N349US, cancelled Nov 8, 2004

Service difficulty reports · 25

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 = 'N349US' AND deregistration_id = 'N349US-2004-11-08'
  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 USA2001F00007Socket · defectivePIT MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD.Dec 12, 2001 · N349US · Boeing 737301 · Emergency LightingSDR USAASB00204Duct · severedBOS - FLT 6507 - FLIGHT RETURNED TO FIELD AT BOS DUE TO AN ELECTRICAL SMELL THROUGHOUT THE CABIN. CAPTAIN ELECTED TO RETURN TO BOS AFTER NUMEROUS COMPLAINTS FROM THE FLIGHT ATTENDANTS AND PASSENGERS. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUAug 1, 2000 · N349US · Boeing 737301 · Air Distribution SystemSDR USAASB00187Sensor · failedBOS - FLT 6527 - AFTER TAKEOFF, THE LANDING GEAR LEVER WOULD NOT MOVE UP TO THE RETRACT POSITION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENJul 9, 2000 · N349US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAA991031Angle · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 59 INCH AREA OF CORROSION AT STATION 285-344, WL 208.1 Z-ANGLE. CORROSION LEVEL 2. REMOVED AND REPLACED Z-ANGLE EPR SRM 51-10-02. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991032Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER T-CAP AT NUTPLATE HOLES 10 INCH AT BS 294.5, LBL 22 TO RBL 22, BEAM CAP. CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991022Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION FLOORBEAM UPPER CHORD STATION 986 FROM BL 3.5 TO RBL 9.5, CORROSION LEVEL 1. INSTALLED DOUBLER PER TR 53-10-05. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991023Floorbeam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION FLOORBEAM BETWEEN STATION 986.5 BY 1016 DIAGONALLY FROM RBL 19 TO RBL 5. CORROSION LEVEL 1. REPAIRED WITH IDENTICAL PART PER SRM 51-10-02. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991002Floorbeam · corrodedCLT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH AREA OF CORROSION FLOORBEAM 967 UPPER CHORD AT LBL 27.5, CORROSION LEVEL 1. REPAIRED DOUBLER PER SRM 53-00-51. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA991102Angle · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT HORIZONTAL STAB CENTER SECTION THRUST BEAM ATTACH ANGLE. REPLACED ANGLE PER REPAIR DOCUMENT 51-10-02. (M)Oct 13, 1999 · N349US · Boeing 737301 · Horizontal Stabilizer StructureSDR USAA991090Skin · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 EACH .50 INCH CRACKS AT BS 5332, RBBL 60, WL 21.5 SKIN ASSEMBLY. INSTALLED REPAIR PLATES PER SRM 53-10-01 FIG 202. (X)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA991081Fitting · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK AT FORWARD SERVICE DOOR LOWER AFT DOOR STOP FITTING ASSEMBLY. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (X)Oct 13, 1999 · N349US · Boeing 737301 · Service DoorsSDR USAA991057Keel Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH CORRODED AREA KEEL BEAM AT BS 500C PLUS 9.5 INCH LBL 5. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER EA 65730. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, KeelSDR USAA991047Keel Beam · corrodedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .75 INCH BY 5 INCH AT STATIN 532, RLB 6.5 STRINGER 28R KEEL BEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-202-01. INSTALLED REPAIR STRAP AND ANGLE PER EA 65811. (M)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, KeelSDR USAA991029Tie Clip · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .3750 INCH CRACK AT BS 907, STR 9L STRINGER TIE CLIP. REPAIRED WITH IDENTICAL PART PER SRM 51-10-2. (X)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA991021Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 480, BETWEEN STR 8L AND STR 9L FRAME. INSTALLED DOUBLER ANGLE PER EA 65618 AND SRM 53-00-07 FIG 202. (X)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, FrameSDR USAA991020Frame · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT BS 887, BETWEEN STR 8L AND STR 9L FRAME. INTALLED DOUBLER ANGLE PER EA 65618. (X)Oct 13, 1999 · N349US · Boeing 737301 · Fuselage Main, FrameSDR USAA990795Stringer · crackedCLT - ON PARKED, OUT OF TIME AIRCRAFT, FOUND 1.5 INCH CRACK AT STR 22R, STA 809. INSTALLED DOUBLER PER SRM 53-00-01. (X)Aug 12, 1999 · N349US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAASB99169Battery Pack · dischargedIAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)Jul 9, 1999 · N349US · Boeing 737301 · Emergency LightingSDR USAASB97286Battery Pack · dischargedPIT - EMERGENCY EXIT SIGN ROW 10 BROKEN AND BATTERY PACK ABOVE ROW 9D INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY (10-1262-3), NO HELP. FOUND BROKEN WIRE UNDER SEAT AND REPAIRED. THE BATTERY CHARGER (2012-1) WAS REPLACED ABOVE ROW 9D. OPERATIONAL CHECOct 18, 1997 · N349US · Boeing 737301 · Emergency LightingSDR USAASB97192Position Ind · failedPHL - FL2191 - IN THE PROCESS OF CONFIGURING THE A/C FOR LANDING. CAPTAIN DID NOT RECEIVE LEADING OR TRAILING EDGE FLAP INDICATION. ADVISED PHL TOWER OF THE PROBLEM AND HIS INTENTION TO GO AROUND. AFTER GO AROUND, FLIGHT LANDED SAFELY WITHOUT FURTHER INCIDEJul 15, 1997 · N349US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAA951034Skin · mis mfgCLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L. INSTALLED PROTRUDING HEAD RIVET 211TT3. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951033Doubler · damagedCLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R. VISUALLY INSPECTED. PREVIOUS REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA951032Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L. PREVIOUS REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951031Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND. EXISTING REPAIR DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA951030Doubler · damagedCLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L. EXISTING REPAIR, DOUBLER INSTALLED. (M)Sep 19, 1995 · N349US · Boeing 737301 · Fuselage Miscellaneous Structure
Back to N349US, cancelled Nov 8, 2004