N61304, cancelled Mar 21, 2013
Service difficulty reports · 56
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 = 'N61304' AND deregistration_id = 'N61304-2013-03-21' 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 = 'N61304' AND deregistration_id = 'N61304-2013-03-21' 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 CALA0700531Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN SKIN AT STA 727E, S24L. REPAIRED IAW SRM 53-00-01, REPAIR 31.SDR CALA0600340Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AT THE CENTER INTERCOSTAL ON THE BOTTOM. A DOUBLER WAS INSTALLED IAW ECRA 5232-01081.SDR CALA0600336Stringer Splice · crackedINSPECTION FOUND A 1/2" CRACK IN THE L-1 DOOR AFT NR 14 INTERCOSTAL STRINGER SPLICE AT STA 344-360, S14L. THE STRINGER SPLICE WAS REPLACED IAW ECRA 5311-01271 AND A DIP WAS INITIATED TO REINSPECT THE AREA.SDR CALA0600335Intercostal · crackedINSPECTION FOUND A 1/2" CRACK IN L-1 DOOR FORWARD SIDE UPPER HINGE INTERCOSTAL LOWER WEB AT STA 294.5-312, S10L. THE INTERCOSTAL WEB WAS REPAIRED IAW ECRA 5311-01270 AND A DIP WAS INITIATED TO REINSPECT THE AREA.SDR CALA0600334Stringer Splice · crackedINSPECTION FOUND A 1/2" CRACK IN L-1 DOOR AFT NR 15 INTERCOSTAL STRINGER SPLICE AT STA 344-360, S15L. A NEW STRINGER SPLICE CHANNEL WAS INSTALLED IAW ECRA 5311-01269 AND A DIP WAS INITIATED TO REINSPECT THE AREA.SDR CALA0600339Fitting · crackedINSPECTION FOUND A 1/4" CRACK IN A FRAME FITTING ON RT SIDE OF FUSELAGE JUST AFT OF STA 639, S15L, FRAME IS JUST BELOW THE CREASE BEAM IN THE MAIN CABIN. REPAIRED IAW SRM 51-10-02.SDR CALA0600333Frame · corrodedINSPECTION FOUND LOWER O/B CHORD OF BULKHEAD CORRODED AT STA 227.8, LBL 5 TO RBL 10, S29L TO 29R. A REPAIR WAS INSTALLED IAW ECRA 5311-01268.SDR CALA0600332Slat Track · crackedINSPECTION FOUND A 1 INCH CRACK AROUND RIVET HOLES IN RT WING NR 6 SLAT I/B AUX TRACK LOWER AREA. THE AREA WAS REPAIRED IAW SRM 57-43-01.SDR CALA0600331Frame · corrodedINSPECTION FOUND UPPER SURFACE OF FRAME CORRODED AT STA 727B BETWEEN S26L AND S27L. THE CORRODED SECTION OF FRAME WAS TRIMMED OFF AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.SDR CALA0600330Fitting · corrodedINSPECTION FOUND LEFT AFT FWD, RIGHT AFT FWD, AND RIGHT AFT O/B VERTICAL STABILIZER DRAG ANGLE FITTINGS CORRODED AT STA 1088, S2L AND S2R. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-73744.SDR CALA0600329Fitting · corrodedINSPECTION FOUND NR 1 FLAP TRACK AFT SPAR FITTING CORRODED AT MOUNT BOLT. THE SPAR FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 65-46429.SDR CALA0600328Shear Tie · corrodedINSPECTION FOUND LOWER CENTER SHEAR CLIP ON FRAME IN FORWARD CARGO COMPARTMENT AT STA 500, S28L TO 28R CORRODED. THE CORRODED AREA WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-00-07.SDR CALA0600327Stringer · corrodedINSPECTION FOUND STRINGER 25L CORRODED AT STA 344-360. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-00-03, REPAIR NR 1.SDR CALA0600324Stringer · corrodedINSPECTION FOUND STRINGER 25L CORRODED AT STA 967. A NEW STRINGER SECTION WAS SPLICED IN IAW SRM 53-00-03.SDR CALA0600338Intercostal · crackedINSPECTION FOUND A 1" CRACK IN L-1 DOOR AFT INTERCOSTAL INNER STRAP AT STA 360, S16L. THE INTERCOSTAL INNER STRAP WAS REPAIRED IAW SRM 53-10-04.SDR CALA0600337Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 4 TO RBL 36. