N271SK, cancelled Aug 6, 2019

Service difficulty reports · 71

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 = 'N271SK' AND deregistration_id = 'N271SK-2019-08-06'
  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 UHLA2015030600152Solenoid · faultyTHE CREW REPORTED THAT THEIR WAS A NOISE IN THE COCKPIT DURING CLIMB AND SUSPECTED THE NLG DOORS WERE OPEN. THE CREW DIVERTED THE ACFT AND LANDED WITHOUT INCIDENT. THE ACFT WAS FOUND SAFE FOR FERRY FLIGHT AND WAS FERRIED FOR MAINTENANCE. MAINTENANCE REPLACEMar 6, 2015 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20141201342Pressure Switch · faultyTHE CREW REPORTED THAT ON CLIMB OUT, THEY RECEIVED A RUDDER OVER BOOST MSG. THE CREW RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE RUDDER SYS 1 PRESS SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 1, 2014 · N271SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20141028325Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20 UNDER THE RAMP ANGLE. THE CTR OMEGA BEAM WAS REPAIRED IAW SRM 51-40-02.Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141028322Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT FRAME 62 & STRINGERS 6R & 8R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 53-31-04.Oct 28, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027327Fitting · crackedDURING INSPECTION THE SHEAR CLIP AT FRAME 80 & STRINGER 8L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027326Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SUPPORT FROM FRAME 44 TO 50. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027324Support · crackedDURING INSPECTION THE LT WING BOX ANGLE SUPPORT WAS FOUND TO BE CRACKED BETWEEN FRAME 44 & 45. THE SUPPORT WAS REPLACED IAW SRM 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20141027323Doubler · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM PREVIOUS REPAIR AT THE CARBON CROSS MEMBER. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10 & 51-40-02.Oct 27, 2014 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20131231472Battery · dischargedDURING INSPECTION, THE NR 1 EMERGENCY LIGHT BATTERY WAS NOT CHARGING. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Dec 31, 2013 · N271SK · Emb EMB145LR · Emergency LightingSDR CHQA20130823325Ballast · inoperativeDURING TAXI, CREW REPORTED A BURNING ODOR AND VISIBLE SMOKE IN THE CABIN COMING FROM THE CABIN LIGHTING BALLAST AT ROW 1. RETURNED TO GATE, REPLACED BALLAST. NO FURTHER DEFECTS HAVE BEEN NOTED.Aug 23, 2013 · N271SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20130728196Flap System · malfunctionedDURING CRUISE, RECEIVED A FLAP FAIL MESSAGE. FOLLOWED QUICK REF HANDBOOK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 28, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20130726195Control Unit · failedDURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20130726194Velocity Sensor · faultyDURING FLIGHT, RECEIVED A FLAP LOW SPEED MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FLAP ELECTRONIC CONTROL UNIT AND LT VELOCITY SENSOR WERE REPLACED. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2013 · N271SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20130516165Gcu · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSUMay 16, 2013 · N271SK · Emb EMB145LR · AC RegulatorSDR CHQA20130516164Generator · failedCREW REPORTED THAT DURING CLIMBOUT THEY RECEIVED A GENERATOR OFF BUSS MESSAGE FROM GENERATORS 1, 3, 4, AND THE APU GENERATOR. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE GENERATORS DID NOT COME BACK ONLINE. DURING THE RETURN TO FIELD FOR THIS ISSUMay 16, 2013 · N271SK · Emb EMB145LR · DC Generator-AlternatorSDR CHQA20130416117Proximity Switch · faultyCREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT RECEIVED SEVERAL WARNING MESSAGES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTEApr 16, 2013 · N271SK · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA20130416116Electronic Unit · faultyCREW REPORTED THAT ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND WERE ABLE TO RETRACT THE LANDING GEAR BUT RECEIVED SEVERAL WARNING MESSAGES. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTEApr 16, 2013 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20130326091Proximity Sensor · faultyCREW REPORTED THAT THE LEFT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED WHEN THE LANDING GEAR LEVER WAS SELECTED DOWN. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN LANDING GEAR DOWNLOCK PROXIMar 26, 2013 · N271SK · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA20130324090Light · defectiveCREW REPORTED THAT DURING LANDING THERE WAS AN ELECTRICAL SMELL COMING FROM THE LIGHTING BALLAST AT ROWS 5 AND 6. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BULBS AT ROWS 5 AND 6. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTEMar 24, 2013 · N271SK · Emb EMB145LR · Passenger Compartment LightingSDR CHQA20130126030Switch · inoperativeCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE DID NOT CLEAR. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED SYSTEM 1 PUJan 26, 2013 · N271SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130125029Bleed Valve · faultyCREW REPORTED THAT DURING CLIMB, THEY RECEIVED A BLEED 1 VALVE CLOSED MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK. THE CREW DIVERTED TO KEVV AND LANDED WITHOUT INCIDENT. MAINTENANCE LOCKED THE BLEED VALVE CLOSED AND DEFERRED THE ITEJan 25, 2013 · N271SK · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20121229004Thermostat · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GODec 29, 2012 · N271SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20121229003Valve · faultyCREW REPORTED, DURING FLIGHT THEY RECEIVED A BLEED 1 LOW TEMPERATURE MESSAGE IN ICING CONDITIONS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FAN AIR VALVE THERMOSTAT AND THE FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD WDec 29, 2012 · N271SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20121126446Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 26, 2012 · N271SK · Emb EMB145LR · Main Landing Gear Strut/Axle/TruckSDR CHQA20121126445Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 26, 2012 · N271SK · Emb EMB145LR · Main Landing Gear Strut/Axle/TruckSDR CHQA20121126444Strut · lowCREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICE THE LEFT, RIGHT, AND NOSE LANDING GEAR STRUTS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 26, 2012 · N271SK · Emb EMB145LR · Nose/Tail Landing Gear Strut/AxleSDR CHQA20120917352Engine · failedCREW REPORTED THAT DURING FLIGHT THAT THE ENGINE 2 OIL PRESSURE DROPPED INTO THE AMBER RANGE AND THE ENGINE ITT ROSE INTO THE RED. THE CREW SHUT DOWN THE ENGINE IN FLIGHT, RAN THE CHECKLIST, AND DECLARED AN EMERGENCY. THE PASSENGER O2 MASKS WERE ALSO DEPLOYESep 17, 2012 · N271SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA20120907331Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R. THE DENT ON THE RIGHT FUSELAGE SKIN BETWEEN FRAME 13 AND FRAME 14 AND STRINGERS 10R AND 11R WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.Sep 7, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120906336Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 12 AND FRAME 13 AND BETWEEN STINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL H.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120806330Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD2012-145-012394 REVISION B, DETAIL E.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120906329Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 10 AND FRAME 11 ON STRINGERS 21R AND 20R WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012394 REVISION B, DETAIL D.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120906328Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 11 AND FRAME 12 AND STRINGERS 21L AND 20L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-012394 REVISION B, DETAILS B AND C.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120906327Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 16 AND FRAME 18 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A DETAILS E AND F.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120906326Skin · damagedDURING HEAVY MAINTENANCE, A PATCH REPAIR BETWEEN FRAME 19 AND FRAME 21 AND STRINGERS 20L AND 21L WAS COMPLETED IN ACCORDANCE WITH ETD 2012-145-012320A.Sep 6, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120903345Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT FRAME 23. THE RIGHT OMEGA BEAM AT FRAME 23 WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.Sep 3, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120830344Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 31 AT STRINGER 15R. FRAME 31 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 30, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120829343Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 30 AT STRINGER 15R. FRAME 30 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120829342Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 25 AT STRINGER 15R. FRAME 25 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120827341Floor Support · corrodedDURING INSPECTION, THE CENTER OMEGA BEAM AROUND THE ANCHOR NUT WAS FOUND CORRODED BETWEEN FRAME 24 AND FRAME 25. THE CENTER OMEGA BEAM AROUND ANCHOR NUT BETWEEN FRAME 24 AND FRAME 25 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012075.Aug 27, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120824340Structure · corrodedDURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053.Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120824339Structure · corrodedDURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053.Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120823338Beam · corrodedDURING INSPECTION, THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED AND THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Aug 23, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822346Skin · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT WING UPPER SKIN AT THE GROUND SPOILER CENTER HINGE CUTOUT. THE LEFT WING UPPER SKIN AT THE GROUND SPOILER HINGE CUTOUT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011887.Aug 22, 2012 · N271SK · Emb EMB145LR · Wing, Plate/SkinSDR CHQA20120822337Floor Support · corrodedDURING INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 HAD AND EXISTING REPAIR THAT WAS FOUND TO BE CORRODED. THE LEFT OMEGA BEAM AT FRAME 20 EXISTING REPAIR WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822335Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822334Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822333Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822332Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822325Uplock Bracket · crackedDURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07.Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20120822324Uplock Bracket · crackedDURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07.Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension System
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