N16981

Service difficulty reports · 113

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 = 'N16981' 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.

SDR ASOA2019042635062Inverter · inoperativeDURING MX INSPECTION THE EMERGENCY SIGN IN FRONT OF 3C WAS INOP.MX REMOVED BAD #3 INVERTER AND INSTALLED NEW INVERTER IAW EMB145 AMMII 33-50-11, OPS CHECK GOOD A/C WAS APPROVED FOR RETURN TO SERVICEApr 23, 2019 · N16981 · Emb EMB145LR · Emergency LightingSDR ASOA201902274010Coffeemaker · odorPVD - FLIGHT 4870 THE CREW REPORTED A BURNED WIRE INSULATION SMELL COMING FROM COFFEE MAKER AREA, AND THAT THE SMELL WENT AWAY AFTER BOTH COFFEE MAKERS WERE TURNED OFF. THE AIRCRAFT LANDED IN PVD WITHOUT INCIDENT WHEFRE CONTRACT MAINTENANCE PERFORMED AN ABMNORFeb 27, 2019 · N16981 · Emb EMB145LR · Buffet/GalleysSDR ASOA201901157009Rib · crackedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT MLG RIB NR 5 CRACKED. MAINTENANCE R/R THE NR 5 RIB IAW ECTC ETD 2018-145-13565,REEF. TASKCARD-145-306 RH REV. D. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 15, 2019 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201901157008Bushing · wornTYS A/CIS IN C-CHECK WHEN THE INSPECTORS FOUND THE RT AND LT VERTICAL STAB BUSHINGS WORN. MAINTENANCE REAMED BOTH BUSHINGS AND INSTALLED THE OVERSIZED BUSHING AND COMPLIED WITH THE DIHEDRAL CHECKS IAW SRM 55-30-02 AND TASK 51--50-01-820-801-A. ALL WORK ACCOMPLJan 15, 2019 · N16981 · Emb EMB145LR · Vertical Stabilizer Miscellaneous StructureSDR ASOA201901097006Bushing · damagedRUDDER 1 2ND FROM BOTTOM ATTACH BRACKET UPPER HAT BUSHING DAMAGED. REMOVED BUSHINGS, REAMED HOLE, INSTALLED NEW OVERSIZE BUSHINGS. AIRCRAFT IN C CHECK.Jan 9, 2019 · N16981 · Emb EMB145LR · Rudder Miscellaneous StructureSDR ASOA201901037002Frame · crackedA/C IS IN FOR A C-CHECK INSPECTION THE INSPECTORS FOUND A CRACKED FRAME ON THE LT SIDE OF THE DV WINDOW CUTOUT AT FR 12A-13. MAINTENANCE HAD TO REMOVE THE PAX DOOR SHOCK ABSORBER ASSEMBLY BRACKET TO GET TO REPAIR THE CRACKED FRAME AND REINSTALLED THE SHOCK ABSJan 3, 2019 · N16981 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA201901027001Frame · corrodedTYS A/C IS IN FOR A C-CHECK INSPECTION WHEN INSPECTION FOUND CORROSION AT STRINGER 21R BETWEEN FRAMES 17 THRU 19. MAINTENANCE REPAIRED THE SECTION BETWEEN FRAME 17 AND 19 IAW SRM 52-00-03. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 2, 2019 · N16981 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA201802284014Stop · brokenDURING A MAINTENANCE INSPECTION, THE PAX DOOR FWD LOWER DOOR STOP SEAT WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE STOP SEAT, RIGGED THE PAX DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 28, 2018 · N16981 · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA201712224068Charger · inoperativeDURING CREW INSPECTION, THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Dec 22, 2017 · N16981 · Emb EMB145LR · Emergency LightingSDR ASOA20170718008VBattery · inoperativeDURING A ROUTINE CHECK, FOUND THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES NUMBER 3 AND 4 IAW AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 20, 2017 · N16981 · Emb EMB145LR · Emergency LightingSDR ASOA201707135094Battery Pack · inoperativeDURING INSPECTION, THE EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE NR 3 AND 4 EMERGENCY LIGHT BATTERY PACKS. OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 13, 2017 · N16981 · Emb EMB145LR · Emergency LightingSDR ASOA201704043066Skin · crackedRIGHT REAR FUSELAGE SKIN CRACKED AROUND RIVETS AT FRAME 75, STRINGER 2R. DAMAGED AREA REPAIRED WITH DOUBLER IAW SRM 53-31-00.Apr 4, 2017 · N16981 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASOA201703303064Channel · corrodedSERVICE DOOR LOWER CHANNEL CORRODED. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.Mar 30, 2017 · N16981 · Emb EMB145LR · Service DoorsSDR ASOA201703293063Floor Support · corrodedREAR FUSELAGE FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.Mar 29, 2017 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201703293062Floor Support · corrodedCABIN NR 1 FLOOR SUPPORT CORRODED. REPLACED IAW SRM 51-40-02.Mar 29, 2017 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201703293061Gusset · corrodedLEFT GUSSET CORRODED AROUND ANCHOR NUT BETWEEN FRAMES 16 AND 17. THE GUSSET WAS REPAIRED IAW SRM 53-21-10, ITEM 2, FIG 201.Mar 29, 2017 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA201703293060Seat Track · corrodedCABIN LT INBOARD SEAT TRACK NR 1 CORRODED. LT INBOARD SEAT TRACK NR 1 REPLACED AS PER 53-01-06.Mar 29, 2017 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20160718036Warning Message · false activationPILOT REPORTED EICAS MESSAGE FOR CARGO BAY SMOKE FOR 5 SECONDS, CLIMBING THROUGH 14000 FEET. MX PERFORMED OPS CHECK OF CARGO SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jul 18, 2016 · N16981 · Emb EMB145LR · Smoke DetectionSDR ASOA20141208097Fire Detector · failedTHE CREW REPORTED A NR 2 ENGINE FIRE DETECT FAIL MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE DETECTOR. OPS CHECKED GOOD.Dec 8, 2014 · N16981 · Emb EMB145LR · Fire DetectionSDR ASOA20140601060Inverter · inoperativeDURING MX INSPECTION THE AFT GALLEY EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R THE EMERGENCY LIGHT SYS INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 1, 2014 · N16981 · Emb EMB145LR · Emergency LightingSDR ASOA20130528053Control Valve · inoperativeCREW REPORTED ZERO BRAKE EFFECTIVENESS IN LT BRAKE DURING TAXI. MX R & R THE OTBD BRAKE CONTROL VALVE WITH OPS AND TAXI CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.May 28, 2013 · N16981 · Emb EMB145LR · Landing Gear Brake SystemSDR ASOA20130113225Seat Track · corrodedNR 2 RT WALL SEAT TRACK SUPPORT IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. CUT-OUT CORRODED SECTION, FABRICATED AND INSTALLED NEW SEAT TRACK SUPPORT.Jan 13, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130110223Frame · corrodedACFT IS IN FOR A C-CHECK INSPECTION, WHEN A LT SPLICE AT FRAME LBL 15 WAS FOUND CORRODED. MX R & R THE REINFORCEMENT SPLICE AT FRAME IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 10, 2013 · N16981 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20130110222Brace · corrodedACFT IS IN FOR A C-CHECK INSPECTION, WHEN THE RT CROSSBRACE WAS FOUND BENT AND CORRODED AT FRAME 17. MX R & R THE CROSSBRACE IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 10, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130110221Seat Track · corrodedACFT IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE RT LONGITUDAL SEAT TRACK FROM FRAME 48 THRU 52. MX R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 10, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130109218Angle · corrodedDURING A C-CHECK, CORROSION FOUND AROUND NUTPLATED AT THE BAGGAGE DOOR. MX R & R THE BAGGAGE DOOR INBD ANGLE IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Cargo/Baggage DoorsSDR ASOA20130109217Seat Track · corrodedDURING C-CHECK INSPECTION, RT OTBD SEAT TRACK SUPPORT FOUND CORRODED AT FR 55. MX REMOVED THE RIVETS AND FABRICATED A NEW SUPPORT AND INSTALL IAW SRM 51-40-02 AND SRM 53-00-11. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130109216Channel · corrodedDURING C-CHECK, LEFT CHANNEL CROSSBEAM AT FRAME 18 WAS FOUND CORRODED. MX BLENDED CORROSION IAW SRM 51-10-03, PERFORMED HFEC, NO CRACKS FOUND AND WAS WITHIN LIMITS IAW SRM 53-21-10. ALL WORK ACCOMPLISHED AND WILL BE RELEASED A THE END OF THE CHECK.Jan 9, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130109213Gusset · corrodedC-CHECK, GUSSET AT FR 17 WAS FOUND WITH MINOR CORROSION AROUND NUTPLATE. MX BLENDED CORROSION LEAVING REMAINING MATERIAL TO BE WITHIN LIMITS IAW SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130109212TFrame · corrodedC-CHECK, CORROSION FOUND AT FRAME 65 AT THE THRESHOLD. MX R & R THE LOWER SECTION OF FRAME 65IAW ETD 2012-145-018140. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Main, FrameSDR ASOA20130108211Support · corrodedACFT IN FOR A C-CHECK, CHECK WHEN THE LT WALL SUPPORT HAD CORROSION ON THE LOWER SIDE OF SUPPORT AT FRAME 60. MX R & R THE LT WALL SUPPORT IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130108210Beam · corrodedACFT IN FOR A C-CHECK, CHECK WHEN THE CARGO DOOR CUTOUT WAS FOUND. CORRODED ON THE THRESHOLD BETWEEN FRAMES 65 AND 68. MX BLENDED THE CORROSION IAW SRM 51-10-03. R & R THE AREAS OUT OF LIMITS WITH FABRICATED PARTS IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AJan 8, 2013 · N16981 · Emb EMB145LR · Fuselage Main, StructureSDR ASOA20130108209Seat Track · corrodedACFT IN FOR A C-CHECK, WHEN THE NR 4 LT SEAT TRACK WAS FOUND CORRODED IN SEVERAL PLACES. BLENDED AREAS IAW SRM 51-10-03, THE OUT OF LIMIT AREAS IAW SRM 53-00-11 WERE CUT OUT AND FABBED PARTS WERE INSTALL IN THE SEAT TRACK SECTION IAW SRM 53-00-11. ALL WORK WJan 8, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130105207Support · corrodedRT OTBD SEAT TRACK SUPPORT CORRODED ON LOWER FOOT. CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105206Support · corrodedNR 1 LEFT WALL SEAT TRACK SUPPORT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SUPPORT.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105205Gusset · corrodedGUSSET AT FRAME 65 TO 68 AT Y=-479 IS CORRODED BEYOND LIMITS. R & R GUSSET.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105204Structure · corrodedFRAME 15 DIGITAL IS CORRODED BEYOND LIMITS. R & R DIGITAL.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130105203Channel · corrodedPAX DOOR U CHANNEL CORRODED BEYOND LIMITS AFTER BLENDING. R & R U CHANNEL.Jan 4, 2013 · N16981 · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA20130105202Seat Track · corrodedNR 3 LEFT ISLE SEAT TRACK GUSSET IS CORRODED OUT OF LIMITS AFTER BLENDING. R & R GUSSET.Jan 4, 2013 · N16981 · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20130103201Sill · corrodedRIGHT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103200Angle · corrodedLEFT ANGLE HAS CORROSION THAT IS OUT OF LIMITS AFTER BLEND OUT. R & R LEFT ANGLE.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103199Gusset · corrodedCORROSION AFT LAVATORY LT FLOOR GUSSET CORRODED OUT OF LIMITS AFTER BLENDING. R & R FLOOR GUSSET.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103198Support · corrodedSUPPORT IN THE LAVATORY AREA HAS CORROSION OUT OF LIMITS AFTER BLENDING. REMOVED AND REPLACED DOUBLER.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103197Brace · corrodedRT CROSS BRACE IS CORRODED BEYOND LIMITS AFTER BLEND OUT. R & R BRACE.Jan 3, 2013 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20130103196Channel · corrodedPAX DOOR U-CHANNELS ARE CORRODED BEYOND LIMITS AFTER BLENDING. R & R CHANNELS.Jan 3, 2013 · N16981 · Emb EMB145LR · Passenger/Crew DoorsSDR ASOA20121224194Floor Support · corrodedLT FLOOR SUPPORET CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.Dec 21, 2012 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121224193Sill · corrodedLAVATORY RT SILL IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.Dec 21, 2012 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121224192Floor Support · corrodedAFT LAV LT OMEGA BEAM IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. REMOVED DAMAGED SECTION, FABRICATED A FILLER AND DOUBLER AND INSTALLED.Dec 21, 2012 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121224191Sill · corrodedLT SILL IS COORODED BEYOND LIMITS AFTER BLEND-OUT. R & R SILL.Dec 21, 2012 · N16981 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20121224190Angle · corrodedCORROSION OUT OF LIMITS AFTER BLEND-OUT AT FRM 68 RT SIDE AT Z=715.7. R & R TEE ANGLE.Dec 21, 2012 · N16981 · Emb EMB145LR · Fuselage Miscellaneous Structure
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