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.SDR CALA0600323Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1016, RBL 4 TO RBL 36. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW ECRA 5310-03851.SDR CALA0600322Stringer · corrodedINSPECTION FOUND STRINGER 24L CORRODED AT STA 1016, LBL 20. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.SDR CALA0600320Crease Beam · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RIGHT SIDE CREASE BEAM WEB JUST AFT OF STA 616, RBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-40-02.SDR CALA0600321Pressure Panel · crackedINSPECTION FOUND A 1.5 INCH CRACK IN MAIN CABIN LOWER PRESSURE DECK AT STA 663.75, LBL 30. A REPAIR WAS INSTALLED IAW SRM 53-60-51, FIGURE 201.SDR CALA0600315Frame · corrodedINSPECTION FOUND HEAVY INTERGRANULAR CORROSION ON FORWARD SIDE OF FRAME AT STA 219.8, S27R, RBL 17, O/B LOWER CHORD. A NEW CHORD WAS INSTALLED IAW SRM 51-2-02 AND 51-40-02.SDR CALA0600311Stringer · crackedINSPECTION FOUND A .5 INCH CRACK IN STRINGER 16L BETWEEN STA 500C AND 500D. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 53-30-03.SDR CALA0600309Seat Track · corrodedINSPECTION FOUND RT OB SEAT TRACK CORRODED AT STA 540-727, RBL 24. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52, REPAIR 2, FIGURE 201.SDR CALA0600308Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME AT STA 616 JUST BELOW FLOOR, S17L. A REPAIR ANGLE AND FILLER WERE INSTALLED IAW ECRA 5311-01158.SDR CALA0600306Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER AFT AIRFRAME MOUNT LUG AT LOWER AND UPPER FORWARD POSITIONS CORRODED. THE AREA WAS REPAIRED AND NEW BUSHINGS WERE INSTALLED IAW SRM 55-10-10.SDR CALA0600305Fitting · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER FORWARD AIRFRAME MOUNT LUG AT LOWER AFT AND FORWARD POSITIONS AND AT UPPER FORWARD AND AFT POSITIONS CORRODED. THE AREA WAS REPAIRED AND NEW BUSHINGS WERE INSTALLED IAW SRM 55-10-10.SDR CALA0600301Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294.5, RBL 42. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0600300Seat Track · corrodedINSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT STA 328. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0600299Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328, RBL 32-50. THE CORRODED AREA WAS BLENDED OUT AND A STRAP DOUBLER WAS INSTALLED IAW SRM 53-00-51 FIGURE 201.SDR CALA0600028Beam · crackedTHE LT AILERON BEAM WAS FOUND CRACKED AT WS 538, THE CRACK WAS STOP DRILLED PER ECRA 5752-01230. A DIP WAS ISSUED TO REINSPECT THE AREA AT 50 FLIGHT HOUR INTERVALS UNTIL A PERMANENT REPAIR IS PERFORMED PER ECRA 5752-01230.SDR CALA0400749Panel · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN NR 2 PYLON PANEL CUTOUT 5824R. THE CRACKS WERE LOCATED AT UPPER FORWARD CORNER OF PANEL. ONE CRACK ORIGINATED FROM RIVET HOLE FOR RUB STRIP AND THE OTHER WAS ON FAYING SURFACE FOR ACCESS PANEL.SDR CALA0400748Keelbeam · corrodedINSPECTION FOUND LT SIDE KEELBEAM CORRODED BETWEEN STA 520 AND 540, LBL 10. A KEEL BEAM SPLICE REPAIR WAS INSTALLED IAW SRM 53-60-12, FIGURE 203.SDR CALA0500029Stringer · corrodedINSPECTION FOUND STRINGER 26L CORRODED BETWEEN STA 440 AND 500D. THE STRINGER WAS REPAIRED USING A SPLICE IAW ECRA 5311-01215.SDR