Boeing 737-217

Service difficulty reports · 308

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '737217'
  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 CAL950098Belt Frame · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN BELT FRAME AT BS 420, STR 22L. THE CRACK WAS REPAIRED IAW BOEING DRAWING 65C25113. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950097Frame · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN STA 578 MAIN CABIN FRAME AT STR 16 - STR 17L. THE FRAME WAS REPAIRED IAW SRM 51-40-3 AND SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, FrameSDR CAL950096Stringer · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STR 5R AT STA 685. THE CRACK WAS STOP DRILLED AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-10-3. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Longeron/StringerSDR CAL950095Chord · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN RT STA 727 OUTBOARD CHORD AT STR 18A. THE CRACKED CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65C33722. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Miscellaneous StructureSDR CAL950094Floor Panel · corrodedGSO - INSPECTION FOUND THE NR 6 FLOOR PANEL SUPPORT CORRODED AT STA 312. THE PANEL SUPPORT WAS REPAIRED IAW SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Floor PanelSDR CAL950093Floorbeam · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN STA 639 LT SIDE FLOORBEAM WEB CABLE CUTOUT. THE FLOORBEAM WEB WAS REPAIRED IAW BOEING DRAWING 65C25211. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Main, Floor BeamSDR CAL950092Frame · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN FORWARD ENTRY DOOR FORWARD FRAME CUT OUT AT UPPER HINGE ARM. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 51-10-2, AND SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Emergency ExitsSDR CAL950091Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT BS 508 BETWEEN STR 28L AND STR 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Feb 1, 1995 · N14233 · Boeing 737217 · Fuselage Miscellaneous Structure
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