N19357, cancelled Mar 21, 2013
Service difficulty reports · 88
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 = 'N19357' AND deregistration_id = 'N19357-2013-03-21' 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 = 'N19357' AND deregistration_id = 'N19357-2013-03-21' 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 CALA0100333Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 380 - 400, LBL 23. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-30, 51-21-01, AND 51-40-02.SDR CALA0100332Skin · dentedINSPECTION FOUND LT WING NR 3 FLIGHT SPOILER DENTED ON TOP SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-70-01, FIGURE 204 AND 51-20-01.SDR CALA0100331Skin · dentedINSPECTION FOUND LT WING NR 2 FLIGHT SPOILER DENTED ON LOWER SURFACE. THE DENTED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-70-01 AND MM 27-61-11.SDR CALA0100330Skin · damagedINSPECTION FOUND THREE CREASES IN LT FUSELAGE EXTERIOR SKIN ALONG LAP SEAM AT STA 275, S19L. THE SKIN WAS REPAIRED IAW SRM 53-00-01.SDR CALA0100329Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 28R AT STA 440. THE CRACKED SECTION OF STRINGER WAS CUT OUT AND A J-ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03.SDR CALA0100328Seat Track · gougedINSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AND WORN AT STA 480-520, LBL 46. THE DAMAGED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 53-00-52, 51-21-01, AND ECRA 5100-01844.SDR CALA0100327Intercostal · bentINSPECTION FOUND AFT PIT DOOR CUTOUT LOWER INTERCOSTAL BENT AT FORWARD FRAME TO AFT FRAME, STA 794-849, LBL 24. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-2.SDR CALA0100326Seat Track · gougedINSPECTION FOUND LEFT O/B SEAT TRACK GOUGED AT STA 540-727, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-20-01 AND 51-40-00.SDR CALA0100325Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 179-294, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-40-02.SDR CALA0100324Doubler · gougedINSPECTION FOUND FWD ENTRYWAY FLOORBEAM AFT FLANGE OUTER DOUBLE STACK REPAIR DOUBLER GOUGED IN RADIUS AND ON HORIZONTAL FLANGE AT STA 312, RBL 24. THE DOUBLER WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 53-10-51.SDR CALA0100298Pan · corrodedINSPECTION FOUND FLOOR PAN CORRODED AT STA 1016 TO AFT PRESSURE BULKHEAD, BL 0 TO RBL 48. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-10-02, DRAWING 65C32677, AND DRAWING 65-52878.SDR CALA0100297Threshold · corrodedINSPECTION FOUND R-2 DOOR THRESHOLD CHORD CORRODED AT STA 977. THE R-2 DOOR THRESHOLD CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100293Floor Support · corrodedINSPECTION FOUND ANGLED FLOOR SUPPORT CORRODED AT AFT END AT STA 986.5-1006, RT SIDE. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0100292Beam · gougedINSPECTION FOUND L-1 DOOR INNER DOOR CHORD BEAM GOUGED IN UPPER TORQUE TUBE SLEEVE BAY AT STA 312. THE CHORD BEAM WAS REMOVED AND A NEW CHORD BEAM WAS INSTALLED IAW SRM 52-10-02 AND 51-30-02.SDR CALA0100291Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AROUND SCREW HOLES AT STA 967, RBL 27, LBL 6, AND LBL 27. REPAIR STRAPS AND SHIMS WERE INSTALLED IAW SRM 53-00-51, FIGURE 203, 51-20-01, AND 51-30-01.SDR CALA0100289Seat Track · corrodedINSPECTION FOUND GOUGES ON TOP OF SEAT TRACK AT STA 344-400, LBL 25. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.SDR CALA0100288Skin · dentedINSPECTION FOUND EXTERIOR FUSELAGE SKIN DENTED BELOW LAP SEAM AT STA 1010, S20R. THE DENTED AREA WAS CUT OUT AND A REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, FIGURE 202 AND 207.SDR CALA0100286Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AROUND SCREW HOLES AT STA 951, RBL 24 - 48. