N13978
Service difficulty reports · 135
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 = 'N13978' AND registry_match = 'registration' 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 = 'N13978' AND registry_match = 'registration' 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 C2XA11RI028Unknown · odorFLIGHT 2419 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL IN COCKPIT AND FORWARD CABIN WITH PACK NR 1 ON AND USING APU BLEED. EWR MX RUN APU AND PACK NR 1 BUT NO SMELL WAS DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA11CL039Brake Assy · lockedGRB FLT 4912 THE CREW REPORTED THE NR 1 BRAKE LOCKED UP DURING TAXI AND THE MAIN WHEEL ASSEMBLY WENT FLAT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY AND MAIN WHEEL. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10SH383Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 59 HAS CORROSION (LEVEL 2 LOCAL) AS SEEN UNDERNEATH AT NUT PLATE. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAMES 59-62 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH382Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 60 HAS CORROSION (LEVEL 2 LOCAL) AS SEEN UNDERNEATH AT NUT PLATES. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM AT FRAME 59-62 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH381Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAMES 17-23 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH380Stringer · corrodedSHV - DURING C-CHECK BETWEEN FRAMES 51-52 STRINGER 19L. MAINTENANCE REMOVED AND REPLACED STRINGER BETWEEN FRAMES 51-52 STRINGER 19L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH379Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 58-60 NUT PLATE HOLES HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM BUTTSTRAP AT FRAME 58-61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH378Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM "L" FLANGE AT FRAME 40-41 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM "L" FLANGE AT FRAME 40-41 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH377Frame · crackedSHV - DURING C-CHECK LT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED LT FRAME 10 BELOW DV WINDOW IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH376Frame · crackedSHV - DURING C-CHECK RT FRAME 10 CRACKED BELOW DV WINDOW CUTOUT. MAINTENANCE REMOVED AND REPLACED RT FRAME 10 BELOW DV WINDOW CUTOUT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH375Floor Support · corrodedSHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON RT OMEGA BEAM AROUND NUT PLATE HOLE AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH374Hinge Fitting · wornSHV - DURING C-CHECK RT SPEED BRAKE I/B HINGE O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RT SPEED BRAKE I/B HINGE FITTING IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH373Bracket · wornSHV - DURING C-CHECK RT GROUND SPOILER I/B BRACKET O/B HAT BUSHING IS MIGRATED. MAINTENANCE REMOVED AND REPLACED RT GROUND SPOILER I/B BRACKET IAW EMB-145 SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW EMB-145 CPM 51-21-06. TORQUED BOLTS TO 42 IN LBS IAW EMSDR C2XA10SH363Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM LWR FLANGE HAS CORROSION (LEVEL 2 LOCAL) FR 35-36. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM LOWER FLANGE FRAME 35-36 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10RI097O-Ring · damagedFLIGHT 2946 - JAX-EWR - FLIGHT CREW DIVERTED FLIGHT TO SAV DUE TO BLEED NR 2 LEAK IN FLIGHT. CREW LANDED ACFT UNEVENTFULLY. EWR MX PERFORMED INSPECTION AND FOUND LEAK AT TEMP CONTROL VALVE HARDWARE. MX REMOVED AND REPLACED HARDWARE (O-RING AND TIE WRAPS) ANDSDR C2XA10RI081Socket · burnedFLIGHT 2614 - EWR - FLIGHT CREW REPORTED BURNING SMELL ABOVE SEAT 1A. EWR MX FOUND BURNED CEILING LIGHT SOCKET AT SEAT 6A. MX REMOVED AND REPLACED CEILING LIGHT ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10CL056Sensor · faultyCLE FLT 2883 THE CREW REPORTED A NR 3 BRAKE OVERHEAT MESSAGE DURING APPROACH. