# Service difficulty reports: N26141 A list on [N26141](https://openairdocs.org/aircraft/N26141.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASOA20130818155](https://openairdocs.org/sdr/ASOA20130818155.md): Battery Pack · discharged · Aug 18, 2013 · N26141 · Emb EMB145XR · Emergency Lighting > DURING MX INSPECTION, THE 2 EMERGENCY LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120614055](https://openairdocs.org/sdr/ASOA20120614055.md): Shuttle Valve · leaking · Jun 14, 2012 · N26141 · Emb EMB145XR · Landing Gear Brake System > THE CREW REPORTED HYD SYS NR 1 DROPPED INTO AMBER RANGE IN FLIGHT AND RECEIVED A WARNING MESSAGE ON THE EICAS. THE ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 AND NR 4 BRAKE SHUTTLE VALVES. SERVICED HYD SYS AND OPS CHECKS WER - [SDR ASOA2011121000033](https://openairdocs.org/sdr/ASOA2011121000033.md): Skin · dented · Dec 10, 2011 · N26141 · Emb EMB145XR · Fuselage Main, Plate/Skin > DURING C-CHECK (FRAME 22/STRINGER 18L) DENT/PROTRUSION IN FUSELAGE. MX PERFORMED REPAIR WITH INSTALLED FABRICATED DOUBLER BETWEEN FRAME 22 AND 23 STRINGER 17L AND 18L IAW SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201112100022](https://openairdocs.org/sdr/ASOA201112100022.md): Sill · corroded · Dec 10, 2011 · N26141 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK CENTER SERVICE DOOR SILL CORRODED. MX R & R CENTER SERVICE DOOR SILL IAW SRM 51-90-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2011121000011](https://openairdocs.org/sdr/ASOA2011121000011.md): Beam · corroded · Dec 10, 2011 · N26141 · Emb EMB145XR · Fuselage Main, Structure > DURING C-CHECK, REMOVED CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68 TO FOM. MX R & R CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68 IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201111261010](https://openairdocs.org/sdr/ASOA201111261010.md): Skin · corroded · Nov 26, 2011 · N26141 · Emb EMB145XR · Fuselage Main, Plate/Skin > DURING C-CHECK SKIN SPLICE BETWEEN (FRAME 13 AND 14 STRINGER 21L-20R) HAS CORROSION. MX PERFORMED REPAIR ON SKIN SPLICE AT FRAME 13-14, STRINGER 20L-20R IAW SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11CL165](https://openairdocs.org/sdr/C2XA11CL165.md): Sensor · faulty · Jul 11, 2011 · N26141 · Emb EMB145XR · Pitot/Static Anti-Ice System > ORD FLT 5814 THE CREW REPORTED A PITOT HEAT 3 FAIL MESSAGE ALONG WITH A ELECTRIC SMELL. MAINTENANCE REPLACED THE NR 3 PITOT CURRENT SENSOR. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA11IA098](https://openairdocs.org/sdr/C2XA11IA098.md): O-Ring · leaking · May 20, 2011 · N26141 · Emb EMB145XR · Pneumatic Distribution System > IAH - FLIGHT 3136, DURING CLIMB THE CREW REPORTED A BLEED TWO LEAK INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE OT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE O-RINGS AT JOINT 24, OPERATIONALLY AND LEAK CHECKED - [SDR C2XA11IA096](https://openairdocs.org/sdr/C2XA11IA096.md): O-Ring · failed · May 18, 2011 · N26141 · Emb EMB145XR · Pneumatic Distribution System > FLIGHT 2049, THE CREW REPORTED A BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO GDL WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BLEED O-RINGS AT JOINTS 10,18 - [SDR C2XA10SH111](https://openairdocs.org/sdr/C2XA10SH111.md): Skin · cracked · Mar 27, 2010 · N26141 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK SEVERAL EXTERNAL SKIN CRACKED AROUND RIVET HEADS AT FRAME 79 BETWEEN STR'S 1R-9R. MAINTENANCE PERFORMED REPAIR OF SEVERAL EXTERNAL SKIN CRACKS AROUND RIVET HEADS AT FRAME 79 BETWEEN STR'S 1R-9R. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE - [SDR C2XA10SH110](https://openairdocs.org/sdr/C2XA10SH110.md): Skin · cracked · Mar 27, 2010 · N26141 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK SEVERAL EXTERNAL SKIN CRACKED AROUND RIVET HEADS AT FRAME 78 BETWEEN STR'S 1R-7R. MAINTENANCE PERFORMED REPAIR OF SEVERAL EXTERNAL SKIN CRACKS AROUND RIVET HEADS AT FRAME 78 BETWEEN STR'S 1R-7R IAW EC5330-02091. THE AIRCRAFT WAS APPROVED - [SDR C2XA09IA249](https://openairdocs.org/sdr/C2XA09IA249.md): Switch · malfunctioned · Oct 4, 2009 · N26141 · Emb EMB145XR · Cabin Cooling System > IAH - FLIGHT 4920, THE CREW REPORTED A PACK 1 OVERLOAD. THE AIRCRAFT DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PACK OVERTEMP SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETU - [SDR C2XA09CL129](https://openairdocs.org/sdr/C2XA09CL129.md): Switch · faulty · Oct 4, 2009 · N26141 · Emb EMB145XR · Cabin Cooling System > IAH FLT 2187 - THE CREW REPORTED A PACK 1 OVERLOAD MESSAGE IN FLIGHT. ALSO REPORTED A NR 1 ENGINE ANTI/ICE FAIL MESSAGE INTERMITTENTLY. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE PACK 1 OVER TE - [SDR C2XA09CL118](https://openairdocs.org/sdr/C2XA09CL118.md): Hydraulic System · low · Sep 21, 2009 · N26141 · Emb EMB145XR · Hydraulic System, Main > EWR - FLT 2403 - THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE NR 1 HYDRAULIC SYSTEM. - [SDR C2XA09CL020](https://openairdocs.org/sdr/C2XA09CL020.md): Switch · faulty · Feb 17, 2009 · N26141 · Emb EMB145XR · Cabin Cooling System > EWR FLIGHT 2394 - THE CREW REPORTED A NR 1 PACK FAIL OUT OF EWR AT 15000. ALSO RECEIVED A WING 1 A/ICE FAIL. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 PACK OVERPRESSURE SWITCH. ALSO REPL - [SDR C2XA08RI113](https://openairdocs.org/sdr/C2XA08RI113.md): Line · leaking · Aug 1, 2008 · N26141 · Emb EMB145XR · Pneumatic Distribution System > FLIGHT 2943 - EWR - FLIGHT CREW PERFORMED AIR RETURN DUE TO BLEED NR 2 LEAK ON EICAS DURING CLIMBOUT. MESSAGE CLEARED AFTER COMPLETION OF QRH PROCEDURES. CREW LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE RESEALED BLEED LINE BETWEEN FRAME 70 AND 74. MAINTENANC - [SDR C2XA08RI048](https://openairdocs.org/sdr/C2XA08RI048.md): Controller · defective · Apr 5, 2008 · N26141 · Emb EMB145XR · Windshield/Door Rain/Ice Removal > FLIGHT 2784 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT DURING CRUISE FLIGHT. THEN SMELL WENT AWAY WHEN WINDSHIELD HEAT WAS TURNED OFF. EWR MX REMOVED AND REPLACED WINDSHIELD CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCR - [SDR C2XA07CL106](https://openairdocs.org/sdr/C2XA07CL106.md): Connector · loose · Dec 24, 2007 · N26141 · Emb EMB145XR · Light System Wiring > DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHT ON THE MAIN CABIN DOOR WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE CONNECTOR ON THE MAIN CABIN DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA07CL075](https://openairdocs.org/sdr/C2XA07CL075.md): Selector · faulty · Sep 5, 2007 · N26141 · Emb EMB145XR · Trailing Edge Flap Control System > CLE FLIGHT 2197 THE CREW REPORTED AFTER TAKEOFF THE GEAR RETRACTED NORMALLY BUT RECEIVED A LANDING GEAR WARNING CONTINUOUSLY. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR CONTROL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA06BT052](https://openairdocs.org/sdr/C2XA06BT052.md): Connector · loose · Nov 22, 2006 · N26141 · Emb EMB145XR · Emergency Lighting > EWR LOG SQUAWK FWD OVERHEAD EXIT SIGN LIGHT IN AISLE INOP. RESECURED LOOSE CONNECTOR FOR EXIT SIGN LIGHT IAW EMB145 AMM 33-50-08. OPS CHECK GOOD. - [SDR C2XA06IA181](https://openairdocs.org/sdr/C2XA06IA181.md): Control Panel · burned · Nov 15, 2006 · N26141 · Emb EMB145XR · Ice/Rain Protection System Wiring > MCO - FLIGHT 3162, THE CREW REPORTED SMOKE & ELECTRICAL FIRE SMELL CONFINED TO THE COCKPIT AT 11,000 FEET WHICH DISAPPEARED AFTER THE RECIRC FAN WAS TURNED OFF, THE CREW PERFORMED AN EMERGENCY DESCENT AND LANDED AT MCO WITHOUT INCIDENT. MAINTENANCE INSPECTED - [SDR C2XA06IA043](https://openairdocs.org/sdr/C2XA06IA043.md): Electronic Unit · inoperative · Mar 20, 2006 · N26141 · Emb EMB145XR · Landing Gear Retraction/Extension System > IAH - FLIGHT 2856, THE CREW REPORTED A LANDING GEAR AURAL WARNING AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RET - [SDR C2XA05CL080](https://openairdocs.org/sdr/C2XA05CL080.md): Light · shorted · Sep 11, 2005 · N26141 · Emb EMB145XR · Passenger Compartment Lighting > MCI FLIGHT NR 2484, THE CREW REPORTED THE PSU READING LIGHT AT SEAT 19B GOT VERY HOT AND OMITTED A HAZE. THE AIRCRAFT WAS RELEASED IAW MEL 25-60-02/4. MAINTENANCE INSPECTED AND REPLACED THE PSU READING LIGHT AT SEAT 19B. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XATY172](https://openairdocs.org/sdr/C2XATY172.md): Flashlight · inoperative · Nov 6, 2004 · N26141 · Emb EMB145XR · Emergency Equipment > DURING 4A INSPECTION, MAINTENANCE FOUND THE EMERGENCY FLASH LIGHT INOP. MAINTENANCE REPLACED THE EMERGENCY FLASH LIGHT AND OPS CHECK WAS GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT WAS RELEASED FOLLOWING THE SCHEDULED INSPECTION. - [SDR C2XA04TY171](https://openairdocs.org/sdr/C2XA04TY171.md): Bulb · inoperative · Nov 6, 2004 · N26141 · Emb EMB145XR · Emergency Lighting > DURING 4A INSPECTION, MAINTENANCE FOUND THE GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE BULB AND OPS CHECK WAS GOOD IAW EMB 145XR AMM 33-50-10. AIRCRAFT RELEASED FOLLOWING THE COMPLETION OF THE SCHEDULED CHECK. - [SDR C2XA03IA088](https://openairdocs.org/sdr/C2XA03IA088.md): Control Unit · malfunctioned · Sep 1, 2003 · N26141 · Emb EMB145XR · Landing Gear Retraction/Extension System > IAH- ON CLIMB THE CREW NOTED THAT THE LANDING GEAR AURAL WARNING ACTIVATED WHEN THE GEAR RETRACTED. THE CREW DID AN AIR RETURN TO IAH, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, AND, THE AIRCRAFT WAS APR ## 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 = 'N26141' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N26141/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.