N13968, cancelled Mar 1, 2016
Service difficulty reports · 57
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 = 'N13968' AND deregistration_id = 'N13968-2016-03-01' 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 = 'N13968' AND deregistration_id = 'N13968-2016-03-01' 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 ASOA20140503083Yoke · crackedDURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE LOWER YOLK FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE R & R THE ENGINE YOKE IAW EC 5450-010073B. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20131209136RBattery Pack · dischargedGALLEY SERVICE DOOR EMERGENCY LIGHT REPORTED NOT TO BE ILLUMINATING. MX R & R NR 2 EMERGENCY LIGHT BATTERY AND SIGN WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121020096RUnknown · odorPASSENGERS REPORTED ELECTRICAL BURNING ODOR COMING FROM VENTS AROUND ROWS 3,4,5 AND 6. MX PERFORMED SUCCESSFUL OPS CHECK OF BOTH PACKS RUNNING WITH NO EVIDENCE OF BURNING ODOR. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120613085Inverter · inoperativeDURING ROUTINE CHECK, MX REPORTED THE EXIT SIGN AT SEAT 12A TO BE INOPERATIVE. MX R & R THE INVERTER FOR AFFECTED EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120404028Inverter · inoperativeDURING SCHEDULED MX INSPECTION, AFT CABIN FLOOR PATHWAY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. R & R THE NR 6 INVERTER IAW AMM 33-50-11 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11CL239Switch · faultyBNA FLT 5955 THE CREW REPORTED THE NR 1 BLEED VALVE WOULD NOT OPEN DURING FLIGHT. CLOSED INDICATION ON THE EICAS. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED VALVE PUSHBUTTON SWITCH. OSDR C2XA11TY166Relay · brokenTYS FOR BNA A/C ON CLIMBOUT HAD A EICIAS WITH A MESSAGE THAT THE NR 1 BLEED VALVE WAS CLOSED IN FLIGHT. THE CREW RETURNED TO BNA AND SWAPPED A/C. MAINTENANCE REMOVED AND REPLACED THE PUSHBUTTON IAW EMB 145 AMM 20-13-04. OPS CHECK GOOD. OPS CHECKED THE NR SDR C2XA11IA191Engine · vibrationDURING CLIMB THE CREW REPORTED A ENGINE ONE HIGH VIBRATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA11TY063Proximity Sensor · crackedTYS - A/C WAS FERRIED FROM ATL TO TYS FOR A SPOILER FAIL MESSAGE AND CIRCUIT BREAKER POP. MAINTENANCE REMOVED AND REPLACED THE LEFT SPEED BRAKE PROX SENSOR IAW EMB 145 AMM 27-63-04, OPS CHECK WAS GOOD AND A/C RELEASED BACK TO SERVICE.SDR C2XA11IA082Hydraulic Line · rupturedIAH - FLIGHT 2044, THE CREW REPORTED THE NUMBER TWO HYDRAULIC SYSTEM HAD A LOW QUANTITY FOLLOWED BY A NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULISDR C2XA11RI054Unknown · odorFLIGHT 3064 - EWR - FLIGHT CREW REPORTED POSSIBLE LIGHTNING STRIKE - CLICKING SOUND IN CEILING AND BURNING SMELL TEMPORARELY. EWR MX PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND NO EVIDENCE OF LIGHTNING DAMAGE NO BURNING SIGNS NOTICED. ACFT WAS APPROVED TSDR C2XA10SH265Floor Support · corrodedSHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH264Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 37-38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH263Floor Support · corrodedSHV - DURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH262Skin · corrodedSHV - DURING C-CHECK THE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 62-63 AND STRINGERS 20-21R. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH261Skin · crackedSHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 75, STRINGER 2L. MAINTENANCE REMOVED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02199. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA251Skin · crackedIAH - DURING MAINTENANCE INSPECTION THE CROWN SKIN PANEL WAS FOUND TO HAVE A 55MM CRACK ON THE LOWER LEG BETWEEN THE CAPTAINS WINDSHIELD AND DV WINDOW. MAINTENANCE REMOVED THE DAMAGED SECTION, AND INSTALLED A REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING CHANSDR C2XA09CL113Actuator · faultyCLE - FLT 2861 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS WHEN THE GEAR WAS SELECTED DOWN AND THEN CLEARED ONCE THE GEAR WAS DOWN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOODSDR C2XA08CL117Oil System · fluctuatesEWR FLIGHT NR 2142 THE CREW REPORTED DURING TAKEOFF ROLL AND INITIAL CLIMBOUT THE OIL PRESSURE REMAINED ABOVE 115 PSI FOR 2 MIN ON THE NR 1 ENGINE. ALSO BELOW 13000 FT THE NR 1 ENGINE OIL PRESSURE WOULD ENTER THE AMBER RANGE WITH THRUST IN DESCENT. MX INSPECSDR C2XA08CL102Wire Harness · defectiveCLE FLIGHT NR 2320 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE IN FLIGHT. THE GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NOSE GEAR WOW HARNESS AND PROXIMITY SWITCH. OPS CHECKS WERE GOOD.SDR C2XA08RI088Solenoid Valve · defectiveFLIGHT 3001 - EWR - FLIGHT CREW REPORTED THAT IT SOUNDED LIKE LANDING GEAR DOORS OPEN IN FLIGHT. EWR MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOOR SOLENOID VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR C2XA08SH075Support · crackedSHV - DURING C-CHECK PAX DOOR INTERNAL HANDLE SUPPORT CRACKED. MX REMOVED AND REPLACED PAX DOOR INTERNAL HANDLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08SH074Support Bracket · corrodedSHV - DURING C-CHECK WASTE DRAIN SUPPORT CORRODED INSIDE AIRCRAFT. MX REMOVED AND REPLACED WASTE DRAIN DUMP VALVE SUPPORT ASSY IAW EMB 145SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08SHO76Floor Support · corrodedSHV - DURING C-CHECK LEFT OMEGA BEAM REPAIR AT FR 20 IS CORRODED. MX REMOVED AND REPLACED PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA08CL018Inverter · inoperativeDURING ROUTINE MAINTENANCE, THE EXIT MARKER LIGHT AT ROW 3 BC WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07IA228Battery Pack · inoperativeIAH - FLIGHT 2618, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE CENTER AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS SDR C2XA07IA190Engine · malfunctionedATL - FLIGHT 3067, THE CREW REPORTED LAV SMOKE WARNING & HAZE IN CABIN DURING FLIGHT. DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE OPS CHECK NR 1/ NR 2 PACKS IAW EMB 145 MM AMM 21-51-00. ALL OPS & INDICATIONS NORMAL. VISUALLY INSPECTED, NOSDR C2XA07IA072Light · inoperativeIAH FLIGHT 2305, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE LAST ROW OF AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAST SECTION OF AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPSDR C2XA07IA064Acm · frozenIAH - FLIGHT 2082, DURING TAKEOFF ROLL, THE CREW REPORTED A STRONG SMOKE ODOR INVADED THE CABIN AND FLIGHT DECK. THE CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY CHECKED WITH NO DEFECTSSDR C2XA06IA114Smoke · detectedTHE CREW REPORTED SMOKE IN THE COCKPIT AND MOISTURE IN THE LINES. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.SDR C2XA06TY035Light · burnedCLT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, ELECTRICAL ODOR, CREW DID AN AIR RETURN, OVERWEIGHT LANDING, NORMAL LANDING AND ROLL OUT. MAINTENANCE FOUND SOURCE OF SMOKE AND ELECTRICAL ODOR TO BE COMING FROM THE READING LIGHTS AT SEATS 6A AND 7A, MAINTENANCESDR C2XA05BT063Sign · faultyDURING 5A INSPECTION, MAINTENANCE FOUND THE AFT GALLEY EMERGENCY EXIT SIGN FAULTY. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-14. OPS CHECKED GOOD.SDR C2XA04TY108Bushing · corrodedDURING A SCHEDULED 3C INSPECTION MAINT FOUND CORRODED BUSHING ON ALL RUDDER 2 HINGE POINTS. MAINT REMOVED AND REPLACED ALL OF THE HINGE POINT BUSHINGS IAW EMB 20-10-08. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA04TY107Bracket · corrodedDURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON THE SINK DRAIN BRACKETS. MAINT REMOVED THE SINK BRACKETS, FAB A NEW PART, ALODINED, PRIMED AND PAINTED AND INSTALL THE NEW BRACKET IAW EMB 13/145 SRM 51-40-02; 51-30-03; 51-21-03; 04; 05 AND 51-40-02. ASDR C2XA04TY106Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION THE LEFT INBD FLOOR SUPPORT WAS FOUND CORRODED AT BOTTOM OF RAMP IN GALLEY. MAINT CUT OUT DAMAGE AND FAB A NEW REPAIR FOR THE EFFECTED AREA AND INSTALL NEW REPAIR PART IAW EMB 135/145 SRM 53-21-10; 53-21-03 AND 51-40-06 ALSO CSDR C2XA04TY105Frame · gougedDURING A SCHEDULED 3C INSPECTION THE BOTTOM OF THE APU FIREWALL HAD A GOUGE. MAINT FOUND THE GOUGES TO BE ON FR 81, BLENDED DYE PEEN GOUGE AREA, REMOVED RIVETS, FAB DOUBLER AND INSTALL IAW EC 5330-01352. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COSDR C2XA04TY104Floorbeam · corrodedDURING A SCHEDULED 3C INSPECTION, CORROSION WAS FOUND ON THE RIGHT LAV FLOORBEAM TOP CAP IN SEVERAL PLACES. MAINT REMOVED AND REPLACED THE RIGHT TOP CAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA04TY103Floor Support · corrodedDURING A SCHEDULED 3C INSPECTION CORROSION WAS FOUND ON LEFT SIDE LAV FLANGE. MAINT REMOVED AND REPLACED THE FLOOR SUPPORT FLANGE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA04TY102Sill · corrodedDURING A SCHEDULED 3C INSPECTION THE PAX DOOR SILL WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE DOOR SILL IAW EMB 135/145 SRM 51-40-02; 03 AND EMB CPM51-21-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA04TY094Gusset · corrodedDURING A SCHEDULED 3C INSPECTION FR 22 GUSSET CAP WAS FOUND CORRODED AROUND THE RIVETS. REMOVED FR 22 GUSSET CAP, FAB A NEW CAP, ALODINED, PRIMED AND PAINTED. THEN INSTALL FAB PART IAW EMB 135/145 SRM 51-30-03; SRM 51-40-02; 03; 04. ALL WORK WAS ACCOMPLISHESDR C2XA04TY098Floorbeam · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA04TY097Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE UNDER THE CARBON FIBER BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA04TY096Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RAMP ANGLE AND AFT NUT PLATE OF THE CENTER TOP CAP UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE CENTER TOP CAP IAW EMB SRM 51-40-02 AND 57-20-03. THE AIRCRAFT WILL BE RELEASED UPON COMPSDR C2XA03CL197Fan · seizedCLE FLIGHT NR 2123) THE CREW REPORTED A VERY STRONG SMELL OF SMOKE FROM CABIN ON APPROACH. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED SYSTEM AND FOUND THE NR 2 RECIRCULATION FAN WAS SEIZED. MAISDR C2XA03CL194Smoke · detectedCLE) FLIGHT NR 3230, THE CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE ON DESCENT INTO CLEVELAND.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 BLEED AIR SYSTEM,THE NR 1 AND NR 2 ENGINES AND APU. NO DEFECTS WERESDR C2XA03CL171Engine · failedSTL FLIGHT NR 2368 THE CREW REPORTED THE NR 1 ENGINE UNCOMMANDED SHUT DOWN ON APPROACH INTO STL.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT RETURNED TO SERVICE.SDR C2XA03TY043Proximity Switch · out of adjustDURING CLIMB RECEIVED A ICAS MESSAGE OF LDG AIR/GND FAIL AT ROTATION. LANDING GEAR WOULDN'T RETRACT. AIR RETURN AND MAINT FOUND PROX SWITCHES OUT OF ADJUSTMENT. DID A RE-ADJUSTMENT OF THE SWITCHES AND DID THE GEAR SWINGS AS REQUIRED. A/C WAS PUT BACK INTO SDR C2XA03BT037Apu · seizedEWR FLT2578 CREW REPORTED DURING APU START APU FAILED INDICATION WAS INSTRUCTED I HAD A FIRE BLEW EXTINGUISHER BOTTLE. MX FOUND APU SIEZED INSPECTED AND PLACED ON MEL. #49-00-00. ACFT RELEASED FOR SERVICE. SDR REMAINS OPEN.SDR C2XA02SH042Sill · corrodedSHV- DURING C-CHECK INSPECTION, FRAME 18-19 RIGHT HAND OUTBOARD SILL FORWARD OF SERVICE DOOR HAD THREE AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OUTBOARD SILL BETWEEN FRAMES 18 AND 19 IAW EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APSDR C2XA02SH041Sill · corrodedSHV- DURING C-CHECK INSPECTION, FRAME 22 RIGHT HAND OUTBOARD SILL AFT OF SERVICE DOOR WAS FOUND TO HAVE FOUR AREAS OF CORROSION. MAINTENANCE OUT OF LIMITS RIGHT HAND OUTBOARD SILL IAW EMB 145-SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
Back to N13968, cancelled Mar 1, 2016