# Service difficulty reports: N575RP, cancelled Nov 7, 2018 A list on [N575RP, cancelled Nov 7, 2018](https://openairdocs.org/deregistered/N575RP-2018-11-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR UHLA2015041500260](https://openairdocs.org/sdr/UHLA2015041500260.md): Light · inoperative · Apr 15, 2015 · N575RP · Emb EMB145LR · Emergency Lighting > DURING 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. - [SDR UHLA2015040300223](https://openairdocs.org/sdr/UHLA2015040300223.md): Controller · failed · Apr 3, 2015 · N575RP · Emb EMB145LR · Cabin Pressure Controller > THE 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 W - [SDR UHLA2015012400047](https://openairdocs.org/sdr/UHLA2015012400047.md): Bleed Valve · failed · Jan 24, 2015 · N575RP · Emb EMB145LR · Compressor Bleed Valve > THE 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 WITH - [SDR CHQA20140701221](https://openairdocs.org/sdr/CHQA20140701221.md): Floor Support · corroded · Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20140701211](https://openairdocs.org/sdr/CHQA20140701211.md): Floor Support · corroded · Jul 1, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 & FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-055505. - [SDR CHQA20140629222](https://openairdocs.org/sdr/CHQA20140629222.md): Fitting · cracked · Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20140629215](https://openairdocs.org/sdr/CHQA20140629215.md): Angle · cracked · Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20140629214](https://openairdocs.org/sdr/CHQA20140629214.md): Fitting · cracked · Jun 29, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20140629212](https://openairdocs.org/sdr/CHQA20140629212.md): Repair · dented · Jun 29, 2014 · N575RP · Emb EMB145LR · Cargo/Baggage Doors > DURING 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. - [SDR CHQA20140628220](https://openairdocs.org/sdr/CHQA20140628220.md): Rib · grooved · Jun 28, 2014 · N575RP · Emb EMB145LR · Elevator, Spar/Rib > DURING 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. - [SDR CHQA20140628219](https://openairdocs.org/sdr/CHQA20140628219.md): Fitting · cracked · Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & 16R WAS FOUND TO CRACKED. THE SHEAR CLIP WAS REPLACED IAW ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20140628217](https://openairdocs.org/sdr/CHQA20140628217.md): Fitting · cracked · Jun 28, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140627218](https://openairdocs.org/sdr/CHQA20140627218.md): Fitting · cracked · Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140627214](https://openairdocs.org/sdr/CHQA20140627214.md): Skin · dented · Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MX, A DENT BELOW & AFT OF ENG 2 ON THE FUSELAGE SKIN WAS REPAIRED IAW ETD 2014-145-054213. - [SDR CHQA20140627213](https://openairdocs.org/sdr/CHQA20140627213.md): Fitting · cracked · Jun 27, 2014 · N575RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING 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. - [SDR CHQA20140511147](https://openairdocs.org/sdr/CHQA20140511147.md): Skin · corroded · May 11, 2014 · N575RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320. - [SDR CHQA20140303072](https://openairdocs.org/sdr/CHQA20140303072.md): Light · inoperative · Mar 3, 2014 · N575RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE RT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20130721282](https://openairdocs.org/sdr/CHQA20130721282.md): Valve · faulty · Jul 21, 2013 · N575RP · Emb EMB145LR · Pneumatic Distribution System > CREW 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. - [SDR CHQA20130702253](https://openairdocs.org/sdr/CHQA20130702253.md): Sign · inoperative · Jul 2, 2013 · N575RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE EMERGENCY EXIT SIGN AND ALL OPS CHECKS WERE GOOD. - [SDR CHQA20120527182](https://openairdocs.org/sdr/CHQA20120527182.md): Shear Tie · corroded · May 27, 2012 · N575RP · Emb EMB145LR · Fuselage Internal Mounting Structure > DURING 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. - [SDR CHQA201100290](https://openairdocs.org/sdr/CHQA201100290.md): Flex Coupling · torn · Jul 25, 2011 · N575RP · Emb EMB145LR · Cabin Cooling System > CREW 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 DAY - [SDR CHQA200800255](https://openairdocs.org/sdr/CHQA200800255.md): Light · inoperative · Dec 24, 2008 · N575RP · Emb EMB145LR · Passenger Compartment Lighting > CREW 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 - [SDR CHQA200800067](https://openairdocs.org/sdr/CHQA200800067.md): Noise Attenuator · melted · Mar 30, 2008 · N575RP · Emb EMB145LR · Cabin Cooling System > FLIGHT 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 INSPEC - [SDR CHQA200800047](https://openairdocs.org/sdr/CHQA200800047.md): Engine · leaking · Mar 6, 2008 · N575RP · Emb EMB145LR · Turbine Engine Oil System > CMH 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 Q - [SDR CHQA200800002](https://openairdocs.org/sdr/CHQA200800002.md): Unknown · smoke · Jan 2, 2008 · N575RP · Emb EMB145LR · Air Distribution System > CVG 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 INFORME - [SDR CHQA200800001](https://openairdocs.org/sdr/CHQA200800001.md): Velocity Sensor · failed · Jan 1, 2008 · N575RP · Emb EMB145LR · Trailing Flap Position Indicating System > CVG 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 O - [SDR CHQA200700041](https://openairdocs.org/sdr/CHQA200700041.md): Ballast · burned out · Aug 21, 2007 · N575RP · Emb EMB145LR · Passenger Compartment Lighting > JFK 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 APPROPRIAT - [SDR CHQA200800003](https://openairdocs.org/sdr/CHQA200800003.md): Smoke Detector · malfunctioned · Jan 2, 2007 · N575RP · Emb EMB145LR · Smoke Detection > CVG 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 ODOR - [SDR CHQA200600066](https://openairdocs.org/sdr/CHQA200600066.md): Probe · burned · May 24, 2006 · N575RP · Emb EMB145LR · Pitot/Static Anti-Ice System > FLIGHT 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 CHECKLI ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N575RP-2018-11-07/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.