N15973, cancelled Jan 5, 2017

Service difficulty reports · 92

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 = 'N15973' AND deregistration_id = 'N15973-2017-01-05'
  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.

SDR ASOA20150104001Battery Pack · inoperativeDURING MAINTENANCE INSPECTION THE NR 1 EMERGENCY LIGHT SYS BATTERY WOULD NOT HOLD A CHARGE. MAINTENANCE R & R NR 1 EMERGENCY LIGHT SYSTEM BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 4, 2015 · N15973 · Emb EMB145LR · Emergency LightingSDR ASOA20140106009Shear Tie · crackedC-CHECK, A CRACKED SHEAR TIE WAS FOUND AT FRAME 24 BETWEEN S15-16R. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02.Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA20140106008Shear Tie · crackedC-CHECK, A CRACK WAS FOUND IN A SHEAR TIE AT FRAME 73 BETWEEN STR8L AND 9L. MAINTENANCE R & R THE CRACKED SHEAR TIE IAW SRM 51-40-02.Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA20140106007Floor Support · crackedC-CHECK, A CRACK WAS FOUND IN THE RT OMEGA BEAM INBD SUPPORT BETWEEN FRAMES 47 AND 48. MAINTENANCE R & R THE OMEGA BEAM SUPPORT IAW SRM 53-23-02 AND SRM 51-40-02. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20140106006Shear Tie · crackedC-CHECK, A SHEAR TIE AT FRAME 26 BETWEEN STR 15R AND 16R WAS FOUND CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-20--01 AND 51-40-02.Jan 6, 2014 · N15973 · Emb EMB145LR · Fuselage Internal Mounting StructureSDR ASOA20140106005Floor Support · crackedCRACK IN RT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT.Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20140106004Floor Support · crackedCRACK IN LT OMEGA BEAM SUPPORT. R & R FLOOR SUPPORT.Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20140106002Beam · corrodedCARGO DOOR CUTOUT THRESHOLD BEAM CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R THRESHOLD BEAM.Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20140106001Floor Support · corrodedRT OTBD FLOOR SUPPORT AT FRAME 50 CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.Jan 5, 2014 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120301018Mount · crackedDURING C-CHECK, NR 1 ENGINE FWD LOWER YOKE FITTING IS CRACKED. REPAIRED YOKE IAW EC5450-01047. ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2012 · N15973 · Emb EMB145LR · Engine Mount SectionSDR C2XA11IA145Unknown · odorIAH - FLIGHT 2818, THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND FORWARD CABIN AFTER LANDING. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN THE ENGINES, PACKS, AND APU ALL WITH NO DEFECTSJul 4, 2011 · N15973 · Emb EMB145LR · Air Distribution SystemSDR C2XA11RI111Fastener · looseFLIGHT 6061 - IAD - FLIGHT CREW REPORTED LOUD NOISE COMING FROM F/O WINDSHIELD. IAD MX RETORQUED F/O WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Jun 17, 2011 · N15973 · Emb EMB145LR · Flight Compartment WindowsSDR C2XA11RI110Conditioner · defectiveFLIGHT 2041 - EWR - FLIGHT CREW REPORTED RT O/B BRAKE OVERTEMP MSG ON EICAS DURING T/O. UPON LANDING MESSAGE CLEARED AND BRAKE INDICATED NORMAL TEMP. EWR MX REMOVED AND REPLACED O/B TEMP SIGNAL CONDITIONER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT Jun 12, 2011 · N15973 · Emb EMB145LR · Landing Gear Brake SystemSDR C2XA10CL031Bleed Valve · failedCLE FLT 2513 THE CREW REPORTED A NR 1 HIGH STAGE BLEED VALVE FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 1 HIGH STAGE VALVE AND THE NR 1 ENGINE INDICATING HARNESS. OPERATIONAL CHECKS WERE GOOD.Feb 20, 2010 · N15973 · Emb EMB145LR · Compressor Bleed ValveSDR C2XA10SH057Trunnion · corrodedSHV - DURING C-CHECK RIGHT MLG AFT UPPER TRUNNION HAS PITTING CORROSION AND IS OUT OF LIMITS. REPAIRED RIGHT MLG AFT UPPER TRUNNION IAW EC57350-01406. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 10, 2010 · N15973 · Emb EMB145LR · Main Landing Gear Attach SectionSDR C2XA10SH056Wire · brokenSHV - DURING C-CHECK LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPAIRED BROKEN WIRE IAW EMB 145 WM 20-21-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 10, 2010 · N15973 · Emb EMB145LR · Landing Gear System WiringSDR C2XA10SH051Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH050Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH049Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH048Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH047Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 49-50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH046Floor Support · corrodedSHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 33. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH045Floor Support · corrodedSHV DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 8, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH042Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED LT OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 1, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH041Structure · corrodedSHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 31, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA10SH038Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 31, 2010 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA09IA051Unknown · odorIAH - FLIGHT 2875 THE FLIGHT ATTENDANT REPORTED A BURNING SMELL WHEN THE HEATER WAS ON. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY TESTED BOTH PACKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SUBSEQUENFeb 17, 2009 · N15973 · Emb EMB145LR · Air Distribution SystemSDR C2XA09CL012Strut · underservicedCLE FLIGHT NR 2847 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MSG AND A THRUST REVERSE 1&2 DISAGREE MSG ON THE EICAS ON CLIMBOUT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND SERVICED THE NOSE GEAR STRUT. OPS CHECK WAJan 27, 2009 · N15973 · Emb EMB145LR · Nose/Tail Landing Gear Strut/AxleSDR C2XA08IA269Muffler · looseIAH - FLIGHT 2434, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED IN FLIGHT, AND WERE UNABLE TO RESET. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE PACK 2 DISTRIBUTION MUFFLER, OPERATIODec 28, 2008 · N15973 · Emb EMB145LR · Air Distribution SystemSDR C2XA08IA268Wire · brokenIAH - FLIGHT 2434, THE CREW REPORTED A PACK 1 VALVE CLOSED ADVISORY MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE W101-2447-22 AT THE BUSHBUTTON FOR PACK ONE, OPERATIONALLY TESTED WITH NO DEFECTS,Dec 28, 2008 · N15973 · Emb EMB145LR · Air Conditioning System WiringSDR C2XA08SH019Floor Support · crackedSHV - DURING C-CHECK LEFT OMEGA BEAM AT FR 22 HAS A CRACK IN WEB THROUGH RIVET. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19 AND 23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Feb 2, 2008 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA08SH018Floor Support · corrodedSHV - DURING C-CHECK LEFT OMEGA BEAM WEB AND FLANGE AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19-23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Feb 2, 2008 · N15973 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR C2XA07IA222Lock · defectiveIAH - FLIGHT 2711, THE CREW REPORTED THAT THE CAPTAINS DV WINDOW POPPED OPEN DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE CAPTAINS DV WINDOW LOCK BAR AND ADJUSTED IAW EMB-145 MOct 10, 2007 · N15973 · Emb EMB145LR · Flight Compartment WindowsSDR C2XA07IA192Ballast · defectiveIAH - FLIGHT 2857, THE CREW REPORTED THAT THE BALLAST ABOVE SEAT 4A SMELLED BURNT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE LIGHTING IN MEL 33-210-00/1 CAT C CONTROL 128447, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNEDSep 2, 2007 · N15973 · Emb EMB145LR · Passenger Compartment LightingSDR C2XA07CL073Sign · inoperativeDURING ROUTINE MAINTENANCE THE EXIT SIGN AT THE RIGHT AFT DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.Aug 28, 2007 · N15973 · Emb EMB145LR · Emergency LightingSDR C2XA07CL064Sensor · shortedFLIGHT NR 2666 THE CREW REPORTED A TAT 1 HEAT INOP MESSAGE ON THE EICAS WITH A FAINT ELECTRICAL BURNING ODOR THAT LASTED FOR 1 TO 2 MINUTES.MAINTENANCE INSPECTED AND REPLACED THE NR 1 TAT CURRENT SENSOR KO064. OPERATIONAL CHECKS OF THE SYSTEM WERE GOOD.Jul 31, 2007 · N15973 · Emb EMB145LR · Ice/Rain Protection System WiringSDR C2XA07RI018Smoke Detector · inoperativeFLIGHT 2882 - EWR - CREW REPORTED NR 2 CARGO SMOKE DETECTOR INOP. EWR MX REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW EMB AMM 26-23-00. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Apr 19, 2007 · N15973 · Emb EMB145LR · Smoke DetectionSDR C2XA07IA079Unknown · odorIAH - FLIGHT 2151, DURING PREFLIGHT INSPECTION THE CREW REPORTED A HOT ELECTRICAL ODOR IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, AND COULD NOT DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 4, 2007 · N15973 · Emb EMB145LR · Air Distribution SystemSDR C2XA07CL030Carbon Seal · leakingEWR FLIGHT 3068 THE CREW REPORTED A LAV SMOKE INDICATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES. THE NR 1 ENGINE WAS FOUND TO BE THE CAUSE OF THE LAV INDICATION AND SMOKEY Mar 12, 2007 · N15973 · Emb EMB145LR · Turbine Engine Oil SystemSDR C2XA07BT020Unknown · smokeEWR LOG SQUAWK FLT NR 2292 ON CLIMB AT 8000 FT. WE GOT LAV SMOKE WARNING. THE FA CONFIRMED SMOKE IN THE CABIN. INSPECTED ALL OVERHEAD LIGHTS IN CABIN AND LAV. NO DEFECTS NOTED. PERFORMED RR FIM TASK 72-00-00-810-814. RAN BOTH ENGINES INDIVIDUALLY WITH BLFeb 23, 2007 · N15973 · Emb EMB145LR · Air Distribution SystemSDR C2XA06TY017Frame · crackedPAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER OUTBOARD HOLE HAS A CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310- 01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOODMar 28, 2006 · N15973 · Emb EMB145LR · Fuselage Main, FrameSDR C2XA06TY015Frame · crackedPAX DOOR FRAME CUTOUT AFT LOWER STOP STRUCTURE LOWER INBOARD HOLE HAS CRACK. REAMED HOLE AND INSTALLED BUSHING AND BRACKET. ALL WORK PERFORMED IAW EC 5310-01377, EA 5310-01054 AND SRM 57-21-03. AC PRESSURE CHECKED GOOD.Mar 17, 2006 · N15973 · Emb EMB145LR · Fuselage Main, FrameSDR C2XA06TY016Bracket · crackedPAX DOOR FRAME CUT-OUT, FWD LOWER STOP STRUCTURE, LOWER INBOARD HOLE HAS TWO CRACKS, ONE ON THE FRAME AND ONE IN THE BACK CASTING. REMOVED CRACKED BRACKET, DRILLED CRACKED HOLE ON SKIN SIDE TO 10MM. DRILLED NEW BRACKET AND INSTALLED. REAMED AND COLD WORKED Mar 17, 2006 · N15973 · Emb EMB145LR · Fuselage Main, StructureSDR C2XA05BT077Power Supply · faultyBNA - CREW REPORTED, ON HEAD START, EXIT ROW OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY POWER SUPPLY IAW EMB145 AMM NR 33-50-04, OPS CHECK GOOD.Oct 30, 2005 · N15973 · Emb EMB145LR · Emergency LightingSDR C2XA05IA106Inverter · inoperativeSTL - DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LOCATOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO Sep 13, 2005 · N15973 · Emb EMB145 · Emergency LightingSDR C2XA04CL120Motor · failedCREW REPORTED FLAP FAILED IN FLIGHT. REPLACED THE NR 1 FLAP DRIVE MOTOR. AIRCRAFT RETURNED TO SERVICE.Nov 28, 2004 · N15973 · Emb EMB145 · Trailing Edge Flap ActuatorSDR C2XA04SH309Cowling · chafedDURING C-CHECK THE NR 1 ENGINE LOWER COWLING WAS FOUND TO BE CHAFED ON THE INNER SKIN. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 22, 2004 · N15973 · Emb EMB145 · Engine Cowling SystemSDR C2XA04SH296Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2004 · N15973 · Emb EMB145 · Fuselage Main, StructureSDR C2XA04SH295Stiffener · chafedSHV - DURING C-CHECK THE NUMBER 2 ENGINE LOWER COWLING AFT EDGEMEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGEMEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2004 · N15973 · Emb EMB145 · Nacelle/Pylon, Frame/Spar/RibSDR C2XA04SH294Skin · dentedDURING C CHECK THE NR 2 ENGINE INTAKE PERFORATED SKIN WAS FOUND TO BE DENTED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 54-20-01, SECTION 7, (FIGURE 207). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2004 · N15973 · Emb EMB145 · Engine Air Intake System
Back to N15973, cancelled Jan 5, 2017