N14308, cancelled Mar 21, 2013

Service difficulty reports · 71

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 = 'N14308' AND deregistration_id = 'N14308-2013-03-21'
  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.

SDR CALA2009062300325Handle · lack of lubeAT FLAPS 10 AT 2000 FT ALL SELECTED GEAR DOWN, RECEIVED LIGHT INDICATION 3 GREEN AND 3 RED STEADY, NO HORN W/ FLAPS 30 AT APROX 400 FT AGL TOO LOW GEAR, WENT AROUND. CONFERRED WITH MX. NEXT APCH AND LANDING COMPLETELY NORMAL INDICATIONS ALL AROUND. CLEANED ANDJun 22, 2009 · N14308 · Boeing 7373T0 · Landing Gear SelectorSDR CALA0700660Skin · crackedA WALKAROUND INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT STA 727D, S23R. THE SKIN WAS REPAIRED IAW ECRA 5330-03745.Oct 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700435Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN AT AFT EDGE OF HANDLE CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, REPAIR 3.Aug 13, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0700434Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR CHANNEL AT FORWARD LOWER STOP. REPAIRED IAW SRM 51-40-02.Aug 13, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0700428Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB UPPER HINGE INTERCOSTAL AT STA 294.5, S10L. A REPAIR WAS INSTALLED IAW ECRA 5311-01350.Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700427Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN L-1 DOOR JAMB LOWER HINGE INTERCOSTAL AT STA 294.5, S13L TO S14L. A REPAIR WAS INSTALLED IAW ECRA 5311-01349.Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700426Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FRAME AT DRAIN HOLE, STA 440, BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 201.Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700424Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN R-1 DOOR SKIN CUTOUT AT STA 328, S16R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5331-01337.Aug 12, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700423Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CARGO DOOR INNER SKIN BETWEEN LIGHTENING HOLES ABOVE HANDLE. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01089.Aug 11, 2007 · N14308 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0700422Seat Track · crackedINSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, RBL 24.8. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0700421Seat Track · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT O/B SEAT TRACK I/B MOUNT FLANGE AT STA 727B, LBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 5321-01492.Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0700420Seat Track · crackedINSPECTION FOUND A 1 INCH CRACK IN RIGHT I/B SEAT TRACK O/B MOUNT FLANGE AT STA 727B, RBL 45.5. A LONGITUDINAL FLOORBEAM REPAIR WAS INSTALLED IAW ECRA 55321-01492.Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0700419Frame · crackedINSPECTION FOUND A 1 INCH CRACK AT TWO EACH HOLES IN I/B CHORD AT STA 639, S16R TO S17R. THE INNER CHORD WAS REPLACED AND A REPAIR WAS INSTALLED IAW ECRA 5311-01347.Aug 11, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700418Frame · corrodedINSPECTION FOUND FORWARD BAGGAGE BIN FRAME CORRODED AT STA 500B BETWEEN STRINGER 25R AND S26R. A SHEAR TIE REPAIR WAS INSTALLED IAW SRM 53-00-07, REPAIR 7.Aug 10, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700415Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 947.5 BETWEEN S21L AND S21R, LBL 10 TO RBL 10. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02.Aug 9, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700452Floorbeam · crackedINSPECTION FOUND CRACKS TO THE LONGITUDINAL FLOORBEAM FLANGES AT STA 727B, LBL 45.5, RBL 45.5 AND RBL 24.8. REPAIRS WERE PERFORMED IAW ECRA 5321-01492.Aug 7, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0700411Skin · damagedINSPECTION FOUND A HOLE IN FUSELAGE SKIN CAUSED BY A LIGHTNING STRIKE AT STA 375, S24R. A SKIN REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.Aug 4, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0700396Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 807, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.Aug 3, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700395Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 827, S9R. REPAIR DOUBLERS WERE INSTALLED IAW ECRA 5310-04647.Aug 3, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700392Strap · crackedINSPECTION FOUND A 1 INCH CRACK IN WEB STRAP JUST FORWARD OF L-2 DOOR AT STA 947.5, S10L TO S11L. A NEW WEB STRAP WAS INSTALLED IAW SRM 51-40-02.Aug 2, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700391Keelbeam · corrodedINSPECTION FOUND LEFT KEEL BEAM CORRODED IN A/C DISTRIBUTION BAY AT STA 500D-520. THE KEEL BEAM WAS REPAIRED IAW SRM 53-30-12, FIGURE 201.Aug 1, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, KeelSDR CALA0700387Stringer · corrodedINSPECTION FOUND STRINGER 28R CORRODED AT STA 294-323. THE STRINGER WAS REPLACED IAW SRM 51-40-02.Aug 1, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700441Door Frame · crackedINSPECTION FOUND A CRACK EMANATING FROM THE DOORSTOP CUTOUT IN THE AFT EDGE BEAM OF THE L-1 DOOR. THE EDGE BEAM WAS REPAIRED IAW ECRA 5210-01944.Jul 30, 2007 · N14308 · Boeing 7373T0 · Passenger/Crew DoorsSDR CALA0700381Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 1006 FROM S25R TO 26L. THE CORRODED SECTION OF FRAME WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 1.Jul 29, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0700377Stringer · corrodedINSPECTION FOUND STRINGER 25L CORRODED AT REPAIR CUTOUT AFT OF STA 1006. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPLACED IAW SRM 53-00-03, FIGURE 201, REPAIR 1.Jul 27, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0700374Shear Web · crackedINSPECTION FOUND A 2.5 INCH CRACK IN LEFT SHEAR WEB FORWARD OF STA 639 FUSELAGE FRAME, LBL 50. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02 AND 51-40-02.Jul 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0700373Floorbeam · corrodedINSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND FASTENER HOLE AT STA 360, BL 0. THE CORRODED AREA WAS CUT OUT AND REPAIR ANGLES WERE INSTALLED IAW SRM 53-30-51, FIGURE 201, REPAIR 2.Jul 24, 2007 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0600245Controller · inoperativeTHE CREW REPORTED SMOKE IN THE CABIN WHILE EN ROUTE TO IAH. THE SMOKE REMOVAL CHECKLIST WAS COMPLETED AND AFTER TURNING OFF THE RECIRCULATION FAN THE SMOKE WENT AWAY. ALSO OBSERVED THAT THE RT FWD WINDOW HEAT CIRCUIT BREAKER HAD POPPED. THE CREW WAITED 10 MJun 16, 2006 · N14308 · Boeing 7373T0 · Windshield/Door Rain/Ice RemovalSDR CALA0500429Shear Tie · corrodedINSPECTION FOUND FRAME/SHEAR TIE CORRODED AT STA 967 BETWEEN STRINGERS 27L-27R. THE CORRODED SECTION OF SHEAR TIE WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07, FIGURE 201, REPAIR 8.Dec 10, 2005 · N14308 · Boeing 7373T0 · Fuselage Internal Mounting StructureSDR CALA0500428Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON FRAME (HORSE COLLAR FITTING) AROUND LOCK FASTENER COLLAR. THE NR 2 PYLON HORSE COLLAR WAS REMOVED AND REPLACED IAW SRM 51-10-2.Dec 9, 2005 · N14308 · Boeing 7373T0 · Nacelle/Pylon, Main FrameSDR CALA0500371Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BETWEEN STA 727E - 747 JUST BELOW S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 31, FIGURE 201, DETAIL XI.Oct 20, 2005 · N14308 · Boeing 7373T0 · Fuselage Main, Plate/SkinSDR CALA0300496Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED AT STA 996. