N256UP

Service difficulty reports · 357

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 = 'N256UP' 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 UPS05M45360Seat Track · corrodedCABIN SEAT TRACK AT STA 824-840 LBL =107.25 FOUND SEVERAL PLACES CORRODED. SEAT/T CORROSION REMOVED FOUND OUT OF LIMIT, (ORI THK 0.080" AND MAT REMOVED THK 0.030", PER SRM 53-70-00.F3.V.1.R37. DAMAGED PORTION OF SEAT/T CUT REMOVED. SPLICE AND NEW SEAT/TRACKAug 17, 2005 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45521Structure · corrodedRT HORIZ STAB BARREL NUT BORE NR 22R FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01.V2R37, B/N HOLE 22R REAMED TO 1.067" AND REMAINING BLEND OUT 0.020" DEEP, FOUND OUT OF LIMIT. REWORKED B/N HOLE 22R BORE RADIUS SMOOTHENED AND PROTECTED PER SRM 51-Aug 15, 2005 · N256UP · Doug MD11F · Horizontal Stabilizer StructureSDR UPS05M45582Longeron · corrodedINSPECTION TYPE:C, CABIN ANGLE FITTING BETWEEN STA 1239-1256 LONGERON 27 RT FOUND CORRODED. CORROSION REMOVED AT CABIN AREA STA 1239 TO 1256, FOUND OUT OF LIMIT. ORIG THK 0.238" & MAT REMOVED IS 0.090" PER SRM 53-00-01 F3.V1 R.37. ANGLE FITTING BRACKET REMJul 20, 2005 · N256UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR UPS05M45361Seat Track · corrodedINSPECTION TYPE:C CABIN STA 1321-1521 LBL=75.25 FOUND SEAT TRACK CORRODED IN SEVERAL PLACES. CORROSION REMOVED & FOUND BEYOND LIMIT PER SRM 53-70-00 F.3.V1.R.37 THK REMAINED 0.050" & ORI THK 0.100" MAT. SEAT/T FASTENERS REMOVED FOR ACCESS & SPICE CUT AT STA Jul 19, 2005 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45362Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK BETWEEN STA 1341-1381 RBL =75.5 FOUND CORRODED. CORROSION REMOVED & FOUND BEYOND LIMIT PER SRM 53-70-00 V1.REV.37.REMAINED THK 0.040" & ORI THK 0.100".SEAT/T FASTENERS REMOVED FOR ACCESS & SPLICE CUT AT STA 1266 & 1391 PER SJul 18, 2005 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45359Seat Track · corrodedCABIN SEAT TRACK AT STA 1841-1921 RBL = 107 FOUND CORRODED IN SEVERAL PLACES CABIN SEAT/T AT STA 1841-1921 RBL 107 CORROSION REMOVAL C/OUT PER SRM 53-70-00 V1.R.37, FOUND OUT OF LIMIT ORI THK 0.080" AND MAT REMOVED BEYOND ACCEPTED LIMIT. SEAT/T FASTENERS REMOJul 18, 2005 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS05M45358Seat Track · corrodedCABIN SEAT TRACK AT STA 1963 LBL =107 FOUND CORRODED CABIN SEAT/T AT STA 1963 LBL 107 SEAT/T CROWN 0102 CORROSION REMOVAL C/OUT FOUND MAT REMOVED OUT OF LIMIT (ORI THK 0.145" AND MAT REMOVED 0.0 55") AS PER SRM 53-70-00 FIG 3 V1 R.37. REMOVE SEAT/T FASTENERS Jul 18, 2005 · N256UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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