N253UP

Service difficulty reports · 363

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 = 'N253UP' 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 UPS02M39085Shear Tie · corrodedINSPECTION TYPE:C, AFT CARGO BILGE AREA FRAME SHEAR TIE FOUND WITH CORROSION AT STA 1953 LONG 51 RT - 52 RT. CORROSION FOUND EXCEEDING LIMIT ON SHEAR TIE AT STA 1953 LONG 51 RT - 52 RT AS PER SRM 53-00-01 VOL I REV 31. SHEAR TIE & SURROUNDING PARTS REMOVED IJul 1, 2002 · N253UP · Doug MD11F · Fuselage Main, StructureSDR UPS02M39083Floorbeam · corrodedINSPECTION TYPE:C, AFT CARGO CORROSION ON FLOORBEAM UPPER CHORD AT STA 1902 0-20 RBL. CORROSION TRIMMED OUT IAW SRM 53-00-01 FIG 9. HFEC INSPECTION CARRIED OUT, NO CRACKS FOUND ON TRIMMED AREA. REPAIR ANGLE & FILLER, FAB & INSTALLED IAW SRM 53-00-01 VOL I &Jun 30, 2002 · N253UP · Doug MD11F · Fuselage Main, Floor BeamSDR UPS02M39031Seat Track · corrodedINSPECTION TYPE:C, AFT CARGO CORROSION ON SEAT TRACK BETWEEN STA 1841 - 1887 LBL 20. CORROSION FOUND EXCEEDING LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK REMOVED, REWORKED IAW DWG AGA3855 AND INSTALLED AS PER SRM 51-31-01 VOL II REV 31.Jun 30, 2002 · N253UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39084Shear Tie · corrodedINSPECTION TYPE:C, AFT WASTE COMPARTMENT STA 1974 BETWEEN LONGERON 50L - LONGERON 50R FOUND CORROSION ON SHEAR TIE. CORROSION FOUND EXCEEDING ON SHEAR TIE AS PER SRM 53-00-01 VOL I REV 31. SHEAR TIE & SURROUNDING PARTS REMOVED IAW SRM 51-35-01 & SRM 51-33-01Jun 24, 2002 · N253UP · Doug MD11F · Fuselage Main, StructureSDR UPS02M38949Floorbeam · corrodedINSPECTION TYPE:C, CTR CARGO STA 1841, BL 0 - RBL 60 FLOORBEAM WEB FOUND CORRODED. FLOORBEAM WEB REMOVED AND REPLACED AS PER DWG AGA7170 AND INSTALLED AS PER SRM 51-35-01 VOL II REV 31.Jun 19, 2002 · N253UP · Doug MD11F · Fuselage Main, Floor BeamSDR UPS02M39082Intercostal · corrodedINSPECTION TYPE:C, FWD CARGO COMPT LT INTERCOSTAL BETWEEN STA 840-859 LONGERON 32 FOUND CORRODED. CORROSION FOUND EXCEEDING LIMIT AT STA 840-859 LONGERON 32 IAW SRM 53-00 -01 FIG 4 VOL 1 REV 31. INTERCOSTAL REMOVED, FABRICATED NEW INTERCOSTAL IAW DWG ACA7043Jun 17, 2002 · N253UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS02M39177Seat Track · corrodedINSPECTION TYPE:C, CABIN SEAT TRACK AT STA 1964 LBL 76 FOUND CORRODED. SEAT TRACK CORROSION BLEND OUT FOUND EXCEED SRM LIMIT PER SRM 53-70-00 FIG 3 VOL I REV 31. SEAT TRACK REPAIR CARRIED OUT AT STA 1831-2007 X=107.25 PER SRM 53-70-00 FIG 1 VOL I REV 31.Jun 5, 2002 · N253UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M38775Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 612 RBL 8.5 FOUND CORRODED. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53-70-00 FIG 3 VOL 1 REV 31. SEAT TRACK REMOVED AND REPLACED FROM STA 605-645 RBL 8.5 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31.Jun 5, 2002 · N253UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M39086Support · corrodedINSPECTION TYPE:C, CENTER CARGO PANEL SUPPORT STRUCTURE AT STA 1841, LBL 30 TO RBL 30 CORRODED. SUPPORT REMOVED AT STA 1841 IAW SRM 51-35-01 VOL II REV 31. NEW SUPPORT INSTALLED IAW SRM 51-35-01 VOL II REV 31.May 30, 2002 · N253UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS02M38946Floorbeam · corrodedINSPECTION TYPE:C, FLOORBEAM AT STA 1841 LBL 27 FOUND CORRODED. FLOORBEAM WEB AT STA 1841 LT REMOVED AND REPLACED AS PER DWG:AGA7170 AND INSTALLED AS PER SRM 51-35-01 VOL II REV 31.May 30, 2002 · N253UP · Doug MD11F · Fuselage Main, Floor BeamSDR UPS02M38777Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 806-840 RBL 8 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-70-00 FIG 3 VOL 1. SEAT TRACK REMOVED AND REPLACED AT STA 799-869 RBL 8 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31.May 30, 2002 · N253UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M38776Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 870-899 LBL 8 FOUND CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-70-00 FIG 3 REV 31. SEAT TRACK REMOVED AND REPLACED AT STA 816-929 AS PER SRM 53-70-00 FIG 1 VOL 1 REV 31.May 30, 2002 · N253UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS02M38951Frame · crackedINSPECTION TYPE:C, EXTENDED TAIL CONE AFT CONE GUIDE PIN LOCATING BLOCK ATTACHMENT FRAME AT CANT STA 2258.846 FOUND CRACKED. EXTENDED TAIL CONE CRACKED AREA TRIMMED AND REPAIR CHANNELS AND ANGLES FABRICATED AS PER SRM 53-00-01 FIG 9 VOL I REV 31. REPAIR CHANMay 29, 2002 · N253UP · Doug MD11F · Aerodynamic Fairings
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