N413US, cancelled Sep 18, 2003

Service difficulty reports · 65

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 = 'N413US' AND deregistration_id = 'N413US-2003-09-18'
  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 USAASB02127Battery Pack · not seatedIND - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 20 THROUGH 23 AND AT THE AFT LEFT SERVICE DOOR INOPERATIVE. MAINTENANCE RERACKED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Jun 29, 2002 · N413US · Boeing 737401 · Emergency LightingSDR USAASB02077Charger · inoperativePIT - FOUND CIRCUIT INOPERATIVE ON EMERGENCY LIGHT BATTERY CHARGER. MAINTENANCE REPLACED THE BATTERY CHARGER. (M)Apr 22, 2002 · N413US · Boeing 737401 · Emergency LightingSDR USAASB02076Fuse · brokenPIT - FOUND BROKEN FUSE ON EMERGENCY LIGHT CHARGER. MAINTENANCE REPLACED THE CHARGER. (M)Apr 22, 2002 · N413US · Boeing 737401 · Emergency LightingSDR USAASB02028Smoke Detector · malfunctionedCLT - FLT 417 - ON CLIMB-OUT FROM CLT, EN ROUTE TO SRQ, THE FLIGHT ATTENDANT REPORTED THE FORWARD LAVATORY SMOKE DETECTOR ALARM SOUNDING. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN ADVISED AFTER LFeb 5, 2002 · N413US · Boeing 737401 · Smoke DetectionSDR USAA011387Skin · crackedTPA - FOUND SKIN .250 INCH, UPPER HINGE CUTOUT ON MAIN ENTRY DOOR. INSTALLED DOUBLER PER SB 737-52-1096 ALSO EA NR 94248. (M)Nov 16, 2001 · N413US · Boeing 737401 · Passenger/Crew DoorsSDR USAA010958Bulkhead · damagedCLT - FOUND PRESSURE WEB WITH ELONGATED HOLES, .281 INCH TO .321 INCH, BS 178, WL 207. DAMAGE REMOVED, INSTALLED ACCESS HOLE DOUBLER PER EA 85146. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010959Bulkhead · crackedCLT - FOUND PRESSURE WEB CRACKED .5 INCH, BS 178 WL 217 AT LBL 6. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA010960Stiffener · crackedCLT - FOUND VERTICAL CHORD CRACKED IN TWO PLACES .25 INCH EACH, BS 178, WL 184 AND 195 AT LBL 5.7. DOUBLER INSTALLED PER EO 5300V155. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA010956Frame · crackedCLT - FOUND SIDE CHORDS .5 INCH, BS 178 WL 207 LEFT AND RIGHT SIDE. DAMAGE SECTION REMOVED, INSTALLED CHORD SPLICE REPAIR AND EXT SKIN STRAP PER EO 5300V157. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA010957Strap · damagedCLT - FOUND VERTICAL STRAP .125 INCH, BS 178, WL 208, LBL 25. DAMAGE SECTION REMOVED, REPLACEMENT SECTION SPLICED IN WITH DOUBLER PER EA 85114. (M)Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA010681Skin · crackedCLT - FOUND SKIN CRACKED, BS 727D, LEFT SIDE, EMERGENCY LIGHT AFT OF WHEEL WELL. DAMAGE REMOVED, INSTALLED DOUBLER PER SRM 53-00-01, FIG 202. (M)Jun 14, 2001 · N413US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA010586Skin · crackedPIT - FOUND SKIN CRACKED 2.5 INCHES, STRINGER 23R STATION 727D. CUT OUT DAMAGE, INSTALLED EXTERNAL DOUBLER PER EA 71032 AND SRM 53-00-01 FIG 202. (M)May 10, 2001 · N413US · Boeing 737401 · Fuselage Structure (General)SDR USAA010277Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 400 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. REMOVED DAMAGED, REPAIRED TR 53-10-14. (M)Feb 14, 2001 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAASB01038Blade · damagedBWI - FLT 1882 - EN ROUTE FROM CLT TO PHL, BOTH ENGINE VIBRATION INDICATORS APPROACHED NR 5. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. UPON ARRIVAL, MAINTENANCE FOUND ACOUSTICAL PANELS BEHIND BOTH N1 FANS TORN. APPEARS ENGINES ENCOUNTERED Feb 5, 2001 · N413US · Boeing 737401 · Turbine Engine Compressor SectionSDR USAASB00327Transmitter · failedPHL - FLT 80 - EN ROUTE FROM PIT TO PHL, THE NR 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI, THEN TO RED RADIAL. OIL TEMPERATURE AND OIL QUANTITY WERE BOTH NORMAL. CREW FOLLOWED CHECKLIST, SHUT DOWN THE NR 2 ENGINE IN FLIGHT AND DECLARED EMERGENCY. CREW NOTED TNov 24, 2000 · N413US · Boeing 737401 · Engine Oil PressureSDR USAASB00249Wire · brokenCLT - FLT 1620 - ON FINAL