N572FE
Service difficulty reports · 258
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 = 'N572FE' 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 = 'N572FE' 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 FDEA200906222232Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT OTBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. REPAIR CARRIED OUT AS PER EA 1-5750-130978, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6- 2-100 RESDR FDEA200906222231Hinge Bracket · corrodedLT WING INBD FLAP OTBD HINGE (FLAP SIDE) PIVOT PIN ATTACHMENT INBD BORE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03 REVISION 64. EXISTING HOLE DIAMETER = 1.1885", FINAL HOLE DIAMETER = 1.252". REPAIR CARRIED OUT AS PER EA 1-5750SDR FDEA200906192176Trunnion · crackedNLG LT WEB TRUNNION FITTING FWD SIDE FOUND WITH CRACK. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS.SDR FDEA200906192175Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA LONGERON 51R FOUND CORRODED BETWEEN STA 1019 AND STA 1039. TRIMMED OUT AND CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192174Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA RT LONGERON 51R FOUND CORRODED AT STA 6-30. REPAIR CARRIED OUT AS PER E.A. 1-5310-131616, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192173Longeron · corrodedFWD CARGO COMPARTMENT BILGE AREA LONGERON 52 AND SPLICE FITTING FOUND CORRODED AT STA 1119 TO 6-30. REPAIR CARRIED OUT AS PER E.A. 1-5310-131617, . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192172Skin · chafedFWD CARGO COMPARTMENT DOOR CUT-OUT AFT LOWER SECTION FOUND EDGE CHAFING. CARRIED OUT DOUBLER REPAIR AS PER SRM 53-50-00 FIGURE 17 VOLUME I REVISION 40. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200906192171Fitting · corrodedBARREL NUT HOLES INSPECT/REPAIR - RT NR 26 FITTING FOUND BORE HOLE CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II REV 40. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 107
Back to N572FE