Embraer EMB-145

Service difficulty reports · 3,003

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'EMB145'
  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 C2XA03SH390Buttstrap · corrodedDURING C-CHECK THE CENTER BUTTSTRAP AT FR 59-60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 17, 2003 · N14959 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH389Sill · corrodedSHV-DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 16, 2003 · N14959 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03SH388Stringer · gougedSHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAME 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 16, 2003 · N14959 · Emb EMB145 · Fuselage Main, Longeron/StringerSDR C2XA03SH379Light · inoperativeDURING C-CHECK THE AFT EMERGENCY LIGHT PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 9, 2003 · N13958 · Emb EMB145 · Emergency LightingSDR C2XA03TY195Floorbeam · corrodedTYS DURING A SCHEDULED 3C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED. MAINT REMOVED CORRODED AREA, FABRICATED A NEW DOUBLER AND INSTALLED FILLER, SHIMS, PLATE AND DOUBLER. ALODINED, PRIMED AND REPAINTED WORK AREA. REINSTALLED RAMP ANGLE. ALL WORK WASOct 8, 2003 · N27962 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA03TY194Floorbeam · corrodedTYS DURING A SCHEDULED 3C INSPECTION THE CENTER OMEGA BEAM AT FR 20 WAS CORRODED. MAINT INSTALLED A NEW OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Oct 8, 2003 · N27962 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA03TY193Angle · corrodedTYS DURING A SCHEDULED 3C INSPECTION THE RT SIDE OF THE RAMP ANGLE WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Oct 8, 2003 · N27962 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03SH369Buttstrap · corrodedSHV-DURING C CHECK THE FWD DIGITAL BUTTSTRAP AT FR 14 TO FR 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 3, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH368Structure · gougedSHV- DURING C-CHECK THE RIGHT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 3, 2003 · N13958 · Emb EMB145 · Engine Cowling SystemSDR C2XA03SH367Buttstrap · corrodedDURING C CHECK THE RT CENTER BUTT STRAP FROM FR 20 TO FR 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 53-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 3, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR CHQA000424Engine · malfunctionedDURING CLIMB OUT OF LGA HIGH ITT WAS NOTED ON NR 2 ENGINE. AT MAX CLIMB THRUST ITT WAS AMBER AND RISING ABOVE 290. WE PULLED POWER BACK 7 PERCENT N1 LOWER THAN NR 1 ENGIN FOR REST OF FLIGHT ITT ON NR 2 ENGINE RAN AT 880-890 DEGREES WHEN N1 WAS PULLED BACK 7 Oct 2, 2003 · N262 · Emb EMB145 · Engine (Turbine/Turboprop)SDR C2XA03SH366Structure · chafedDURING C-CHECK THE LT LOWER ENGINE COWLING AFT EDGE MEMBER WAS FOUND TO CHAFED THRU. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 2, 2003 · N13958 · Emb EMB145 · Nacelle/Pylon, Main FrameSDR C2XA03SH365Angle · corrodedSHV- DURING C-CHECK THE RAMP ANGLE AT FR 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 2, 2003 · N13958 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03SH364Floorbeam · corrodedDURING C-CHECK THE RIGHT CENTER FLOORBEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Oct 2, 2003 · N13958 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA03CL171Engine · failedSTL FLIGHT NR 2368 THE CREW REPORTED THE NR 1 ENGINE UNCOMMANDED SHUT DOWN ON APPROACH INTO STL.