# Service difficulty reports: N346US, cancelled Dec 7, 2004 A list on [N346US, cancelled Dec 7, 2004](https://openairdocs.org/deregistered/N346US-2004-12-07.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 · 58 reports - [SDR USAASB02158](https://openairdocs.org/sdr/USAASB02158.md): Coupler · faulty · Aug 20, 2002 · N346US · Boeing 737301 · Autopilot System > ENROUTE, CLIMBING THROUGH FL210, AIRCRAFT EXPERIENCED A PULSING LEFT/RIGHT YAWING CONDITION. ONCE AUTOPILOT, AUTOTHROTTLE AND YAW DAMPER WERE OFF, YAWING STOPPED. CREW WAS UNABLE TO DUPLICATE CONDITION. PRIOR FLIGHT OF THIS AIRCRAFT WAS UNEVENTFUL. FLIGHT - [SDR USAA011362](https://openairdocs.org/sdr/USAA011362.md): Skin · corroded · Nov 12, 2001 · N346US · Boeing 737301 · Fuselage Main, Plate/Skin > TPA - FOUND SKIN CORRODED 3 SQUARE INCHES, STRINGER 25L STATION 975. SPLICED IN SECTION OF STRINGER PER SRM 53-00-03 PAGE 201. (M) - [SDR USAA010389](https://openairdocs.org/sdr/USAA010389.md): Bulkhead · cracked · Apr 16, 2001 · N346US · Boeing 737301 · Fuselage Main, Bulkhead > CLT - FOUND WEB CRACKED 2 INCHES, BS 178, RBL 6, BETWEEN WL 197 AND 205. INSTALLED DOUBLER SRM 53-10-08, EO 5300V153. (M) - [SDR USAA010386](https://openairdocs.org/sdr/USAA010386.md): Skin · cracked · Apr 16, 2001 · N346US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - FOUND SKIN CRACKED 2 INCHES, STATION 947 AT STRINGER 34L, FORWARD OF POTABLE WATER SERVICE PANEL. INSTALLED DOUBLER PER SRM 53-00-01, FIG 201. (M) - [SDR USAASB01091](https://openairdocs.org/sdr/USAASB01091.md): Coffeemaker · shorted · Mar 27, 2001 · N346US · Boeing 737301 · Buffet/Galleys > MIA - FLT 1191 - EN ROUTE FROM CLT-MIA, FLIGHT ATTENDANT REPORTED A SCORCHING SMELL IN THE FORWARD GALLEY APPROXIMATELY TEN MINUTES BEFORE LANDING AT MIA. OVENS WERE NOT IN USE AT THE TIME. COFFEE MAKER CIRCUIT BREAKERS WERE ALL PULLED AND GALLEY POWER WAS T - [SDR USAASB01012](https://openairdocs.org/sdr/USAASB01012.md): Warning System · malfunctioned · Jan 19, 2001 · N346US · Boeing 737301 · Landing Gear Position and Warning > ORF - FLT 12 - AFTER TAKEOFF FROM MCO, CREW RECEIVED A RIGHT MLG RED LIGHT WHEN PLACING THE GEAR HANDLE TO THE UP POSITION AS WELL AS THE OFF POSITION. AFTER RECYCLING GEAR TO THE DOWN POSITION, INDICATIONS WERE NORMAL AS THREE GEAR GREEN LIGHTS ILLUMINATED. - [SDR USAASB00309](https://openairdocs.org/sdr/USAASB00309.md): Door · not closed · Nov 6, 2000 · N346US · Boeing 737301 · Service Doors > ATL - FLT 1273 - AFTER TAKEOFF FROM ATL, THE AIRCRAFT WOULD NOT PRESSURIZE. CRWE NOTICED THE AFT RIGHT SERVICE DOOR WAS LEAKING AIR. FLIGHT RETURNED TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT R - [SDR USAASB00245](https://openairdocs.org/sdr/USAASB00245.md): Battery Pack · discharged · Sep 5, 2000 · N346US · Boeing 737301 · Emergency Lighting > GSO - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHTS AT THE OVERHEAD BIN DOORS WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) - [SDR USAA000039](https://openairdocs.org/sdr/USAA000039.md): Frame · corroded · Jan 17, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > STATION 747 - AFT BAG BIN FRAME HAS A 1 INCH AREA OF CORROSION, LEVEL 1. FABRICATED REPAIR PER SRM 51-30-01 AND 53-00-07. (M) - [SDR USAA000033](https://openairdocs.org/sdr/USAA000033.md): Keelbeam · corroded · Jan 13, 2000 · N346US · Boeing 737301 · Fuselage Main, Keel > RBL 6.5 STATION 528 TO 533 KEEL BEAM HAS A 5 INCH BY 1 INCH AREA OF CORROSION, LEVEL 2. INSTALLED REPAIR ANGLE PER EA 66434, SRM 51-70-12. (M) - [SDR USAA000032](https://openairdocs.org/sdr/USAA000032.md): Keelbeam · corroded · Jan 13, 2000 · N346US · Boeing 737301 · Fuselage Main, Keel > FOUND LBL 6.5, STATION 528, 537 