# Service difficulty reports: N13975 A list on [N13975](https://openairdocs.org/aircraft/N13975.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 · 75 reports - [SDR ASOA2019082324047](https://openairdocs.org/sdr/ASOA2019082324047.md): Skin · cracked · Aug 22, 2019 · N13975 · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING A-CHECK INSPECTION, THE CROWN SKIN AT THE UPPER AFT CORNER OF THE F/O'S DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACK AREA AND PERFORMED A TRIPLER REPAIR IN ACCORDANCE WITH EMBRAER TECHNICAL DISPOSITION ETD2019-145-106582, AND THE AI - [SDR ASOA2018101624053](https://openairdocs.org/sdr/ASOA2018101624053.md): Charger · inoperative · Oct 12, 2018 · N13975 · Emb EMB145LR · Emergency Lighting > IAH - THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT AT ROW THREE TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201808127147](https://openairdocs.org/sdr/ASOA201808127147.md): Window Post · cracked · Aug 12, 2018 · N13975 · Emb EMB145LR · Fuselage Main, Structure > LEFT COCKPIT WINDSHIELD LATERAL POST WAS CRACKED. REPAIRED THE POST IAW SB 145-53-0029. - [SDR ASOA201807277143](https://openairdocs.org/sdr/ASOA201807277143.md): Door Sill · corroded · Jul 27, 2018 · N13975 · Emb EMB145LR · Fuselage Miscellaneous Structure > TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LT FLOOR SILL AT FRAME 32 AND 33 WITH CORROSION. MAINTENANCE R&R THE ENTIRE SILL IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. - [SDR ASOA201802117012](https://openairdocs.org/sdr/ASOA201802117012.md): Rib · cracked · Jan 27, 2018 · N13975 · Emb EMB145LR · Wing, Rib/Bulkhead > LT WING RIB 5 CRACKED. REMOVED AND REPLACED LT RIB 5 IAW ECTC ETD2017-145-104919. AIRCRAFT RELEASED AND RETURNED TO SERVICE. - [SDR ASOA201703254012](https://openairdocs.org/sdr/ASOA201703254012.md): Battery Pack · discharged · Mar 25, 2017 · N13975 · Emb EMB145LR · Emergency Lighting > MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTE - [SDR ASOA201703254011](https://openairdocs.org/sdr/ASOA201703254011.md): Power Supply · inoperative · Mar 25, 2017 · N13975 · Emb EMB145LR · Emergency Lighting > MAINTENANCE REPORTED THAT THE NR 1 & 2 OVERWING EMERGENCY LIGHTS AND AFT INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOT - [SDR ASOA20150913069](https://openairdocs.org/sdr/ASOA20150913069.md): Battery Pack · discharged · Sep 13, 2015 · N13975 · Emb EMB145LR · Emergency Lighting > DURING MAINTENANCE INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150830047](https://openairdocs.org/sdr/ASOA20150830047.md): Charger · inoperative · Aug 30, 2015 · N13975 · Emb EMB145LR · Emergency Lighting > DURING MAINTENANCE INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT SYSTEM BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150610032](https://openairdocs.org/sdr/ASOA20150610032.md): Sign · inoperative · Jun 10, 2015 · N13975 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE MAIN DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE SIGN ASSY AND OPS CHECKS WERE GOOD. - [SDR ASOA20140118009](https://openairdocs.org/sdr/ASOA20140118009.md): Charger · inoperative · Jan 18, 2014 · N13975 · Emb EMB145LR · Emergency Lighting > DURING MAINTENANCE INSPECTION, THE MAIN CABIN DOOR EXTERIOR AND