N279SK, cancelled Oct 10, 2019
Service difficulty reports · 53
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 = 'N279SK' AND deregistration_id = 'N279SK-2019-10-10' 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 = 'N279SK' AND deregistration_id = 'N279SK-2019-10-10' 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 CHQA20140323090Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20140201036Tire · separatedCREW REPORTED THAT NY CENTER INFORMED THEM OF A POSSIBLE TIRE SEPARATION ON TAKEOFF. THE CREW DIVERTED TO KCMH & DID A FLY-BY ON THE CONTROL TOWER. THE TOWER COULD NOT CONFIRM ANY DEFECTS. THE ACFT LANDED WITHOUT INCIDENT. THE MLG LT INBD TIRE SEPARATION WSDR CHQA20140117017Sign · inoperativeDURING INSPECTION, THE FWD CABIN EMERGENCY LIGHTED SIGN WAS FOUND TO BE INOPERATIVE. REPLACED THE SIGN, OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20131127441Fitting · corrodedCRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 66 AT STRINGER 6L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130709265Wire · brokenDURING INSPECTION, EMERGENCY LIGHT AT ROW 7 FOUND TO HAVE A BROKEN WIRE. WIRE REPAIRED. OPS CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130613203Light · inoperativeDURING INSPECTION, CREW REPORTED THAT THE SECOND EMERGENCY LIGHTING FLOOR STRIP WAS FOUND INOPERATIVE. EMERGENCY LIGHT REPLACED. OPS CHECKED GOOD.SDR CHQA20130501142Battery · dischargedDURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20121203468Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 20L AND 21L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121130462Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 53 THROUGH FRAME 58. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129467Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 59. THE LEFT OMEGA BEAM GUSSET AT FRAME 59 WAS REPLACED IN ACCORDANCE WITH 51-40-02.SDR CHQA20121129466Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 30 THROUGH FRAME 36. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129465Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACORDANCE WITH AMM 53-01-06.SDR CHQA20121129464Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK AT FRAME 36 THROUGH FRAME 45. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129463Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SEAT TRACK AT FRAME 42. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129461Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 23 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121129460Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SEAT TRACK AT FRAME 47 THROUGH FRAME 52. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH AMM 53-01-06.SDR CHQA20121030396Thermostat · faultyCREW REPORTED THAT UPON TAKEOFF, RECEIVED A BLEED 1 OVERHEAT MESSAGE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR CONTROL THERMOSTAT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120628201O-Ring · leakingCREW REPORTED A BLEED 1 LEAK MESSAGE IN FLIGHT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O-RING AT JOINT 11. OPS AND LEAK CHECKED GOOD, WITH NO FURTHER DEFECTS NOTED.SDR CHQA20120609186Control Valve · malfunctionedCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUSDR CHQA20120609185Sleeve · failedCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUSDR CHQA20120609184Flapper Valve · brokenCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED ONE LEAK MESSAGE. APPROXIMATELY ONE MINUTE LATER THE CABIN