TO 539 KEEL BEAM HAS A 2 INCH BY 1 INCH AREA OF CORROSION, LEVEL 2. INSTALLED REPAIR ANGLE PER EA 66434, SRM 51-70-12. (M) - [SDR USAA991447](https://openairdocs.org/sdr/USAA991447.md): Bulkhead · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Bulkhead > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.75 INCH CRACK AT STATION 178, RBL 4.75, WL 201 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-8 AND EA 66276. (M) - [SDR USAA991448](https://openairdocs.org/sdr/USAA991448.md): Angle · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.500 INCH CRACK AT STATION 294, OUTBOARD SIDE OF Z-ANGLE VERTICAL LEG SUPPORT ANGLE. REMOVED AND REPLACED PER SRM 51-10-02. (M) - [SDR USAA991449](https://openairdocs.org/sdr/USAA991449.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK FORWARD SERVIEC DOOR CUTOUT UPPER FORWARD FRAME WEB UPPER DOOR STOP FRAME. REMOVED AND REPLACED PER SRM 51-10-02. (M) - [SDR USAA991450](https://openairdocs.org/sdr/USAA991450.md): Door Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5I NCH CRACK DOOR FRAME CUTOUT UPPER FORWARD STOP FITTING DOOR FRAME WEB. REMOVED AND REPLACED PER SRM 51-10-02. (M) - [SDR USAA991451](https://openairdocs.org/sdr/USAA991451.md): Seat Track · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage, Seat/Cargo Attach Fittings > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT FORWARD END OF SEAT TRACK STATION 345, LBL 20. REPLACED SEAT TRACK PER SRM 53-00-02. (M) - [SDR USAA991452](https://openairdocs.org/sdr/USAA991452.md): Angle · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 4 INCH AREA OF CORROSION AT STATION 294.6 UPPER CHORD AFT FLANGE RBL 50.5, CORROSION LEVEL 1. INSTALLED ANGLE PER SRM 53-10-51 FIG 101. (M) - [SDR USAA991467](https://openairdocs.org/sdr/USAA991467.md): Skin · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Plate/Skin > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO 1.9 INCH CRACKS BS 328 FORWARD SERVICE DOORWAY, DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN. INSTALLED OUTER DOUBLER AND 2 MIDDLE DOUBLERS PER SRM 53-10-01 FIG 202. (M) - [SDR USAA991468](https://openairdocs.org/sdr/USAA991468.md): Skin · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Leading Edge Devices > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FIVE 1 INCH CRACKS ALONG ACTUATOR LOWER SKIN NR 1 SLAT. INSTALLED FILLER AND DOUBLER PER TR 57-50-01. (M) - [SDR USAA991475](https://openairdocs.org/sdr/USAA991475.md): Window Post · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK L-1 WINDOW AFT UPPER POST. INSTALLED DOUBLER PER EA 66274. (M) - [SDR USAA991476](https://openairdocs.org/sdr/USAA991476.md): Frame · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AFT CARGO BS 793 STRINGER 25R FRAME, CORROSION LEVEL 1. REPAIRED PER SRM 51-20-01 AND SRM 51-10-02. (M) - [SDR USAA991477](https://openairdocs.org/sdr/USAA991477.md): Angle · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 36 INCH BY 2 INCH AREA OF CORROSION FORWARD SERVICE DOOR Z-ANGLE STATION 289-325, RBL 61. CORROSION LEVEL 1. REPLACED Z-ANGLE PER SRM 51-10-02. (M) - [SDR USAA991494](https://openairdocs.org/sdr/USAA991494.