# Service difficulty reports: N11565 A list on [N11565](https://openairdocs.org/aircraft/N11565.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 · 76 reports - [SDR ASOA2018060871051](https://openairdocs.org/sdr/ASOA2018060871051.md): Housing · damaged · Jun 8, 2018 · N11565 · Emb EMB145LR · Vertical Stabilizer > RT AND LT SPHERICAL BEARING HOUSINGS HAVE DISPLACED METAL. REPAIRED LT AND RT SPHERICAL BEARING HOUSING IN ACCORDANCE WITH SRM 55-30-02. - [SDR ASOA201806087105](https://openairdocs.org/sdr/ASOA201806087105.md): Skin · cracked · Jun 8, 2018 · N11565 · Emb EMB145LR · Fuselage Main, Plate/Skin > RT REAR FUSELAGE SKIN AT FRAME 75, STRINGER 2R-3R CRACKED. REPAIRED FUSELAGE SKIN IN ACCORDANCE WITH SRM 53-31-01. - [SDR ASOA201806067098](https://openairdocs.org/sdr/ASOA201806067098.md): Skin · cracked · Jun 4, 2018 · N11565 · Emb EMB145LR · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CUTOUT THE DAMAGE SECTION, FABRICATED A FILLER, AND DOUBLER. INSTALLED THE REPAIR. - [SDR ASOA201805277094](https://openairdocs.org/sdr/ASOA201805277094.md): Skin · cracked · May 27, 2018 · N11565 · Emb EMB145LR · Fuselage Main, Plate/Skin > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK IN THE REAR FUSELAGE SKIN AT FRAME 75 AND STRINGER 2R. MAINTENANCE CUTOUT A 2" BY 2" SECTION OF SKIN AND INSTALLED A FILLER AND DOUBLER IAW SRM 51-31-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT TH - [SDR ASOA20151215060](https://openairdocs.org/sdr/ASOA20151215060.md): Display · failed · Dec 15, 2015 · N11565 · Emb EMB145LR · Attitude and Direction Data System > CREW REPORTED AN ELECTRICAL ODOR AFTER CAPTAINS MFD WENT BLANK. MAINTENANCE R & R CAPTAIN`S MFD WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20151215091](https://openairdocs.org/sdr/ASOA20151215091.md): Display · shorted · Dec 15, 2015 · N11565 · Emb EMB145LR · Attitude and Direction Data System > THE CREW REPORTED MFD 1 IS OUT WITH BURNING ODOR IN FLIGHT DECK. THE ACFT LANDED IN ECP WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE AFFECTED MFD ON MEL 34-22-01-1 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R & R THE NR 1 MFD, OPERATIONALL - [SDR ASOA20151009058](https://openairdocs.org/sdr/ASOA20151009058.md): Fuel Control · leaking · Oct 9, 2015 · N11565 · Emb EMB145LR · APU Engine Fuel and Control > THE CREW REPORTED A FUEL ODOR COMING FROM APU BLEED. AFTER ROTATION WHEN APU WAS PROVIDING AIR TO THE PACKS. MAINTENANCE INSPECTED AND REPLACED THE APU FUEL CONTROL ASSY. OPS CHECKED WERE GOOD. - [SDR ASOA20150210009](https://openairdocs.org/sdr/ASOA20150210009.md): Unknown · odor · Feb 10, 2015 · N11565 · Emb EMB145LR · Cabin Cooling System > CREW REPORTED A BURNING ODOR BEFORE LANDING. MAINTENANCE PERFORMED TROUBLESHOOTING AND NO UNUSUAL ODORS COULD BE DETECTED OR REPRODUCED. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20141117092](https://openairdocs.org/sdr/ASOA20141117092.md): Light · unknown · Nov 17, 2014 · N11565 · Emb EMB145LR · Emergency Lighting > THE CREW REPORTED EMERGENCY LIGHT WAS INTERMITTENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR ASOA20141014109](https://openairdocs.org/sdr/ASOA20141014109.md): Structure · damaged · Oct 14, 2014 · N11565 · Emb EMB145LR · Fuselage Main, Structure > ACFT WAS ON TAKEOFF WHEN A BIRD HIT THE NOSE. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED THE BAD RIVETS AND INSTALL 5 OF A OVERSIZE RIVETS. ALODINED, PRIMED AND PAINTED IAW SRM 51-40-02 AND CPM 51-=21-07. PERFORMED A HIGH FREQUENCY EDDY CURRENT IN - [SDR ASOA20140804085](https://openairdocs.org/sdr/ASOA20140804085.md): Socket · dirty · Aug 4, 2014 · N11565 · Emb EMB145LR · Emergency Lighting > DURING MX INSPECTION, THE LT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED BULB, CLEANED DEBRIS FROM SOCKET AND REINSTALLED BULB, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140706089](https://openairdocs.org/sdr/ASOA20140706089.md): Controller · melted · Jul 6, 2014 · N11565 · Emb EMB145LR · Windshield/Door Rain/Ice Removal > THE CREW REPORTED A STRONG SMOKE ODOR, CIGARETTE & PAPER ODOR EMITTING FROM MCD, F/A JUMPSEAT, AROUND EQUIPMENT CLOSET. THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR 1 WINDSHIELD TEMP CONTROLLER TO HAVE M - [SDR ASOA20140417046](https://openairdocs.org/sdr/ASOA20140417046.md): Coffeemaker · dirty · Apr 17, 2014 · N11565 · Emb EMB145LR · Buffet/Galleys > F/A REPORTED AN ODOR COMING FROM THE GALLEY COFFEEMAKERS. MAINTENANCE CLEANED THE WARMERS ON BOTH COFFEE BREWERS AND PERFORMED AN OPS CHECK, CHECKED GOOD, WITH NO BURNING ODORS DETECTED. