N119US
Service difficulty reports · 340
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 = 'N119US' 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 = 'N119US' 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 USAA2011121900005Coupling · corroded2S CHECK - CORROSION ON COUPLING AT FR67+17 INCHES, -Y1162. REPLACED COUPLING AT FR67+17 INCHES, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2011121600017Coupling · corroded2S CHECK - CORROSION ON COUPLING AT FR. 67+17 INCHES, -Y1162. REPLACED COUPLING AT FR. 67+17 INCHES, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2011121600016Floorbeam · corroded2S CHECK - CORROSION ON FLOORBEAM BETWEEN FR67+17 INCHES TO FR69+5 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR67+17 INCHES TO FR69+5 INCHES, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2011101800016Valve · defectiveDUCT BURNING SMELL REPORTED FROM AFT GALLEY WHICH DISSIPATED AFTER TURNING OFF GALLEY AND CABIN PUSH BUTTON AND CARGO HEAT. MAINTENANCE REMOVED AND REPLACED AFT CARGO HEAT PRESSURE REDUCING VALVE IAW AIRBUS MAINTENANCE MANUAL 21-43-00-440-003.SDR USAA2011101900013Valve · defectiveDUCT BURNING SMELL REPORTED FROM AFT GALLEY WHICH DISSIPATED AFTER TURNING OFF GALLEY AND CABIN PUSH BUTTON AND CARGO HEAT. MAINTENANCE REMOVED AND REPLACED CARGO TRIM AIR VALVE IAW AIRBUS MAINTENANCE MANUAL 21-43-51.SDR USAA2011091200014Lens · missingPILOT REPORT FOR SEVERAL EMERGENCY LIGHTING LENSES MISSING. MAINTENANCE REPLACED MISSING LENSES AS REQUIRED.SDR USAA2011062100022Floor Panel · corrodedPIT - GALLEY MAT - CORROSION ON FLOOR PANEL FASTENER INSERTS BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO Y765. REPLACED FLOOR PANEL FASTENER BETWEEN FR66 TO FR68 & BETWEEN -Y765 TO Y765 IAW CMM MCGILL IRM 9701 REV G.SDR USAA2011062100021Floorbeam · corrodedPIT - GALLEY MAT - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPAIRED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW EA 200142.SDR USAA2011062100020Floorbeam · corrodedPIT - GALLEY MAT - CORROSION ON UPPER CAP OF FLOORBEAM BETWEEN FR66 TO FR68 + 3 INCHES, -Y765. REPAIRED UPPER CAP OF FLOORBEAM BETWEEN FR66 TO FR68 + 3 INCHES, -Y765 IAW A320 53-00-14 & EA 200143.SDR USAA2011012090293Fan · defectiveFLT 1774 - DTW - ODOR - FORWARD CABIN RECIRCULATION FAN IS INOPERATIVE CAUSING STRONG ODOR THROUGHOUT AIR CONDITIONING SYSTEM. MAINTENANCE REMOVED AND REPLACED THE LT SIDE RECIRCULATION FAN IAW AIRBUS MAINTENANCE MANUAL 21-54-51-04.SDR USAA2010121393024Power Supply · dischargedFLT 1774 - MIA-CLT - EMERGENCY LIGHTS - FORWARD EMERGENCY POWER SUPPLY UNIT (EPSU) SHOWS BATTERY FAULT DURING BITE TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38. OPERATIONAL CHECK WAS GOOD.SDR USAA2010010590028Pin · corrodedPIT - GEAR CHANGE - MAJOR REPAIR - CORROSION ON LEFT MAIN LANDING GEAR PINTLE PIN FLANGE. REPLACED LEFT MAIN LANDING GEAR PINTLE PIN IAW JOB CARD 26T00032001.SDR USAA2009122993445Slide · loosePIT - EES - A CHECK - R1 DOOR SLIDE PACKED TOO LOOSE