N24SW, cancelled Oct 7, 1997
Service difficulty reports · 18
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 = 'N24SW' AND deregistration_id = 'N24SW-1997-10-07' 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 = 'N24SW' AND deregistration_id = 'N24SW-1997-10-07' 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 SWAA961072Chord · crackedDURING SCHEDULED TERMINAL CHECK, FOUND BS 727 OUTBOARD CHORD CRACKED AT S18A, LEFT SIDE. FORWARD HOLE. REPAIRED PER BOEING SRM.SDR SWAA961025Guide Plate · crackedDURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR FRAME UPPER HINGE GUIDE PLATE CRACKED BETWEEN FASTENERS TO EDGE. REPLACED WEB PER BOEING SRM.SDR SWAA960980Floorbeam · crackedDURING SCHEDULED C1 CHECK, FOUND FLOORBEAM T-CAP AT BS 312 CRACKED ABOVE FWD UPPER AIRSTAIR DOOR STOP AT LWR RADIUS. REPAIRED PER BOEING SRM.SDR SWAA960979Skin · crackedDURING SCHEDULED C1 CHECK, FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT FWD ENTRY DOOR CUTOUT UPPER FWD CORNER. REPAIRED PER SWA ACO 6317-53.SDR SWAA960978Ceiling · crackedDURING SCHEDULED C1 CHECK, FOUND A 4.5 CRACK IN NOSE WHEEL WELL CEILING RIGHT SIDE JUST AFT OF MANUAL GEAR EXTENSION RETURN SPRING BRACKET. REPAIRED PER BOEING SRM.SDR SWAA960965Pwr Supply · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN CEILING LIGHT INOP. REPLACED POWER SUPPLY PER BOEING M/M.SDR SWAA960865Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 9R CRACKED AT BS 727B. REPAIRED PER BOEING SRM.SDR SWAA960864Clips · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS CRACKED AT 10R, BS 727, AND AT 9R, BS 727B. REPLACED PER BOEING SRM.SDR SWAA960863Clips · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIPS 3L CRACKED AT BS 559, S3R, S4R AND S5R CRACKED AT BS 559, AND S5L AT BS 578. REPLACED ALL PER BOEING SRM.SDR SWAA960862Clip · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER TIE CLIP 10R CRACKED AT BS 597. REPLACED PER BOEING SRM.SDR SWAA960861Stringer · crackedDURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER 10R CRACKED AT BS 727B. REPAIRED PER BOEING SRM.SDR SWAA950677Oil Temp Ind · malfunctionedEXPERIENCED NR 1 ENGINE OIL HIGH OIL TEMP. CREW PERFORMED ENGINE SHUT-DOWN CHECK LIST. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE. REPLACED OIL TEMP INDICATOR, OIL TEMP BULB, OIL, AND MAIN OIL FILTER.SDR SWAA950391Bulkhead · crackedFOUND PRESSURE BULKHEAD CRACKED AT BS 727, AFT WALL OF WHEEL WELL. REPAIRED PER SWA RA 253-1194.SDR SWAA95293Skin · crackedDURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .75 INCH AT BS 767 AND STRINGER 19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950190Blkhd Angle · crackedDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT BS 178 PRESSURE BULKHEAD VERTICAL T-ANGLE AT LBL 5.7 AT WL 184, IN THE I/B AND O/B FLANGE RADIUS. REPAIRED PER SWA RA 1-253-1250.SDR SWAA950189Skin · crackedDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION NEAR SEVERAL FASTENERS IN PRESSURE WEB AT I/B SIDE OF STRAP, BS 178, LBL 5.7, FROM WL 205 TO 186. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR SWAA950188Skin · crackDURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT FUSELAGE SKIN LAP, BS 480, S10L, AT BS 500B+10, S14L AND AT BS 530, S10R. REPAIRED PER SWA RA 1-253-1251 AND SI 8615-53.SDR SWAA950182Control Valve · failedAFTER LEVELING AT 28,000, CABIN PRESSURE WARNING HORN SOUNDED. CABIN ALTITUDE CONTINUED TO CLIMB. USING STANDBY OR MANUAL SYSTEM, NO HELP. CREW INITIATED DESCENT. OXYGEN MASKS WERE DEPLOYED. CREW REGAINED CABIN PRESSURE USING APU AND LEFT PACK. AIRCRAFT
Back to N24SW, cancelled Oct 7, 1997