# Service difficulty reports: N25134 A list on [N25134](https://openairdocs.org/aircraft/N25134.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASOA202004164013](https://openairdocs.org/sdr/ASOA202004164013.md): Acm · frozen · Apr 16, 2020 · N25134 · Emb EMB145XR · Cabin Cooling System > IAH - DURING FLIGHT THE CREW REPORTED THAT THEY SMELLED BURNING / SMOKE. RAN QRH TURNED OFF THE RECIRC FAN AND THE SMELL DISSIPATED. THE AIRCRTAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 ACM, OPERATIONALLY TESTED WITH - [SDR ASOA2019100294054](https://openairdocs.org/sdr/ASOA2019100294054.md): Light · inoperative · Sep 27, 2019 · N25134 · Emb EMB145XR · Emergency Lighting > FLIGHT 4087, THE CREW REPORTED THAT THE EMERGENCY STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201906284037](https://openairdocs.org/sdr/ASOA201906284037.md): Acm · failed · Jun 28, 2019 · N25134 · Emb EMB145XR · Cabin Cooling System > IAH - FLIGHT 4403, THE CREW REPORTED SMOKE IN THE CABIN, SUSPECT ACM. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE #2 ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA2018053025139](https://openairdocs.org/sdr/ASOA2018053025139.md): Charger · inoperative · May 23, 2018 · N25134 · Emb EMB145LR · Emergency Lighting > DURING A MX INSPECTION, THE CEILING EMERGENCY LIGHT AT PANEL 253CLC AND 263ALC WERE FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 3 BATTERY CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA201804187066](https://openairdocs.org/sdr/ASOA201804187066.md): Mount · damaged · Apr 18, 2018 · N25134 · Emb EMB145XR · Engine Mount Section > DURING A C-CHECK, THE RT SIDE ENGINE YOLK FWD. UPPER AFT FITTING HAS MECHANICAL DAMAGE INSIDE THE HAT BUSHING OF THE YOLK FITTING. MAINTENANCE REMOVED AND REPLACED THE YOLK FITTING IAW EA48-2018-026. - [SDR ASOA201804117058](https://openairdocs.org/sdr/ASOA201804117058.md): Skin · delaminated · Apr 11, 2018 · N25134 · Emb EMB145XR · Trailing Edge Flaps > LT INBOARD FLAP DELAMINATED AREAS ON THE UPPER AND LOWER SIDES. REPAIRED LT INBOARD FLAP DELAMINATED AREAS IAW SRM 57-52-00. REPAIR IS CONSIDERED MAJOR PER SOP 5702. - [SDR ASOA20151007182](https://openairdocs.org/sdr/ASOA20151007182.md): Support · corroded · Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK THE WASTE DRAIN SUPPORT WAS FOUND TO BE CORRODED BETWEEN FRAMES 60-61 STRINGERS 18R-20R. MAINTENANCE R & R THE SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20151007181](https://openairdocs.org/sdr/ASOA20151007181.md): Beam · corroded · Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Main, Structure > DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20151007180](https://openairdocs.org/sdr/ASOA20151007180.md): Floor Support · corroded · Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Miscellaneous Structure > DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20150802042C](https://openairdocs.org/sdr/ASOA20150802042C.md): Light · odor · Aug 2, 2015 · N25134 · Emb EMB145XR · Passenger Compartment Lighting > THE CREW REPORTED ELECTRICAL BURNING ODOR AT ROW 4CD IN LIGHT AREA. OPEN - [SDR ASOA20150302004](https://openairdocs.org/sdr/ASOA20150302004.md): Skin · dented · Feb 28, 2015 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > FUSELAGE DENT BETWEEN 7-8 AND STR 11L-13L. CUT OUT DENT INSTALLED FILLER, DOUBLER AND TRIPLER. - [SDR ASOA20150302003](https://openairdocs.org/sdr/ASOA20150302003.md): Skin · dented · Feb 28, 2015 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > 2 DENTS ON FUSELAGE BETWEEN FRM 7 & 8, STR 11L-13L. CUTOUT DAMAGED SKIN INSTALLED FILLER DOUBLER AND TRIPLER IAW ETD2014-145-060373. - [SDR ASOA20140923082C](https://openairdocs.org/sdr/ASOA20140923082C.md): Socket · burned · Sep 23, 2014 · N25134 · Emb EMB145XR · Passenger Compartment Lighting > THE CREW REPORTED STRONG ELECTRICAL BURNING ODOR WITH BOTH PACKS RUNNING. MAINTENANCE FOUND BURNED LIGHT SOCKET AT ROW 5A. THE ACFT WAS RELEASED FOR SERVICE IAW MEL. SUPPLEMENT TO FOLLOW. - [SDR ASOA20130919374](https://openairdocs.org/sdr/ASOA20130919374.md): Tank · chafed · Sep 19, 2013 · N25134 · Emb EMB145XR · Fuel Storage > DURING C-CHECK, FOUND A CHAFE IN THE VENTRAL TANK. MX BLENDED THE CHAFE AREA AND FOUND TO BE IN LIMITS. PLACED A DOUBLER OVER THE AREA AFTER FABRICATING THE PART, ALLODINED AND PAINTED IAW EC2810-01053. PERFORMED LEAK CHECKS IAW EC 2810-01053. NO LEAKS N - [SDR ASOA20130420031](https://openairdocs.org/sdr/ASOA20130420031.md): Wire Harness · faulty · Apr 20, 2013 · N25134 · Emb EMB145XR · Light System Wiring > THE CREW REPORTED A BURNING ODOR COMING FROM FRONT OF CABIN. MX INSPECTED AND REPLACED WIRING HARNESS FOR SEAT 1A SIDEWALL LIGHT. THEY ALSO REPLACED THE SIDEWALL LIGHT. OPS CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE. - [SDR C2XA11RI169](https://openairdocs.org/sdr/C2XA11RI169.md): Fire Loop · defective · Oct 18, 2011 · N25134 · Emb EMB145XR · Fire Detection > FLT 4489 EWR-JAX CREW REPORTED E1 FIRE DETECT MESSAGE ON EICAS DURING TAKEOFF. CREW PERFORMED AIR RETURN BACK TO EWR WITHOUT INCIDENT. EWR MX PERFORMED ALL ELECTRICAL CHECKS OUTLINED IN FIM 26-11-00-810-803-A WITH NO FAULTS NOTED. MX REMOVED AND REPLACED EN - [SDR C2XA11SH142](https://openairdocs.org/sdr/C2XA11SH142.md): Stringer · corroded · Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Longeron/Stringer > SHV - DURING C-CHECK STRINGER 21R HAS CORROSION BETWEEN FRAMES 7-13. MAINTENANCE REMOVED AND REPLACED STRINGER 21R BETWEEN FRAMES 7-13 IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA11SH141](https://openairdocs.org/sdr/C2XA11SH141.md): Skin · cracked · Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 6R-7R. DAMAGE FOUND TO BE AT STRINGER 5R-6R AND NOT STRINGER 6R-7R. MAINTENANCE PERFORMED REPAIR TO EXTERNAL FUSELAGE SKIN AT FRAME 79 STRINGER 5R-6R AND INITIATED DMI IAW EC5330-02483. - [SDR C2XA11SH140](https://openairdocs.org/sdr/C2XA11SH140.md): Skin · cracked · Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79 STRINGER 4R-5R. DAMAGE WAS FOUND TO BE AT STRINGER 3R-4R AND NOT STRINGER 4R-5R. MAINTENANCE PERFORMED REPAIR TO EXTERNAL FUSELAGE SKIN AT FRAME 79 STRINGER 3R-4R AND INITIATED DMI IAW EC5330-024 - [SDR C2XA11SH139](https://openairdocs.org/sdr/C2XA11SH139.md): Skin · cracked · Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 78 STRINGER 7R-8R. DAMAGE WAS FOUND TO BE AT STRINGER 5R-6R AND NOT 7R-8R. MAINTNENANCE PERFORMED REPAIR TO EXTERNAL FUSELAGE AT FRAME 78 STRINGER 5R-6R AND INITIATED DMI IAW EC5330-02483. THE AIRC - [SDR C2XA11SH138](https://openairdocs.org/sdr/C2XA11SH138.md): Skin · cracked · Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > SHV - DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 78 STRINGER 6R-7R. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN AT FRAME 78 STRINGER 6R-7R IAW EC5330-02483 AND INITIATED DMI. