N719FD

Service difficulty reports · 159

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 = 'N719FD' 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 05FDEA04425Switch · looseAVIONICS LIGHT, CHIME CAME ON PASSING 10000, EXECUTED TURNBACK TO KSMP BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE/ RETIGHTENED. SWITCH OPDec 30, 2005 · N719FD · Airbus A300F4622R · Door Warning SystemSDR 06FDEA0001Switch · looseAVIONICS LIGHT, CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LANDING WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCHDec 30, 2005 · N719FD · Airbus A300B4622R · Door Warning SystemSDR 05FDEA04426Switch · looseAVIONICS LIGHT/CHIME CAME ON PASSING 10000 EXECUTED TURNBACK TO KSMP. BURN TO MAX LNDG WEIGHT. FOUND AVIONICS DOOR FLUSH TO FUSELAGE AND DOOR LATCH APPROX 1/8 INCH DOWN. ON INSPECTION FOUND DOOR LOCKED SWITCH WITH BROKEN SAFETY WIRE. RETIGHTENED SWITCH. Dec 30, 2005 · N719FD · Airbus A300B4622R · Door Warning SystemSDR 05FDEA04042Smoke Detector · malfunctionedAVIONICS SMOKE WARN DURING CLIMB-OUT. COMPLIED WITH CHECKLIST. DID NOT SMELL SMOKE. RETURNED TO KMCO. REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR 13WA. OPERATIONAL TEST WAS NORMAL. REF A300 M/M 26-15-12-4 AND 26-15-00-5. R/I FROM FACT PREMATURE REMOVALNov 30, 2005 · N719FD · Airbus A300B4622R · Smoke DetectionSDR 05FDEA01685Frame · damagedFRAME 41 LT SIDE BETWEEN STRINGERS 25 AND 26 FRAME FITTING HOLE H1 HAS A BUSHING INSTALLED WITH A FASTENER HOLE AT 2ND OVERSIZE AT .278 DIA FOUND UPON REMOVAL OF FASTENER FOR NDT ON EO 6-5310-7-5006 PT3 REF N CARD N00059. COMPLIED WITH EA 6-5310-90201 PT1.Jun 24, 2005 · N719FD · Airbus A300B4622R · Fuselage Main, FrameSDR 05FDEA01684Frame · damagedFRAME 46 RT SIDE AT STRINGER 27 FRAME FITTING HOLE NR H1 HAS A BUSHING IN THE FITTING MEASURING AT .436 DIA WITH A 2ND OVERSIZE HOLE AT .278 DIA FOUND UPON REMOVAL OF FASTENER ON EO 6-5310-7-5006 PT4 REF N CARD N00062. COMPLIED WITH EA 6-5310-90201 PT1.Jun 24, 2005 · N719FD · Airbus A300B4622R · Fuselage Main, FrameSDR 05FDEA01683Frame · damagedFRAME 45 RT SIDE JUST ABOVE STRINGER 27 FRAME FITTING HOLE NR H2 MEASURE AT .372 DIA UPON REMOVAL OF FASTENER FOR NDT ON EO NR E6-5310-7-5006 PT 4. REF N CARD N00061. COMPLIED WITH EA 6-5310-90201 PT2.Jun 24, 2005 · N719FD · Airbus A300B4622R · Fuselage Main, FrameSDR 04FDEA02463Pump · leakingLOST NEARLY ALL GREEN HYDRAULIC QUANITY DURING CRUISE AT FL 290. FOUND LT HYD PUMP SHAFT SEAL LEAKING. REMOVED AND REPLACED LT OR FWD HYD PUMP ON NR 2 ENG ISW M/M 29-11-32-4-1, OPS AND LEAK CHECK, GOOD.Aug 12, 2004 · N719FD · Airbus A300B4622R · Hydraulic Pump (Electric/Engine), MainSDR 04FDEA01276Smoke Detector · faultyINFLIGHT AVIONIC SMOKE WARNING AT FL 310 SEVERAL WARNINGS ON AND OFF DURING ICING CONDITIONS THEN OFF WHEN CLEAR FOR SEVERAL MIN THEN ON CONTINUOUSLY. DIVERTED INTO DEN 170NM OUT, FOLLOWED ECAM PROCEDURES NEVER NOTICED ANY SMOKE. UNEVENTFUL LANDING AND TAXIMay 15, 2004 · N719FD · Airbus A300B4622R · Smoke Detection
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