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140112005](https://openairdocs.org/sdr/ASOA20140112005.md): Brake Assy · faulty · Jan 12, 2014 · N11565 · Emb EMB145LR · Landing Gear Brake System > A "BRAKE DEGRADE" MESSAGE APPEARED ON EICAS DURING LANDING AND REPORTED MORE THAN NORMAL BRAKE PEDAL PRESSURE NEEDED. ACFT PULLED TO THE LEFT. R & R NR 4 BRAKE ASSY, TEMP SENSOR, HYD FUSE AND BRAKE CONTROL VALVE, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED - [SDR ASOA20140109011](https://openairdocs.org/sdr/ASOA20140109011.md): Web · cracked · Jan 9, 2014 · N11565 · Emb EMB145LR · Trailing Edge Flaps > DURING C-CHECK, LT OTBD FLAP INBD ROOT RIB INTERNAL WEBBING CRACKED. MAINTENANCE REPAIRED IAW EC 5750-01562. - [SDR ASOA20140107010](https://openairdocs.org/sdr/ASOA20140107010.md): Fitting · corroded · Jan 7, 2014 · N11565 · Emb EMB145LR · Fuselage Main, Attach Fittings > DURING C-CHECK, INSPECTION FOUND VERTICAL STAB SPAR TO FRAME 75 FRETTING AT THE FUSELAGE. MAINTENANCE COMPLIED WITH THE EC 5310-01317 TO REMOVED FITTING, REMOVED CORROSION, CHECK LIMITS AND REINSTALL FITTING. - [SDR ASOA20130724078](https://openairdocs.org/sdr/ASOA20130724078.md): Unknown · odor · Jul 24, 2013 · N11565 · Emb EMB145LR · Air Distribution System > PILOT REPORTED A STRONG ODOR OF PLASTIC/ELECTRICAL SMOKE INFLIGHT DURING DESCENT WITH THE TOP OF GLARESHIELD/AVIONICS PANEL EXTREMELY HOT TO THE TOUCH. MX INSPECTED CABIN AND COCKPIT FOR PLASTIC/ELECTRICAL ODOR WITH NONE FOUND OR NOTED. ALSO RAN BOTH ENGINES - [SDR ASOA20130609328](https://openairdocs.org/sdr/ASOA20130609328.md): Switch · failed · Jun 9, 2013 · N11565 · Emb EMB145LR · Flight Control System > MAIN PITCH TRIM INOPERATIVE MESSAGE ON CLIMBOUT, AUTO TRIM FAIL, ELEVATOR MISTRIM. R & R PITCH TRIM SWITCH AND ACTUATOR. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA20120806068](https://openairdocs.org/sdr/ASOA20120806068.md): Ballast · failed · Aug 6, 2012 · N11565 · Emb EMB145LR · Passenger Compartment Lighting > THE CREW REPORTED SMOKE FROM 4C SIDEWALL LIGHT. MX REPLACED 4 B & C LIGHT ASSY AND 4 B&C LIGHT BALLAST. OPS CHECKS WERE GOOD. - [SDR ASOA20120201004](https://openairdocs.org/sdr/ASOA20120201004.md): Wire · broken · Feb 1, 2012 · N11565 · Emb EMB145LR · Light System Wiring > EMERGENCY LIGHT FLOOR STRIP INOP. R & R LIGHT STRIP. OPS CHECK GOOD. - [SDR C2XA11IA248](https://openairdocs.org/sdr/C2XA11IA248.md): Contactor · inoperative · Nov 3, 2011 · N11565 · Emb EMB145LR · AC Power Distribution System > IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BACKUP BATTERY PUSHBUTTON SWITCH, AND CONTACTOR K0305, OPERATIONALLY TESTED - [SDR C2XA11CL179](https://openairdocs.org/sdr/C2XA11CL179.md): Inverter · inoperative · Aug 1, 2011 · N11565 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE RIGHT AFT EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11IA249](https://openairdocs.org/sdr/C2XA11IA249.md): Switch · inoperative · Jul 3, 2011 · N11565 · Emb EMB145LR · AC Power Distribution System > IAH - FLIGHT 4457 THE CREW REPORTED A BACKUP BATTERY OFF BUSS INDICATION IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BACKUP BATTERY PUSHBUTTON SWITCH, AND CONTACTOR K0305, OPERATIONALLY TESTE - [SDR C2XA11CL144](https://openairdocs.org/sdr/C2XA11CL144.md): Control Unit · faulty · Jun 15, 2011 · N11565 · Emb EMB145LR · Drag Control System > CLE FLT 2521 CREW REPORTED THAT THE SPOILERS