHEAR PLATE IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001037Web · corrodedCORROSION ON CABIN FLOOR SIDE PANEL (WEB) FR 16 Y1732. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. WEB IS LISTED AS PRIMARY STRUCTURE. R & R WEB IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001036Floor Support · corrodedCORROSION ON BULK CARGO COMPARTMENT FLOOR SUPPORT PROFILE CORNER FR 65, STR 38LH TO STR 38RT. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE CORNER IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE CORNER IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001035Floor Support · corrodedCORROSION ON BULK CARGO COMPARTMENT FLOOR SUPPORT PROFILE CORNER STR 38RH BETWEEN FR 63 AND FR 65. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE CORNER IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE CORNER IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001034Floor Support · corrodedCORROSION ON BULK CARGO COMPARTMENT FLOOR SUPPORT PROFILE CORNER FR 63 STR 38LT. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE CORNER IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE CORNER IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001033Floor Support · corrodedCORROSION ON BULK CARGO COMPARTMENT FLOOR SUPPORT PROFILE (SEALING ASSY) FR 63 STR 38RT TO STR 38LT. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. SEALING ASSY IS LISTED AS PRIMARY STRUCTURE. R & R SEALING ASSY IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001032Floorbeam · corrodedCORROSION ON CABIN FLOORBEAM FR 16 Y 1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. FLOORBEAM IS LISTED AS PRIMARY STRUCTURE. REMOVED AND REPLACED FLOORBEAM IAW A320 SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001031Floorbeam · corrodedCORROSION ON CABIN FLOOR SUPPORT BEAM FR 16 Y254. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001030Floor Support · corrodedCORROSION OF AFT CABIN FLOOR SUPPORT BEAM FR 68 TO FR 69 Y1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001029Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORT FR 68 TO FR 70 Y 765. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001028Floorbeam · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT BEAM FR 70 -Y 254. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001027Floorbeam · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT BEAM FR 68 TO FR 70 -Y 765. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001026Floorbeam · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT BEAM FR 68 TO FR 69 -Y 1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. REMOVED AND REPLACED BEAM IAW A320 SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001025Floorbeam · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT BEAM FR 66 -Y 765. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW A320 SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001024Floor Support · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT PROFILE Z, FR 66, Y1732. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. PROFILE Z IS LISTED AS PRIMARY STRUCTURE. R & R PROFILE Z IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Miscellaneous StructureSDR 2010FA0001023Floorbeam · corrodedCORROSION ON AFT CABIN FLOOR SUPPORT BEAM FR 66 Y 1292. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R BEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor BeamSDR 2010FA0001022Floorbeam · corrodedCORROSION ON AFT CABIN FLOORBEAM FR 66 Y 765. NO CORROSION REMOVAL LIMITS AVAILABLE IN SRM. BEAM IS LISTED AS PRIMARY STRUCTURE. R & R FLOORBEAM IAW SRM 51-42-11.Sep 20, 2010 · N508JL · Airbus A320232 · Fuselage Main, Floor Beam
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