N12142

Service difficulty reports · 91

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 = 'N12142' 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 ASOA20131123441Stiffener · crackedSTIFFENER CRACKED AT FRAME 30 & STRINGER 3L. R & R STIFFENER.Nov 23, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131123440Floor Support · corrodedRIGHT OTBD FLOOR SUPPORT AT FRAME 23 CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.Nov 23, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131121439Floor Support · corrodedRT OTBD FLOOR SUPPORT BETWEEN FRAMES 33 AND 34 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131121438Floor Support · corrodedLEFT FLOOR SUPPORT BETWEEN FRAMES 59 TO 60 CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R FLOOR SUPPORT.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131121437Floor Support · corrodedLT OMEGA BEAM CAP BETWEEN FRAMES 59 TO 60 HAS CORROSION BEYOND LIMITS AROUND NUTPLATE AREA. R & R OMEGA BEAM CAP.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131121436Floorbeam · corrodedLT FLOORBEAM 65 AFT CARGO AREA CORRODED BEYOND LIMITS AFTER BLEND-OUT. REMOVED AND INSTALLED LT FLOORBEAM.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Main, Floor BeamSDR ASOA20131121435Splice Plate · crackedCRACK IN SPLICE PLATE FOR LT OTBD FLOOR SUPPORT BETWEEN FRAMES 23-24. R & R SPLICE PLATE.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20131121434Floor Support · corrodedLT OTBD FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.Nov 21, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20130816095Generator · failedCREW REPORTED DURING POSTFLIGHT INSPECTION, A LONG THICK STREAK OF BLACK SOOT COMING FROM OTBD GENERATOR VENT ON NR 2 ENGINE ACCOMPANIED WITH SCHRAPNEL AND DEBRIS HANGING OUT OF VENT. MX INSPECTED AND FOUND THE NR 4 ENGINE GENERATOR TO HAVE COME APART DURING Aug 16, 2013 · N12142 · Emb EMB145XR · DC Generating SystemSDR ASOA20130715338Floor Support · corrodedCORROSION BEYOND LIMITS AFTER BLEND OUT AROUND NUT PLATE FLOOR SUPPORT. CUT-OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR.Jul 15, 2013 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR ASOA20121216117Battery Pack · dischargedDURING MX INSPECTION, THE LOWER SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 16, 2012 · N12142 · Emb EMB145XR · Emergency LightingSDR ASOA20120916076Engine · leakingTHE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN IN FLIGHT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.Sep 16, 2012 · N12142 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR ASOA20120311036Axle · crackedDURING MX INSPECTION, THE UPPER ATTACH AXLE FOR THE LT MLG SHOCK ABSORBER WAS FOUND TO BE CRACKED. MX R & R THE AFFECTED AXEL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 11, 2012 · N12142 · Emb EMB145XR · Main Landing Gear Strut/Axle/TruckSDR ASOA20120116001Sign · inoperativeDURING SCHEDULED OVERNIGHT MX THE GALLEY DOOR LOWER EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX RESET AND PERFORMED AN OPS CHECK OF THE GALLEY DOOR LOWER EXIT SIGN IAW AMM 33-50-09. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 16, 2012 · N12142 · Emb EMB145XR · Emergency LightingSDR C2XA11CL038Clamp · looseORD FLT 5959 THE CREW REPORTED A BLEED 1/2 LOW TEMPERATURE MESSAGE ON THE EICAS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED THE NR 1 FAN AIR VALVE CLAMP. OPERATIONAL CHECKS WERE GOOD.Feb 6, 2011 · N12142 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA11IA028Thermostat · inoperativeFLT 6091, CREW REPORTED A BLEED TWO OVERTEMP INDICATION IN ICING CONDITIONS. THE ACFT RETURNED TO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HIGH TEMP THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR REFeb 4, 2011 · N12142 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA11TY014Precooler · blownTYS - A/C WAS EN ROUTE TO ORD FROM TYS WHEN CREW GOT A MESSAGE "BLEED 2 OVERTEMP" DURING CLIMBOUT. A/C RETURNED TO TYS AND EXCHANGED PLANE WITH A/C124. MAINTENACE REMOVED AND REPLACED THE NR 2 PRECOOLER IAW EMB 145XR AMM 36-11-04. OPS CHECK AND LEAK CHECK Feb 2, 2011 · N12142 · Emb EMB145XR · Pneumatic Distribution SystemSDR C2XA11CL034Electronic Unit · faultyLNK FLT 6177 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO LNK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.Jan 30, 2011 · N12142 · Emb EMB145XR · Landing Gear Retraction/Extension SystemSDR C2XA10IA344Seal · leakingCREW REPORTED AN AIR GROUND FAIL MESSAGE ON EICAS WHEN LOWERING THE LANDING GEAR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE SEAL IN THE NOSE LANDING GEAR SHOCK STRUT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ADec 26, 2010 · N12142 · Emb EMB145XR · Nose/Tail Landing Gear Strut/AxleSDR C2XA10RI0147Warning System · false activationFLIGHT 2511 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX APPLIED BREAK OUT BOX AND PERFOREMD OPERATIONAL CHECK BUT COULD NOT DUPLICATE THE MESSAGE. A CFT WAS APPROVED TO RETURN TO SERVICE.Nov 25, 2010 · N12142 · Emb EMB145XR · Landing Gear Position and WarningSDR C2XA10IA281Engine · vibrationFLIGHT 3145, THE CREW REPORTED THE ENGINE ONE HP VIBRATION IN AMBER AT THRUST SET DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND TOct 31, 2010 · N12142 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA10TY107Engine · malfunctionedEWR - CREW REPORTED SMOKE IN CABIN AND COCKPIT AFTER T/O AND RETURNED TO GATE. THE A/C WAS MX FERRIED TO TYS FOR REPAIR. TYS REMOVED AND REPLACED THE NR 1 ENGINE AND THE LT PACK CONDENSER/MIXER. ALL OPS AND LEAK CHECKS GOOD AND PROBLEM WAS RESOLVED.Jul 29, 2010 · N12142 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA10SH084Attach Fitting · damagedSHV - DURING C-CHECK LT SPOILER CENTER HINGE POINT HOUSING IS DAMAGED. REPLACED SPOILER ATTACHMENT IAW EMB 145XR AMM 57-51-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2010 · N12142 · Emb EMB145XR · SpoilersSDR C2XA10SH083Sill · corrodedSHV - DURING C-CHECK SERVICE DOOR FORWARD SILL CORRODED. REPLACED SERVICE DOOR FORWARD SILL IAW EC5320-01137. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2010 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA10SH082Sill · corrodedSHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS AREAS OF CORROSION. REPAIRED CARGO DOOR CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2010 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA10SH081Skin · corrodedSHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACKS AROUND SEVERAL RIVETS AT FR 79. REPAIRED FUSELAGE SKIN IAW EC5330-02081. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2010 · N12142 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA10SH080Skin · crackedSHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACKS AROUND SEVERAL RIVETS AT FR 80. REPAIRED FUSELAGE SKIN IAW EC5330-02081. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 1, 2010 · N12142 · Emb EMB145XR · Fuselage Main, Plate/SkinSDR C2XA10SH78Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Feb 27, 2010 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA10IA063Proximity Switch · inoperativeIAH - FLIGHT 3151, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE WITH THE LANDING GEAR DOWN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NFeb 12, 2010 · N12142 · Emb EMB145XR · Landing Gear Position and WarningSDR C2XA08RI151Inverter · inoperativeFLT 2276 - EWR - FLT CREW REPORTED RT EXIT IDENTIFIER UPPER AT EMERGENCY EXIT INOPERATIVE. MX R&R NR 5 EMERGENCY LIGHT INVERTER AND PERFORMED OPS CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE.Oct 1, 2008 · N12142 · Emb EMB145XR · Emergency LightingSDR C2XA08TY087Inverter · inoperativeRT SIDEWALL LARGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S)Aug 20, 2008 · N12142 · Emb EMB145XR · Emergency LightingSDR C2XAA08TY057Panel · corrodedTYS - DURING A CURRENT 3C INSPECTION THE BONDIND STRIP ON PANEL 197CL WAS FOUND CORRODED. MAINTENANCE REPAIRED THE PANEL IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145 XR AMM 2 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE EJun 2, 2008 · N12142 · Emb EMB145XR · Wing Miscellaneous StructureSDR C2XAA08TY056Panel · corrodedTYS - DURING A CURRENT 3C INSPECTION PANEL 197 CL WAS FOUND CORRODED AT THE BONDING STRAP. MAINTENANCE REPAIRED THE PANEL IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145XR AMM 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE ENDJun 2, 2008 · N12142 · Emb EMB145XR · Wing Miscellaneous StructureSDR C2XA08TY055Bracket · corrodedTYS - DURING A CURRENT 2C INSPECTION THE VENTRAL TANK FWD CENTER BRACKET WAS FOUND CORRODED. MAINTENANCE CUT OUT THE DAMAGE AREA, FAB A FILLER, SHIM AND EXTERNAL DOUBLER. APPLIED SEALANT AND ANTI-BACTERIAL COMPOUND PLUS A FUEL BARRIER SEALANT. LEAK CHECK GOJun 1, 2008 · N12142 · Emb EMB145XR · Fuel StorageSDR C2XA07IA174Sign · inoperativeAUS - DURING SERVICE CHECK THE UPPER EMERGENCY EXIT LIGHT ON THE RIGHT HAND SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jul 21, 2007 · N12142 · Emb EMB145XR · Emergency LightingSDR C2XA07RI026Unknown · smokeFLT 2496 - EWR - CREW REPORTED ENGINE NR 1 SMOKE COMING OUT FROM THE EXHAUST AND CONTINUING FOR 15 MINUTES AFTER SHUT DOWN ON TAXI IN. EWR MX PERFORMED OPERATIONAL CHECK OF NR 1 ENGINE (HIGH POWER RUN) AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TMay 4, 2007 · N12142 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR C2XA07RI013Oil System · overservicedFLT 2287, CREW REPORTED COCKPIT SMELLS OF SMOKE WHEN PACK NR 2 IS SELECTED. MX INSPECTED APU AND FOUND SIGNS OF EXCESSIVE OIL SERVICE. MX CLEANED APU AREA AND PERFORMED OPS CHECK OF PACK NR 2. OPS CHECK GOOD, NO SIGNS OF SMOKE FOUND.Apr 1, 2007 · N12142 · Emb EMB145XR · APU Oil SystemSDR C2XA06SH102Tie Clip · corrodedSHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 65 BETWEEN STRINGERS 15 AND 16L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REAPAIR IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 12, 2006 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA06SH103Tie Clip · corrodedSHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 68 BETWEEN STRINGERS 15 AND 16L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A DOUBLER REPAIR IAW EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 12, 2006 · N12142 · Emb EMB145XR · Fuselage Miscellaneous StructureSDR C2XA05CL030Wire · chafedCLE - THE CREW REPORTED THE AURAL WARNING SOUNDED CONTINUOUSLY IN FLIGHT AT ALL ALTITUDES UNTIL THE LANDING GEAR WAS LOWERED. MAINTENANCE FOUND AND REPAIRED CHAFED WIRES IN THE CENTER PEDESTAL JUST AFT OF THE FLAP SELECTOR HANDLE. OPERATIONAL TESTS OF THE AUMay 2, 2005 · N12142 · Emb EMB145XR · Landing Gear System WiringSDR C2XA03BT075Coffeemaker · smokeCREW REPORTED, FLIGHT ATTENDANT SMELLED ELECTRICAL SMOKE FROM GALLEY LIGHT CIRCUIT BREAKER. MAINTENANCE INSPECTED COFFEE POT(S) SOCKET AND GALLEY LIGHT ASSEMBLY, NO FAULT FOUND. OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.Jul 24, 2003 · N12142 · Emb EMB145 · Buffet/Galleys
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