HITS FUSELAGE BEFORE DOOR LOCKS IN OPEN POSITION. REPLACED THE R1 DOOR SLIDE IAW TASK CARD 26L00025011.SDR USAA2009122893441Floor Panel · delaminatedSAL - Q4 - MAJOR REPAIR - CABIN FLOOR PANEL 222EF DELAMINATED BETWEEN FR15 TO FR20. FABRICATED & REPLACED CABIN FLOOR PANEL 222EF BETWEEN FR15 TO FR20.SDR USAA2009102392854Lens · missingFLT 1537 - DEN - EEL - ROW 10R EMERGENCY EXIT DOOR LIGHT MISSING LENS COVER. MAINTENANCE REPLACED LENS AS REQUIRED.SDR USAA2009091792560Lens · missingFLT 729 - DEN - EEL - SEAT 1C EMERGENCY LIGHT LENS MISSING. MAINTENANCE INSTALLED LENS AS REQUIRED.SDR USAA2009051191144Lens · brokenFLT 865 - PHL - EEL - 1C COVER TO FLOOR LEVEL EMERGENCY LIGHT BROKEN. MAINTENANCE REPLACED EMERGENCY LIGHT LENS AT 1C.SDR USAA920080919Electrical Box · defectiveFLT NR 1005 PHL-SJU - BURNING ODOR, CREW REPORTED ELECTRICAL SMOKE IN THE AFT CABIN AND DECLARED AN EMERGENCY. IT WAS REPORTED THAT THE ELECTRICAL SMOKE AND ODOR APPEARED TO BE GENERATED FROM THE 17A/B PASSENGER ENTERTAINMENT SYSTEM BOX. AIRCRAFT DIVERTED TOSDR SA07037Epsu · failedLAX - THE MID-CABIN, LEFT HAND EMERGENCY POWER SUPPLY UNIT FAILED THE OPERATIONAL CHECK. MAINTENANCE REPLACED THE MID-CABIN, LEFT HAND EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR SA07009Proximity Sensor · out of adjustPHX - FLT 1161 EN ROUTE MSP TO PHX. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT RAISE. AFTER A SECOND ATTEMPT, THE GEAR HANDLE DID GO UP, BUT THE GEAR DID NOT COME UP FOR ABOUT A MINUTE. AFTERWARDS, THE GEAR CAME UP AND ALL SYSTEMS WERE NORMAL FOR THE REST OF SDR SA06032Fuel Divider · faultyFLIGHT 25, BDA-PHL, APU AUTO SHUTDOWN TWICE AT FL380 AND FL320. MAINTENANCE FOUND EXCITER AND OIL PRESSURE FAULTS ON TEST PAGE OF MCDU. REMOVED AND REPLACED APU EXCITER, OIL PRESSURE SWITCH AND FLOW DIVIDER. APU FAULTS REMOVED, OPS AND LEAK CHECKS ARE GOOD.SDR SA06030Exciter · faultyFLIGHT 25, BDA-PHL - APU AUTO SHUTDOWN TWICE AT FL380 AND FL320. MAINTENANCE FOUND EXCITER AND OIL PRESSURE FAULTS ON TEST PAGE OF MCDU. REMOVED AND REPLACED APU EXCITER, OIL PRESSURE SWITCH AND FLOW DIVIDER. APU FAULTS REMOVED, OPS AND LEAK CHECKS ARE GOODSDR SA06029Idg · making metalFLIGHT 25, BDA-PHL - THE CREW REPORTED PROBLEMS WITH THE NUMBER 1 GENERATOR AND HAD TO DISCONNECT THE IDG. ALSO, WHILE EN ROUTE, ATTEMPTED TO START THE APU GENERATOR TWO TIMES UNSUCCESSFULLY. THE AC RETURNED TO THE FIELD IN BDA AND LANDED WITHOUT FURTHER PROSDR USAA060223Floor Panel · damagedAFT WET AREA FLOOR PANEL 261DF. REPLACED WITH MANUFACTURED PART PER SRM 53-02-00, DEFECT SIZE: 2 X 2 INCH.SDR USAA060224Floor Support · corrodedAROUND MOUNT HOLES, FLOOR SUPPORT BEAM -Y765 RT AT FRAMES 64 & 66. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-25503, DEFECT SIZE: 1 INCH DIA, TWO AREAS.SDR USAASA07009Landing Gear · faultyPHX FLT 1161 - EN ROUTE MSP TO PHX. