# Service difficulty reports: N566RP, cancelled Dec 17, 2018 A list on [N566RP, cancelled Dec 17, 2018](https://openairdocs.org/deregistered/N566RP-2018-12-17.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 · 53 reports - [SDR UHLA201508040633](https://openairdocs.org/sdr/UHLA201508040633.md): Shear Tie · corroded · Aug 4, 2015 · N566RP · Emb EMB145LR · Fuselage Internal Mounting Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR TIE AT STRINGER 16L AT FRAME 65. THE SHEAR TIE WAS R & R IAW SRM 51-21-06. - [SDR UHLA201508030631](https://openairdocs.org/sdr/UHLA201508030631.md): Seat Track · corroded · Aug 3, 2015 · N566RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND ON THE RT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 43-47. THE LATERAL SUPPORT WAS R & R IAW SRM 51-40-02. - [SDR UHLA201508030629](https://openairdocs.org/sdr/UHLA201508030629.md): Seat Track · corroded · Aug 3, 2015 · N566RP · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING INSPECTION, CORROSION WAS FOUND BETWEEN FRAMES 48-50 ON THE RT WALL SEAT TRACK SUPPORT. THE RT LATERAL SUPPORT WAS R & R IAW SRM 51-40-02. - [SDR UHLA201508020636](https://openairdocs.org/sdr/UHLA201508020636.md): Structure · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE PILOT FLOOR FRAME OTBD OF INBD SEAT TRACK BETWEEN FRAMES 10-12. THE CORROSION WAS REPAIRED IAW ETD2015-145-072011. - [SDR UHLA201508020635](https://openairdocs.org/sdr/UHLA201508020635.md): Floorbeam · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Floor Beam > DURING INPSECTION, CORROSION WAS FOUND ON THE PILOT INBD FLOOR FRAME AFT OF THE RT RUDDER PEDAL AT FRAME 10. THE CORROSION WAS REPAIRED IAW ETD2015-145-072011. - [SDR UHLA201508020634](https://openairdocs.org/sdr/UHLA201508020634.md): Floor Support · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE RT FLOOR SILL AT FRAME 61. THE RIGHT FLOOR SILL WAS R & R IAW SRM 51-40-02. - [SDR UHLA201508020632](https://openairdocs.org/sdr/UHLA201508020632.md): Tee Fitting · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT FORWARD LOWER T-FITTING AT FRAME 65. THE PROFILE TEE FITTING WAS R & R IAW SRM 51-40-02. - [SDR UHLA201508020630](https://openairdocs.org/sdr/UHLA201508020630.md): Threshold · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD AT FRAME 65. THE CARGO DOOR THRESHOLD WAS R & R IAW SRM 51-40-02. - [SDR UHLA201508020627](https://openairdocs.org/sdr/UHLA201508020627.md): Striker · corroded · Aug 2, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND BEHIND THE LOWER FORWARD STRIKER PLATE AT FRAME 65. THE CORROSION WAS REPAIRED IAW SRM 53-31-04. - [SDR UHLA201508010639](https://openairdocs.org/sdr/UHLA201508010639.md): Frame · cracked · Aug 1, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 79 BETWEEN STR 5LT AND 6LT. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-073315. - [SDR UHLA201508010638](https://openairdocs.org/sdr/UHLA201508010638.md): Frame · cracked · Aug 1, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 78 BETWEEN STRINGERS 5R-6R. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-075243. - [SDR UHLA201508010637](https://openairdocs.org/sdr/UHLA201508010637.md): Frame · cracked · Aug 1, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 78 BETWEEN STRINGERS 6RT-7RT. