N819FX
Service difficulty reports · 139
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 = 'N819FX' 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.
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 = 'N819FX' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR COEA2016030409819Floor Support · crackedHEAVY CHECK COE & MAJOR REPAIR. RT LONGITUDINAL FLOORBEAM AT FLOORBEAM 29 IS CRACKED. REPAIR IAW EO 5315-02.SDR COEA2016030402819Floor Support · crackedHEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM AT FLOORBEAM 29 IS CRACKED. REPAIR IAW EO 5315-02.SDR COEA2016022601819Unknown · malfunctionedFLIGHT 200 EN-ROUTE FOR HEAVY CHECK & AIR TURN BACK DISCREPANCY. CREW REPORTED LOSS OF CABIN PRESS IN AUTO MODE. ELECTED TO RETURN ACFT. NO EMER WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. ITEM DEFERRED. ACFT NOW IN HEAVY CHECK.SDR COEA2015042302819Skin · damagedFLIGHT 7277, BIRD STRIKE, DISCREPANCY. ON APPROACH, THE ACFT FLEW THROUGH A FLOCK OF BIRDS. THE CREW ELECTED TO CONTINUE AFTER DETERMINING THAT THE ACFT WAS MANEUVERING NORMALLY, NO VIBRATION COULD BE DETECTED & ALL ENG GAUGES WERE INDICATING NORMAL. THE ACSDR COEA2015031901819Unknown · malfunctionedAIR TURN BACK, DISCREPANCY, DURING CLIMB OUT, THE CREW EXPERIENCED A TORQUE FLUCTUATION ON THE NR 2 ENG CAUSING THE ACFT TO YAW BACK & FORTH. THE CREW RETURNED THE ACFT BACK. NO EMER WAS DECLARED. PERFORMED ENG RUNS TO TRY & FIND THE ISSUE, BUT COULD NOT DUSDR COEA2014010606819Door · detachedDURING POST FLIGHT INSPECTION, RIGHT MLG DOOR DETACHED FROM ACFT DURING TAXI IN, CAUSING GOUGE IN PANEL 194CR, RT MAIN GEAR DOOR, PANEL & ALL OTHER DAMAGED AREAS WERE REPLACED IAW JIC 52-81-00 RAI 10000 002. PERFORMED LG NORMAL, EMER TEST & OPERATIONS CHECKSDR COEA2014013005819Door Frame · crackedPREVIOUS REPAIR IN THE FWD CARGO DOOR FRAME IS CRACKED ON THE UPPER END OF THE SECOND FROM AFT FRAME. REPAIRED IAW SRM 52-31-00 REPAIR 411.SDR COEA2014012304819Skin · damagedUPPER WING CUT OUT FOR ACCESS PANEL 622CT HAS FRETTING. REPAIR IAW SRAS DO TS-531 06 3474 ISSUE D.SDR COEA2014012202819Floor Support · crackedLEFT LONGITUDINAL FLOOR BEAM IS CRACKED FWD OF FRAME 35. REPAIRED IAW EO 5315-02 REV ORIGINAL 8/20/2013.SDR COEA2014012101819Floorbeam · crackedRIGHT LONGITUDINAL FLOOR BEAM IS CRACKED AFT OF FRAME 33 & FWD OF FRAME 34. REPAIR IAW EO 5315-02 REV ORIGINAL 8/20/2013.SDR COEA2014012203819Skin · dentedLEFT FUSELAGE SKIN IS DENTED BETWEEN FRAMES 34 & 35 ABOVE STRINGER 14L. REPAIR IAW ATR72 SRM 53-00-00 FIG 403.SDR COEA2012012313819Seat Track · corrodedHEAVY CK COE / LEVEL 2 CORROSION: FOUND PITTING CORROSION ON RT SEAT TRACK FR 36-40 (LENGTH 1.8", WIDTH 1", DEPTH .066"). REMOVED CORROSION AND REPLACED SEAT TRACK WITH OEM PART IAW SRM.SDR COEA2012012012819Skin · damagedHEAVY CK COE / MAJOR REPAIR: RT WING UPPER ACCESS DOOR CUTOUT FOR PANEL 622CT HAS FRETTING. SUBMITTED TO ATR FOR STRUCTURAL REPAIR INSTRUCTIONS RT WING BETWEEN RIBS 4 & 5 AND STIFFENERS 5 & 7.SDR COEA2012012011819Skin · damagedHEAVY CK COE / MAJOR REPAIR: LT UPPER WING ACCESS DOOR CUTOUT FOR PANEL 522CT HAS FRETTING. SUBMIT TO ATR FOR STRUCTURAL REPAIR INSTRUCTIONS. LT WING BETWEEN