N118US

Service difficulty reports · 266

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 = 'N118US' 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 SA06052Lanyard · tornLAX - DURING INSPECTION, FOUND THE R-1 DOOR EMERGENCY SLIDE/RAFT YELLOW LANYARD TORN. MAINTENANCE RELEASED THE AIRCRAFT ON MEL.Jul 10, 2006 · N118US · Airbus A320214 · Escape SlideSDR USAA060398Beam · corrodedFOUND CORROSION ON BEAM Y1292 FR 66-68. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11; CORROSION TASK JA-260-53500, DEFECT SIZE: 0.5" AND 1.0".Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Main, StructureSDR USAA060405Beam · corrodedFR 68 AT -Y1292; CORROSION TASK JA-260-53500. REPLACED BEAM PER SRM 51-72-11, DEFECT SIZE: .75 X 4 INCH.Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Main, StructureSDR USAA060397Beam · corrodedY1292 AFT OF FR 68 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 0.5 X 0.75 INCH.Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Main, StructureSDR USAA060399Beam · corrodedY503.2 BETWEEN FRAME 14 & 16 CORRODED. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 0.5 X 1.0 INCH.Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Main, StructureSDR USAA060400Floor Panel · puncturedFOUND PUNTURE FLOOR TOP SURFACE CENTER PANEL NR 261DF. REMANUFACTURED PANEL PER AIRBUS SRM 53-02-00 AND MCGILL MANUAL, DEFECT SIZE: 1/2" X 1/2".Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Floor PanelSDR USAA060401Sill · corrodedFOUND SILL BEAM CORRODED RIGHT AFT DOOR SILL AT FRAME 66; CORROSION TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 53-41-14, 51-42-11, DEFECT SIZE: 1" DIA.Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA060402Sill · corrodedFOUND AFT LT DOOR SILL FS 66; CORROSION TASK JA-260-53500. CUT OUT CORROSION AND REPLACED WITH FILLER AND ANGLE PER SRM 53-41-41, DEFECT SIZE: 1/4" X 1/4".Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA060403Shear Tie · corrodedFOUND CORROSION LT AFT SHEAR TIE; CORRODED TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 1/4" X 1/4".Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Internal Mounting StructureSDR USAA060404Beam · corrodedFOUND BEAM CORRODED BETWEEN FS 66 - 68 AT -Y1292; CORROSION TASK JA-260-53500. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-72-11, DEFECT SIZE: 2" X 6".Mar 2, 2006 · N118US · Airbus A320214 · Fuselage Main, StructureSDR SA05117Precooler · damagedCLT FLT 1130 WHILE EN ROUTE, THE NR 1 ENGINE BLEED SYSTEM INDICATED INOPERATIVE WHEN ECAM MESSAGE -AIR L WING LEAK-, GENERATED. WITH THE NR 2 ENGINE BLEED SYSTEM ON MEL, THE AIRCRAFT DID NOT HAVE SOURCE AIR TO MAINTAIN CABIN PRESSURE, CAUSING BOTH AIR CONDITNov 19, 2005 · N118US · Airbus A320214 · Pneumatic Distribution SystemSDR SA05079Apu · leakingICT FLT 100 EN ROUTE SAN TO PHL - DURING THE FLIGHT, THE NR 1 IDG LOW OIL PRESSURE LIGHT ILLUMINATED. THE IDG WAS DISCONNECTED PER PROCEDURES. SHORTLY AFTER THE APU WAS STARTED, THE APU HAD AN AUTO-SHUTDOWN. THE FLIGHT DIVERTED TO THE NEAREST SUITABLE AIRJun 23, 2005 · N118US · Airbus A320214 · APU Oil SystemSDR SA05070Fuel Control · failedEN ROUTE, PHL TO SFO - DURING FLIGHT, THE APU AUTO-SHUTDOWN WITH THE NR 1 ENGINE IDG ON MEL. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE APU WITH 2.5 QUARTS OF OIL AND TIGHTENED A LINE TO THE APU FUEL CONTROLJun 12, 2005 · N118US · Airbus A320214 · APU Engine Fuel and ControlSDR SA05059Lanyard · missingDCA - AFT RIGHT DOOR SLIDE/RAFT ASSEMBLY SURVIVAL LANYARD AND RELEASE SNAP FOUND MISSING. REPLACED AFT RIGHT DOOR SLIDE/RAFT ASSEMBLY. OK FOR SERVICE.Jun 1, 2005 · N118US · Airbus A320214 · Escape SlideSDR USAASA03112Battery · inoperativeRECEIVED 'EPSU BATTERY EMER R' MESSAGE WHEN PERFORMING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE BATTERY IN THE MID-CABIN, RIGHT SIDE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)Sep 10, 2003 · N118US · Airbus A320214 · Emergency LightingSDR USAASA01070Battery · dischargedCLT - THE AFT LEFT PSEU EMERGENCY LIGHT BATTERY SUPPLY WAS LOW. MAINTENANCE REPLACED THE AFT LEFT PSEU BATTERY SUPPLY. OPERATIONALLY CHECKED OK. (M)Dec 28, 2001 · N118US · Airbus A320214 · Emergency Lighting
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