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 BRAKE ASSEMBLY AND BRAKE TEMP SENSOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10CL055Warning System · false activationBOS FLT 2883 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE DURING TAKEOFF. THE TAKEOFF WAS ABORTED. THE CREW RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA08TY122Fitting · wornRT AILERON PCA FITTING OTBD LUG (ON AILERON) MISSING HAT BUSHING. REMOVED AND REPLACED FITTING IAW EC5750-01177, REV B. AIRCRAFT CURRENTLY IN C-CHECK. (K)SDR C2XA08TY121Bushing · wornACFT CURRENTLY IN A C-CHECK STATUS WAS FOUND WITH THE LT AILERON PCA BRACKET WITH MIGRATING BUSHINGS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR C2XA08TY119Mount · corrodedAC CURRENTLY INA C-CHECK STATUS AND THE NR 2 ENGINE INLET MOUNTING FLANGE BOLT HOLES HAD SEVERAL HOLE`S THAT WERE FOUND CORRODED. MAINT REPAIRED THE INLET BOLTHOLES IAW EC5420-01161. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (KSDR C2XA08IA164Check Valve · leakingIAH-FLIGHT 2350, THE CREW REPORTED A FUEL LEAK FROM THE RT HAND WING. THE AIRCRAFT LANDED AT ORD WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RT WING NACA INLET FLAPPER CHECK VALVE. LEAK CHECKED WITH NOT DEFECTS AND THE AIRCRAFT WAS APPROVED FOSDR C2XA08IA079Engine · leakingIAH - FLIGHT 2156 - AFTER TAKEOFF THE LAVATORY SMOKE INDICATOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE NR 2 ENGINE WAS FOUND TO BE THE SOURCE OF THE SMOKE. MAINTENANCE REMOVED AND REPLACED THESDR C2XA08RI020Acm · malfunctionedFLIGHT 2985 - EWR - CREW REPORTED LAV SMOKE AND SMOKE IN THE CABIN DURING TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 ACM IAW EMB 145 AMM 21-51-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WSDR C2XA08TY025Unknown · smokeGSP - DURING CLIMB THE CREW HAD A LAV SMOKE INDICATION ON EICAS WITH VISIBLE SMOKE AND SMOKE SMELL. CREW AIR RETURNED TO GSP, MX PERFORMED HIGH POWER ENG RUNS FOR APPROXIMATELY 3 MINUTES AND COULD NOT DUPLICATE DISCREPANCY. A/C WAS RETURNED TO SERVICE.SDR C2XA07TY070Skin · puncturedDENT AND PUNCTURE UNDERNEATH SERVICE DOOR. REPAIRED DAMAGE TO AIRCRAFT IAW EC 5330-01752. PRESSURE CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR C2XA07IA170Unknown · odorFLT 2072, CREW REPORTED THAT FIRST ENG START HAD BEEN ABORTED DUE TO A HUNG START & A STRONG ODOR OF FUEL, ENGINE DRY MOTORED, & STARTED SUCCESSFULLY OFF OF FADEC B. ACFT LANDED WITHOUT INCIDENT. MX PLACED IGNITION SYSTEM ON MEL 74-20-00 CAT B CTL 125656, & SDR C2XA06SH128Skin · dentedSHV - DURING C-CHECK THE LEFT ELEVATOR UPPER SKIN WAS FOUND TO BE DENTED OUT OF LIMITS DUE TO LENGTH. EDDY CURRENT INSPECTION OF THE AREA REVEALED NO RELEVANT INDICATIONS. SUBMITTED TO ENGINEERING FOR DISPOSITION.SDR C2XA06SH127Skin · dentedSHV - DURING C-CHECK THE MAIN DOOR WAS FOUND TO BE DENTED FORWARD OF THE WINDOW. DENT WAS FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 52-10-01. EDDY CURRENT INSPECTION OF THE AREA REVEALED NO RELEVANT INDICATIONS. SUBMITTED TO ENGINEERING FOR DISPOSITION.SDR C2XA06SH125Case · corrodedSHV - DURING C-CHECK THE NR 1 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSITION.SDR C2XA06SH126Case · corrodedSHV - DURING C-CHECK THE NUMBER 2 ENGINE FAN CASE FORWARD ATTACHMENT HOLES WERE FOUND TO BE CORRODED. INFORMATION WAS SUBMITTED TO ENGINEERING FOR REPAIR AND DISPOSTION.SDR C2XA06SH123Floor Support · corrodedSHV - DURING C-CHECK THE LEFT OMGEA BEAM FLANGE WAS FOUND TO BE CORRODED BETWEEN FR 23-30. DAMAGE AT FR 24 WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 AND EC 53-00-10, FIG 202 SHSDR C2XA06SH124Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED FROM FR 23-30. AN AREA AT FR 24 WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REPAIR DOUBLER IAW EMB 145 SRM 53-00-10 AND EC 5330-01137. THE AIRSDR C2XA06CL087Bracket · burnedTHE CREW REPORTED SMOKE COMING FROM LIGHT ASSEMBLY ABOVE SEAT 1A. MAINTENANCE INSPECTED AND REPLACED SEAT 1A LIGHT BRACKET AND HARNESS ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05IA137Charger · inoperativeMCI - DURING MAINTENANCE INSPECTION, THE RT WING FAIRING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETSDR C2XA05CL094Wire · brokenDURING ROUTINE MAINTENANCE THE EXTERIOR RIGHT OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND REPAIRED WIRE W102-8500-22. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05SH122Skin · gougedSHV - RON AIRCRAFT GOUGE IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L. MAINTENANCE REPAIRED GOUGES IN SKIN FWD OF FRAME 20 AFT OF FRAME 19 BETWEEN STRINGERS 11L AND 12L IAW EMB 145 SRM 53-21-01 & IC 2005-145/4770. AIRCRAFT WAS APPROVSDR C2XA05IA107Inverter · inoperativeMCI - DURING MAINTENANCE INSPECTION, THE EMERGENCY EXIT MARKER AT ROW 12BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER FOR THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED SDR C2XA04SH567Floor Support · crackedDURING C CHECK, THE LEFT OMEGA BEAM SPLICE WAS CORRODED AND CRACKED BETWEEN FRAMES 23 AND 24. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01179. AIRCRAFT RETURNED TO SERVICE.SDR C2XA04SH564Floor Support · corrodedDURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 22 AND 23. REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE.SDR C2XA03IA097Light · inoperativeTHE CREW NOTED DURING PREFLIGHT THE EMERGENCY FLOOR PROXIMITY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE PLACED FLOOR LIGHTING ON DMIDO TO PARTS NOT IN STOCK.THE AIRCRAFT WAS RETURNED TO SERVICE. IAH- MAINTENANCE REMOVED AND REPLACED THE FLOOR PROXIMITY LIGSDR C2XA02SH176Frame · damagedSHV - DURING C-CHECK HOLES ON FRAME 15 WHERE COCKPIT TO CABIN LEFT FORWARD PORTION ATTACHES WERE FOUND ELONGATED. MAINTENANCE REPAIRED ELONGATED HOLES IAW CONTINENTAL EXPRESS EC 5340-01050. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH175Skin · scratchedSHV - DURING C-CHECK THE PASSENGER DOOR WAS FOUND TO HAVE SEVERAL SCRATCHES ON SKIN. MAINTENANCE REMOVED DAMAGED AREAS AND REPAIRED AFFECTED SECTIONS IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH174Skin · gougedSHV DURING C CHECK FUSELAGE SKIN WAS FOUND GOUGED JUST AFT OF LOWER AFT CORNER OF SERVICE DOOR CUT OUT. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01209. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH173Skin · dentedSHV DURING C CHECK THE PASSENGER DOOR WAS FOUND TO HAVE A DENT JUST FOWARD OF DOOR'S WINDOW. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5210-01070. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH170Stringer · gougedSHV-DURING C CHECK THE T REINFORCEMENT ON STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND GOUGED. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH169Floorbeam · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AREA AND REPAIRED AFFECTED OMEGA BEAM IAW EMB SRM 145 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH168Crossbeam · corrodedSHV- DURING C-CHECK FLOORBOARD ANGLE CROSS BEAM JUST AFT OF FRAME 23 WAS FOUND WITH CORROSION. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-04-02. THE AIRCRAFT WAS APPROVED TO RETURNED TO SERVICE.SDR C2XA02SH167Butt Strap · corrodedSHV- DURING C-CHECK FOWARD DIGITAL BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 14 AND 19. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED FOWARD DIGITAL BUTT STRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH166Sill · corrodedSHV- DURING C CHECK SILL BY SERVICE DOOR FOUND TO HAVE CORRSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AREA AND REPLACED AFFECTED SILL IAW EMB SRM 145 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
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