# Service difficulty reports: N413US, cancelled Sep 18, 2003 A list on [N413US, cancelled Sep 18, 2003](https://openairdocs.org/deregistered/N413US-2003-09-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 65 reports - [SDR USAASB02127](https://openairdocs.org/sdr/USAASB02127.md): Battery Pack · not seated · Jun 29, 2002 · N413US · Boeing 737401 · Emergency Lighting > IND - 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) - [SDR USAASB02077](https://openairdocs.org/sdr/USAASB02077.md): Charger · inoperative · Apr 22, 2002 · N413US · Boeing 737401 · Emergency Lighting > PIT - FOUND CIRCUIT INOPERATIVE ON EMERGENCY LIGHT BATTERY CHARGER. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) - [SDR USAASB02076](https://openairdocs.org/sdr/USAASB02076.md): Fuse · broken · Apr 22, 2002 · N413US · Boeing 737401 · Emergency Lighting > PIT - FOUND BROKEN FUSE ON EMERGENCY LIGHT CHARGER. MAINTENANCE REPLACED THE CHARGER. (M) - [SDR USAASB02028](https://openairdocs.org/sdr/USAASB02028.md): Smoke Detector · malfunctioned · Feb 5, 2002 · N413US · Boeing 737401 · Smoke Detection > CLT - 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 L - [SDR USAA011387](https://openairdocs.org/sdr/USAA011387.md): Skin · cracked · Nov 16, 2001 · N413US · Boeing 737401 · Passenger/Crew Doors > TPA - FOUND SKIN.250 INCH, UPPER HINGE CUTOUT ON MAIN ENTRY DOOR. INSTALLED DOUBLER PER SB 737-52-1096 ALSO EA NR 94248. (M) - [SDR USAA010958](https://openairdocs.org/sdr/USAA010958.md): Bulkhead · damaged · Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA010959](https://openairdocs.org/sdr/USAA010959.md): Bulkhead · cracked · Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - FOUND PRESSURE WEB CRACKED.5 INCH, BS 178 WL 217 AT LBL 6. DAMAGE REMOVED, REPAIR DOUBLER INSTALLED PER EO 5300V153. (M) - [SDR USAA010960](https://openairdocs.org/sdr/USAA010960.md): Stiffener · cracked · Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA010956](https://openairdocs.org/sdr/USAA010956.md): Frame · cracked · Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA010957](https://openairdocs.org/sdr/USAA010957.md): Strap · damaged · Jul 27, 2001 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - FOUND VERTICAL STRAP.125 INCH, BS 178, WL 208, LBL 25. DAMAGE SECTION REMOVED, REPLACEMENT SECTION SPLICED IN WITH DOUBLER PER EA 85114. (M) - [SDR USAA010681](https://openairdocs.org/sdr/USAA010681.md): Skin · cracked · Jun 14, 2001 · N413US · Boeing 737401 · Fuselage Main, Plate/Skin > CLT - 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) - [SDR USAA010586](https://openairdocs.org/sdr/USAA010586.md): Skin · cracked · May 10, 2001 · N413US · Boeing 737401 · Fuselage Structure (General) > PIT - 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) - [SDR USAA010277](https://openairdocs.org/sdr/USAA010277.md): Frame · cracked · Feb 14, 2001 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - FOUND FRAME CRACKED.5 INCH, STATION 400 FRAME RIGHT SIDE BETWEEN STRINGER 8R AND 9R. REMOVED DAMAGED, REPAIRED TR 53-10-14. (M) - [SDR USAASB01038](https://openairdocs.org/sdr/USAASB01038.md): Blade · damaged · Feb 5, 2001 · N413US · Boeing 737401 · Turbine Engine Compressor Section > BWI - 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 - [SDR USAASB00327](https://openairdocs.org/sdr/USAASB00327.md): Transmitter · failed · Nov 24, 2000 · N413US · Boeing 737401 · Engine Oil Pressure > PHL - 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 T - [SDR USAASB00249](https://openairdocs.org/sdr/USAASB00249.md): Wire · broken · Sep 10, 2000 · N413US · Boeing 737401 · Trailing Edge Flap Control System > CLT - 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. C - [SDR USAASB00070](https://openairdocs.org/sdr/USAASB00070.md): Controller · failed · Mar 11, 2000 · N413US · Boeing 737401 · Cabin Pressure Controller > BDL - 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 50 - [SDR USAASB99130](https://openairdocs.org/sdr/USAASB99130.md): Connector · loose · May 17, 1999 · N413US · Boeing 737401 · Emergency Lighting > TPA - 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. - [SDR USAA990429](https://openairdocs.org/sdr/USAA990429.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990428](https://openairdocs.org/sdr/USAA990428.md): Angle · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990427](https://openairdocs.org/sdr/USAA990427.md): Floorbeam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA990426](https://openairdocs.org/sdr/USAA990426.md): Beam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990425](https://openairdocs.org/sdr/USAA990425.md): Bulkhead · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA990424](https://openairdocs.org/sdr/USAA990424.md): Strap · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990419](https://openairdocs.org/sdr/USAA990419.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990418](https://openairdocs.org/sdr/USAA990418.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990417](https://openairdocs.org/sdr/USAA990417.md): Floor · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Floor Panel > CLT - 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) - [SDR USAA990416](https://openairdocs.org/sdr/USAA990416.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990415](https://openairdocs.org/sdr/USAA990415.md): Web · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990414](https://openairdocs.org/sdr/USAA990414.md): Tie Clip · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990413](https://openairdocs.org/sdr/USAA990413.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990412](https://openairdocs.org/sdr/USAA990412.md): Floorbeam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA990399](https://openairdocs.org/sdr/USAA990399.md): Angle · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990398](https://openairdocs.org/sdr/USAA990398.md): Floorbeam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Floor Beam > CLT - 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) - [SDR USAA990397](https://openairdocs.org/sdr/USAA990397.md): Web · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990381](https://openairdocs.org/sdr/USAA990381.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990380](https://openairdocs.org/sdr/USAA990380.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990379](https://openairdocs.org/sdr/USAA990379.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990378](https://openairdocs.org/sdr/USAA990378.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990377](https://openairdocs.org/sdr/USAA990377.md): Beam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990372](https://openairdocs.org/sdr/USAA990372.md): Bulkhead · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA990371](https://openairdocs.org/sdr/USAA990371.md): Bulkhead Web · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA990370](https://openairdocs.org/sdr/USAA990370.md): Bulkhead · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) - [SDR USAA990369](https://openairdocs.org/sdr/USAA990369.md): Beam · corroded · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990368](https://openairdocs.org/sdr/USAA990368.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990367](https://openairdocs.org/sdr/USAA990367.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990366](https://openairdocs.org/sdr/USAA990366.md): Frame · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Main, Frame > CLT - 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) - [SDR USAA990362](https://openairdocs.org/sdr/USAA990362.md): Web · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990361](https://openairdocs.org/sdr/USAA990361.md): Web · cracked · May 2, 1999 · N413US · Boeing 737401 · Fuselage Miscellaneous Structure > CLT - 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) - [SDR USAA990510](https://openairdocs.org/sdr/USAA990510.md): Bulkhead Angle · drill marks · Apr 30, 1999 · N413US · Boeing 737401 · Fuselage Main, Bulkhead > CLT - 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) Next page: https://openairdocs.org/deregistered/N413US-2003-09-18/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N413US-2003-09-18/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.