OPENED ON TAKEOFF ROLL AT APPROXIMATELY 100 KIAS. THE SPOILERS INDICATED OPEN ON THE EICAS SYSTEM. THE CREW THEN ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. CLE MAINTENANCE CHECKED ALL SPOILER - [SDR C2XA11TY022](https://openairdocs.org/sdr/C2XA11TY022.md): Inverter · inoperative · Mar 4, 2011 · N11565 · Emb EMB145LR · Emergency Lighting > SECOND FLOOR PROXIMITY EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. - [SDR C2XACL006](https://openairdocs.org/sdr/C2XACL006.md): Thermostat · faulty · Jan 6, 2011 · N11565 · Emb EMB145LR · Pneumatic Distribution System > IAD FLT 3153 THE CREW REPORTED A BLEED NR 1 OVERTEMP INDICATION IN FLIGHT DURING ICING CONDITIONS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FAN AIR CONTROL THERMOSTAT. OPERATIONAL CHECKS WERE GO - [SDR C2XA10RI0148](https://openairdocs.org/sdr/C2XA10RI0148.md): Control Panel · inoperative · Nov 26, 2010 · N11565 · Emb EMB145LR · Smoke Detection > FLIGHT 2030 - YYZ - FLIGHT CREW REPORTED LAV SMOKE DETECTOR IN GALLEY TEST INOPERATIVE. EWR MX REMOVED AND REPLACED SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10RI0144](https://openairdocs.org/sdr/C2XA10RI0144.md): Control Panel · inoperative · Nov 26, 2010 · N11565 · Emb EMB145LR · Smoke Detection > FLIGHT 2030 - EWR - FLIGHT CREW REPORTED SMOKE DETECTOR SWITCH IN GALLEY NOT WORKING. EWR MX REMOVED AND REPLACED GALLEY SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10SH076](https://openairdocs.org/sdr/C2XA10SH076.md): Skin · corroded · Feb 22, 2010 · N11565 · Emb EMB145LR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK FUSELAGE SKIN HAS CORROSION AT FR 58 POTABLE WATER SUPPORT DOUBLER MATING SURFACE. REPAIRED SKIN IAW EC5330-02079. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH075](https://openairdocs.org/sdr/C2XA10SH075.md): Stringer · corroded · Feb 22, 2010 · N11565 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > SHV - DURING C-CHECK STR 21R HAS CORROSION AT FR 13. REPAIRED STR 21R IAW EC5310-01507. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH073](https://openairdocs.org/sdr/C2XA10SH073.md): Floor Support · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LEFT OMEGA BEAM CORROSION FRM 29-34. REPAIRED LEFT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH072](https://openairdocs.org/sdr/C2XA10SH072.md): Sill · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS CORROSION. REPAIRED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH071](https://openairdocs.org/sdr/C2XA10SH071.md): Sill · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. REPAIRED SERVICE DOOR SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH070](https://openairdocs.org/sdr/C2XA10SH070.md): Floor Support · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 35-38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 51-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH069](https://openairdocs.org/sdr/C2XA10SH069.md): Support · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Waste Disposal System > SHV - DURING C-CHECK WASTE DRAIN VALVE SUPPORT HAS CORROSION. REMOVED AND REPLACED SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH068](https://openairdocs.org/sdr/C2XA10SH068.md): Attach Fitting · damaged · Feb 21, 2010 · N11565 · Emb EMB145LR · Ailerons > SHV - DURING C-CHECK LEFT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EC5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH067](https://openairdocs.org/sdr/C2XA10SH067.md): Attach Fitting · damaged · Feb 21, 2010 · N11565 · Emb EMB145LR · Spoilers > SHV - DURING C-CHECK LEFT O/B GROUND SPOILER ATTACHMENT HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 AMM 57-51-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH061](https://openairdocs.org/sdr/C2XA10SH061.md): Floor Support · corroded · Feb 21, 2010 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > LT OMEGA BEAM PREVIOUS REPAIR AT FR 20 HAS CORROSION (LEVEL 3). MAINTENANCE REMOVED AND REPLACED PREVIOUS REPAIR WITH