PRESSURIZATION WOULD NOT KEEP UP WITH THE CABIN ALTITUDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE Y-DUSDR CHQA20120322088Control Unit · faultyCREW REPORTED THAT AFTER LANDING, THE CAPTAIN'S LEFT BRAKE FAILED AT APPROXIMATELY 80 KNOTS. THE BRAKES BEGAN WORKING AGAIN WHEN THE AIRCRAFT SLOWED TO 20 KNOTS. MAINTENANCE REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECSDR CHQA201100494Transducer · faultyCREW REPORTED THAT DURING LANDING ROLLOUT, THE BRAKES FAILED AT 80 KNOTS. THE CREW SLOWED THE AIRCRAFT USING THE EMERGENCY BRAKE. THE BRAKE SYSTEM BEGAN WORKING AS NORMAL WITHIN 10 KNOTS. THEY ALSO RECEIVED A RUDDER 1/2 INOP MSG ON THE EICAS. MAINTENANCE RSDR CHQA201100370Unknown · malfunctionedCREW REPORTED THAT DURING DESCENT, FUEL TANK TWO'S QUANTITY INDICATIONS WERE DECREASING FUEL QUANTITY INDICATIONS WENT FROM NORMAL TO AMBER, THEN RED, THEN DASHED. THE CREW DECLARED AN EMERGENCY. FUEL TANK 2 QUANTITY INDICATED NORMAL 100 FEET ABOVE LANDING. SDR CHQA201100156Controller · inoperativeCREW REPORTED THAT ON CLIMBOUT AUTO PRESSURIZATION FAILED AND ALL INDICATIONS BLANKED OUT. THEY SWITCHED TO MANUAL MODE BUT STILL WOULD NOT PRESSURIZE. THE AIRCRAFT THEN RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE AUTO PRESSURIZATION SYSTEM WAS PLACESDR CHQA201100108Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE OMEGA BEAM BETWEEN FRAME 19 AND 25. MAINTENANCE REPLACED THE FLOOR STRUCTURE CENTER FUSELAGE I MIDDLE OMEGA BEAM BETWEEN FRAME 19 AND 25 AND INSTALLED WITH A SOLID RIVET IAWSDR CHQA201100107Angle · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD SIDE ANGLE. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE FORWARD SIDE ANGLE AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100118Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE LEFT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100117Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100116Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100115Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE RIGHT OMEGA BEAM ANGLE AT FRAME 47. MAINTENANCE REPAIRED THE RIGHT OMEGA BEAM ANGLE AT FRAME 47 IAW SRM 53-23-02.SDR CHQA201100106Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I ANGLE MIDDLE SUPPORT. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I ANGLE MIDDLE SUPPORT AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100105Rib · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I AFT GALLEY RIB. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I AFT GALLEY RIB AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100104Structure · corrodedDURING INSPECTION THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I PASSENGER DOOR U SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE CENTER FUSELAGE I PASSENGER DOOR U SHAPE AND INSTALLED WITH A SOLID RIVET IAW SRM 51-40-02.SDR CHQA201100103Floor Support · corrodedDURING INSPECTION THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM AFT ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM AT FRAME 20 IAW SRM 51-40-02.SDR CHQA201100102Beam · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM IAW SRM 51-40-02.SDR CHQA201100101Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR ON THE LEFT OMEGA BEAM FLANGE AT FRAME 20. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM FLANGE AT FRAME 20 AND RE-INSTALLED IAW SRM 53-00-10.SDR CHQA201100017Receptacle · inoperativeDURING INSPECTION, THE RIGHT LOWER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT LOWER EMERGENCY LIGHT RECEPTACLE WITH NO FURTHER DEFECT NOTED.SDR CHQA201000073Inverter · defectiveDURING INSPECTION THE LAST TWO ROWS OF EMERGENCY FLOOR LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE FOUND MULTIPLE FUSES IN BATTERY NR 4 BLOWN AND INVERTER NR 6 PRODUCING A HIGH PITCHED WHINE. THE NR 4 BATTERY PACK AND NR 6 INVERTER WERE REPLACED WITH NO FURTHSDR CHQA201000049Trunnion · crackedDURING THE INSPECTION OF THE AFT UPPER TRUNNION ON THE RIGHT MAIN LANDING GEAR, A 20MM CRACK WAS FOUND ON THE TRUNNION FITTING ON THE FORWARD OUTBOARD FACE AND AN 8MM CRACK WAS FOUND ON THE WRAPPING AROUND SIDE. MAINTENANCE REMOVED AND REPLACED THE AFT UPPER SDR CHQA201000005Unknown · malfunctionedDURING CLIMBOUT OF KCLE THE CREW NOTICED THE CABIN ALTITUDE INDICATOR WAS DISPLAYING AMBER DASHES. THE AUTO PRESSURIZATION SYSTEM WAS ALREADY DEFERRED AND THE PROCEDURES WERE REVIEWED. THE MEL ALLOWED CONTINUED FLIGHT IF THE MANUAL SYSTEM WAS OPERATING NORMASDR CHQA200900191Light · out of positionDURING THE WALK AROUND INSPECTION THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND TO BE UPSIDE DOWN. MAINTENANCE REPOSITIONED THE LIGHT TO THE CORRECT ORIENTATION AND CHECKS WERE SATISFACTORY. NO OTHER ACTIONS WERE REQUIRED.SDR CHQA200900151Pressure Switch · faultyDURING CLIMB OUT, AT APPROX 8,000FT, THE CREW RECEIVED AN OXY LO PRESS EICAS MESSAGE. THE CREW O2 INDICATED ZERO PSI ON THE MFD. THE ACFT LEVELED AT 10,000 FT AND IT WAS DECIDED TO RETURN TO DEPARTURE. THE CREW OXYGEN SYS WAS PLACED ON MEL AND THE ACFT DEPASDR CHQA200800176Light · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. THE BULB FOR THE RT OVER WING EMERGENCY LIGHT WAS REPLACED IAW EMB 145 AMM 33-50-07-4. THE EMERGENCY LIGHTING SYSTEM OPERATED NORMALLY.SDR CHQA200800172Strut · underservicedFLIGHT 3080, SDF TO LGA. WHEN THE CREW SELECTED THE LANDING GEAR DOWN THEY HEARD A THUD FROM THE NOSE AREA AND RECEIVED LG AIR/GND FAIL AND T/R DISAGREE MESSAGES ON EICAS. UPON LANDING THEY RECEIVED A STEERING INOP MESSAGE ON EICAS. AFTER STOPPING THE ACFTSDR CHQA200700079Control Panel · faultyGSP TO LGA - UPON REACHING 10,000 FT DURING DESCENT, THE APU WAS STARTED DUE TO AN MEL'D NR 3 GENERATOR. SHORTLY AFTER STARTING APU, CREW RECEIVED A FIRE WARNING EICAS MESSAGE. AFTER TAKING THE APPROPRIATE ACTION THE APU FIRE INDICATION WENT AWAY. THE AIRCRSDR CHQA200600107Trim System · malfunctionedWHILE CLIMBING THROUGH 14000 FEET UP TO 17000 FEET, HAD RUDDER TRIM RUN AWAY TO THE LT. APPLIED THE APPROPRIATE MEMORY ITEMS AND CHECK LIST, DECLARED AN EMERGENCY AND RETURNED BACK. MAINTENANCE PERFORMED RUDDER TRIM AND AUTOPILOT ENGAGEMENT TEST, PERFORMED SDR CHQA200500129Bulb · burned outREAR CEILING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED THE AFT CEILING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-08. OPS CHECK GOOD IAW EMB 145 J/C E33-50-00-710-001.SDR CHQA200500054Smoke · detectedFLIGHT 3039 BOS-MYR - DURING INTIAL CLIMB A LAV SMOKE INDICATION APPEARED ON EICAS. THE FLIGHT ATTENDANT REPORTED THERE WAS NO EVIDENCE OF ODOR, SMOKE, OR FIRE IN THE CABIN. ALL OTHER INDICATIONS IN THE COCKPIT WERE NORMAL. THE AIRCRAFT WAS HEAVILY DE-ICED SDR AE0R200400002Turbine Blades · fracturedENGINE S/N CAE311220 WAS DELIVERED TO SHOP FOR REPAIR 11/03/04 DUE TO IN-FLIGHT SHUTDOWN. DURING DISASSEMBLY, DAMAGE WAS NOTED TO THE TURBINE. ONE 1ST STAGE TURBINE BLADE WAS FRACTURED BELOW THE PLATFORM.
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