# Service difficulty reports: N562RP, cancelled Oct 1, 2022 A list on [N562RP, cancelled Oct 1, 2022](https://openairdocs.org/deregistered/N562RP-2022-10-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 67 reports - [SDR UHLA201602100043](https://openairdocs.org/sdr/UHLA201602100043.md): Light · misinstalled · Feb 10, 2016 · N562RP · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHT OVER LT WING IS INSTALLED UPSIDE DOWN. REPOSITIONED LEFT EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD. - [SDR UHLA201602060042](https://openairdocs.org/sdr/UHLA201602060042.md): Washer · missing · Feb 6, 2016 · N562RP · Emb EMB145LR · Passenger/Crew Doors > AREA WASHER MISSING ON MED STEP ACTUATOR RAMP. INSTALLED WASHER TO MED STEP ACTUATOR ARM IN REF WITH AMM 52-10-01. - [SDR UHLA201602060041](https://openairdocs.org/sdr/UHLA201602060041.md): Bolt · sheared · Feb 6, 2016 · N562RP · Emb EMB145LR · Fuselage, Door Hinge > MED REAR HINGE HAS SHEARED BOLT AT ACTUATOR ATTACH. R & R BOLT IN REAR HINGE ROTATING ARM IAW AMM 52-11-03. - [SDR UHLA201602060040](https://openairdocs.org/sdr/UHLA201602060040.md): Arm · damaged · Feb 6, 2016 · N562RP · Emb EMB145LR · Passenger/Crew Doors > MED REAR ROTATING ARM FOUND DAMAGED. R & R MED REAR ROTATING ARM IAW AMM 52-11-03. - [SDR CHQA20141203350](https://openairdocs.org/sdr/CHQA20141203350.md): Profile · punctured · Dec 3, 2014 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, PUNCTURE DAMAGE WAS FOUND ON THE PAX DOOR U LATERAL PROFILE. THE PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141203344](https://openairdocs.org/sdr/CHQA20141203344.md): Profile · corroded · Dec 3, 2014 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, THE PAX DOOR U PROFILE WAS FOUND TO BE CORRODED. THE PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141202349](https://openairdocs.org/sdr/CHQA20141202349.md): Step · corroded · Dec 2, 2014 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE PAX DOOR ON THE NR 1 STEP. THE NR 1 PAX DOOR STEP WAS REPLACED IAW SRM 51-21-02. - [SDR CHQA20141201343](https://openairdocs.org/sdr/CHQA20141201343.md): Service Door · corroded · Dec 1, 2014 · N562RP · Emb EMB145LR · Service Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE BOTTOM OF THE SERVICE DOOR. THE SERVICE DOOR WAS REPAIRED IAW ETD 2014-145-101279. - [SDR CHQA20141130348](https://openairdocs.org/sdr/CHQA20141130348.md): Fitting · corroded · Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AT SHEAR CLIP AT FRAME 65. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141130347](https://openairdocs.org/sdr/CHQA20141130347.md): Door Sill · corroded · Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR FLOOR SILL AT FRAME 66. THE CARGO DOOR SILL WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20141130346](https://openairdocs.org/sdr/CHQA20141130346.md): Floor Support · corroded · Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE BEAM WAS REPLACED IAW SRM 51-40-02 & SRM 53-00-10. - [SDR CHQA20141130345](https://openairdocs.org/sdr/CHQA20141130345.md): Support · cracked · Nov 30, 2014 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE RT OMEGA BEAM INBD SUPPORT WAS FOUND TO BE CRACKED AT FRAMES 47 & 48. THE SUPPORT WAS REPLACED IAW SRM 53-23-02. - [SDR CHQA20140602184](https://openairdocs.org/sdr/CHQA20140602184.md): Control Unit · faulty · Jun 2, 2014 · N562RP · Emb EMB145LR · Landing Gear Brake System > CREW REPORTED THAT THEY RECEIVED A BRAKE OTBD INOPERATIVE CAUTION MSG WHEN THE LG WAS SELECTED DOWN. THE CREW DECLARED AN EMER. THE ACFT LANDED WITHOUT INCIDENT & SAFETY CREWS INSPECTED THE BRAKE & FOUND THE ACFT SAFE TO TAXI TO THE GATE UNDER ITS OWN POWER. - [SDR CHQA20131124436](https://openairdocs.org/sdr/CHQA20131124436.md): Seat Track · corroded · Nov 24, 2013 · N562RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > LEFT OTBD SEAT TRACK BEAM AT THE OVERWING EXIT WAS FOUND TO BE CORRODED. THE SEAT TRACK BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20131124435](https://openairdocs.org/sdr/CHQA20131124435.md): Seat Track · corroded · Nov 24, 2013 · N562RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDEWALL TRACK MOUNTING FLANGE AT FRAME 42 - 48 WAS FOUND TO BE CORRODED. THE SEAT TRACK MOUNTING FLANGE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130815314](https://openairdocs.org/sdr/CHQA20130815314.md): Valve · leaking · Aug 15, 2013 · N562RP · Emb EMB145LR · Fuel Storage > CREW REPORTED DURING CLIMB, FUEL REPORTED TO BE LEAKING FROM LEFT WING. VERIFIED VAPOR COMING FROM THE LT WING AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. MX REPLACED THE FUEL TANK VALVE AT THE LT WING RIB 19. OPS CHECKED GOOD WITH NO LEAKS NOTED. - [SDR CHQA20130712270](https://openairdocs.org/sdr/CHQA20130712270.md): Radar · malfunctioned · Jul 12, 2013 · N562RP · Emb EMB145LR · Weather Radar System > CREW REPORTED THAT DURING FLIGHT, WEATHER RADAR BEGAN MALFUNCTIONING. DUE TO WEATHER CONDITIONS ALONG FLIGHT ROUTE, ELECTED TO RETURN TO FIELD. LANDED WITHOUT INCIDENT. MX COULD NOT DUPLICATE MALFUNCTION AND PERFORMED SUCCESSFUL OPS CHECK OF WEATHER RADAR - [SDR CHQA20130622227](https://openairdocs.org/sdr/CHQA20130622227.md): Wire · inoperative · Jun 22, 2013 · N562RP · Emb EMB145LR · Light System Wiring > DURING INSPECTION, THE MAIN ENTRY DOOR HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX FOUND A DAMAGED WIRE IN THE MAIN ENTRY DOOR WIRING HARNESS. REPAIRED WIRE, OPS CHECKED GOOD AND NO FUTHER DEFECTS WERE NOTED. - [SDR CHQA20121210458](https://openairdocs.org/sdr/CHQA20121210458.md): Profile · corroded · Dec 10, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE SERVICE DOOR LOWER AFT CORNER WAS FOUND TO BE CORRODED AT THE DOOR TRIM ATTACH POINT. THE AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-017580. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT. - [SDR CHQA20121206564](https://openairdocs.org/sdr/CHQA20121206564.md): Rib · damaged · Dec 6, 2012 · N562RP · Emb EMB145LR · Elevator, Spar/Rib > DURING INSPECTION, THE LEFT ELEVATOR INTERNAL RIB AT STATION YH-1310 HAS TWO DAMAGED HOLES. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-017677. - [SDR CHQA20121206455](https://openairdocs.org/sdr/CHQA20121206455.md): Frame · bent · Dec 6, 2012 · N562RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN RIGHT STRINGER 14R AND 15R. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04. - [SDR CHQA20121205457](https://openairdocs.org/sdr/CHQA20121205457.md): Gusset · corroded · Dec 5, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE NUT PLATES ON THE CENTER OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR CROSS BEAM. THE GUSSET WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-017227. PART INFORMATION WILL BE SUBMITTED AS A SUPPLEME - [SDR CHQA20121205456](https://openairdocs.org/sdr/CHQA20121205456.md): Gusset · corroded · Dec 5, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND AROUND THE NUT PLATES AND FASTENER ON THE RIGHT OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR. THE GUSSET PLATE WAS REPLACED IN ACCORDANCE WITH ETD 2012-145-017227-A. - [SDR CHQA20121125453](https://openairdocs.org/sdr/CHQA20121125453.md): Floor Support · corroded · Nov 25, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM JUST FORWARD OF THE "Z" PROFILE AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10. - [SDR CHQA20121125452](https://openairdocs.org/sdr/CHQA20121125452.md): Beam · corroded · Nov 25, 2012 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR ENTRY BEAM AFT OF THE NUT PLATE. THE CORROSION WAS BLENDED IN ACCORDANCE WITH SRM 51-10-03 AND A PREVIOUS REPAIR WAS FOUND TO HAVE COVERED THE DAMAGED AREA PER SRM 53-21-02. - [SDR CHQA201100486](https://openairdocs.org/sdr/CHQA201100486.md): Battery · discharged · Dec 14, 2011 · N562RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY AISLE LIGHTS FROM THE ROW 8 TO ROW 12. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100465](https://openairdocs.org/sdr/CHQA201100465.md): Battery · discharged · Dec 3, 2011 · N562RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY AND THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100456](https://openairdocs.org/sdr/CHQA201100456.md): Fadec · malfunctioned · Nov 18, 2011 · N562RP · Emb EMB145LR · Fuel Control/Turbine Engines > CREW REPORTED THAT WHILE ON APPROACH, E2 N1 ROLLED BACK TO 38 PERCENT WHILE E1 N1 STAYED AT 68 PERCENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET FADECS AND PERFORMED ENGINE RUNS WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100436](https://openairdocs.org/sdr/CHQA201100436.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 53. MAINTENANCE REPAIRED THE FLOOR SILL AT FRAME 53 IN ACCORDANCE WITH ETD 2011-145-107752 WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100435](https://openairdocs.org/sdr/CHQA201100435.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 49. MAINTENANCE REMOVED THE CORROSION AT FLOOR SILL FRAME 49 RIGHT SIDE. THE REMAINING THICKNESS WAS 0.045 INCHES, WITH CORROSION LESS THEN 30 PERCENT OF ORIGINAL MATERIAL THICKNESS. NO - [SDR CHQA201100434](https://openairdocs.org/sdr/CHQA201100434.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 44. MAINTENANCE REMOVED THE CORROSION AT FRAME 44 RIGHT FLOOR SILL. THE REMAINING THICKNESS WAS 0.044 INCHES, WITH LESS THAN 30 PERCENT OF THE THICKNESS REMOVED. NO CRACK INDICATIONS WE - [SDR CHQA201100433](https://openairdocs.org/sdr/CHQA201100433.