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.250 INCH CRACK AT BS 311.9, STRINGER 5L CORNER OF FRAME. INSTALLED DOUBLER PER EA 66257 AND TR 53-10-14. (M) - [SDR USAA991495](https://openairdocs.org/sdr/USAA991495.md): Web · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT BS 294.5, STRINGER 7L, IN CORNER MOUNT POINT WEB. REMOVED AND REPLACED PER SRM 51-10-02 AND BOEING DWG 65-17684. (M) - [SDR USAA991496](https://openairdocs.org/sdr/USAA991496.md): Web · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT BS 306.0, STRINGER 4L MIDDLE LOWER LEG WEB. REMOVED AND REPLACED PER SRM 53-00-03. (M) - [SDR USAA991497](https://openairdocs.org/sdr/USAA991497.md): Stringer · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Longeron/Stringer > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.375 INCH CRACK AT STATION 726, STRINGER 18A SHELF, RBL 61, WL 188. REPAIRED PER SERM 51-10-02. (M) - [SDR USAA991498](https://openairdocs.org/sdr/USAA991498.md): Web · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Nose/Tail Landing Gear > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT N/G UPPER DRAG HRM WEB. INSTALLED NEW WEB PER REPAIR DOCUMENT 51-10-02. (M) - [SDR USAA991506](https://openairdocs.org/sdr/USAA991506.md): Floorbeam · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, BL 0 UPPER CHORD, CORROSION LEVEL 2. SPLICED IN NEW T-CPA PER SRM 53-10-51 FIG 205. (M) - [SDR USAA991499](https://openairdocs.org/sdr/USAA991499.md): Frame · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 1.5 INCH AREA OF CORROSION ON FRAME STATION 927 BETWEEN STRINGER 27L AND STRINGER 7R. CORROSION LEVEL 2. INSTALLED REPAIR DOUBLER PER SRM 53-00-07 AND SRM 51-40-01. (M) - [SDR USAA991373](https://openairdocs.org/sdr/USAA991373.md): Tie Clip · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 887, STRINGER 9L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M) - [SDR USAA991417](https://openairdocs.org/sdr/USAA991417.md): Tie Clip · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 663, STRINGER 10R TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M) - [SDR USAA991418](https://openairdocs.org/sdr/USAA991418.md): Tie Clip · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT BS 807, STRINGER 6R TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M) - [SDR USAA991419](https://openairdocs.org/sdr/USAA991419.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT BS 847, STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA991420](https://openairdocs.org/sdr/USAA991420.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A.25 INCH CRACK AT BS 480, STRINGER 8R AND 9R FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA991421](https://openairdocs.org/sdr/USAA991421.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK BS 847 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M) - [SDR USAA991423](https://openairdocs.org/sdr/USAA991423.md): Floorbeam · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH AT 3 AREAS UPPER CHORD TOP SURFACE BS 312, LBL 12 - RBL 24. FLOORBEAM CORROSION LEVEL 2. INSTALLED T-CAP PER SRM 53-10-51. (M) - [SDR USAA991440](https://openairdocs.org/sdr/USAA991440.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.250 INCH CRACK BS 480 BETWEEN STRINGER 8 AND 9 LEFT FRAME. INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M) - [SDR USAA991439](https://openairdocs.org/sdr/USAA991439.md): Stringer · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Longeron/Stringer > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND TWO.25 INCH CRACKS STRINGER 4L AT BS 908 AND 909 STRINGER. INSTALLED STRINGER PER SRM 51-40-00. (M) - [SDR USAA991438](https://openairdocs.org/sdr/USAA991438.md): Frame · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Frame > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.5 INCH CRACK AT BS 827 BETWEEN STRINGER 8L AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 66285. (M) - [SDR USAA991437](https://openairdocs.org/sdr/USAA991437.md): Splice · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK STRINGER 4R STATION 908 SPLICE. INSTALLED STRINGER PER SRM 51-40-00. (M) - [SDR USAA991436](https://openairdocs.org/sdr/USAA991436.md): Stringer · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Longeron/Stringer > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY.5 INCH, AREA OF CORROSION ON STRINGER 10R, STATION 337. CORROSION LEVEL 1. INSTALLED NEW STRINGER PER SRM 51-10-02. (M) - [SDR USAA991431](https://openairdocs.org/sdr/USAA991431.md): Floorbeam · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY.05 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, LBL 9.5 UPPER CHORD OF T-CAP. CORROSION LEVEL 1. SPLICED IN NEW T-CAP PER SRM 53-10-51 FIG 205. (M) - [SDR USAA991430](https://openairdocs.org/sdr/USAA991430.md): Floorbeam · corroded · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Main, Floor Beam > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY.05 INCH AREA OF CORROSION ON FLOORBEAM STATION 344, RBL 2.5 AFT EDGE OF T-CAP. CORROSION LEVEL 1. SPLICED IN NEW T-CAP PER SRM 53-10-51 FIG 205. (M) - [SDR USAA991424](https://openairdocs.org/sdr/USAA991424.md): Tie Clip · cracked · Jan 12, 2000 · N346US · Boeing 737301 · Fuselage Miscellaneous Structure > CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A.125 INCH CRACK AT BS 663, STRINGER 10L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M) - [SDR USAASB99264](https://openairdocs.org/sdr/USAASB99264.md): Sensor · failed · Nov 2, 1999 · N346US · Boeing 737301 · Landing Gear Position and Warning > CHS - FLT 542 - DURING CLIMB-OUT FROM CHS, FLIGHT EXPERIENCED A FAILURE OF BOTH ATC TRANSPONDERS AND THE LEFT NAV FUNCTION OF THE AUTOPILOT. FLIGHT RETURNED TO FIELD AT CHS AND LANDED WITHOUT FURTHER INCIDENT. FLIGHT THEN TAXIED TO THE GATE. NO EMERGENCY WA - [SDR USAA980381](https://openairdocs.org/sdr/USAA980381.md): Skin · cracked · Aug 21, 1998 · N346US · Boeing 737301 · Fuselage Main, Plate/Skin > TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN SKIN E/E DUCT COOLING OUTLET STATION 379 LBL 30. INSTALLED DOUBLER OF.100 INCH 2024-T3 PER EA 62079 AND BOEING SB 737-53-1117. (M) - [SDR USAASB98155](https://openairdocs.org/sdr/USAASB98155.md): Detector · failed · Jun 24, 1998 · N346US · Boeing 737301 · Fire Detection > SBN - FLT 7002 - ABOUT 60 MILES OUT OF SBN, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER GOING THROUGH CHECKLIST, CAPTAIN ELECTED TO RETURN TO FIELD AT SBN. AN EMERGENCY WAS DECLARED WITH THE TOWER. WHEN THE CREW PULLED BACK THE POWER ON THE NR 2 ENGIN - [SDR USAASB97342](https://openairdocs.org/sdr/USAASB97342.md): Wire · failed · Dec 20, 1997 · N346US · Boeing 737301 · Light System Wiring > CLT - CREW REPORTED THAT THE EMERGENCY FLOOR LIGHTS AT ROW 10 WERE INOP. MAINTENANCE REPAIRED/SPLICED WIRES. OPERATIONAL CHECK GOOD. (M) - [SDR USAASB97104](https://openairdocs.org/sdr/USAASB97104.md): Control Module · malfunctioned · Apr 16, 1997 · N346US · Boeing 737301 · Fire Detection > RDU - FLT 1416 - EN ROUTE MCO TO BWI, FLIGHT ENCOUNTERED NR 1 ENGINE GENERATOR FAILURE. NR 1 ENG FIRE WARNING LIGHT ILLUMINATED, BELL DID NOT SOUND. CREW SHUT DOWN ON NR 1 ENG. EMERGENCY DECLARED AND FLT DIVERTED TO RDU. FLT LANDED WITHOUT INCIDENT. TOTAL - [SDR 97ZZZX2012](https://openairdocs.org/sdr/97ZZZX2012.md): Control Panel · malfunctioned · Apr 16, 1997 · N346US · Boeing 737301 · Fire Detection > RDU - FLT 1416 - EN ROUTE MCO TO BWI, FLIGHT ENCOUNTERED NR 1 ENGINE GENERATOR FAILURE. NR 1 ENG FIRE WARNING LIGHT ILLUMINATED, BELL DID NOT SOUND. CREW SHUT DOWN ON NR 1 ENG. EMERGENCY DECLARED AND FLT DIVERTED TO RDU. FLT LANDED WITHOUT INCIDENT. TOTAL Next page: https://openairdocs.org/deregistered/N346US-2004-12-07/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 = 'N346US' AND deregistration_id = 'N346US-2004-12-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N346US-2004-12-07/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.