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0100283Web · dentedINSPECTION FOUND AFT CARGO DOOR AFT LOWER FRAME WEB DENTED AT STA 847. THE DENTED AREA WAS REMOVED AND A NEW REPAIR WEB WAS INSTALLED IAW SRM 51-70-13 AND 51-40-02.SDR CALA0100280Stiffener · gougedINSPECTION FOUND VERTICAL T-SUPPORT (STIFFENER) ON AFT SPAR JUST I/B OF MLG SUPPORT BEAM O/B FITTING GOUGED AT WS 133. A NEW STIFFENER WAS INSTALLED IAW SRM 51-40-5 AND 51-40-6.SDR CALA0100279Frame · gougedINSPECTION FOUND NR 1 ENGINE PYLON FORWARD O/B UPPER CHORD GOUGED. THE NR 1 ENGINE PYLON O/B UPPER CHORD WAS REPAIRED IAW ECRA 5440-01221 AND EA 04-5440-0836.SDR CALA9900118Skin · creasedINSPECTION FOUND THE RT FORWARD LOWER FUSELAGE SKIN CREASED AT STA 456, STRINGERS 29R-27R. THE SKIN WAS REPAIRED IAW ECRA 5330-02767.SDR CALA9900108Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 480-500B, STRINGER 19L. A REPAIR WAS INSTALLED IAW SRM 53-00-01.SDR CALA9700217Intercostal · corrodedINSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT NUTPLATE HOLE BS 950 LBL 30. THE INTERCOSTAL WAS REPLACED IAW ECRA 5310-03413.SDR CALA9700221Web · corrodedINSPECTION FOUND CORROSION ON WEB BETWEEN STA 1121 AND 1129 LOOKING THROUGH APU INLET DUCT OPENING, RT SIDE TOP. THE WEB WAS REPAIRED IAW SRM 51-70-11.SDR CALA9700220Fitting · crackedINSPECTION FOUND A 3 INCH CRACK ON FITTING ATTACHED TO THE HORIZONTAL STABILIZER CENTER SECTION BOX. THE FITTING WAS REPLACED IAW SRM 51-40-02.SDR CALA9700219Beam · corrodedINSPECTION FOUND CORROSION ON RIGHT SIDEWALL BEAM OF APU BOX AT STA 1104. THE CORRODED SECTION WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-70-11.SDR CALA9700209Stringer · crackedINSPECTION FOUND A .375 INCH CRACK IN STRINGER 16L AND A .375 INCH CRACK IN STRINGER 16R AT STA 500C. A REPAIR CHANNEL AND DOUBLER WERE INSTALLED AT EACH LOCATION IAW ECRA 5310-03418.SDR CALA9700218Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AROUND NUTCLIP HOLES NEXT TO G-1 GALLEY TRACK AT STA 294.5. A FLOORBEAM UPPER CHORD WAS INSTALLED IAW SRM 53-10-51.SDR CALA9700216Support · crackedINSPECTION FOUND .25 INCH CRACKS IN FLOOR SUPPORT AT BL 0 BETWEEN STA 380 AND 400. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-30-51.SDR CALA9700213Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON RIGHT SIDE AT STA 328. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.SDR CALA9700212Floorbeam · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AROUND NUTPLATE HOLES BETWEEN STA 312 AND 328 TO THE LEFT OF BL 0 AND TO THE RIGHT OF BL 0. THE FLOORBEAM SECTIONS WERE REMOVED, NEW FLOORBEAM SECTIONS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03413 AND BOEING DRAWINSDR CALA9700211Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES FROM BL 0 TO L-1 DOOR AT STA 344. THE CORRODED SECTION WAS REMOVED AND A NEW FLOORBEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-51.SDR CALA9700210Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT NUT CLIP HOLES, STA 312. REPAIRED IAW SRM 53-10-51, FIGURE 205.SDR CALA9700215Intercostal · corrodedINSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED ON NUTPLATE AT BS 967 TO 986, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03413.SDR CALA9700214Intercostal · corrodedINSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AROUND NUTPLATE AT BS 950, LBL 45. A REPLACEMENT INTERCOSTAL WAS FABRICATED AND INSTALLED IAW ECRA 5310-03413.SDR CALA9601321Fan · inoperativeTHE FLIGHT ATTENDANT REPORTED ODOR AND SMOKE IN CABIN DURING CRUISE. THE LT PACK WAS SECURED, THEN THE FORWARD LAV SMOKE DETECTOR ACTIVATED. THE RECIRCULATION FAN WAS TURNED OFF AND THE LEFT PACK WAS RESTORED TO OPERATION. THE FLIGHT CONTINUED WITHOUT FURTHSDR CAL960634Hyd Pump · leakingEWR - FLT 1556 - THE AIRCRAFT LOST A-SYSTEM HYDRAULIC FLUID ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AT FAULT. THE PUMP WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND LEAK CHECK WAS
Back to N19357, cancelled Mar 21, 2013