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 39. MAINTENANCE BLENDED THE CORROSION ON THE LEFT FLOOR SILL AT FRAME 39. CORROSION WAS FOUND TO BE LESS THAN 30 PERCENT, REMAINING MATERIAL THICKNESS WAS 0.038 INCHES. NO CRACK INDICATI - [SDR CHQA201100432](https://openairdocs.org/sdr/CHQA201100432.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL FROM FRAME 43 TO FRAME 44. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 43 TO FRAME 44 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100431](https://openairdocs.org/sdr/CHQA201100431.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100430](https://openairdocs.org/sdr/CHQA201100430.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100429](https://openairdocs.org/sdr/CHQA201100429.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 39. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 39 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100428](https://openairdocs.org/sdr/CHQA201100428.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100427](https://openairdocs.org/sdr/CHQA201100427.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100426](https://openairdocs.org/sdr/CHQA201100426.md): Sill · corroded · Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 28. MAINTENANCE INSPECTED AND REMOVED THE CORROSION FROM THE FLOOR SILL AT FRAME 28 RIGHT. CORROSION WAS LESS THEN 30 PERCENT OF MATERIAL THICKNESS, THE REMAINING THICKNESS IS 0.041 INCH - [SDR CHQA201100422](https://openairdocs.org/sdr/CHQA201100422.md): Hydraulic System · low · Oct 31, 2011 · N562RP · Emb EMB145LR · Hydraulic System, Main > CREW REPORTED THAT AFTER LANDING GEAR RETRACTION RECEIVED A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE. THE CREW CONTINUED TO MONITOR THE HYDRAULIC SYSTEM DURING THE FLIGHT. THE LEVELS CONTINUED TO DROP. AN EMERGENCY WAS DECLARED BY CHARLESTON APPROACH. THE A - [SDR CHQA201100310](https://openairdocs.org/sdr/CHQA201100310.md): Relay · failed · Aug 6, 2011 · N562RP · Emb EMB145LR · Cabin Pressure Control System > CREW REPORTED THAT DURING FLIGHT RECEIVED A COOLING PACK 2 VALVE CLOSED MESSAGE. COOLING PACK 1 WAS DEFERRED THE PREVIOUS DAY. AS A RESULT THE AIRCRAFT LOST PRESSURIZATION. THE CREW ALSO REPORTED, RECEIVED WING ANTI-ICE 1 AND WING ANTI-ICE 2 VALVE FAIL MESS - [SDR CHQA201100303](https://openairdocs.org/sdr/CHQA201100303.md): Transceiver · defective · Jul 29, 2011 · N562RP · Emb EMB145LR · Weather Radar System > CREW REPORTED THAT THE WEATHER RADAR WAS NOT DEPICTING THE WEATHER AS SEEN VISUALLY OUTSIDE THE AIRCRAFT. THE CREW TRIED USING BOTH AUTOMATIC AND MANUAL GAIN MODES, BUT RADAR REMAINED THE SAME. THE CREW DIVERTED TO KCMH AND THE AIRCRAFT LANDED WITHOUT INCIDE - [SDR CHQA201100167](https://openairdocs.org/sdr/CHQA201100167.md): Profile · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER. THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100166](https://openairdocs.org/sdr/CHQA201100166.md): Frame Splice · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME SPLICE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME SPLICE WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100165](https://openairdocs.org/sdr/CHQA201100165.md): Door Frame · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FRAME 1. THE MAIN PASSENGER DOOR STRUCTURE FRAME 1 WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100164](https://openairdocs.org/sdr/CHQA201100164.md): Structure · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT BOTTOM CORNER. THE MAIN PASSENGER DOOR STRUCTURE AFT BOTTOM CORNER WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100163](https://openairdocs.org/sdr/CHQA201100163.md): Rib · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 1ST FROM FORWARD. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 1ST FROM FORWARD WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100162](https://openairdocs.org/sdr/CHQA201100162.md): Rib · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 2ND FROM FORWARD. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 2ND FROM FORWARD WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100161](https://openairdocs.org/sdr/CHQA201100161.md): Door Frame · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100160](https://openairdocs.org/sdr/CHQA201100160.md): Casting · corroded · Apr 24, 2011 · N562RP · Emb EMB145LR · Passenger/Crew Doors > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE DOOR OPENING HANDLE BACK CASTING. THE PASSENGER DOOR STRUCTURE DOOR OPENING HANDLE BACK CASTING WAS REPLACED WITH NO FURTHER DEFECTS NOTED. Next page: https://openairdocs.org/deregistered/N562RP-2022-10-01/reports.md?page=2 ## 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 = 'N562RP' AND deregistration_id = 'N562RP-2022-10-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N562RP-2022-10-01/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.