CEILING LIGHTS WERE FOUND INOPERATIVE. R & R THE NR 1 EMERGENCY LIGHT SYS BATTERY POWER SUPPLY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20131001114](https://openairdocs.org/sdr/ASOA20131001114.md): Control Panel · faulty · Oct 1, 2013 · N13975 · Emb EMB145LR · Smoke Detection > PILOT REPORTED LAVATORY SMOKE WARNING ON EICAS IN FLIGHT BUT NO SMOKE OBSERVED IN CABIN OR LAVATORY. MX R & R THE LAVATORY SMOKE DETECTOR PANEL OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20130909104](https://openairdocs.org/sdr/ASOA20130909104.md): Light · inoperative · Sep 9, 2013 · N13975 · Emb EMB145LR · Emergency Lighting > DURING SCHEDULED MX INSPECTION THE NR 1 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 1 FLOOR PROXIMITY LIGHT STRIP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120820062](https://openairdocs.org/sdr/ASOA20120820062.md): Controller · faulty · Aug 20, 2012 · N13975 · Emb EMB145LR · Cabin Pressure Controller > CREW REPORTED LOST AUTO PRESSURIZATION. CABIN PRESSURE CLIMBED TO 8400FT, NO EICAS MESSAGE PRESENT. CREW PERFORMED AIR RETURN. MX R & R DIGITAL PRESSURE CONTROLLER AND ALSO R & R ELECTROPNEUMATIC OUTFLOW VALVE WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FO - [SDR ASOA20120813130](https://openairdocs.org/sdr/ASOA20120813130.md): Seat Track · corroded · Aug 13, 2012 · N13975 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings > DURING C-CHECK, FOUND THE RT WALL SEAT TRACK SUPPORT AT FRAME 50 CORRODED. MX BLENDED OUT THE CORROSION IAW SRM 51-10-03. FOUND AREA TO BE WITHIN LIMITS IAW 53-23-10. R & R ALL CORRODED FASTENERS IAW SRM 51-40-02. REMOVED ALL CORRODED NUTPLATES IAW SRM 51- - [SDR ASOA20120813127](https://openairdocs.org/sdr/ASOA20120813127.md): Skin · corroded · Aug 10, 2012 · N13975 · Emb EMB145LR · Fuselage Main, Plate/Skin > CORROSION OUT OF LIMITS ON INNER SKIN BAYS BETWEEN STR 20R & 21L & 22L AT FRM 13 & 14. CUTOUT CORRODED AREAS, FABRICATED 2 FILLERS AND ONE DOUBLER. ACFT STILL IN C CHECK. - [SDR C2XA11CL114](https://openairdocs.org/sdr/C2XA11CL114.md): Controller · faulty · Apr 30, 2011 · N13975 · Emb EMB145LR · Cabin Pressure Controller > ORD FLT 5999 THE CREW REPORTED CABIN ALTITUDE BEGAN TO CLIMB AT A HIGH RATE UNTIL IT REACHED 10,500. THE AIRCRAFT WAS AT 34,000. BEGAN A RAPID DESCENT TO 10,500. AMBER DASHES ON CABIN RATE. MASKS DID NOT DEPLOY. LEVELED OUT AT 11,000 MSL AND THE PRESSURIZ - [SDR C2XA10RI106](https://openairdocs.org/sdr/C2XA10RI106.md): Coffeemaker · defective · Aug 26, 2010 · N13975 · Emb EMB145LR · Buffet/Galleys > FLIGHT 2699 - FLIGHT CREW REPORTED LT COFFEEMAKER SMOKING. EWR MX REMOVED AND REPLACED LT COFFEEMAKER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10CL136](https://openairdocs.org/sdr/C2XA10CL136.md): Button · faulty · Aug 24, 2010 · N13975 · Emb EMB145LR · Extinguishing System > CLE - FLT 2339 - THE CREW REPORTED THE BAG EXTINGUISHER PUSH BUTTON DID NOT ILLUMINATE DURING FIRE DETECTION TEST. MAINTENANCE INSPECTED AND REPLACED THE BAG EXTINGUISHER PUSH BUTTON. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10TY113](https://openairdocs.org/sdr/C2XA10TY113.md): Cap · corroded · Aug 15, 2010 · N13975 · Emb EMB145LR · Fuselage Miscellaneous Structure > RIGHT LAV TOP CAP HAS SURFACE CORROSION AT CARBON CROSS BEAM. REMOVED AND REPLACED RT TOP CAP IAW EMB SRM 51-40-09. - [SDR C2XA10IA200](https://openairdocs.org/sdr/C2XA10IA200.md): Light · malfunctioned · Jul 12, 2010 · N13975 · Emb EMB145LR · Emergency Lighting > IAH - FLIGHT 2804, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE RESET THE ELECTRICAL SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10RI054](https://openairdocs.org/sdr/C2XA10RI054.md): Inverter · inoperative · Apr 15, 2010 · N13975 · Emb EMB145LR · Emergency Lighting > FLIGHT 2074 - EWR - FLIGHT CREW REPORTED NR 1 FLOOR EMERGENCY LIGHT STRIP AND SERVICE DOOR EXIT LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA10CL033](https://openairdocs.org/sdr/C2XA10CL033.md): Inverter · inoperative · Feb 21, 2010 · N13975 · Emb EMB145LR · Emergency Lighting > DURING ROUTINE MAINTENANCE THE NR 4 AND 5 EMERGENCY AISLE PATH LIGHT STRIPS WERE FOUND INOPERATIVE. THE NR 5 EMERGENCY LIGHT INVERTER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA10CL030](https://openairdocs.org/sdr/C2XA10CL030.md): Connector · loose · Jan 24, 2010 · N13975 · Emb EMB145LR · Landing Gear System Wiring > CLE FLT 2866 THE CREW REPORTED THE LANDING GEAR HANDLE AND GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND RESECURED THE NOSE LANDING GEAR PROXIMITY SWITCH HARNESS CONNECTOR. THE NOSE STRUT WAS ALSO SERVICED. - [SDR C2XA10TY008](https://openairdocs.org/sdr/C2XA10TY008.md): Battery · defective · Jan 9, 2010 · N13975 · Emb EMB145LR · Emergency Lighting > EMERGENCY LIGHT CIRCUIT BREAKER POPPING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 1, MOUNT TRAY AND CONNECTOR IAW EMB145 AMM 33-50-04, 20-13-07 AND 20-50-00. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. BATTERY CHARGER ASSY PN 11-0049, - [SDR C2XA09RI164](https://openairdocs.org/sdr/C2XA09RI164.md): Light · inoperative · Sep 19, 2009 · N13975 · Emb EMB145LR · Emergency Lighting > RIC MX - DURING ROUTINE INSPECTION, MX FOUND EMERGENCY LIGHT STRIP BY SEATS 1A AND 2A INOPERATIVE. RIC MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA09TY039](https://openairdocs.org/sdr/C2XA09TY039.md): Light · inoperative · Mar 1, 2009 · N13975 · Emb EMB145LR · Emergency Lighting > AIRCRAFT IN FOR A OVERNIGHT INSPECTION WHEN THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-07. OPS CHECK GOOD AND WAS RELEASED. - [SDR C2XA09IA010](https://openairdocs.org/sdr/C2XA09IA010.md): Connector · dirty · Jan 1, 2009 · N13975 · Emb EMB145LR · Landing Gear System Wiring > ON TAKEOFF ROLL THE CREW REPORTED RELAYS CLICKING, AND AFTER TAKEOFF CLICKED AGAIN VERY LOUD AND A JOLT WAS FELT THROUGH THE YOLK AND RUDDER PEDALS. AT 12000 FT, THE LOUD CLICKING OCCURRED SEVERAL TIMES AND RECEIVED EMERG LIGHTS NOT ARMED AND ELEC EMERG ABNOR - [SDR C2XA08RI141](https://openairdocs.org/sdr/C2XA08RI141.md): Wire · loose · Sep 26, 2008 · N13975 · Emb EMB145LR · Light System Wiring > RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND FORWARD EMERGENCY LIGHT STRIP NOT ILLUMINATING. MX RECONNECTED LOOSE WIRING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA08RI142](https://openairdocs.org/sdr/C2XA08RI142.md): Wire · disconnected · Sep 26, 2008 · N13975 · Emb EMB145LR · Light System Wiring > RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MX FOUND ONE WIRE DISCONNECTED FROM THE SPLICE. MX RECONNECTED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA08SH101](https://openairdocs.org/sdr/C2XA08SH101.md): Firewall · cracked · Aug 9, 2008 · N13975 · Emb EMB145LR · APU Cowling/Containment > SHV - DURING C-CHECK IT WAS FOUND THAT THE APU FIREWALL WAS CRACKED AROUND RIVETS AT 3 O`CLOCK POSITION. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5330-01827. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) - [SDR C2XA07IA251](https://openairdocs.org/sdr/C2XA07IA251.md): Unknown · odor · Dec 19, 2007 · N13975 · Emb EMB145LR · Air Distribution System > FLIGHT 2875 IAH-MFE, THE CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION AND SYSTEM CHECKS. THE BURNING SMELL COULD NOT BE DUPLICATED AND THE DISCREPANCY - [SDR C2XA07RI098](https://openairdocs.org/sdr/C2XA07RI098.md): Wire · broken · Nov 11, 2007 · N13975 · Emb EMB145LR · Light System Wiring > FLT 3035 - EWR - CREW REPORTED 3 AFT EMERGENCY LIGHT STRIPS INOPERATIVE. EWR MX FOUND BROKEN WIRE AT EMERGENCY LIGHT NR 8. ME REPAIRED WIRING AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07IA169](https://openairdocs.org/sdr/C2XA07IA169.md): Battery Pack · inoperative · Jul 9, 2007 · N13975 · Emb EMB145LR · Emergency Lighting > BAN - DURING MAINTENANCE INSPECTION THE NUMBER 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T - [SDR C2XA06CL075](https://openairdocs.org/sdr/C2XA06CL075.md): Light · inoperative · Sep 21, 2006 · N13975 · Emb EMB145LR · Emergency Lighting > CLE FLIGHT NR 2351 - THE CREW REPORTED THE AISLE PATH EMERGENCY LIGHT STRIP AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA06SH087](https://openairdocs.org/sdr/C2XA06SH087.md): Stringer · corroded · Sep 1, 2006 · N13975 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > SHV - DURING C-CHECK STR 21L HAS CORROSION BETWEEN FR12-13. MAINTENANCE REMOVED AND REPLACED STR 21 FR 8-13 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA06SH085](https://openairdocs.org/sdr/C2XA06SH085.md): Stringer · corroded · Sep 1, 2006 · N13975 · Emb EMB145LR · Fuselage Main, Longeron/Stringer > SHV - DURING C-CHECK STR 21R HAS CORROSION BETWEEN FR 12-13. MAINTENANCE REMOVED DAMAGE STR & SPLICED IN NEW SECTION 21R FR 10-13 IAW EMB 145 SRM 53-00-03 ITEM 2 CPE 11001-1 FIGURE 201. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. - [SDR C2XA06SH084](https://openairdocs.org/sdr/C2XA06SH084.md): Tie Clip · corroded · Aug 22, 2006 · N13975 · Emb EMB145LR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 65 BETWEEN STRINGERS 15 AND 16 L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA06CL037](https://openairdocs.org/sdr/C2XA06CL037.md): Door · broken · Apr 3, 2006 · N13975 · Emb EMB145LR · Doors > CLE FLIGHT NR 2541, CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE. AIR RETURN. MAINTENANCE INSPECTED FOUND AIR SERVICE CHECK VALVE DOOR BROKEN. DOOR ASSEMBLY REMOVED AND REPLACED. ALL OPERATIONAL CHECKS REPORTED GOOD. - [SDR C2XA06IA050](https://openairdocs.org/sdr/C2XA06IA050.md): Light · inoperative · Mar 25, 2006 · N13975 · Emb EMB145LR · Emergency Lighting > CRP - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING STRIP AT SEAT 14A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER - [SDR C2XA05CL098](https://openairdocs.org/sdr/C2XA05CL098.md): Ballast · burned · Dec 13, 2005 · N13975 · Emb EMB145LR · Passenger Compartment Lighting > DURING ROUTINE MAINTENANCE THE GALLEY HAD A BURNING ODOR. MAINTENANCE INSPECTED AND FOUND THE GALLEY LIGHT BALLAST BURNED. THE BALLAST WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA05BT054](https://openairdocs.org/sdr/C2XA05BT054.md): Odor · detected · Aug 2, 2005 · N13975 · Emb EMB145LR · Air Distribution System > CREW REPORTED, ODOR OF BURNING PLASTIC OCCURRED IN CRUISE, TURNED OFF RECIRCULATING FAN, ODOR WENT AWAY. ODOR ONLY IN COCKPIT. INSPECTED CABIN AND COCKPIT FOR BURNING ODOR. NO UNUSUAL ODOR. PERFORMED OPERATIONAL CHECK OF RECIRCULATION FAN IAW EMB145 MM 21-0 - [SDR C2XA04IA145](https://openairdocs.org/sdr/C2XA04IA145.md): Wire · broken · Nov 20, 2004 · N13975 · Emb EMB145LR · Light System Wiring > IAH - FLIGHT 2890, DURING THE PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NO - [SDR C2XA04SH474](https://openairdocs.org/sdr/C2XA04SH474.md): Floorbeam · corroded · Aug 1, 2004 · N13975 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT THE CROSSBEAM BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH472](https://openairdocs.org/sdr/C2XA04SH472.md): Floorbeam · corroded · Jul 30, 2004 · N13975 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10, STEP 3 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV - [SDR C2XA04SH468](https://openairdocs.org/sdr/C2XA04SH468.md): Floorbeam · corroded · Jul 27, 2004 · N13975 · Emb EMB145LR · Fuselage Main, Floor Beam > SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA04SH466](https://openairdocs.org/sdr/C2XA04SH466.md): Battery · discharged · Jul 22, 2004 · N13975 · Emb EMB145LR · Emergency Lighting > DURING C-CHECK THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY, THE ENSUUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA03CL044](https://openairdocs.org/sdr/C2XA03CL044.md): Harness · shorted · Feb 18, 2003 · N13975 · Emb EMB145LR · Passenger Compartment Lighting > LIT FLIGHT#2474 THE CREW REPORTED THE CABIN LIGHT AT ROW 6A SHORTED OUT CAUSING SPARKS AND ELECTRICAL SMELL IN THE CABIN.MAINTENANCE INSPECTED AND REPLACED THE WIRING HARNESS ASSEMBLY FOR ROW 6A LIGHTING.OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA02TY167](https://openairdocs.org/sdr/C2XA02TY167.md): Fitting · bent · Nov 8, 2002 · N13975 · Emb EMB145LR · Ailerons > TYS. During a scheduled inspection, the left aileron PCA fitting attach lug was found bent. Maintenance removed and replaced the fitting. I/A/W-EC5750-01177. The repair was satisfactory and the aircraft will be released upon complection of the check. - [SDR C2XA02TY166](https://openairdocs.org/sdr/C2XA02TY166.md): Intake · damaged · Nov 6, 2002 · N13975 · Emb EMB145LR · Engine Air Intake System > DURING A SCHEDULED 2-C INSPECTION, THE NR 1 ENGINE INLET INNER SKIN WAS FOUND PROTRUDING ON AFT SIDE OF SKIN AT 4:00 AND 10:00 O`CLOCK POSITIONS. MAINT. MEASURED THE PROTRUDING SKINS ON THE AFT SIDE.THEY RECONTOURED THE AFFECTED AREA TO THE ORIGINAL SHAPE AN Next page: https://openairdocs.org/aircraft/N13975/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 = 'N13975' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N13975/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.