N575RP, cancelled Nov 7, 2018

Service difficulty reports · 29

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 = 'N575RP' AND deregistration_id = 'N575RP-2018-11-07'
  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 UHLA2015041500260Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Apr 15, 2015 · N575RP · Emb EMB145LR · Emergency LightingSDR UHLA2015040300223Controller · failedTHE CREW REPORTED THAT WHILE THE AUTO PRESSURIZATION SYSTEM WAS DEFERRED, THE MANUAL PRESSURIZATION SYSTEM WOULD NOT PRESSURIZE THE CABIN. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE LOCKED OPEN BOTH OUTFLOW VALVES AND THE DEFERRAL WApr 3, 2015 · N575RP · Emb EMB145LR · Cabin Pressure ControllerSDR UHLA2015012400047Bleed Valve · failedTHE CREW REPORTED THAT THEY RECEIVED A NR 1 BLEED VALVE FAIL MESSAGE AND A STAB ANIT-ICE VALVE FAIL MESSAGE DURING CLIMB OUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE BLEED VALVE. OPS CHECKED GOOD WITHJan 24, 2015 · N575RP · Emb EMB145LR · Compressor Bleed ValveSDR CHQA20140701221Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 BETWEEN FRAME 19 & 23. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140701211Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 & FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-055505.Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629222Fitting · crackedDURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629215Angle · crackedDURING INSPECTION, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE WAS REPLACED IAW SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629214Fitting · crackedDURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR CLIP ON THE APU FIREWALL AT STRINGER 10L & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL CLIP AT FRAME 80 & STRINGER 10L WAS REPLACED IAW SRM 51-40-02.Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140629212Repair · dentedDURING INSPECTION, A PREVIOUS REPAIR ON THE CARGO DOOR WAS FOUND TO BE DENTED AT THE LOWER AFT EDGE. THE DENT WAS REPAIRED IAW ETD 2014-145-055666.Jun 29, 2014 · N575RP · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA20140628220Rib · groovedDURING INSPECTION, A GROOVE WAS FOUND ON THE RT ELEVATOR NOSE RIB AT ELEVATOR STATION YH-1280.00 & HORIZONTAL & STAB YH=1310.00. THE RIB WAS REPLACED IAW SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Elevator, Spar/RibSDR CHQA20140628219Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & 16R WAS FOUND TO CRACKED. THE SHEAR CLIP WAS REPLACED IAW ACCORDANCE WITH SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140628217Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140627218Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140627214Skin · dentedDURING HEAVY MX, A DENT BELOW & AFT OF ENG 2 ON THE FUSELAGE SKIN WAS REPAIRED IAW ETD 2014-145-054213.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20140627213Fitting · crackedDURING INSPECTION, THE SHEAR CLIP AT FRAME 26 AND STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20140511147Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320.May 11, 2014 · N575RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20140303072Light · inoperativeDURING INSPECTION THE RT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Mar 3, 2014 · N575RP · Emb EMB145LR · Emergency LightingSDR CHQA20130721282Valve · faultyCREW RECEIVED A NR 2 BLEED LOW TEMPERATURE MESSAGE DURING ICING CONDITIONS IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED NR 2 HIGH STAGE VALVE. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.Jul 21, 2013 · N575RP · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA20130702253Sign · inoperativeDURING INSPECTION, THE RT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE EMERGENCY EXIT SIGN AND ALL OPS CHECKS WERE GOOD.Jul 2, 2013 · N575RP · Emb EMB145LR · Emergency LightingSDR CHQA20120527182Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON FRAME 65 SHEAR TIE. MAINTENANCE REPLACED THE SHEAR TIE AT FRAME 65 IN ACCORDANCE WITH ETD 2012-145-007624.May 27, 2012 · N575RP · Emb EMB145LR · Fuselage Internal Mounting StructureSDR CHQA201100290Flex Coupling · tornCREW REPORTED THAT DURING FLIGHT THE NUMBER 2 COOLING PACK WAS MAKING A LOUD RUSHING AIR NOISE. THEY ALSO REPORTED A SLIGHT BURNING SMELL FROM THE NUMBER 2 COOLING PACK. MAINTENANCE DEFERRED THE NUMBER 2 COOLING PACK. THE DEFERRAL WAS CLEARED LATER THAT DAYJul 25, 2011 · N575RP · Emb EMB145LR · Cabin Cooling SystemSDR CHQA200800255Light · inoperativeCREW REPORTED A SMOKE SMELL FROM EMERGENCY ROW AROUND SEAT 10A. THE FLIGHT DIVERTED TO LEX AND LANDED WITHOUT INCIDENT. FOUND SIDEWALL LIGHT AT 10A INOPERATIVE AND DEFERRED THE LIGHT. THE LIGHT WAS LATER RELAMPED, CLEARING THE MEL AND NO OTHER DEFECTS WERE Dec 24, 2008 · N575RP · Emb EMB145LR · Passenger Compartment LightingSDR CHQA200800067Noise Attenuator · meltedFLIGHT 6380, STL TO CVG - AFTER LEVELING OFF AT FL230, THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. THE AIRCRAFT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. DURING ENGINE RUNS, MAINTENANCE WAS ABLE TO DUPLICATE THE SMELL AND INSPECMar 30, 2008 · N575RP · Emb EMB145LR · Cabin Cooling SystemSDR CHQA200800047Engine · leakingCMH TO BOS - WHILE CLIMBING THROUGH FL190, THE CREW RECEIVED AN E1 IMPENDING OIL BYPASS MESSAGE. THE FIRST OFFICER PERFORMED THE QRH CHECKLISTS, WHILE THE CAPTAIN CHECKED THE ENGINE STATUS ON THE MFD. THE CAPTAIN NOTICED THAT THE OIL QUANTITY WAS DOWN TO 3 QMar 6, 2008 · N575RP · Emb EMB145LR · Turbine Engine Oil SystemSDR CHQA200800002Unknown · smokeCVG TO IND, ON INITIAL CLIMB AT APPROXIMATELY 1500 FEET, THE CREW RECEIVED A "LAV SMOKE" EICAS MESSAGE. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECK LISTS AND PREPARED TO RETURN TO FIELD. DURING THIS TIME THE FLIGHT ATTENDANT CALLED THE COCKPIT AND INFORMEJan 2, 2008 · N575RP · Emb EMB145LR · Air Distribution SystemSDR CHQA200800001Velocity Sensor · failedCVG TO IND - ATTEMPTED TO RETRACT FLAPS DURING CLIMB AND RECEIVED A FLAP FAIL EICAS MESSAGE. RAN ALL APPLICABLE QRH CHECK LISTS, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE DUPLICATED THE FLAP FAIL WITH A RIGHT TRANSMISSION BRAKE FAIL WHILE OJan 1, 2008 · N575RP · Emb EMB145LR · Trailing Flap Position Indicating SystemSDR CHQA200700041Ballast · burned outJFK TO IND JUST AFTER LIFT OFF RECEIVED THE "LAV SMOKE" WARNING. FA CHECKED FOR SMOKE OR FIRE AND NOTICED A HOT ELECTRICAL BURNING SMELL IN THE REAR OF THE CABIN. THE SMELL QUICKLY DISSIPATED. FLIGHT CREW DECLARED AN EMERGENCY AND RAN THROUGH THE APPROPRIATAug 21, 2007 · N575RP · Emb EMB145LR · Passenger Compartment LightingSDR CHQA200800003Smoke Detector · malfunctionedCVG TO IND - DURING TAKEOFF A "LAV SMOKE" EICAS MESSAGE WAS DISPLAYED AT APPROXIMATELY 1500 FEET. THE FLIGHT CREW PREPARED TO RETURN TO FIELD AND PERFORMED THE APPLICABLE QRH CHECK LISTS. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS NO VISIBLE SMOKE OR ODORJan 2, 2007 · N575RP · Emb EMB145LR · Smoke DetectionSDR CHQA200600066Probe · burnedFLIGHT 6383 - CVG-STL - WHILE ON VISUAL APPROACH AT APPROXIMATELY THE OUTER MARKER, NOTICED A HOT OR BURNING SMELL IN THE AIRCRAFT. WHILE RUNNING LANDING CHECK LIST, PITOT 3 INOP EICAS MESSAGE APPEARED. MESSAGE CLEARED, BUT SMELL REMAINED. COMPLETED CHECKLIMay 24, 2006 · N575RP · Emb EMB145LR · Pitot/Static Anti-Ice System
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