RIBS 4 & 5 AND STIFFENERS 5 & 7.SDR COEA2012011910819Stringer · crackedHEAVY CK COE / MAJOR REPAIR: STRINGER 1L BETWEEN FRAMES 15 - 16 HAS CRACK AT FASTENER HOLE. PERFORM STRINGER REPAIR SPLICE IAW SRM.SDR COEA2012011815819Skin · corrodedHEAVY CK / MAJOR REPAIR / LEVEL 2 CORROSION: RT LOWER WING SKIN IS CHAFED AT RIB 13, STR 8-9 ABOUT 12 INCHES FWD OF REAR SPAR CAUSED BY FLAP FAIRING FRETTING ON SKIN. DAMAGE BLENDED PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2012011814819Skin · corrodedHEAVY CK / MAJOR REPAIR / LEVEL 2 CORROSION: RT LOWER WING SKIN IS CHAFED AT RIB 13, STR 8-9 ABOUT 12 INCHES FWD OF REAR SPAR CAUSED BY FLAP FAIRING FRETTING ON SKIN. DAMAGE BLENDED PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.SDR COEA2012011809819Skin · dentedHEAVY CK COE / MAJOR REPAIR: DENT OUT OF LIMITS 2.4" FWD OF FR 31, 2.2" ABOVE LT STR 20 WITH LOCALIZED GOUGE. DENT DEPTH 0.001" WITH DISTANCE TO STIFFENER OF 1.9" IS WITHIN LIMITS. INSTALL ONE RIVET REPAIR RIVET IAW SRM 2.4" FWD OF FRAME 31, 2.2" ABOVE STR 2SDR COEA2012011808819Floorbeam · crackedHEAVY CK COE / MAJOR REPAIR: LONGITUDINAL FLOORBEAM CRACKED LEFT O/B AFT FR 30. REMOVED CRACKED SECTON, FABRICATED AND INSTALLED NEW SECTION LEFT O/B LONGITUDINAL FLOORBEAM FROM FRAME 30-31, WL 2327.5, BL 640L IAW M7 DWG & M7 SB ATR72-53-015.SDR COEA2012011107819Floorbeam · bentHEAVY CK / MAJOR REPAIR: LEFT O/B LONGITUDINAL FLOORBEAM IS BENT JUST FWD OF FRAME 23C. REMOVED DAMAGED SECTION / FABRICATED AND INSTALLED NEW FLOORBEAM AND CLIPS IAW M7 SB ATR72-53-015.SDR COEA2012011106819Floorbeam · bentHEAVY CK / MAJOR REPAIR: RIGHT O/B LONGITUDINAL FLOORBEAM IS BENT JUST AFT OF FRAME 23C. REMOVED DAMAGED SECTION / FABRICATED AND INSTALLED NEW FLOORBEAM AND CLIPS IAW M7 SB ATAR72-53-015.SDR COEA2012011105819Floorbeam · crackedHEAVY CK / MAJOR REPAIR: LEFT O/B LONGITUDINAL FLOORBEAM IS CRACKED JUST FWD OF FRAME 25. REMOVED DAMAGED SECTION / FABRICATED AND INSTALLED NEW FLOORBEAM AND CLIPS IAW M7 SB ATR72-53-015.SDR COEA2012011104819Floorbeam · crackedHEAVY CK / MAJOR REPAIR: LT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED JUST FWD OF FRAME 26. REMOVED DAMAGED SECTION / FABRICATED AND INSTALLED NEW FLOORBEAM AND CLIPS IAW M7 SB ATR72-53-015.SDR COEA2012011103819Floorbeam · crackedHEAVY CK / MAJOR REPAIR: RIGHT O/B LONGITUDINAL FLOORBEAM IS CRACKED JUST AFT OF FRAME 28C. REMOVED DAMAGED SECTION / FABRICATED AND INSTALLED NEW FLOORBEAM AND CLIPS IAW M7 SB ATR72-53-015.SDR COEA2012010902819Floorbeam · crackedHEAVY CK / MAJOR REPAIR: RT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED JUST FWD FOR FRAME 31. FABRICATED, DRILLED AND INSTALLED NEW LONGITUDINAL FLOORBEAM AND 8 EACH ATTACH CLIPS IAW M7 SB72-53-015.SDR COEA2012010901819Floorbeam · crackedHEAVY CK / MAJOR REPAIR: LT OUTBOARD LONGITUDINAL FLOORBEAM IS CRACKED JUST FWD OF FRAME 33. FABRICATED AND DRILLED AND INSTALLED NEW LONGITUDINAL FLOORBEAM AND 8 EA ATTACH CLIPS IAW M7 SB ATR72-53-015.SDR COEA2010012503819Strip · chafedHEAVY CHECK COE - MAJOR REPAIR: RT WING FRONT SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 5, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 6 