APPROACH, AT FL030, A FLAP ASYMMETRY OCCURRED. AS CREW EXTENDED FLAPS FROM 5 TO 10 DEGREES, RIGHT FLAP NEEDLE WENT OT 10 DEGREES AND LEFT FLAP NEEDLE REMAINED AT 5 DEGREES. CREW TRIED TO BRING FLAPS UP BUT THEY WOULD NOT RETRACT. CSep 10, 2000 · N413US · Boeing 737401 · Trailing Edge Flap Control SystemSDR USAASB00070Controller · failedBDL - FLT 519 - DURING CLIMB-OUT FROM BDL, AT APPROXIMATELY FL210, THE CABIN WARNING HORN SOUNDED. NO OTHER WARNING INDICATORS ILLUMINATED. CABIN ALTITUDE WAS CLIMBING THROUGH 12,000 AS PRESSURE DIFFERENTIAL WAS 4.2 PSI AND RATE OF CLIMB WAS APPROXIMATELY 50Mar 11, 2000 · N413US · Boeing 737401 · Cabin Pressure ControllerSDR USAASB99130Connector · looseTPA - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTING AT SEAT ROW 6A AND THE FIRST CLASS CABINET, LEFT SIDE INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG AT THE FIRST CLASS CABINET, LEFT SIDE, DISCONNECTED. RECONNECTED CANNON PLUG. OPERATIONAL CHECK GOOD. May 17, 1999 · N413US · Boeing 737401 · Emergency LightingSDR USAA990429Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK IN FRAME AT BS 400 BETWEEN STRINGER 8L AND STRINGER 9. FABRICATED DOUBLER AND INSTALLED PER EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990428Angle · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK IN RADIUS AT STATION 294.5 RBL 54.75 WL 208 ANGLE. INSTALLED DOUBLER ANGLE PER SRM 51-70-11. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990427Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT STATION 986.5 ALONG ENTIRE FLOORBEAM CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP, STRAPS, AND SPLICE PER TR 53-60-01. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990426Beam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH SPOT OF SURFACE CORROSION AT FS 328 RBL 40 BEAM, CORROSION TASK NR C53-107-02. SPLICED IN NEW SECTION OF T-CAP PER SRM 53-10-51. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990425Bulkhead · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 5.3 INCH BY 3.5 INCH AREA OF CORROSION AT RBL 3 STATION 1016 PLUS 5 INCHES BL 0 PRESS BULKHEAD. INSTALLED DOUBLER PER SRM 53-80-08. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA990424Strap · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 67 INCH AREA OF SPOTTED CORROSION AT RBL 20 STATION 780-847 STRAP. INSTALLED NEW STRAP PER SRM 51-10-02. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990419Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 867 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990418Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 907 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990417Floor · crackedCLT - DURING Q-2 CHECK, NDT VISUAL INSPECTION, FOUND A .75 INCH CRACK AT BS 663.75 LBL 32 FLOOR. INSTALLED DOUBLER PER EA 64378. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Floor PanelSDR USAA990416Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT BS 787 BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990415Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 LBL 4.5 W/L 201 WEB. FABRICATED AND INSTALLED DOUBLER PER EA 6420. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990414Tie Clip · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT TIE CLIP STATION 767 STRINGER 26L. REMOVED AND REPLACED STRINGER TIE CLIP PER SRM 51-10-2. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990413Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 9 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8L AND STRINGER 9L. INSTALLED DOUBLER PER EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990412Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 32 INCH AREA OF CORROSION AT STATION 947.5 LT AND RT OF BL 0 FLOORBEAM. REPAIRED 'T' CAP PER TR 53-60-02. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990399Angle · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 26 INCH AREA OF CORROSION AT FORWARD ENTRY DOOR THRESHOLD 'Z' ANGLE F/S 270 TO FS 344 LBBL 55. REMOVED AND REPLACED 'Z' ANGLE PER REPAIR DOCUMENT 51-70-13. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990398Floorbeam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF SPOTTED CORROSION FROM STATION 787 TO 847 RBL 14 FLOORBEAM. CORROSION TASK NR C53-208-01. REMOVED AND REPLACED PER TR 53-00-53. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA990397Web · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 14 INCH BY 30 INCH AREA OF SPOTTED CORROSION UNDER AFT CARGO SILL PANEL WEB. CORROSION TASK NR C53-202-07. REMOVED AND REPLACED PER SRM 51-10-02. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990381Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727A BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990380Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727D BETWEEN STRINGER 8L AND STRINGER 9L. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990379Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 727F BETWEEN STRINGER 8R AND 9R. DOUBLER REPAIRED PER SRM 53-00-07 GIF 202. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990378Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN FRAME AT BS 747 BETWEEN STRINGER 8R AND STRINGER 9R. REPAIRED DOUBLER PER EA 64326 AND SRM 53-00-07 FIG 202. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990377Beam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND AN AREA OF SURFACE CORROSION SPOTS APPROX 1 INCH AT FS 312, LBBL 24 TO RBBL 12. CORROSION TASK NR C53-107-02. SPLICED IN NEW SECTION OF 'T' CAP PER SRM 53-10-51. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990372Bulkhead · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT PRESSURE BULKHEAD RT OF BL 0 JUST AFT STATION 1016. INSTALLED DOUBLER PER SRM 53-80-08. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA990371Bulkhead Web · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AFT PRESSURE BULKHEAD DOME WEB STIFFENER AT BOTTOM OF BL 0 STATION 1016. INSTALLED REPAIR STIFFENER AND REPAIR SPLICES PER SRM 53-70-11. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA990370Bulkhead · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT BS 178 RBL .5 WL 188 BULKHEAD WEB. INSTALLED DOUBLER PER SRM 53-10-08. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, BulkheadSDR USAA990369Beam · corrodedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION FS 344 BL 0 TO LBBL 10 BEAM. CORROSION TASK NR C53-107-02. INSTALLED T-CHORD PER EA 64363 AND TR 53-10-03. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990368Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 727F BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07, SRM 53-30-07, 53-60-07 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990367Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT BS 867 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990366Frame · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED FILLER AND DOUBLER PER SRM 53-00-07, 53-30-07, 53-60-07 AND EA 64326. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, FrameSDR USAA990362Web · crackedCLT - DURNG Q-2 CHECK VISUAL INSPECTION, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 201 BULKHEAD WEB. INSTALLED DOUBLER AND FILLER PER T/R 53-10-07 REV A. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990361Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTIOIN, FOUND A CRACK .5 INCH VERTICAL ON WEB AT STATION 178 RBL 4.5 WL 198 BULKHEAD WEB. INSTALLED DOUBLER AND FILLER PER T/R 53-10-07 REV A. (M)May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA990510Bulkhead Angle · drill marksCLT - DURING Q-2 CHECK, FOUND 3 PLACES .125 INCH DRILL MARKS AT BS 1030 RBL 23 (UNDER FLOOR ATTACH ANGLE) AT 1016 PRESSURE BULKHEAD. BLENDED AREAS/DRILLED HOLE AT DAMAGE AND RIVETS INSTALLED PER SRM 53-80-08. (M)Apr 30, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead
Back to N413US, cancelled Sep 18, 2003