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.Aug 26, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0300495Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2.Aug 25, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Longeron/StringerSDR CALA0300493Floorbeam · corrodedINSPECTION FOUND FORWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 500D BETWEEN S26L AND S27L, LOWER AREA. THE CORRODED AREA WAS CUT OUT AND FILLER, DOUBLER AND A SHIM WERE INSTALLED IAW SRM 53-00-07, FIGURE 203 AND 204.Aug 25, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300490Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 296, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-40352 AND SRM 51-40-02.Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0300489Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 294.5, RBL 41. THE FLOORBEAM UPPER CHORD SECTION WAS REMOVED AND A NEW UPPER CHORD WAS INSTALLED IAW SRM 53-10-51.Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300487Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED FROM STA 947.5 TO 967 AT RBL 7 AND RBL 46. NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-40-02 AND ECRA 5310-03585.Aug 24, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300486Channel · crackedINSPECTION FOUND THE LT WING T/E NR 3 FLAP TRACK FAIRING AFT END U-CHANNEL CRACKED IN TWO PLACES UNDER THE TRACK. THE CRACKS WERE .25 INCH LONG. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-02.Aug 24, 2003 · N14308 · Boeing 7373T0 · Wing Miscellaneous StructureSDR CALA0300086Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACES OF UPPER CAP AT STA 1006 FROM BL 0 TO RBL 40. REMOVED AND REPLACED T-CAP IAW ECRA 5310-03851.Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300085Channel · corrodedINSPECTION FOUND CHANNEL CORRODED ON UPPER SURFACE AND AT NUTPLATES AT STA 1006-1016, LBL 5 TO LBL 9. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02.Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300084Angle · corrodedINSPECTION FOUND CORROSION ON UPPER SURFACE OF ANGLE AT NUTPLATES, STA 1006, LBL 10. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Miscellaneous StructureSDR CALA0300083Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED IN AFT GALLEY AREA AT STA 967, LBL 25. REPAIRED IAW ECRA 5320-01726.Mar 2, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300081Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE OF CAP AND AT FASTENER HOLES AT STA 1006, BL 0 TO RBL 30. THE T-CAP WAS REMOVED AND REPLACED IAW SRM 51-40-04.Mar 1, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, Floor BeamSDR CALA0300068Frame · corrodedINSPECTION FOUND R/H O/B FRAME CORRODED AT STA 986, RBL 40. REPAIRED IAW ECRA 5310-03851.Feb 23, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, FrameSDR CALA0300054Pressure Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN PRESSURE DECK AT BS 664 - 675, LBL 30 - 35. REPAIRED IAW SRM 53-60-51, PAGE 213-221.Feb 18, 2003 · N14308 · Boeing 7373T0 · Fuselage Floor PanelSDR CALA0300052Pressure Panel · crackedINSPECTION FOUND A 2.75 INCH CRACK IN RT WHEEL WELL PRESSURE DECK AT FS 663, RBL 35. REPAIRED IAW SRM 53-60-51, PAGE 213-231.Feb 17, 2003 · N14308 · Boeing 7373T0 · Fuselage Main, BulkheadSDR CALA0200028Skin · crackedINSPECTION FOUND A 3/4" CRACK AT LIGHTENING HOLE CUTOUT OF FORWARD CARGO DOOR INNER SKIN. A DOUBLER WAS INSTALLED IAW ECRA 5232-01014.Jan 21, 2002 · N14308 · Boeing 7373T0 · Cargo/Baggage DoorsSDR CALA0200025Skin · delaminatedINSPECTION FOUND L/H WING LEADING EDGE SKIN DELAMINATED AND HILOCK PULLED THROUGH SKIN BEHIND #2 SLAT AT O/B END. REPAIRED IAW ECRA 5721-01048.Jan 17, 2002 · N14308 · Boeing 7373T0 · Wing, Plate/SkinSDR CALA0200024Skin · delaminatedINSPECTION FOUND R/H WING LEADING EDGE SKIN UNDER O/B EDGE OF #5 SLAT DELAMINATED. REPAIRED IAW ECRA 5721-01048.Jan 17, 2002 · N14308 · Boeing 7373T0 · Wing, Plate/SkinSDR CALA0200022Attach Angle · wornINSPECTION FOUND ATTACH ANGLE ON BOTTOM OF VERTICAL STABILIZER ON R/H SIDE WORN THIN AT STA 1104-1121. THE ATTACH ANGLE WAS REPLACED IAW ECRA 5300-01013, REV B.Jan 17, 2002 · N14308 · Boeing 7373T0 · Fuselage, Stabilizer Attach Fittings
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