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-075243. - [SDR UHLA201508010628](https://openairdocs.org/sdr/UHLA201508010628.md): Floorbeam · corroded · Aug 1, 2015 · N566RP · Emb EMB145LR · Fuselage Main, Floor Beam > DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN CABIN DOOR FLOORBEAM AT FRAME 16. THE CROSSBEAM WAS R & R IAW SRM 51-40-02. - [SDR UHLA201507080551](https://openairdocs.org/sdr/UHLA201507080551.md): Light · smoke · Jul 8, 2015 · N566RP · Emb EMB145LR · Flight Compartment Lighting > THE F/O'S YOKE CHART HOLDER LIGHTS BEGAN SMOKING IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING AND MAINTENANCE REMOVED THE CHART HOLDER AND SECURED THE CONNECTOR. MAINTENANCE LATER REPLACED THE CHART HOLDER AND NO FURTHER DISCREPANCIES HAVE BEEN NOTED. - [SDR UHLA201505030338](https://openairdocs.org/sdr/UHLA201505030338.md): Clamp · loose · May 3, 2015 · N566RP · Emb EMB145LR · Air Distribution System > THE CREW REPORTED A BLEED SYSTEM 2 LEAK MESSAGE ON CLIMBOUT. THE CREW MADE AN UNEVENTFUL UNSCHEDULED LANDING AT THE FIELD OF DEPARTURE. MAINTENANCE FOUND A LOOSE CLAMP ON THE RT PACK VALVE AND RESECURED THE CLAMP. ALL OPS AND LEAK CHECKS WERE GOOD AND THERE - [SDR CHQA20140920279](https://openairdocs.org/sdr/CHQA20140920279.md): Skin · cracked · Sep 20, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION A HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND THE SKIN TO CRACKED AT 1 FASTENER ABOVE STRINGER 6R & 1 BELOW STRINGER 6R AT FRAME 79. THE SKIN WAS REPAIRED IAW ETD 2014-145-079864. - [SDR CHQA20140920277](https://openairdocs.org/sdr/CHQA20140920277.md): Floor Support · corroded · Sep 20, 2014 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 19 - 23. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140919280](https://openairdocs.org/sdr/CHQA20140919280.md): Skin · damaged · Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 24 & STRINGER 15R IAW ETD2014-145-015228A. - [SDR CHQA20140919278](https://openairdocs.org/sdr/CHQA20140919278.md): Skin · damaged · Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 25 & STRINGER 15R IAW ETD2014-145-015228A. - [SDR CHQA20140919276](https://openairdocs.org/sdr/CHQA20140919276.md): Skin · damaged · Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 17 & STRINGER 17R IAW ETD2014-145-015228A. - [SDR CHQA20140912275](https://openairdocs.org/sdr/CHQA20140912275.md): Skin · gouged · Sep 19, 2014 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE GOUGED AT THE INSIDE PYLON ACCESS PANEL 424DB AT FRAME 67 & STRINGER 9R. THE SKIN WAS REPAIRED IAW ETD2014-145-079860. - [SDR CHQA20140210047](https://openairdocs.org/sdr/CHQA20140210047.md): Battery · discharged · Feb 10, 2014 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. REPLACED THE BATTERY & ALL OPERATIONS CHECKED ARE GOOD. - [SDR CHQA20130719305](https://openairdocs.org/sdr/CHQA20130719305.md): Beam · corroded · Jul 19, 2013 · N566RP · Emb EMB145LR · Fuselage Main, Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT LOWER BEAM. THE THRESHOLD PLATE WAS REPAIRED IAW SRM 53-40-02. - [SDR CHQA20130719304](https://openairdocs.org/sdr/CHQA20130719304.md): Threshold · corroded · Jul 19, 2013 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD BENEATH THE FLOOR PANEL 271FF. THRESHOLD REPAIRED IAW SRM 51-40-02. - [SDR CHQA20130709262](https://openairdocs.org/sdr/CHQA20130709262.md): Control Module · faulty · Jul 9, 2013 · N566RP · Emb EMB145LR · Extinguishing System > RECEIVED A BAGGAGE EXTINGUISHING BOTTLE INOPERATIVE MESSAGE DURING CRUISE. MESSAGE CLEARED ON ITS OWN AND THE F/A REPORTED THAT THERE WAS NO INDICATION OF SMOKE OR FIRE IN THE BAGGAGE AREA. DURING DESCENT BAGGAGE EXTINGUISHING LIGHT CAME ON WITH NO OTHER MESS - [SDR CHQA20130623232](https://openairdocs.org/sdr/CHQA20130623232.md): Wire · broken · Jun 23, 2013 · N566RP · Emb EMB145LR · Light System Wiring > DURING INSPECTION, MAIN ENTRY DOOR HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX FOUND A DAMAGED WIRE IN THE MAIN ENTRY DOOR WIRING HARNESS AND REPAIRED THE WIRE AFTER WHICH OPS CHECKED GOOD AND NO FUTHER DEFECTS WERE NOTED. - [SDR CHQA20130315081](https://openairdocs.org/sdr/CHQA20130315081.md): Battery · discharged · Mar 15, 2013 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE 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. - [SDR CHQA20121202449](https://openairdocs.org/sdr/CHQA20121202449.md): Skin · damaged · Dec 2, 2012 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. THE CREW DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. DURING THE LIGHTNING STRIKE INSPECTION, MAINTENANCE FOUND BURN MARKS BETWEEN STRINGERS 2L AND 3L, BETWEEN FRAMES 56 AND 57. MAINTENANCE REPAIRED THE AREA IN - [SDR CHQA20121015384](https://openairdocs.org/sdr/CHQA20121015384.md): Battery · discharged · Oct 15, 2012 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, BOTH EXTERNAL 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. - [SDR CHQA20120607190](https://openairdocs.org/sdr/CHQA20120607190.md): Skin · corroded · Jun 8, 2012 · N566RP · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION, CORROSION WAS FOUND AT A SCREW HOLE ON THE LOWER SERVICE DOOR CUT-OUT AT FRAME 22. FRAME 22 WAS REPAIRED IN ACCORDANCE WITH ETD2012-145-008241 REVISION A. - [SDR CHQA201100308](https://openairdocs.org/sdr/CHQA201100308.md): Battery · discharged · Aug 5, 2011 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100269](https://openairdocs.org/sdr/CHQA201100269.md): Frame · corroded · Jul 7, 2011 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE REPLACED FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE NEW PART WAS INSTALLED WITH A SOLID RIVET I - [SDR CHQA201100268](https://openairdocs.org/sdr/CHQA201100268.md): Fitting · corroded · Jul 7, 2011 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAME BAGGAGE DOOR SHEAR CLIP. THE AIRCRAFT IS STILL IN INSPECTION AND THE FINAL CORRECTIVE ACTION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT. - [SDR CHQA201100267](https://openairdocs.org/sdr/CHQA201100267.md): Floor Support · corroded · Jul 5, 2011 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE TOILET OMEGA BEAM 5 INCHES FORWARD OF FRAME 61. MAINTENANCE REPAIRED THE MIDDLE TOILET OMEGA BEAM IN ACCORDANCE WITH ETD 2011-145-101785 AND SRM 53-21-10. - [SDR CHQA201100264](https://openairdocs.org/sdr/CHQA201100264.md): Frame · corroded · Jul 4, 2011 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, CORROSION WAS FOUND ON THE CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE REPLACED FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACC - [SDR CHQA201100263](https://openairdocs.org/sdr/CHQA201100263.md): Support Bracket · cracked · Jul 4, 2011 · N566RP · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT SUPPORT BRACKET AT FRAME 8 AND STRINGER 9R IN THE FORWARD FUSE II SECTION. MAINTENANCE REPLACED THE RIGHT FORWARD FUSELAGE II FRAME 8 ANGLE SUPPORT ABOVE STRINGER 9R IN ACCORDANCE WITH SRM 51-0-02. - [SDR CHQA201100281](https://openairdocs.org/sdr/CHQA201100281.md): Frame · cracked · Jul 1, 2011 · N566RP · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, A CRACK WAS FOUND AT FORWARD FUSELAGE II, LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE EMERGENCY ESCAPE HATCH LOWER BEAM. MAINTENANCE REPLACED THE FORWARD FUSELAGE II LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FRAME 10 AT T - [SDR CHQA201100280](https://openairdocs.org/sdr/CHQA201100280.md): Skin · dented · Jun 29, 2011 · N566RP · Emb EMB145LR · Wing, Plate/Skin > DURING INSPECTION, THE RIGHT WING LEADING EDGE II WAS FOUND TO HAVE TWO DENTS ON THE SKIN COUPLED WITH A CRACK ON THE RIGHT LEADING EDGE II RIB. THE TWO DENTS ON THE RIGHT LEADING EDGE SKIN (PN:145-11450-604) COUPLED WITH THE CRACK ON THE RIGHT LEADING EDGE II - [SDR CHQA201100053](https://openairdocs.org/sdr/CHQA201100053.md): Light · inoperative · Mar 9, 2011 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000191](https://openairdocs.org/sdr/CHQA201000191.md): Flap System · malfunctioned · Oct 3, 2010 · N566RP · Emb EMB145LR · Trailing Edge Flap Control System > ON DESCENT INTO LGA, CREW SELECTED FLAPS FROM 0 TO 9 AND RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE FLAPS DID NOT MOVE FROM 