N296SK

Service difficulty reports not matched to an aircraft · 64

They name N296SK, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N296SK' AND registry_match IS NULL
  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 UHLA201602250076Hand Rail · inoperativeMAIN ENTRY DDOOR HANDRAIL DOES NOT STOW WHEN CLOSED. RETORQUED MAIN CABIN DOOR HAND RAIL IAW AMM 52-10-05. OPS CHECK GOOD.Feb 25, 2016 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR UHLA201506240545Cable · damagedTHE MAIN CABIN DOOR WAS UNABLE TO BE OPENED FROM THE INSIDE. THE DOOR WAS OPENED FROM THE OUTSIDE AND THE ACFT WAS FERRIED TO A MAINTENANCE BASE WHERE THE INTERNAL HANDLE CONNECTION CABLE WAS FOUND TO HAVE A CREASE IN THE CABLE AT THE BELL CRANK. MAINTENANCEJun 24, 2015 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20141213353Skin · crackedDURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 1R. THE SKIN WAS REPAIRED IAW ETD2014-145-105115.Dec 13, 2014 · N296SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20141212352Fitting · damagedDURING INSPECTION, THE LT AILERON ATTACH FITTING WAS FOUND TO BE DAMAGED. THE AILERON FITTING WAS REPLACED IAW SRM 51-40-02.Dec 12, 2014 · N296SK · Emb EMB145LR · AileronsSDR CHQA20141211360Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR BEAM FLOOR FLANGE AT FRAME 23. THE BEAM WAS REPAIRED IAW SRM 53-00-10.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211359Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 46 BELOW THE FLOOR SILL WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211358Angle · corrodedDURING INSPECTION, THE LT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211357Beam · corrodedDURING INSPECTION, THE LT BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE BEAM WAS REPAIRED IAW SRM 51-20-03 & SRM 51-23-04.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211356Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211355Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 26 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141211354Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Dec 11, 2014 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121214452Valve · inoperativeCREW REPORTED A BLEED ONE LEAK EICAS MESSAGE & PACK ONE VLV CLOSED MESSAGE WHILE IN FLIGHT IN ICING CONDITIONS. AFTER FOLLOWING THE QRH, THE CREW MADE A SUCCESSFUL UNSCHEDULED LANDING. MX SECURED THE BLEED ONE VLV CLAMP & THE BLEED SYS THEN PASSED OPERATIONADec 14, 2013 · N296SK · Emb EMB145LR · Cabin Cooling SystemSDR CHQA20131019376Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING LIGHT ASSEMBLY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Oct 19, 2013 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20130813309Battery · dischargedDURING INSPECTION, BOTH EMERGENCY LIGHT EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 13, 2013 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20121021395Floor Support · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE Y=0 OMEGA BEAM AT FRAME 23 LEFT FLOORBOARD FLANGE. THE CRACK WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-015124.Oct 21, 2012 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20121017394Cup · corrodedDURING INSPECTIONS, THE LAVATORY SHUT OFF VALVE SUPPORT WAS FOUND TO BE CORRODED. THE LAVATORY CUP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 53-30-02.Oct 17, 2012 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120324092Inverter · inoperativeDURING INSPECTION, THE FORWARD MAIN ENTRY DOOR EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECK WERE GOOD WITH NO FURTHER DEFECTS NOTED.Mar 24, 2012 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20120324091Battery · dischargedDURING INSPECTION, ALL FOUR EMERGENCY OVERWING LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 AND NUMBER 4 EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Mar 24, 2012 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20120324090Battery · dischargedDURING INSPECTION, ALL FOUR EMERGENCY OVERWING LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 AND NUMBER 4 EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Mar 24, 2012 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA20120312075Battery · dischargedDURING INSPECTION, THE OVERWING EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Mar 12, 2012 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA201100439Beam · corrodedDURING INSPECTION, THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CARGO DOOR CUT OUT SILL BEAM IN ACCORDANCE WITH SRM 51-20-03, 51-40-06, AND 51-40-02.Nov 11, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100438Skin · damagedCREW REPORTED THAT THE AIRCRAFT WAS DAMAGED BY THE RAMP CREW BAGGAGE BELT LOADER, BELOW THE BAGGAGE PIT DOOR NEAR FRAME 67 AND STRINGER 19L. THE AIRCRAFT WAS FERRIED TO KCMH. CMH MAINTENANCE REPLACED THE SKIN (PN:145-35010-003 AND 145-23056-007) AND RE-CONTOUNov 3, 2011 · N296SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA201100372Battery · dischargedDURING INSPECTION, THE EMERGENCY LIGHTS FROM ROW 13 TO ROW 18 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Sep 14, 2011 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA201100309Battery · inoperativeDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 6, 2011 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA201100151Chip Detector · not seatedDURING FLIGHT THE CREW REPORTED A LOW OIL QUANTITY INDICATION ON E1. THE QRH WAS FOLLOWED AND E1 WAS SHUT DOWN IN FLIGHT. THE AIRCRAFT DIVERTED TO KCRW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED E1 AND FOUND THE NON-INDICATING MAGNETIC CHIP DETApr 24, 2011 · N296SK · Emb EMB145LR · Turbine Engine Accessory DriveSDR CHQA201100055O-Ring · tornCREW REPORTED THAT DURING CRUISE REPORTED A BLEED 2 LEAK MESSAGE IN ICING CONDITIONS ACCOMPANIED BY A BURNT RUBBER ODOR. THE AIRCRAFT DIVERTED TO KBTV AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LEAK AT JOINT 19 BEHIND THE CARGO COMPARTMENT SIDE WALL. Mar 10, 2011 · N296SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA201100098Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR SURROUND LOWER PORTION AT FRAME NR 22. A THICKNESS MEASUREMENT WAS DONE BY UT IAW NDI MANUAL, INTRODUCTION P 22 (F). MINIMUM MATERIAL REMAINING IS 0.22 INCHES. A HIGH FREQUENCY EDDY CURRENT INSPECTIOMar 3, 2011 · N296SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA201100097Skin · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR SURROUND LOWER PORTION AT FRAME NR 20. A THICKNESS MEASUREMENT WAS DONE BY UT IAW NDI MANUAL, INTRODUCTION P 22 (F). MINIMUM MATERIAL REMAINING IS 0.66 INCHES. A HIGH FREQUENCY EDDY CURRENT INSPECTIOMar 3, 2011 · N296SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA201100080Casting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE OPEN HANDLE BACK CASTING. THE MAIN PASSENGER DOOR OPEN HANDLE BACK CASTING WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100079Channel · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD CHANNEL SPLICE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD CHANNEL SPLICE WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100092Reinforcement · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR AFT SURROUND STRUCTURE. THE THICKNESS MEASUREMENT DONE BY UT IAW NDI MANUAL P.22 (F) ON REWORKED AREA FOUND THE MINIMUM MATERIAL THICKNESS REMAINING AT 0.022 INCHES. HFEC DONE ON THE AREA FOUND NO CRAMar 3, 2011 · N296SK · Emb EMB145LR · Service DoorsSDR CHQA201100091Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 25. THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM LOWER FLANGE AT FRAME 25 WAS REPAIRED IAW ETD2011-145/02427.Mar 3, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100090Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON EXISTING REPAIR ON LEFT OMEGA BEAM FLANGE AT FRAME 20. THE REPAIR WAS REPLACED ON THE LEFT OMEGA BEAM FLANGE IAW SRM 53-00-10.Mar 3, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100089Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT FITTING ON BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE AFT FITTING ON BOTTOM RIB WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100088Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE ANGLE BETWEEN FRAME 2 AND BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE ANGLE BETWEEN FRAME 2 AND BOTTOM RIB WERE REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100087Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT SUPPORT ASSEMBLY ON BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE AFT SUPPORT ASSEMBLY ON BOTTOM RIB WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100086Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 2. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 2 WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100085Door Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 1. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM FRAME 1 WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100084Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB. THE MAIN PASSENGER DOOR BOTTOM RIB WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100083Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD ANGLE ON AFT SIDE OF BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE FORWARD ANGLE ON AFT SIDE OF BOTTOM RIB WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100082Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SUPPORT ASSEMBLY BOTTOM RIB. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SUPPORT ASSEMBLY BOTTOM RIB WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100081Channel · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER CHANNEL. THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER CHANNEL WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100078Profile · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD U PROFILE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE "U" PROFILE WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100077Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD STEP FITTING ASSEMBLY. THE MAIN PASSENGER DOOR STRUCTURE FORWARD STEP FITTING ASSEMBLY WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100076Fitting · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT STEP FITTING ASSEMBLY. THE MAIN PASSENGER DOOR STRUCTURE AFT STEP FITTING WAS REPLACED.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100075Doubler · crackedDURING INSPECTION A CRACK WAS FOUND ON THE INTERNAL DOUBLER ON THE AFT BOTTOM CORNER OF THE MAIN PASSENGER DOOR. THE INTERNAL DOUBLER ON THE AFT BOTTOM CORNER OF THE MAIN PASSENGER DOOR WAS REPAIRED IAW ETD 2011-145/02468.Mar 3, 2011 · N296SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100096Window Frame · damagedDURING INSPECTION THE TOP WINDSHIELD CUT OUT STRUCTURE WAS FOUND TO BE DAMAGED AT THE RIGHT FAIRING ATTACHMENT BRACKET. EDDY CURRENT INSPECTION CARRIED OUT ON LEFT BLEND IAW NDI MANUAL, INTRODUCTION P 17, NO CRACK FOUND. THE TOP WINDSHIELD CUTOUT STRUCTURE AMar 1, 2011 · N296SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA201100095Window Frame · damagedDURING INSPECTION THE TOP WINDSHIELD CUTOUT STRUCTURE WAS FOUND TO BE DAMAGED AT THE LEFT FAIRING ATTACHMENT BRACKET. EDDY CURRENT INSPECTION CARRIED OUT ON LEFT BLEND IAW NDI MANUAL, INTRODUCTION P 17, NO CRACK FOUND. THE TOP WINDSHIELD CUT OUT STRUCTURE AT Mar 1, 2011 · N296SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA201100094Angle · crackedDURING INSPECTION THE RIGHT INBOARD ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB UPPER SKIN WAS FOUND TO BE CRACKED. THE RIGHT INBOARD ANGLE WAS REPAIRED IAW SRM 53-23-02.Feb 28, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100093Angle · crackedDURING INSPECTION THE RIGHT OUTBOARD ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB UPPER SKIN WAS FOUND TO BE CRACKED. THE RIGHT OUTBOARD ANGLE WAS REPAIRED IAW SRM 53-23-02.Feb 28, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous Structure
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