N710TW

Service difficulty reports · 256

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 = 'N710TW' 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 ZW0A0303604Light · inoperativeTHE MOST FORWARD EGRESS LIGHT STRIP IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPAIRED BROKEN FEEDER SYSTEM. CHECK-C 11-14-01 MCI.Mar 30, 2003 · N710TW · Boeing 7572Q8 · Emergency LightingSDR ZW0A0211201Power Supply · dischargedTHE EMERGENCY LIGHTS AT THE RH SIDE NUMBER 3 CABIN DOOR, AND AT THE MID LAVATORY AREA, WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT THE R3 DOOR. CHECK-C 11-14-01 MCI. --CLOSED--Nov 8, 2002 · N710TW · Boeing 7572Q8 · Emergency LightingSDR ZW0A0203601Lamp · burned outRIGHT FWD AND LEFT FWD EMERGENCY DOOR SLIDE LIGHTS INOP. RELAMPED RIGHT FWD AND LEFT FWD EMERGENCY SLIDE LIGHTS. LAST CHECK C PERFORMED 14NOV2001 MCI --CLOSED--Mar 26, 2002 · N710TW · Boeing 7572Q8 · Emergency LightingSDR TWAA0105502Light · inoperativeTHE EGRESS LIGHT WAS INOPERATIVE BY THE LEFT SIDE LAV AND AT SEAT ROW 1 LEFT SIDE. REPLACED THE LAMP AT BOTH LOCATIONS. CHECK-C 5-4-00 LAX.Mar 27, 2001 · N710TW · Boeing 7572Q8 · Emergency LightingSDR 99ZZZX3574Blade · failedENGINE SURGED WITH OVERTEMP - METAL IN BLEEDS. DISASSEMBLED, INSPECTION DISCLOSED FAILURE OF 6TH STAGE COMPRESSOR BLADE. BLADES WILL BE FORWARDED TO P&W ENGINEERING FOR ANALYSIS. CYCLES, 2,867.Sep 15, 1999 · N710TW · Boeing 7572Q8 · Turbine Engine Compressor SectionSDR TWAA9818404Skin · crackedDURING CHECK-C MAINT, FOUND LEFT WING LEADING EDGE. BULLNOSE CRACK 10 INCH LONG ON COMPOSITE PANEL LOCATED AFT OF AND BETWEEN NR 3 AND 4 LEADING EDGE SLATS. INSTALLED 3 IN BY 10 IN HOT BOND REPAIR PER SRM 57-41-01 AND 51-70-07.Nov 3, 1998 · N710TW · Boeing 7572Q8 · Wing, Plate/Skin
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