0 DEGREES. THE CREW ABORTED THE APPROACH AND RAN THE REQUIRED QRH CHECKLISTS THEN LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLA - [SDR CHQA201000151](https://openairdocs.org/sdr/CHQA201000151.md): Light · inoperative · Aug 6, 2010 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY LIGHT ON THE AIR STAIR HANDRAIL WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE AIR STAIR EMERGENCY LIGHT AND THE EMERGENCY LIGHTS OPERATED NORMALLY. - [SDR CHQA201000116](https://openairdocs.org/sdr/CHQA201000116.md): Amplifier · faulty · Jun 9, 2010 · N566RP · Emb EMB145LR · Interphone/Passenger Announcement (PA) System > AFTER TAKEOFF THE CREW REPORTED A CONSTANT CABIN TO COCKPIT CHIME AND WERE UNABLE TO COMMUNICATE WITH THE FLIGHT ATTENDANT. THE FLIGHT RETURNED TO LEX AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS THEN FERRIED TO CMH FOR FURTHER TROUBLESHOOTING. CMH MAINTEN - [SDR CHQA201000060](https://openairdocs.org/sdr/CHQA201000060.md): Battery Pack · discharged · Mar 20, 2010 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 BATTERY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. - [SDR CHQA201000009](https://openairdocs.org/sdr/CHQA201000009.md): O-Ring · blown · Jan 17, 2010 · N566RP · Emb EMB145LR · Pneumatic Distribution System > THE FLIGHT CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS UPON ENTERING ICING CONDITIONS DURING CLIMB. THE CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND A LEAK AT JOINT 15 UNDER THE CARGO COMPARTMENT FLOOR. - [SDR CHQA200900134](https://openairdocs.org/sdr/CHQA200900134.md): Battery Pack · discharged · May 27, 2009 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE OVER-WING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE NR4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE OVER-WING EMERGENCY LIGHTS OPERATED NORMALLY. - [SDR CHQA200900081](https://openairdocs.org/sdr/CHQA200900081.md): Battery Pack · discharged · Mar 14, 2009 · N566RP · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. - [SDR CHQA200900068](https://openairdocs.org/sdr/CHQA200900068.md): Proximity Switch · dirty · Mar 2, 2009 · N566RP · Emb EMB145LR · Landing Gear Position and Warning > FLIGHT 9940, AVL TO TRI. AFTER TAKEOFF WHEN THE GEAR WAS COMMANDED UP, THE FLIGHT CREW NOTICED THAT THE NOSE GEAR DOORS HAD NOT CLOSED. THE AIRCRAFT CONTINUED ITS CLIMB TO 9,000 FT WHILE THE CREW RAN THE QRH CHECKLISTS. AFTER LEVELING OFF THE CREW RECEIVED - [SDR CHQA200900006](https://openairdocs.org/sdr/CHQA200900006.md): Cabin Pressure · malfunctioned · Jan 5, 2009 · N566RP · Emb EMB145LR · Cabin Pressure Control System > ON CLIMB OUT AT 4,000 FT THE DIFFERENTIAL PRESSURE INDICATION DROPPED FROM 1.6 TO ZERO IN AUTO PRESSURIZATION MODE. THE CREW DID NOT FEEL A CHANGE IN PRESSURIZATION AND DID NOT SWITCH TO MANUAL MODE. THE FLIGHT LANDED BACK AT DEPARTURE WITHOUT INCIDENT. MX - [SDR CHQA200900266](https://openairdocs.org/sdr/CHQA200900266.md): Battery Pack · inoperative · Jan 3, 2009 · N566RP · Emb EMB145LR · Emergency Lighting > DURING A SERVICE CHECK THE OVER WING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYS OPERATED NORMALLY. - [SDR CHQA200800079](https://openairdocs.org/sdr/CHQA200800079.md): Gasket · missing · Apr 14, 2008 · N566RP · Emb EMB145LR · Fuel Storage > FLIGHT 6239, BOS TO SAV, DURING CRUISE, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A FLUID LEAK COMING FROM THE LEFT WING. THE FLIGHT CREW VERIFIED THE FLUID LEAK AND DIVERTED TO IAD. THE FLIGHT LANDED WITHOUT INCIDENT IN IAD. MAINTENANCE INSPECTED TH Next page: https://openairdocs.org/deregistered/N566RP-2018-12-17/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 = 'N566RP' AND deregistration_id = 'N566RP-2018-12-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N566RP-2018-12-17/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.