NEW REPAIR IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH058](https://openairdocs.org/sdr/C2XA10SH058.md): Light · inoperative · Feb 10, 2010 · N11565 · Emb EMB145LR · Emergency Lighting > SHV - DURING C-CHECK RT LOWER EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IAW EMB 145 AMM 33-50-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10TY005](https://openairdocs.org/sdr/C2XA10TY005.md): Sign · inoperative · Dec 30, 2009 · N11565 · Emb EMB145LR · Emergency Lighting > A 12BC UPPER SIDEWALL EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXIT MARKING SIGN ASSY IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. - [SDR C2XA09IA254](https://openairdocs.org/sdr/C2XA09IA254.md): Display · burned · Oct 12, 2009 · N11565 · Emb EMB145LR · Central Display > CLL - FLIGHT 2593 - DURING FLIGHT THE CREW REPORTED THAT THE PFD1 CIRCUIT BREAKER POPPED WITH A CHECK PFD1 MESSAGE ON EICAS AND SMOKE COMING FROM UNDER THE PFD1. THE AIRCRAFT LANDED AT CLL WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE - [SDR C2XA08RI140](https://openairdocs.org/sdr/C2XA08RI140.md): Relay · burned · Sep 16, 2008 · N11565 · Emb EMB145LR · Electrical Power System > FLIGHT 2654 EWR FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR IN COCKPIT NOTICED AFTER LANDING. EWR MX R&R RELAY KO437 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA08IA070](https://openairdocs.org/sdr/C2XA08IA070.md): Unknown · odor · Feb 26, 2008 · N11565 · Emb EMB145LR · Air Distribution System > IAH - FLIGHT 2656, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA08SH025](https://openairdocs.org/sdr/C2XA08SH025.md): Floor Support · corroded · Feb 16, 2008 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 18-23. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA07TY010](https://openairdocs.org/sdr/C2XA07TY010.md): Power Supply · discharged · Mar 2, 2007 · N11565 · Emb EMB145LR · Emergency Lighting > 602 NR 482585- RT FWD EXTERIOR EMERGENCY LIGHT AND NR 2 AISLE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY UNIT IAW EMB 145AMM 33-50-04 OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR C2XA07IA029](https://openairdocs.org/sdr/C2XA07IA029.md): Fuse · blown · Feb 6, 2007 · N11565 · Emb EMB145LR · Emergency Lighting > DURING MAINTENANCE INSPECTION THE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A FUSE IN THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN - [SDR C2XA06IA198](https://openairdocs.org/sdr/C2XA06IA198.md): Windshield · malfunctioned · Dec 24, 2006 · N11565 · Emb EMB145LR · Flight Compartment Windows > BRO FLIGHT 3229 - THE CREW REPORTED SMOKE IN THE COCKPIT WHILE ARRIVING AT THE GATE. THE WINDSHIELD LEADS WERE RESECURED. LATER THAT DAY AT IAH, FLIGHT 3295, THE AIRCRAFT DISPLAYED A WINDSHIELD NR 2 HEAT FAIL MESSAGE. THE WINDSHIELD WAS REPLACED AND THE AIR - [SDR C2XA06BT018](https://openairdocs.org/sdr/C2XA06BT018.md): Power Supply · discharged · Apr 6, 2006 · N11565 · Emb EMB145LR · Emergency Lighting > EWR - DURING ROUTINE MAINTENANCE FOUND THE AISLE EMERGENCY LIGHT AT ROW 1 - 3 NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY OVER SERVICE DOOR IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. - [SDR C2XA06SH040](https://openairdocs.org/sdr/C2XA06SH040.md): Beam · corroded · Mar 28, 2006 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C CHECK, THE LOWER BAGGAGE DOOR CUT OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA06SH042](https://openairdocs.org/sdr/C2XA06SH042.md): Floor Support · corroded · Mar 28, 2006 · N11565 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C CHECK, THE LEFT OMEGA BEAM LOWER FLANGE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND COMPLETED THE REPAIR IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. Next page: https://openairdocs.org/aircraft/N11565/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 = 'N11565' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N11565/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.