N761CX
Service difficulty reports · 209
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 = 'N761CX' 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 = 'N761CX' 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 IXXA10WSAP005SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND CORRODED FASTENERS ON RT WING BETWEEN STATION WS404- WS538. REMOVED CORRODED FASTENERS. INSTALLED NEW FASTENERS IAW SRM 51-40-02 REV 101 AND SRM 51-20-01 REV 101.SDR IXXA10WSAP004SAccess Panel · corrodedDURING ROUTINE C-CHECK INSP FOUND CORROSION ON RT WING ACCESS PANEL NR 633AB, 642AB, 642BB AND 642CB. REMOVED CORROSION. FOUND TO BE WITHIN LIMIT’S. PERFORMED NDT. NO CRACK’S OR CORROSION. CLEANED, TREATED AND PRIMED AREA IAW SRM 57-20-01 FIGURE 201 REV 10SDR IXXA10WSAP003SFairing · erodedDURING ROUTINE C-CHECK INSP, FOUND LT WING OTBD T/E FLAP SUPPORT FAIRING FWD FAIRING EXTERIOR SURFACE ERODED. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101 AND MM 51-21-10-REV 97.SDR IXXAWSAP002SAccess Panel · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FUEL PUMP ACCESS PANEL NR 631AB CRACKED. REMOVED CRACKED ACCESS PANEL. INSTALLED NEW PANEL IAW MM 20-11-000 REV 97.SDR IXXA10WSAP001SFairing · erodedDURING ROUTINE C CHECK INSP, FOUND EROSION ON THE LT WING OTBD T/E FLAP INBD FLAP SUPPORT FAIRING FORWARD AND MID FAIRING EXTERIOR SURFACE. ACCOMPLISHED REPAIR IAW SRM 51-70-06 REV 101, AND MM 51-21-10 REV 97.SDR IXXA090067OEngine · vibrationDURING CRUISE, THE CREW NOTICED AN ABNORMAL VIBRATION FROM THE NR 2 ENG, THEN A LOSS OF OIL PRESSURE AND OIL QUANTITY. SHUTDOWN NR 2 ENG AND RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT.SDR ABXR080228Skin · dentedOUTWARD DENT STA 544, STRINGER 31-30 LT REQUIRES REPAIR. REPAIRED AREA IAW B767 SRM 53-00-01, FIGURE 201. (S)SDR ABXR080226Skin · damagedAPPROX 6 INCH CREASE AT STA 1510, LONGERON STRINGER 36-35 LT, BELOW BULK CARGO DOOR IS OUT OF LIMITS. REPAIRED SKIN IAW B767-200 SRM 53-60-1. (S)SDR ABXR080225Skin · damagedSCREW AND COUNTERSINK WASHER INSTALLED IN FUSELAGE SKIN OVER PREVIOUSLY BLENDED AREA AT APPROX STA 615 LONGERON STRINGER 34 RT. DAMAGED AREA COMPLIED WITH ON PREVIOUS REPAIR. (S)
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