N185DN

Service difficulty reports · 255

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 = 'N185DN' 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 DL76L961651Control Cable · severedDURING CLIMB, FLIGHT CREW HEARD A CRACK FOLLOWED BY A/C ROLL TO THE LEFT. TEMPORARILY LOST LEFT IDG BUT QUICKLY RETURNED. FOUND AILERON CONTROL CABLE A2B-3 SEVERED AND RIGHT GENERATOR FEEDER CABLE WORN JUST FORWARD AND RIGHT OF THE FORWARD CARGO COMPARTMENT Jun 25, 1996 · N185DN · Boeing 767332 · Aileron Control SystemSDR DL76L961525Control Cable · brokenON CLIMBOUT THROUGH 5000 FT, LOST RIGHT GENERATOR. NO EICAS MESSAGES. ALMOST CONCURRENT WITH GEN LOSS, EXPERIENCED LEFT AILERON HARD OVER WITH NO ASSOCIATED EICAS CAUTION OR STATUS MESSAGE. REPLACED A2B-3 AILERON CONTROL CABLE.Jun 25, 1996 · N185DN · Boeing 767332 · Aileron Control SystemSDR DL76L953988Eec · malfunctionedRT ENGINE COMPUTED THRUST LIMIT INDICATOR IN EPR GAUGE INDICATES APPROXIMATELY .10 LOW IN CRUISE, LT ENGINE 1.69 RT ENGINE 1.57. REPLACED RT ENG EEC, R/U OK AT HIGH POWER. R/U REP TEST 15 PFHB.Oct 12, 1995 · N185DN · Boeing 767332 · Fuel Control/Turbine EnginesSDR DL76L953241Actuator · brokenLE FLAP ASYMMETRY MSG ILLUMINATED AT 100 FEET AIRBORNE ON TAKEOFF. FLAPS RET PER MAINT CORD. INSTRUCTIONS VISUAL INSP BY F/O REVEALED LE SLATS EXTENDED APROX 6 INCHES FROM UP. RETURNED JFK. FOUND NR 6 SLAT ACTUATOR ROD BROKEN IN HALF PREVENTING FULL RETRAJul 31, 1995 · N185DN · Boeing 767332 · Leading Edge Slat ActuatorSDR DL76L953236Prox Sw · failedLEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED AS FLAPS WERE RETRACTED FROM 5 TO 1 DEGREES. CORRECTIVE ACTION: REPLACED PROX SWITCH ELECTRONICS UNIT. BITE AND OPS CHECK NOW OK.Jul 31, 1995 · N185DN · Boeing 767332 · Leading Edge Slat Control System
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