N415US, cancelled Nov 4, 2003

Service difficulty reports · 26

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 = 'N415US' AND deregistration_id = 'N415US-2003-11-04'
  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 USAA020283Mount · wornPIT - FOUND ENGINE MOUNT WORN BEYOND LIMITS. MACHINED, CHAMFER, MPI, ROTOPEEN PER TYPICAL REP 50-50-08 REV B. (M)Jul 26, 2002 · N415US · Boeing 737401 · Engine Mount SectionSDR USAASB02004Battery Pack · dischargedPIT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT DIMS DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPLY ASSEMBLY PER MM 33-50-04. OPS CHECK GOOD. (M)Jan 6, 2002 · N415US · Boeing 737401 · Emergency LightingSDR USAASB01076Adc · failedCLT - FLT 2138 - ON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CAPTAIN REPORTED THAT THE NR 2 AIR DATA COMPUTER HAD FAILED RESULTING IN LOSS OF THE FIRST OFFICERS ALTIMETER AND AIRSPEED INDICATIONS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENMar 10, 2001 · N415US · Boeing 737401 · Air Data ComputerSDR USAASB00143Circuit Board · failedPIT - FLT 710 - AFTER TAKEOFF AND GEAR RETRACTION FROM PIT, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY TWO MINUTES. CREW RECYCLED GEAR AND LGHT EXTINGUISHED. FLIGHT CONTINUED ON TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE May 16, 2000 · N415US · Boeing 737401 · Landing Gear Position and WarningSDR USAA990305Frame · crackedCLT - DURING VISUAL CHECK INSPECTION, FOUND A 3 INCH CRACK ON FRAME STATION 870 BL 0 BOTTOM FLANGE. REMOVED CRACKED SKIN, FILLER AND REPAIRED PER SRM 53-00-07. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, FrameSDR USAA990288Skin · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION BS 757 BL 0 SKIN. INSTALLED DOUBLER PER SRM 53-00-01. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA990284Support · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT BS 330, WL 208.10 AND RBBL 52 FLOOR SUPPORT. REPLACED FLOOR SUPPORT PER SRM 51-10-02. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990283Skin · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .1 INCH BY .4 INCH AREA OF CORROSION AT BS 797 BL 0 SKIN. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA990277Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AROUND NUT PLATES BS 986 LBL 44 - RBL 30 'T' CAP OF FLOORBEAM. CORROSION TASK NR C53-107-02. REPAIRED PER TR 53-60-01. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990255Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .800 INCH CRACK AT FORWARD FRAME OF AFT CARGO DOOR 2 INCH ABOVE FORWARD LATCH ARM. INSTALLED DOUBLER PER SRM 52-30-02. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990254Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 807 OBL FRAME. INSTALLED REPAIR PLATE AND FILLERS PER SRM 53-00-07. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, FrameSDR USAA990234Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 277 STRINGER 24L TIE CLIP. REPAIRED PER SRM 51-10-02. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990225Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION AT NUT PLATE HOLES BS 947 LBL 24 - RBL 24 FLOORBEAM, CORROSION TASK NR C53-107-02. INSTALLED REPAIR 'T' SECTION AND REPAIR ANGLE PER SRM 53-00-51. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990217Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK BS 294 WL 208.10 RBBL 55 ANGLE STIFFENER. REPAIRED PER SRM 51-10-02. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990216Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 294, WL 208.10 RBBL 55 FRAME. INSTALLED DOUBLER PER SRM 51-70-11 EA 63977. (M)Apr 1, 1999 · N415US · Boeing 737401 · Fuselage Main, FrameSDR USAA950564Floorbeam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 10 INCHES CORRODED AREA ON FLOORBEAM AT STATION 967 RBL 9 TO RBL 36. REPAIRED PER EA 39247. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)May 9, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950563Intercostal · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT STATION 967 TO 986.5, LBL 17. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)May 3, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950565Angle · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 36 INCHES OF CORROSION, AFT ENTRY THRESHOLD. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)May 2, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950560Support · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA CORRODED ON FLOOR SUPPORT AT STATION 947 TO STATION 967, LBL 50. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)May 2, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950559Floorbeam · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH AREA ON FLOORBEAM, CORRODED AT STATION 947, LBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Apr 28, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950558Floorbeam · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 5 INCH CORROSION ON FLOORBEAM AT STATION 947, RBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Apr 28, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA950567Door Sill · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH DIAMETER AND 3 INCH DIAMETER SPOTS OF CORROSION 40 TO 50 PERCENT LOSS TO .375 INCH DIAMETER 100 PERCENT LOSS 3 INCH BY 4 INCH CORROSION BS 807 TO BS 845 ON DOOR SILL BELOW AFT CARGO DOOR. REPAIRED PER SRMApr 27, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950562Intercostal · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 7 INCH BY 1 INCH CORROSION ON INTERCOSTAL BETWEEN BS 947 AND BS 967 RBL 25 INCHES. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M)Apr 26, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950561Intercostal · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 1 INCH TOTAL CORROSION ON INTERCOSTAL, BETWEEN BS 967 AND BS 947 LBL 16 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-10-02, CORROSION LEVEL 2. (M)Apr 25, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950566Angle · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 2 INCHES BY 30 INCHES 'Z' ANGLE IN THRESHOLD OF AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-2, CORROSION LEVEL 2. (M)Apr 24, 1995 · N415US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA950557Floorbeam · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION (FULL WIDTH OF T-CAP) STATION 986.5 FLOORBEAM FROM 44 LBL TO 44 RBL. REPAIRED PER SRM 51-70-13 EA 39205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)Apr 24, 1995 · N415US · Boeing 737401 · Fuselage Main, Floor Beam
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