N13929, cancelled Dec 29, 2015
Service difficulty reports · 112
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 = 'N13929' AND deregistration_id = 'N13929-2015-12-29' 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.
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 = 'N13929' AND deregistration_id = 'N13929-2015-12-29' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASOA20130713115Skin · crackedDURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.SDR ASOA20130713120Skin · crackedDURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 ABOVE STR 06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130713119Skin · crackedDURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR78 BELOW S4L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130713118HSkin · crackedDURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR 77 ABOVE S6L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130713117Skin · crackedDURING 1A CHECK THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR77 BELOW STR 04L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/13.SDR ASOA20130713116Skin · crackedDURING 1A CHECK THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FR79 BELOW STR 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130713114Skin · crackedDURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR78 BETWEEN STRINGERS 5 & 6R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130713113Skin · crackedDURING 1A INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET AT FR77 STRINGER 04R. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 07/15/2013.SDR ASOA20121209166Inverter · inoperativeGALLEY EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.SDR ASOA20120820112HUnknown · odorTHE CREW REPORTED A BURNING ODOR IN THE CABIN NOTICED BY THE F/A. MX INSPECTED THE ACFT AND WAS UNABLE TO DUPLICATE ANY BURNING ODOR OR SMELL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120124012Sign · inoperativeTHE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE ROW 1A WAS INOPERATIVE. MX R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11ASH134Skin · corrodedSHV - DURING C-CHECK INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 18R-20R IS CORRODED. MAINTENANCE PERFORMED REPAIR ON INNER FUSELAGE SKIN BETWEEN FRAMES 14-15, STRINGERS 17R-21L IAW EC5330-02474. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11SH133Skin Splice · corrodedSHV - DURING C-CHECK LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L-19L CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON LONGITUDINAL SKIN SPLICE BETWEEN FRAME 14-15, STRINGER 18L- 19L IAW EMB-145 CPM 51-21-00. THE AIRCRAFT WAS APPROVED SDR C2XA11SH132Skin Splice · corrodedSHV - DURING C-CHECK CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14-15, STRINGERS 20L-15R CORRODED (LOCAL LEVEL 2). MAINTENANCE PERFORMED REPAIR ON CIRCUMFERENTIAL SPLICE BETWEEN FRAMES 13-15, STRINGERS 20L-15R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROSDR C2XA11SH131Stringer · corrodedSHV - DURING C-CHECK STRINGER 21L BETWEEN FRAMES 11-12 IS CORRODED. MAINTENANCE REMOVED AND REPLACED STRINGER 21L FRAME 9-13 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11SH130Skin · corrodedSHV - DURING C-CHECK SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R HAS IMPROPERLY PAINTED SKIN AND CORROSION IN UNPAINTED AREAS. MAINTENANCE PERFORMED REPAIR ON SKIN BETWEEN FRAMES 7-14 STRINGER 18L-18R IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETSDR C2XA11SH129Bushing · migratedSHV - DURING C-CHECK RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET HAS MIGRATING HAT BUSHING. MAINTENANCE PERFORMED REPAIR ON RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT HINGE FITTING BRACKET IAW EMB-145 AMM 27-62-05, OPERATIONAL CHECK GOOSDR C2XA11SH128Crossbeam · corrodedSHV - DURING C-CHECK CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON CROSSBEAM BETWEEN LT OMEGA BEAM AND CENTER OMEGA BEAM AT FRAME 20 IAW ETD 2011-145-103674. THE AIRCRAFT WAS APPROVED FOR RETURN TSDR C2XA11SH127Skin · corrodedSHV - DURING C-CHECK CORROSION FOUND ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 57-58, STRINGER 21L-21R. MAINTENANCE PERFORMED REPAIR ON INTERNAL FUSELAGE SKIN, BETWEEN FRAMES 57-58 STRINGER 21L-21R IAW EC5330-02475. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR C2XA11SH121Frame · crackedSHV - DURING C-CHECK THE RT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 10R-11R, DIRECTLY BELOW THE RT DV WINDOW. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XAII1A105Trim Switch · malfunctionedIAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLSDR C2XA11IA104Trim Switch · shortedIAH - THE CREW REPORTED A PITCH TRIM RUNAWAY ON TAKEOFF, FOLLOWED BY A PITCH TRIM INOP MESSAGE AND BOTH PITCH TRIM CIRCUIT BREAKERS POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLSDR C2XA11IA044Power Supply · inoperativeIAH - FLIGHT 2913, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH AND EXIT ROW SIGN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPSDR C2XA11IA047Connector · looseIAH - DURING MAINTENANCE INSPECTION THE RIGHT OVERWING FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR C2XA11IA043Battery Pack · dischargedIAH - FLIGHT 2093, THE CREW REPORTED THAT THE EMERGENCY LIGHTS AFT OF ROW 12 WOULD NOT ILLUMINATE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA296Power Supply · inoperativeIAH - THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON WHEN THE AIRCRAFT WAS DOWN POWERED WITH ALL SWITCHES IN CORRECT POSITIONS. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE SDR C2XA10IA245Unknown · odorIAH - FLIGHT 2104, THE CREW REPORTED A STRONG ODOR AFTER T/O. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED BOTH ENGINES WITH NO DEFECTS OR ODORS FOUND, AND THE AIRCRAFT WAS APPROVED SDR C2XA10IA179Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE NR 4 AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHT STRIP ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IAH MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE SDR C2XA10IA144Skin · crackedIAH - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA120Ballast · overheatedIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL SMELL IN THE AREA OF SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE BALLAST 2A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA207Ballast · burnedFLIGHT 2195, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE LAV. MAINTENANCE INSPECTED THE LAV, AND REMOVED THE LIGHT BULB FROM THE LAV CEILING LIGHT, AND PLACED THE LAV LIGHTING ON NEF-LV-05 CAT "D" CTL NUMBER 176224, AND THSDR C2XA09SH104Frame · corrodedDURING C-CHECK. FR 75 SHOWS SIGNS OF CORROSION BTW STR 2L-2R. REPAIRED FR 75 IAW EC 5310-01317. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH103Stringer · corrodedDURING C-CHECK, STR 21L CORRODED BTW FR 65-66. REPAIRED STR 21L IAW IC 2009-145/01544. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH102Support · corrodedDURING C-CHECK, TOILET WASTE DRAIN VALVE SUPPORT CORRODED. REPAIRED TOILET WASTE DRAIN SUPPORT IAW SRM 53-31-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH101Floor Support · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 33. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH100Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 33. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH099Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 38. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH098Floor Support · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 29. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH097Floor Support · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED CENTER OMEGA BEAM IAW EMS 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH096Floor Support · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 59. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH095Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 59. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-24-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH094Floor Support · corrodedSHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 49. CENTER OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH093Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 54. LT OMEGA BEAM WAS REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH092Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 49. REPAIRED LT OMEGA AT FR 49 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH091Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 44. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH090Floor Support · corrodedSHV - DURING C-CHECK, LT OMEGA BEAM FLANGE HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM AT FR 29 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH089Floor Support · corrodedSHV - DURING C-CHECK, RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED OMEGA BEAM AT FR 23 IAW IC 2009-145/01857. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH088Splice · corrodedSHV - DURING C-CHECK, LONGITUDINAL SPLICE CORRODED BETWEEN FR 61-66 STR 19L-20L. REPAIRED SPLICE IAW EMB 145 SRM 51-14-00. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH087Skin · corrodedSHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 70-73 STR 19L-19R. REPAIRED SKIN IAW EMB 145 SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH086Skin · corrodedSHV - DURING C-CHECK, CORROSION ON SKIN BETWEEN FR 60-61. REPLACED SKIN IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Back to N13929, cancelled Dec 29, 2015