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT RAISE. AFTER A SECOND ATTEMPT, THE GEAR HANDLE DID GO UP, BUT THE GEAR DID NOT COME UP FOR ABOUT A MINUTE. AFTERWARDS, THE GEAR CAME UP AND ALL SYSTEMS WERE NORMAL FOR THE REST OF SDR USAA060221Floorbeam · corrodedLOCATION: BEAM Y512 @ STA 66 ACTION: REMOVED & REPLACED PER SRM 51-72-11; CORR. LEVEL 1; TASK JA-260-53500 DEFECT SIZE: 3" X 76"SDR USAA060215Sill · corrodedFWD SIDE OF LEFT DOOR SILL AT STA 66 CORROSION. REMOVED AND REPLACED AFT DOOR SILL BEAM ANGLE PER SRM 53-41-14; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 1 X 7 INCH.SDR USAA060216Floorbeam · corrodedAT FLOOR SUPPORT Y354 AND C16 CORRODED. INSTALLED REPAIR & DOUBLER PER SRM 53-00-14; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 4' X 8".SDR USAA060217Seat Track · corrodedRAIL DUMMY AT Y510, C16 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: .75 INCH DIA AROUND MOUNT HOLE.SDR USAA060218Floorbeam · corrodedAT -Y81 FRAME 12-16 CORROSION. REPLACED BEAM WITH SAME P/N PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-220-53500, DEFECT SIZE: 1 X 2 X .040 INCH DEEP.SDR USAA060219Floorbeam · corrodedFLOORBEAM -Y1292, RIGHT STA 64-68 CORRODED. REMOVED & REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 3" X 9'.SDR USAA060220Floorbeam · corrodedFLOORBEAM Y1292 LEFT STA 66-68 CORRODED. REMOVED & REPLACED WITH IDENTICAL PART PER SRM 51-72-11; CORROSION LEVEL 1; TASK JA-260-53500, DEFECT SIZE: 3" X 9'.SDR SA06009Light · no testTHE EMERGENCY LIGHTS DID NOT ILLUMINATE FOR THE RT SIDE, OFF-WING ESCAPE SLIDE OPERATIONAL TEST. MAINTENANCE REPLACED THE RT SIDE, OFF-WING EPSU. (OPEN)SDR USAA06008Aspirator · leakingTHE AFT LT SLIDE FAILED TO INFLATE IN THE MINIMUM TIME REQUIRED DURING OPERATIONAL CHECK, AND DID NOT HOLD PRESSURE AFTERWARDS. ALSO, THE EMERGENCY EQUIPMENT LANYARD VELCRO WAS FOUND WEAK. MAINTENANCE INSPECTED THE SLIDE AND FOUND THE FLAPPER ASPIRATOR VALVESDR USA2004F00085Slide · unserviceableTHE RT SIDE REAR SERVICE DOOR HAS A SLIDE PACK STRAP EXTENDING OUT OF THE DOOR. MAINTENANCE REPLACED THE RT SIDE REAR SERVICE DOOR SLIDE ASSY. OK FOR SERVICE.SDR USA2004F00008Fan · odorENROUTE, THE FLIGHT CREW NOTED A STRONG ELECTRICAL ODOR AT FL 330 DURING CLIMB. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AIRCRAFT ON MEL AND RELEASED FOR SERVICE. MAINTENANCE REPLACED THE EXTRACT VALVE. OPS CHECKSDR USAASA03027Battery · inoperativeCLT - THE AFT EMERGENCY LIGHTS FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY PACK. OPERATIONALLY CHECKED OK. (M)SDR USAASA03047Doubler · damagedBOS - THE TELESCOPING PORTION OF THE GIRT BAR ASSEMBLY WAS FOUND TO COLLAPSE WITHOUT PULLING ON THE TRIGGER. ADDITIONALLY, THE DOUBLER WAS FOUND BEYOND LIMITS. MAINTENANCE REPLACED THE DOUBLER. OK FOR SERVICE. (M)SDR USAASA02063Computer · malfunctionedDURING CRUISE, THE CREW RECEIVED AN ECAM MESSAGE MESSAGE FOR A NR 1 ENGINE FIRE, HOWEVER NO MASTER WARNING OR BELLS OPERATED. SHORLY AFTERWARDS, RECEIVED ECAM MESSAGES FOR DUAL ENGINE FLAMEOUT AND AVIONICS SMOKE. ALL OTHER INDICATIONS WERE NORMAL, BUT A SMOK
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