CALA0400608Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN EXTERNAL SKIN BETWEEN STA 947.5 AND 967, S10L TO S11L (L-2 DOOR UPPER HINGE CUTOUT FORWARD CORNER RADIUS JUST BELOW THE RAIN GUTTER). A REPAIR WAS INSTALLED IAW SRM 53-60-01, FIGURE 205. A DIP WAS ISSUED TO REINSPECT THE ARSDR CALA0300650Skin · crackedINSPECTION FOUND A 5 INCH CRACK IN FUSELAGE BELLY SKIN AFT OF E&E COOLING DUCT AT BS 380, S28L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02894.SDR CALA0200465Angle · crackedINSPECTION FOUND A 3" CRACK IN L/H WING LOWER/AFT O/B SUPPORT ANGLE. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0200463Doubler · crackedINSPECTION FOUND A 2" CRACK IN R/H WING UPPER I/B T/E PANEL DOUBLER, WBL 80. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-70-11.SDR CALA0200461Stiffener · corrodedINSPECTION FOUND CENTER STIFFENER ON AFT PRESSURE BULKHEAD FORWARD FACE CORRODED ON R/H SIDE, IN BILGE, BS 1016-1022. REPAIRED STIFFENER IAW SRM 51-70-11 AND 53-80-08.SDR CALA0200460Web · crackedINSPECTION FOUND A .5 INCH CRACK IN CABIN FLOOR VERTICAL WEB AT STA 1016, LBL 26 BELOW STRAP. A REPAIR WAS INSTALLED IAW SRM 51-40-00.SDR CALA0200459Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 312, RBL 36, WL 201. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-10-51.SDR CALA0200458Stiffener · crackedINSPECTION FOUND A .5 INCH CRACK IN STIFFENER ACROSS BOTTOM OF FLOORBEAMS AT STA 328, RBL 45, WL 201. A DOUBLER WAS INSTALLED IAW SRM 53-10-51.SDR CALA0200455Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 34. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. A CHORD AND SPLICE ANGLE REPAIR WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.SDR CALA0200129Ground Wire · unsecureTHE RIGHT WING EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE FOUND LIGHT ASSEMBLY GROUND WIRE NOT SECURED TO GROUND STUD. TIGHTENED LOCKING NUT AND OPERATION OF THE LIGHT CHECKED GOOD.SDR CALA0100402Access Panel · crackedLEFT ENGINE PYLON UPPER OUTBOARD ACCESS PANEL CRACKED AT CUTOUT (.75 INCH). STOP DRILLED CRACK AND INSTALLED A REPAIR DOUBLER PER EC/RA 5430C01230.SDR CALA0100401Skin · crackedPILOTS OUTBOARD WINDOW POST CRACKED AT TOP OUTBOARD CORNER (.75 INCH). INSTALLED REPAIR DOUBLER ON PST PER SRM 53-10-01 FIG 210.SDR CALA0100110Bulkhead · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN BULKHEAD WITH A STIFFENER BROKEN IN HALF AT STA 178. THE BULKHEAD WAS REMOVED AND REPLACED IAW EA 5310-03040.SDR CALA0000991Skin · corrodedINSPECTION FOUND SKIN CORRODED AND RIVET HEADS PULLED THROUGH SKIN AT STA 530-538, RBL 6.25. THE SKIN, KEEL BEAM LOWER CHORD, AND WING CENTER SECTION FRONT SPAR WERE REPAIRED IAW ECRA 5310-04024.SDR CALA9901440Frame/Beam · crackedINSPECTION FOUND A 1 INCH CRACK IN LOWER AFT FRAME AND A 2 INCH CRACK IN T-BEAM OF FORWARD CARGO DOOR LOWER FORWARD CORNER. THE FRAME WAS REPLACED IAW SRM 51-10-02 AND 51-40-02. THE BEAM WAS REPAIRED IAW ECRA 5230-01491.SDR CALA9801982Floorbeam · corrodedINSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT STA 1006, LBL 16 TO LBL 28. REPAIRED IAW SRM 53-00-51.SDR CALA9801978Floorbeam · corrodedINSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT FASTENER HOLE, STA 1016, WL 208, LBL 5 TO LBL 38. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03450.
Back to N61304, cancelled Mar 21, 2013