N25134

Service difficulty reports · 40

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA202004164013Acm · frozenIAH - 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 WITHApr 16, 2020 · N25134 · Emb EMB145XR · Cabin Cooling SystemSDR ASOA2019100294054Light · inoperativeFLIGHT 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.Sep 27, 2019 · N25134 · Emb EMB145XR · Emergency LightingSDR ASOA201906284037Acm · failedIAH - 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.Jun 28, 2019 · N25134 · Emb EMB145XR · Cabin Cooling SystemSDR ASOA2018053025139Charger · inoperativeDURING 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.May 23, 2018 · N25134 · Emb EMB145LR · Emergency LightingSDR ASOA201804187066Mount · damagedDURING 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.Apr 18, 2018 · N25134 · Emb EMB145XR · Engine Mount SectionSDR ASOA201804117058Skin · delaminatedLT 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.Apr 11, 2018 · N25134 · Emb EMB145XR · Trailing Edge FlapsSDR ASOA20151007182Support · corrodedDURING 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.Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20151007181Beam · corrodedDURING 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.Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Main, StructureSDR ASOA20151007180Floor Support · corrodedDURING 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.Oct 7, 2015 · N25134 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20150802042CLight · odorTHE CREW REPORTED ELECTRICAL BURNING ODOR AT ROW 4CD IN LIGHT AREA. OPENAug 2, 2015 · N25134 · Emb EMB145XR · Passenger Compartment LightingSDR ASOA20150302004Skin · dentedFUSELAGE DENT BETWEEN 7-8 AND STR 11L-13L. CUT OUT DENT INSTALLED FILLER, DOUBLER AND TRIPLER.Feb 28, 2015 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20150302003Skin · dented2 DENTS ON FUSELAGE BETWEEN FRM 7 & 8, STR 11L-13L. CUTOUT DAMAGED SKIN INSTALLED FILLER DOUBLER AND TRIPLER IAW ETD2014-145-060373.Feb 28, 2015 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR ASOA20140923082CSocket · burnedTHE 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.Sep 23, 2014 · N25134 · Emb EMB145XR · Passenger Compartment LightingSDR ASOA20130919374Tank · chafedDURING 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 NSep 19, 2013 · N25134 · Emb EMB145XR · Fuel StorageSDR ASOA20130420031Wire Harness · faultyTHE 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.Apr 20, 2013 · N25134 · Emb EMB145XR · Light System WiringSDR C2XA11RI169Fire Loop · defectiveFLT 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 ENOct 18, 2011 · N25134 · Emb EMB145XR · Fire DetectionSDR C2XA11SH142Stringer · corrodedSHV - 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.Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Longeron/StringerSDR C2XA11SH141Skin · crackedSHV - 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. Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA11SH140Skin · crackedSHV - 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 EC5330-024Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA11SH139Skin · crackedSHV - 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 AIRCSep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA11SH138Skin · crackedSHV - 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.Sep 20, 2011 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA10IA262Outflow Valve · inoperativeIAH - 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, ASep 27, 2010 · N25134 · Emb EMB145XR · Pressure Regulator/Outflow ValveSDR C2XA10IA159Windshield · crackedQRO, 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 May 25, 2010 · N25134 · Emb EMB145XR · Flight Compartment WindowsSDR C2XA10CL068Screw · backed outDURING 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 EMEMay 10, 2010 · N25134 · Emb EMB145XR · Emergency ExitsSDR C2XA10CL044Tube · crackedCLE 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 CONTROMar 15, 2010 · N25134 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA10SH086Attach Bracket · corrodedSHV - 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 51-40Mar 7, 2010 · N25134 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA10SH085Door Frame · corrodedSHV - 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.Mar 7, 2010 · N25134 · Emb EMB145XR · Fuselage Main, StructureSDR C2XA10SH079Floor Support · corrodedSHV - 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.Feb 28, 2010 · N25134 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA09TY275Outflow Valve · malfunctionedPRESSURE 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 21-3Dec 24, 2009 · N25134 · Emb EMB145XR · Pressure Regulator/Outflow ValveSDR C2XA09IA244Battery Pack · dischargedLCH - 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.Sep 23, 2009 · N25134 · Emb EMB145XR · Emergency LightingSDR C2XA09TY127Light · inoperativeRT EMERGENCY SIDE WALL EXIT LIGHT AT 12BC INOP. EXIT MARKER SIGN ASSY WAS REMOVED AND REPLACED.Jun 24, 2009 · N25134 · Emb EMB145XR · Emergency LightingSDR C2XA08RI026Control Unit · defectiveRIC - 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.Feb 28, 2008 · N25134 · Emb EMB145XR · Landing Gear Retraction/Extension SystemSDR C2XA07RI105Tat Probe · inoperativeFLT 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.Dec 7, 2007 · N25134 · Emb EMB145XR · Outside Air Temperature Indicator/SensorSDR C2XA07CL081Control Unit · faultyCLE 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 Sep 20, 2007 · N25134 · Emb EMB145XR · Landing Gear Position and WarningSDR C2XA07TY002Skin · damagedAIRCRAFT 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 145-5Jan 23, 2007 · N25134 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA06CL094Charger · brokenCLE FLIGHT 3150 THE CREW REPORTED THE AFT F/A FLASHLIGHT CHARGER WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE FLASHLIGHT CHARGER. OPERATIONAL CHECKS WERE GOOD.Dec 4, 2006 · N25134 · Emb EMB145XR · Emergency LightingSDR C2XA06TY045Bracket · gougedTYS 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-CHJul 25, 2006 · N25134 · Emb EMB145XR · AileronsSDR C2XA06TY042Bracket · damagedPCA BRACKET MISSING BUSHINGS & DISPLACED METAL IN BUSHING HOLES. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177 REV B AND EMB145 SRM 51-40-02.Jul 13, 2006 · N25134 · Emb EMB145XR · Aileron Control SystemSDR C2XA06TY043Bracket · damagedLT AILERON DAMPNER BRACKET DAMAGED. REMOVED AND REPLACED LT AILERON DAMPNER BRACKET IAW EMB145 SRM 51-40-02 & CPM51-21-06.Jul 13, 2006 · N25134 · Emb EMB145XR · AileronsSDR C2XA04SD002Glowstrip · crackedSDF - DURING 3A CHECK INSPECTION FOUND CABIN FLOOR FWD EMERGENCY PHOTOLUMINESCENT PATH LIGHTING STRIP COVER CRACKED.Jul 1, 2004 · N25134 · Emb EMB145XR · Emergency Equipment
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