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS.SDR COEA2010012502819Strip · chafedHEAVY CHECK COE - MAJOR REPAIR: LT WING FRONT SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 5, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 6 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS.SDR COEA2010011801819Spar · chafedHEAVY CHECK COE: MAJOR REPAIR: LT WING REAR SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 4, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 3 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS DO/TS-299/SDR COEA2009121805819Uplock · wornAIR TURN BACK TO JNU ON FLIGHT 8216: PRIMARY AND SECONDARY NOSE GEAR INDICATOR SHOWS GEAR UNLOCK WITH GEAR HANDLE IN UP POSITION. PILOT DIVERTED BACK TO JNU, LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR UPLOCK BOX ASSEMBLY. AIRCRAFT SDR COEA2009082404819Fuel Control · faultyFLT 8216 RETURN TO GATE AT JNU: ON TAXI OUT AT JNU NR 1 BLEED FAULT LIGHT ILLUMINATED. ON TAXI BACK TO GATE NR 2 ENGINE EEC FAULT LIGHT ILLUMINATED. THE PILOT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLEED VALVE AND THE NR 2 MECHANICAL FSDR COEA2009082103819Eec · faultedFLT 7202 RETURN TO GATE AT SEA: AFTER BLOCK OUT IN SEA NR 2 ENGINE EEC FAULT LIGHT ILLUMINATED, AFTER RESETTING THERE WAS NO CHANGE. THE PILOT RETURNED BACK TO GATE. MAINTENANCE DEFERRED THE EEC AND TOOK A WEIGHT RESTRICTION FOR FREIGHT. AIRCRAFT CONTINUED.SDR COEA2009050602819Structure · corrodedHEAVY CHECK: FOUND LEVEL 2 CORROSION ON RT WING FEEDER TANK CUTOUT FLANGE FOR UPPER ACCESS PANEL 622CT.SDR COEA2009050601819Flange · corrodedHEAVY CHECK: FOUND LEVEL 2 CORROSION ON LT WING FEEDER TANK CUTOUT FLANGE FOR UPPER ACCESS PANEL 522CT.SDR COEA0803819Angle · crackedFOUND DURING HEAVY CHECK, LT AND RT AFT UPPER WING PRESSURE DECK INTERNAL SPLICE ANGLES CRACKED. AFT OF FRAME 27 AT STRINGERS 4L AND 4R. LT ANGLE PN IS S53573201210, RT S53573201211. SRAS, SHEET REF: SO/TS-232/08/4462. DAMAGES LEFT, AS IS AFTER INSPECTION SDR COEA0801819Bleed Valve · failedFLIGHT NR 8091 ON 1/2/08, DURING TAXI TO RUNWAY, THE NR 1 ENGINE BLEED FAULTED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. AIRCRAFT RETURNED SAFELY TO BLOCKS. REPLACED NR 1 ENGINE HIGH PRESSURE BLEED AIR SHUTOFF VALVE. (K)SDR COEA0802819Starter Gen · failedFLIGHT NR 8091 ON 1/2/08, DURING TAXI TO RUNWAY THE NR 2 DC GENERATOR FAULTED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. AIRCRAFT RETURNED SAFELY TO BLOCKS. REPLACED NR 2 ENGINE DC STARTER GENERATOR. NR 40670.SDR COEA0702819Pitot Head · obstructedFLT 8080 - ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOT NOTICED NR 2 AIRSPEED INDICATOR READ ZERO, FOLLOWED BY (DACD DATA INVALID) ON AFCS CONTROL PANEL. PILOT RETURNED TO RAMP AT OAK. MAINTENANCE FOUND AND REMOVED DEBRIS IN PITOT PROBE, TWO INSECTS. AIRCRAFTSDR COEA0701819Indicator · malfunctionedFLIGHT 8080 - ABORTED TAKEOFF, DURING TAKEOFF ROLL PILOT NOTICED NR 2 AIRSPEED INDICATOR READ ZERO, FOLLOWED BY (DACD DATA INVALID) ON AFCS CONTROL PANEL. PILOT RETURNED TO RAMP AT OAK. REMOVED AND REPLACED ASI. AIRCRAFT RETURNED TO SERVICE. DISCREPANCY RE
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