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10IA262](https://openairdocs.org/sdr/C2XA10IA262.md): Outflow Valve · inoperative · Sep 27, 2010 · N25134 · Emb EMB145XR · Pressure Regulator/Outflow Valve > IAH - FLIGHT 2601, THE CREW REPORTED THE AUTO PRESSURIZATION TO BE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, A - [SDR C2XA10IA159](https://openairdocs.org/sdr/C2XA10IA159.md): Windshield · cracked · May 25, 2010 · N25134 · Emb EMB145XR · Flight Compartment Windows > QRO, FLIGHT 2100, THE CREW REPORTED THAT THE CAPTAINS WINDSHIELD INNER PLY CRACKED ON CLIMB. THE AIRCRAFT RETURNED TO QRO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE CAPTAINS WINDSHIELD, OPERATIONAL AND - [SDR C2XA10CL068](https://openairdocs.org/sdr/C2XA10CL068.md): Screw · backed out · May 10, 2010 · N25134 · Emb EMB145XR · Emergency Exits > DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WAS FOUND HARD TO OPEN. MAINTENANCE INSPECTED AND FOUND THE AFT UPPER SHROUD BRACKET SCREW HAD BACKED OUT AND WAS CATCHING ON THE DOOR FRAME. THE SCREW WAS REPLACED AND OPERATIONAL CHECKS OF THE EME - [SDR C2XA10CL044](https://openairdocs.org/sdr/C2XA10CL044.md): Tube · cracked · Mar 15, 2010 · N25134 · Emb EMB145XR · Pneumatic Distribution System > CLE FLT 2958 THE CREW REPORTED A BLEED LEAK NR 1 ENGINE AND NR 1 PACK VALVE FAILURE ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT PACK BLEED TUBE BETWEEN THE PACK VALVE AND DUAL TEMP CONTRO - [SDR C2XA10SH086](https://openairdocs.org/sdr/C2XA10SH086.md): Attach Bracket · corroded · Mar 7, 2010 · N25134 · Emb EMB145XR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK BAGGAGE COMPARTMENT RAMP PANEL FWD ATTACHMENT BRACKET AT FRAME 65 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR OF FRAME BAGGAGE COMPARTMENT RAMP PANEL FWD ATTACHMENT BRACKET AT FRAME 65 IAW EMB-145XR SRM 51-40 - [SDR C2XA10SH085](https://openairdocs.org/sdr/C2XA10SH085.md): Door Frame · corroded · Mar 7, 2010 · N25134 · Emb EMB145XR · Fuselage Main, Structure > SHV - DURING C-CHECK BAGGAGE DOOR UPPER CUTOUT HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 65. MAINTENANCE PERFORMED REPAIR TO BAGGAGE DOOR UPPER CUTOUT IAW EC5320-01535. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA10SH079](https://openairdocs.org/sdr/C2XA10SH079.md): Floor Support · corroded · Feb 28, 2010 · N25134 · Emb EMB145XR · Fuselage Miscellaneous Structure > SHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) FRAME 20 TO 23. MAINTENANCE INSTALLED REPAIR DOUBLER RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 51-40-02 & EC5320-01443. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09TY275](https://openairdocs.org/sdr/C2XA09TY275.md): Outflow Valve · malfunctioned · Dec 24, 2009 · N25134 · Emb EMB145XR · Pressure Regulator/Outflow Valve > PRESSURE FLUCTUATING BETWEEN 8000-8300 AT 37000 FT. FLIGHT DIVERTED. AUTO AND MANUAL PRESSURIZATION INOP COULD NOT RECOVER CONTROL W/ THE MANUAL SYSTEM PER CHECK LIST. REMOVED AND REPLACED PNEUMATIC AND ELECTRO PNEUMATIC OUTFLOW VALVES IAW 21-31-03 AND 21-3 - [SDR C2XA09IA244](https://openairdocs.org/sdr/C2XA09IA244.md): Battery Pack · discharged · Sep 23, 2009 · N25134 · Emb EMB145XR · Emergency Lighting > LCH - DURING MX INSPECTION A GALLEY AREA EMERGENCY EXIT LIGHT WAS FOUND NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR C2XA09TY127](https://openairdocs.org/sdr/C2XA09TY127.md): Light · inoperative · Jun 24, 2009 · N25134 · Emb EMB145XR · Emergency Lighting > RT EMERGENCY SIDE WALL EXIT LIGHT AT 12BC INOP. EXIT MARKER SIGN ASSY WAS REMOVED AND REPLACED. - [SDR C2XA08RI026](https://openairdocs.org/sdr/C2XA08RI026.md): Control Unit · defective · Feb 28, 2008 · N25134 · Emb EMB145XR · Landing Gear Retraction/Extension System > RIC - DURING A-CHECK, AIRCRAFT FAILED LANDING GEAR AIR-GROUND CHECK. RIC MX PERFORMED TROUBLESHOOTING AND FOUND LGEU NOT WORKING PROPERLY. MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. - [SDR C2XA07RI105](https://openairdocs.org/sdr/C2XA07RI105.md): Tat Probe · inoperative · Dec 7, 2007 · N25134 · Emb EMB145XR · Outside Air Temperature Indicator/Sensor > FLT 2993 - EWR - CREW REPORTED TAT 2 HEAT INOP MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 TAT PROBE IAW EMB145XR AMM 34-15-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. - [SDR C2XA07CL081](https://openairdocs.org/sdr/C2XA07CL081.md): Control Unit · faulty · Sep 20, 2007 · N25134 · Emb EMB145XR · Landing Gear Position and Warning > CLE FLIGHT 2178 - THE CREW REPORTED A CLICKING NOISE FROM THE NOSE WHEN THE GEAR WAS RETRACTED AND THE MAIN GEAR CYCLED BETWEEN INTRANSIT AND LOCKED FOR ABOUT 15 SECONDS THEN LOCKED. GEAR EXTENSION NORMAL. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR - [SDR C2XA07TY002](https://openairdocs.org/sdr/C2XA07TY002.md): Skin · damaged · Jan 23, 2007 · N25134 · Emb EMB145XR · Fuselage Main, Plate/Skin > AIRCRAFT HAD BIRDSTRIKE WHILE AIRBORNE AT 210 KNOTS AND 5000 FEET, AIRCRAFT LANDED UNEVENTFULLY. AFTER TEMPORARY REPAIR AND FERRY FLIGHT EWR TO TYS, TYS MAINTENANCE REPAIRED DAMAGE TO FRAMES 1A THROUGH FRAME 3 PART NUMBERS: 145-21705-403, 145-51202, AND 145-5 - [SDR C2XA06CL094](https://openairdocs.org/sdr/C2XA06CL094.md): Charger · broken · Dec 4, 2006 · N25134 · Emb EMB145XR · Emergency Lighting > CLE FLIGHT 3150 THE CREW REPORTED THE AFT F/A FLASHLIGHT CHARGER WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT CHARGER. OPERATIONAL CHECKS WERE GOOD. - [SDR C2XA06TY045](https://openairdocs.org/sdr/C2XA06TY045.md): Bracket · gouged · Jul 25, 2006 · N25134 · Emb EMB145XR · Ailerons > TYS DURING A 2C INSPECTION THE LEFT AILERON PCA BRACKET WAS MISSING A BUSHION AND BRACKET WAS GOUGED. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB 145XR EC 5770-01177 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE C-CH - [SDR C2XA06TY042](https://openairdocs.org/sdr/C2XA06TY042.md): Bracket · damaged · Jul 13, 2006 · N25134 · Emb EMB145XR · Aileron Control System > PCA BRACKET MISSING BUSHINGS & DISPLACED METAL IN BUSHING HOLES. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177 REV B AND EMB145 SRM 51-40-02. - [SDR C2XA06TY043](https://openairdocs.org/sdr/C2XA06TY043.md): Bracket · damaged · Jul 13, 2006 · N25134 · Emb EMB145XR · Ailerons > LT AILERON DAMPNER BRACKET DAMAGED. REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW EMB145 SRM 51-40-02 & CPM51-21-06. - [SDR C2XA04SD002](https://openairdocs.org/sdr/C2XA04SD002.md): Glowstrip · cracked · Jul 1, 2004 · N25134 · Emb EMB145XR · Emergency Equipment > SDF - DURING 3A CHECK INSPECTION FOUND CABIN FLOOR FWD EMERGENCY PHOTOLUMINESCENT PATH LIGHTING STRIP COVER CRACKED. ## 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 = 'N25134' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N25134/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.