N266SK, cancelled May 23, 2018

Service difficulty reports · 65

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 = 'N266SK' AND deregistration_id = 'N266SK-2018-05-23'
  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 UHLA201507300614Apu · fireWHILE APPROACHING THE GATE, THE CREW DISCHARGED THE APU FIRE BOTTLES AFTER A CONFIRMED APU FIRE. THE APU WAS R & R.Jul 30, 2015 · N266SK · Emb EMB145LR · Airborne Auxiliary Power Unit (APU) SystemSDR UHLA2015022200118None · noneTHE CREW REPORTED THAT THEY SUSPECTED A FUEL LEAK IN THE RT WING TANK DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RT WING SURFACES AND PERFORMED OPS CHECKS OF THE FUEL SYSTEM WITH NO LEAKS OR DEFECTS NOTEDFeb 22, 2015 · N266SK · Emb EMB145LR · Standard Practices/StructuresSDR CHQA20141119328Light · inoperativeDURING INSPECTION, THE EMER FLOOR PROXIMITY LIGHT STRIP AT ROW 6 WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 19, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20140829255Floor Support · corrodedDURING INSPECTION THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE BEAM WAS REPLACED IAW ETD 2014-145-073053.Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140829253Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Aug 29, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140828252Skin · chafedDURING INSPECTION THE CARGO DOOR INNER SKIN WAS FOUND TO HAVE CHAFE MARKS ON THE LOWER AFT END. THE SKIN WAS REPLACED IAW SRM 51-40-02.Aug 28, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140827254Firewall · crackedDURING INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER LT SUPPORT ROD. THE APU FIREWALL WAS REPAIRED IAW SRM 53-32-13.Aug 27, 2014 · N266SK · Emb EMB145LR · Fuselage Main, BulkheadSDR CHQA20140826256Doubler · corrodedDURING INSPECTION THE LT OMEGA BEAM REPAIR DOUBLER ON THE INBD SIDE WAS FOUND TO BE CORRODED AT FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140826250Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SEAT TRACK FROM FRAME 25 - 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20140826249Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.Aug 26, 2014 · N266SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA20140825251Profile · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LOWER PROFILE ON THE CARGO DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-02.Aug 25, 2014 · N266SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140518150Flap · malfunctionedDURING APPROACH, THE FLIGHT CREW RECEIVED A FLAP FAIL MSG ON THE EICAS DISPLAY. AFTER RUNNING THE CHECKLIST IN THE QRH, AN EMERGENCY WAS DECLARED & A SUCCESSFUL LANDING WAS COMPLETED. RESET THE FLAP SYS & THE MSG CLEARED. NO FURTHER DEFECTS HAVE BEEN NOTED.May 18, 2014 · N266SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20140430128Inverter · inoperativeDURING INSPECTION, THE FWD CABIN COCKPIT ENTRANCE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE FWD CLOSET INVERTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 30, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20140429127Transceiver · faultyCREW REPORTED THAT THE WEATHER RADAR WAS INOPERATIVE. THE CREW DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE WEATHER RADAR RECEIVER & TRANSMITTER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 29, 2014 · N266SK · Emb EMB145LR · Weather Radar SystemSDR CHQA20140218062Battery · dischargedDURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY BATTERY & ALL OPERATIONAL CHECKS WERE GOOD.Feb 18, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20140116016Battery · dischargedDURING INSPECTION, THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jan 16, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20140102001Battery · dischargedDURING INSPECTION, THE RT & LT AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jan 2, 2014 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20131219457Warning System · false activationCREW REPORTED THAT ON APPROACH THEY RECEIVED AN AURAL WARNING FOR LG. ALL THREE GEAR INDICATED DOWN & LOCKED. THE CREW DID A GO AROUND & ON THE SECOND APPROACH THE AURAL MESSAGE REPEATED. AGAIN, ALL THREE GEAR INDICATED DOWN & LOCKED & THERE WERE NO EICAS IDec 19, 2013 · N266SK · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA20131210444Battery Pack · dischargedTHE AFT EXTERIOR LT & RT FUSELAGE LIGHTS FAILED TO ILLUMINATE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK & ALL OPERATIONS CHECKED GOOD.Dec 10, 2013 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20131016370Duct · disconnectedCREW REPORTED THAT DURING CLIMB THERE WAS SMOKE IN THE CABIN AROUND SEAT 9A. DECLARED AND EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AIR CONDITIONING DUCT DISCONNECTED AND PRODUCING CONDENSATION INSIDE CABIN. DUCT RECONNECTEOct 16, 2013 · N266SK · Emb EMB145LR · Air Distribution SystemSDR CHQA20130822329Frame · damagedDURING INSPECTION, A HOLE WAS FOUND ON THE RT SIDE OF FRAME 65 BETWEEN STRINGERS 12R AND 13R. THE FRAME WAS REPAIRED IAW ETD 2013-145-032262.Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130822328Support · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE RT INBD OMEGA BEAM SUPPORT AT FRAME 47 AND 48. THE OMEGA BEAM SUPPORTS WERE REPLACED IAW SRM 51-40-02.Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130822327Channel · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER OF LT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IAW SRM 53-00-10.Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20130822326Frame · bentDURING INSPECTION, FRAME 72 WAS FOUND BENT AT STRINGER 16R. FRAME REPAIRED IAW ETD 2013-145-032192-A.Aug 22, 2013 · N266SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20130820320Battery Pack · inoperativeDURING INSPECTION, NR 4 AND 5 EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED GOOD.Aug 20, 2013 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20130621226Battery Pack · inoperativeDURING INSPECTION, OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jun 21, 2013 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20130509163Battery · 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.May 9, 2013 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20130222061Connector · corrodedCREW REPORTED THAT ON TAKEOFF THEY SELECTED THE CLIMB THRUST RATING AND THE MODE AUTOMATICALLY REVERTED TO T/O THRUST MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CORROSION FROM THE PINS ON RESISTOR MODULES A7055 AND A705Feb 22, 2013 · N266SK · Emb EMB145LR · Engine Control System WiringSDR CHQA20130114014Bleed Valve · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 2 VALVE FAIL MESSAGE ALONG WITH A BLEED 2 VALVE CLOSED MESSAGE. DUE TO WEATHER RESTRICTIONS THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE 2 BLEED VALVE. OPERATIONAL CHJan 14, 2013 · N266SK · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20121210469Ecu · faultyCREW REPORTED, FLAP FAIL MESSAGE ON APPROACH TO KRHI. THE CREW RETURNED TO FIELD IN KMKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 10, 2012 · N266SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20121209459Ecu · faultyCREW REPORTED, RECEIVED A FLAP FAIL MESSAGE AFTER GEAR RETRACTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS AND A FLAP LOW SPEED MESSAGE APPEARED. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 12/10/2012 BY RDec 9, 2012 · N266SK · Emb EMB145LR · Trailing Edge Flap Control SystemSDR CHQA20120906312Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53-12-04 AND 51-40-02.Sep 6, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120906311Skin Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 14 AND 16 AND STRINGERS 21L TO 20R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-02.Sep 6, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120904320Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R FROM FRAME 8 TO FRAME 13. THE STRINGER 21R AT FRAME 8 TO FRAME 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-20-02.Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR CHQA20120904317Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120904319Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 11 AND 12. THE RIGHT STANCHION BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120904318Stanchion · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT STANCHION AT FRAMES 12 AND 13. THE RIGHT STANCHION BETWEEN FRAMES 12 AND 13 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120904316Web · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12. THE RIGHT WEB ASSEMBLY BETWEEN FRAMES 11 AND 12 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Sep 4, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120828315Skin Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012305.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120828313Fitting · crackedDURING INSPECTION, THE SHEAR FOOT AT FRAME 68 BETWEEN STRINGERS 6L AND 7L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED AND INSTALLED IN ACCORDANCE WITH SRM 53-31-04.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120828310Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLES ON THE SERVICE DOOR THRESHOLD. MAINTENANCE REPLACED THE SERVICE DOOR SILL IN ACCORDANCE WITH SRM 53-20-10.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120816314Skin · dentedDURING HEAVY MAINTENANCE A PREVIOUSLY DAMAGED SECTION OF SKIN AFT OF THE PASSENGER DOOR NEAR FRAME 19-20 AND STRINGER 12L -13L WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-03683A CLOSING DMI 591816/3 AND 591816/1.Aug 16, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120609187Battery Pack · dischargedDURING INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jun 9, 2012 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA20120321085Battery · dischargedDURING INSPECTION, THE LEFT AND RIGHT 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.Mar 21, 2012 · N266SK · Emb EMB145LR · Emergency LightingSDR CHQA201200027Coupling · defectiveCREW REPORTED DURING CLIMB THEY RECEIVED A BLEED 1 LEAK MESSAGE. AFTER FOLLOWING THE QUICK REFERENCE HANDBOOK THE MESSAGE CLEARED. DUE TO SINGLE BLEED OPERATIONS, CREW DECIDED TO DIVERT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A COUPLING Jan 27, 2012 · N266SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA201100410Connector · disconnectedDURING INSPECTION, THE RIGHT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE CONNECTOR DISCONNECTED FROM THE LIGHT ASSEMBLY. THE CONNECTOR WAS REATTACHED AND OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Oct 22, 2011 · N266SK · Emb EMB145LR · Light System WiringSDR CHQA201100397Warning System · malfunctionedCREW REPORTED THAT ON DESCENT, RECEIVED A SPOILER FAIL MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DISCOVERED THAT THEIR LANDING DISTANCE WOULD BE LONGER PER THE QUICK REFERENCE HANDBOOK AND THEY DID NOT HAVE THE CORRECT VAPP AND Oct 4, 2011 · N266SK · Emb EMB145LR · Drag Control SystemSDR CHQA201100041Connector · corrodedCREW REPORTED THAT AFTER TAKEOFF THE THRUST MODE WOULD NOT CHANGE FROM TAKEOFF MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CORROSION ON CONNECTOR P0885. THE CORROSION WAS CLEANED AND THE CONNECTOR WAS RE-CONNECTED. OPERAFeb 23, 2011 · N266SK · Emb EMB145LR · Engine Control System WiringSDR CHQA201100030Shutoff Valve · faultyCREW RETURNED TO FIELD DUE TO A BLEED 2 VALVE FAIL MESSAGE ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE E2 PRSOV AND HIGH STAGE PRESSURE SWITCH WITH NO FURTHER DEFECTS NOTED.Feb 3, 2011 · N266SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA201100002Connector · dirtyAFTER TAKEOFF THE CREW REPORTED THAT THE COMM 2 RMU WAS BLANKED OUT AND THE BACK-UP HEAD COULD NOT BE TUNED AND THAT COMM 1 WAS SWITCHING BETWEEN ACTIVE AND TUNING FREQUENCIES. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOTJan 3, 2011 · N266SK · Emb EMB145LR · Communications System Wiring
Back to N266SK, cancelled May 23, 2018