N276SK, cancelled Feb 22, 2023
Service difficulty reports · 43
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 = 'N276SK' AND deregistration_id = 'N276SK-2023-02-22' 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 = 'N276SK' AND deregistration_id = 'N276SK-2023-02-22' 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 4VAA20211216003Inverter · failedDURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS THREE AND FOUR. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS FAILED. MAINTENANCE THEN REPLACED THE NUMBER 3 INVERTER. OPERATIONAL CHECKS WERE GOOD WITSDR 4VAA202111190002None · noneDURING INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INTERMITTENTLY INOPERATIVE IN THE FRONT SECTION OF THE AIRCRAFT. A LOOSE CONNECTOR WAS RESECURED AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
*NOTE* THE FINAL CORRECTIVE ACTION ISDR UHLA201607140363Stop · inoperativeMAIN ENTRY DOOR STEPS WILL NOT DEPLOY. R & R MAIN DOOR FOLD OUT BACK STOP IAW AMM 52-13-02. OPS TEST GOOD.SDR UHLA201605140239Control Panel · malfunctionedSIDE WALL LIGHT BUTTON TURNS ON EMERGENCY LIGHTS. R & R ATTENDANT CONTROL PANEL IAW AMM 25-27-09. OPS CHECK GOOD.SDR UHLA2015020100068Seat Track · corrodedDURING INSPECTION, THE INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE CAPTAINS SEAT TRACK LOCATIONS. THE FLANGES WERE REPAIRED IAW ETD 2015-145-010166.SDR UHLA2015020100067Floor Support · corrodedDURING INSPECTION, THE COCKPIT INBD AND OTBD FLOOR FLANGES WERE FOUND TO BE CORRODED ON THE F/O SEAT TRACKS. THE INBD AND OTBD FLOOR FLANGES WERE REPAIRED IAW ETD 2015-145-010166.SDR UHLA2015012300070Attach Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD PASSENGER DOOR ATTACH FITTING BELOW THE HINGE ARM. THE ATTACH FITTING WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-008649.SDR UHLA2015012200069Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR BOTTOM SIDE STRUCTURE, THE STRUCTURE WAS REPLACED IAW SRM 51-40-02.SDR UHLA2015012200066Attach Angle · crackedDURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5R-7R. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-40-02.SDR UHLA2015012200065Attach Angle · crackedDURING INSPECTION, THE ATTACH ANGLE ON THE FORWARD SIDE OF THE APU FIREWALL WAS FOUND TO BE CRACKED AT FRAME 80 AND STRINGERS 5L-7L. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-40-02.SDR CHQA20140705207Pump · leakingCREW REPORTED THAT THEY RECEIVED A HYD 1 LOW QTY MSG FOLLOWED BY A HYD SYS 1 FAIL MSG. THE CREW PERFORMED A MANUAL EXTENSION ON THE LG. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE HYD SYS 1 ENG DRIVEN PUMP & PERFORMED THE LG FREE FALL CHECK. SDR CHQA20140306082Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPAIRED IAW SRM 53-0010 & SRM 51-40-02.SDR CHQA20140306081Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 23. THE LT OMEGA BEAM WAS REPAIRED IAW ETD 2014-145-014567.SDR CHQA20140306080Service Door · corrodedDURING INSPECTION THE SERVICE DOOR BOTTOM STRUCTURE ATTACHMENT FOR THE LINER NUT PLATE AREAS WAS FOUND TO BE CORRODED. THE SERVICE DOOR WAS REPAIRED IAW ETD 2014-145-019393-A.SDR CHQA20131016371Switch · faultyCREW REPORTED THAT THEY RECEIVED A "BLEED 2 VALVE CLOSED" MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 2 PUSH BUTTON. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130706260Wire Harness · inoperativeDURING INSPECTION, EMERGENCY LIGHT ON MAIN ENTRY DOOR HANDRAIL WAS FOUND TO BE INOPERATIVE. MX REPLACED THE CAUTION INDICATION HARNESS OPS CHECKED GOOD.SDR CHQA20130208046Display · inoperativeCREW REPORTED THE PRIMARY FLIGHT DISPLAY NUMBER 1 FAILED IN FLIGHT WITH AN ELECTRICAL ODOR PRESENT IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED THE NUMBER 1 PRIMARY FLIGHT DISPLAY WITH NUMBER 2 MULTI-FUNCTION DISPLAY AND SDR CHQA20121207475Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD BEAM. THE THRESHOLD BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121207474Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR THRESHOLD BEAM AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPLACED IN ACCORDANCE WITH SRM 53-21-02.SDR CHQA20121207473Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT RIGHT OMEGA FRAME 61. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND SRM 51-20-03.SDR CHQA20121207472Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE GUSSET AT LEFT OMEGA FRAME 59. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20121207471Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT SILL AT FRAME 20 TO FRAME 21. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-00.SDR CHQA20121207470Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RAMP ANGLE FRAME 20 AT THE CENTER OMEGA BEAM. THE ANGLE AT FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-03.SDR CHQA20120801229Pressure Switch · faultyCREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, THEY RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYS 1/SDR CHQA20120801228Pressure Switch · faultyCREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYSTEM 1/2 SDR CHQA201100286Carbon Seal · leakingCREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKE-OFF AND REPORTED THAT THEY RECEIVED NO FIRE INDICATIONS AND ALL ENGINE INDICATIONS WERE GOOD. AS SOON AS THE TAKEOFF WAS ABORTED THE SMOKE BEGAN TO CLEAR. MAINSDR CHQA201100046Light · inoperativeDURING INSPECTION THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA201000113Unknown · malfunctionedAFTER TAKEOFF, CREW ATTEMPTED TO RETRACT LANDING GEAR, RECEIVED A LDG AIR/GND FAIL MESSAGE ON EICAS AND THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE AIRCRAFT ON JACKS AND CYCLED THE LANDING GESDR CHQA201000081Solenoid Valve · faultyCREW REPORTED THAT DURING CLIMBOUT A VIBRATION AND LOW RUMBLE COULD BE HEARD AND FELT. AFTER LEVELING OFF, THE AIRCRAFT WOULD NOT ACCELERATE PAST 0.70 MACH IN CLIMB MODE. THE AIRCRAFT DIVERTED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSSDR CHQA200900261Battery Pack · dischargedDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT AND THE NR 4 BATTERY PACK WITH NO FURTHER DEFECTS NOTED.SDR CHQA200900148Battery Pack · dischargedDURING INSP, THE LT AND RT OVER-WING EMERGENCY EXTERIOR LIGHTS WERE FOUND TO BE INOP. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE EXTERIOR LIGHTS OPERATED NORMALLY.SDR CHQA200900114Wire · brokenFLIGHT 7822, IAD TO IND - SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FT THE CREW RECEIVED A SERVICE DOOR OPEN EICAS MESSAGE. THE QRH CHECKLIST WAS COMPLETED AND IT WAS DECIDED TO RETURN TO IAD WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. THE SERVICE DOOR INDSDR CHQA200900017Battery Pack · inoperativeDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE INOP ON THE LEFT AND RIGHT SIDES. THE NR 3 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY.SDR CHQA200700029Flap System · malfunctionedFLIGHT 3438 - ATL-CLE - ON DESCENT WHEN FLAPS SELECTED TO 9, EICAS MESSAGES SPS ADV AND FLAP FAIL APPEARED. PERFORMED THE QRH AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE RESET FLAPS AND CYCLED THROUGH, OPS CHECK GOOD.SDR CHQA200600119Inverter · inoperativeFLOOR PROXIMITY LIGHT NR 2 AND NR 2 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW MM 33-50-00. OPS CHECK GOOD.SDR CHQA200600114Bulb · burned outNR 1 EMERGENCY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT IAW MM 33-26-06.SDR CHQA200600112Battery · inoperativeEMERGENCY LIGHTING PROXIMITY STRIPS 2 AND 3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB 145 MM 33-50-06. OPS CHECK GOOD.SDR CHQA200600091Windshield · malfunctionedDURING DESCENT THROUGH FL200, THERE WAS A THIN CLOUD LAYER WITH ICING CONDITIONS. HEARD WHAT SOUNDED LIKE WATER DROPLETS SIZZLING. THEN SMELLED ELECTRICAL SMOKE AND AFTER A FEW SECONDS, SAW SMOKE COMING FROM THE FRONT OF THE GLARESHIELD WHERE THE HEATING ELEMSDR CHQA200500215Hub Cap · missingFLIGHT 900 - LAN-OKC - DURING INITIAL CLIMBOUT, RETRACTED GEAR DURING NORMAL SCHEDULE. RIGHT MAIN SHOWED IN TRANSITION (AMBER BOX) FOR APPROXIMATELY 10 SECONDS, THEN WENT TO RED. RAN QRH, RECYCLED GEAR PER QRH. WHILE PUTTING GEAR IN THE UP POSITION AGAIN, SSDR CHQA200500171Odor · detectedFLIGHT 6320 - FLL-MCO - ON FINAL APPROACH, NOTICED SMOKE AND AN ODOR OF SMOKE. THE ELECTRIC PAGE INDICATED GEN 3 AMP 105. PERFORMED GENERAL VISUAL INSPECTION OF COMPONENTS IN THE FORWARD AVIONICS BAY. NO BURNS OR ODOR OF SMOKE. RAN BOTH ENGINES FOR 20 MINUTSDR CHQA200500115Light · inoperativeLEFT HAND OVERWING EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.SDR CHQA200500042Lamp · burned outLEFTHAND OVERWING EMERGENCY EXIT LIGHT IS INOP. REPLACED THE LEFTHAND OVERWING EMERGENCY EXIT LIGHT BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.SDR 00050Gasket · leakingRT ENGINE ITT 50 DEGREES HOTTER THAN LT ITT. INSPECTED AIRCRAFT NR 2 ENG, PERFORMED BORESCOPE OF COMPRESSOR TURBINE SECTION HOT SECTION WITHIN LIMITS. PERFORMED LEAK CHECK OF BLEED LINE, FOUND LEAKS AND REPLACED GASKETS. ALL CHECK GOOD AT THIS TIME.
Back to N276SK, cancelled Feb 22, 2023