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT RETURNED TO SERVICE.Oct 1, 2003 · N13968 · Emb EMB145 · Engine (Turbine/Turboprop)SDR C2XA03SH362Buttstrap · corrodedDURING C CHECK THE LT BUTTSTRAP IN THE CARGO COMPARTMENT AT FR 65-68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH360Sill · corrodedDURING C CHECK THE AFT SERVICE DOOR SILL AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03SH359Buttstrap · corrodedDURING C CHECK THE LEFT BUTTSTRAP BETWEEN FRAMES 65 AND 68 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH358Buttstrap · corrodedDURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH357Sill · corrodedDURING C CHECK THE LEFT SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03SH356Buttstrap · corrodedDURING C CHECK THE RT BUTTSTRAP BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR C2XA03SH355Buttstrap · corrodedDURING C CHECK THE AFT DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 30, 2003 · N13958 · Emb EMB145 · Fuselage Main, StructureSDR RAIA00309251Bleed Valve · stuck5316- STL- HIGH STAGE BLEED VALVE FAIL MESSAGE AND REPORTED SMOKE IN CABIN. MAINTENANCE REMOVED AND REPLACED HIGH STAGE VALVE. VALVE STUCK OPEN CAUSED SMOKE IN CABIN.Sep 28, 2003 · N806HK · Emb EMB145 · Pneumatic Distribution SystemSDR C2XA03IA101Pump · leakingFLIGHT 2680, DURING DESCENT THE CREW NOTED THAT HYD. 2 LOW QTY MES ON EICAS, LOSS OF FLUID IN FLIGHT, DECLAIRED EMERGENCY, AND, PERFORMED EMERGENCY DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN Sep 26, 2003 · N12957 · Emb EMB145 · Hydraulic Pump (Electric/Engine), MainSDR CHQA000423Heater · smokeODOR NOTED IN COCKPIT FOLLOWED BY VISIBLE TRAIL OF WHITE SMOKE EMANATING FROM JUNCTION OF F/O WINDSHIELD AND GLARESHIELD. EMERGENCY DECLARED, QRH MEMORY ITEMS ACCOMPLISHED FOR SMOKE/FUMES AND IMMEDIATE DIVERSION TO NEAREST AIRPORT(CLE). SMOKE DISSIPATED AFTESep 26, 2003 · N262 · Emb EMB145 · Windshield/Door Rain/Ice RemovalSDR CHQA000422Control Unit · malfunctionedLANDING GEAR WOULD NOT RETRACT, LG A/G FAIL EICAS MESSAGE. REMOVED AND REPLACED LGEU.Sep 22, 2003 · N272 · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR RAIA00309269Thrust Reverser · out of rig5310-MKE- NR 1 THRUST REVERSER DISAGREE. MAINTENANCE DEFERRED T/R NR 1 IAW MEL 78-34-00. SUBSEQUENTLY CLEARED DMI BY PERFORMING THRUST REVERSER RIGGING PER EMB 78-31-01.Sep 20, 2003 · N805HK · Emb EMB145 · Engine Thrust ReverserSDR C2XA03CL169Antenna · faultyCLE FLIGHT NR 2068 THE CREW REPORTED A LANDING GEAR WARNING AT 10,000 FT. MAINTENANCE INSPECTED AND REPLACED BOTH NR 2 RADIO ALTIMETER ANTENNAS. OPERATIONAL CHECKS WERE GOOD.Sep 18, 2003 · N13956 · Emb EMB145 · Localizer/VOR SystemSDR RAIA00309243Proximity Sensor · failedAIR GROUND FAIL INDICATION AFTER TAKE OFF. MAINTENANCE ADJUSTED NR 2 MAIN FWD PROX SENSOR AND OPS CK OK.Sep 17, 2003 · N807HK · Emb EMB145 · Landing Gear Position and WarningSDR SIMA200326507Floorbeam · corrodedDURING AN MBV INSPECTION, THE CENTER FLOORBEAM FLANGE WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. COMPLETELY REMOVED CORROSION BY BLENDING. FABRICATED A REINFORCEMENT PLATE FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145Sep 16, 2003 · N610AE · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA03CL167Light · inoperativeFLIGHT NR 2448 THE CREW REPORTED 2 ADJACENT EXIT ROW LIGHTS WERE INOPERATIVE IN MIDDLE OF CABIN. MAINTENANCE INSPECTED AND RESET EMERGENCY LIGHT SYSTEM. OPERATIONAL CHECKS WERE GOOD.Sep 15, 2003 · N14959 · Emb EMB145 · Emergency LightingSDR CHQA000421Engine · shutdownDURING CLIMB WITH NORMAL INDICATIONS ON OIL LEVELS, TEMPS, AND PRESSURES THE RIGHT NR 2 ENGINE SHUTDOWN AS WE CLIMBED THROUGH 26,000 FT. AN EMERGENCY WAS DECLARED AND DIVERTED TO DFW. ENGINE WAS CHANGED ON SEPTEMBER 15.Sep 14, 2003 · N278 · Emb EMB145 · Engine (Turbine/Turboprop)SDR RAIA00309252Apu · malfunctioned5283-PIT- SMOKE IN CABIN. MAINTENANCE PLACED APU ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARING THE DMI BY REMOVING AND REPLACING THE APU.Sep 13, 2003 · N804HK · Emb EMB145 · APU Core EngineSDR CHQA000420Proximity Sensor · crackedAFTER TAKEOFF GEAR WOULD NOT RETRACT. EICAS MESSAGE LANDING GEAR AIR/GRND FAIL. RAN QRH CHECKLIST, CONTACT DISPATCH AND MTX AND RETURNED TO MCO FOR LANDING. NO EMERGENCY WAS DECLARED, BUT EMERGENCY EQUIPMENT WAS DISPATCHED. FOUND LF AFT (WOW) PROXIMITY SENSSep 13, 2003 · N272 · Emb EMB145 · Landing Gear Position and WarningSDR RAIA00309238Potentiometer · intermittentAIRCRAFT WILL NOT STEER PROPERLY. MAINTENANCE REMOVED AND REPLACED NWS FEED BACK POT.Sep 11, 2003 · N802HK · Emb EMB145 · Landing Gear Steering SystemSDR RAIA00309253Wire Harness · defective52366-PIT- ENG NR 1 T/R DISAGREE. MAINTENANCE PLACED NR 1 T/R ON DEFERRAL PER MEL. SUBSEQUENTLY CLEARED DMI BY REPAIRING T/R ELECTRICAL HARNESS.Sep 8, 2003 · N805HK · Emb EMB145 · Engine Exhaust System WiringSDR RAIA00309237Shoulder Belt · inoperativeFIRST OFFICERS SHOULDER HARNESS WILL NOT RETRACT OR EXTEND. MAINTENANCE REMOVED AND REPLACED SHOULDER HARNESS.Sep 8, 2003 · N809HK · Emb EMB145 · Flight Compartment EquipmentSDR CHQA000419Smoke · detectedFLYING SHORT FINAL FOR RUNWAY 35 INTO MCO. RECIEVED A CALL STATING - SMOKE IN THE CABIN. NO INDICATIONS ON EICAS BUT COULD DETECT A BURNING SCENT ON THE FLIGHT DECK. DECLARED AN EMERGENCY, TURNED OFF RECIRCS, DEPLOYED PILOT O2 MASK, LANDED UNEVENTFULLY, TURNEDSep 7, 2003 · N836 · Emb EMB145 · Air Distribution SystemSDR CHQA000418Smoke · detectedSMOKE IN CABIN DURING FLT TOWARDS REAR OF PAX CABIN. INSPECTED ENGINE BLEED SYSTEM IAW EMB 135 MM 36-11. INSPECTED APU BLEED SYSTEM IAW EMB 135 MM 36-10. INSPECTED NR 1 AND NR 2 PACKS IAW EMB 135 MM 21-00. NO DEFECTS NOTED AT THIS TIME.Sep 7, 2003 · N836 · Emb EMB145 · Air Distribution SystemSDR C2XA03TY146Skin · dentedTYS AIRCRAFT FERRIED FROM BNA, A LARGE DENT WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF THE SERVICE DOOR WITH A DEEP SCRATCH, MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, ALLIDINED, INSTALLED PATCH, PRIMED AND PAINTED I/A/W-EMB-135/145Sep 6, 2003 · N16963 · Emb EMB145 · Fuselage Main, Plate/SkinSDR RAIA00309236Switch · dirtyTHRUST REVERSER DISAGREE MESSAGE. MAINTENANCE CLEANED BOTH STOW SWITCHES.Sep 4, 2003 · N805HK · Emb EMB145 · Engine Thrust ReverserSDR C2XA03CL158Charger · inoperativeDURING ROUTINE MAINTENANCE THE LEFT HAND EMERGENCY LIGHT FORWARD OF THE WING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.Sep 3, 2003 · N13965 · Emb EMB145 · Emergency LightingSDR C2XA03IA089Uplock · inoperativeIAH- MAINTENANCE NOTED THAT THE LANDING GEAR INDICATION DISAGREES WITH THE LEVER. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 3, 2003 · N27962 · Emb EMB145 · Landing Gear Position and WarningSDR RAIA00309233Connector · looseEMERGENCY LIGHT ON STAIR INOP. SECURED CONNECTOR TO STAIR EMERGENCY LIGHT.Sep 1, 2003 · N806HK · Emb EMB145 · Emergency LightingSDR C2XA03BT089Wire · looseEWR LOG SQUAWK EMERGENCY EXIT SIGN ROW 12 LEFT SIDE BURNED OUT. RESECURED SPLICE FOR EMERGENCY EXIT SIGN AT ROW 12 LEFT HAND IAW EMB145 MM 33-50-00. OPS CHECK GOOD.Aug 24, 2003 · N15973 · Emb EMB145 · Light System WiringSDR C2XA03TY139Housing · corrodedTYS DURING A SCHEDULED INSPECTION THE HORIZONTAL SATB SPHERICAL BEARING HOUSING WAS FOUND TO BE WORN AND PITTED. MAINTENANCE ACCOMPLISHED A BLEND-OUT AND REAM REPAIR IAW E.C. 5510-01062 AND EMB M.M. 51-50-01. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL Aug 24, 2003 · N13956 · Emb EMB145 · Horizontal Stabilizer StructureSDR C2XA03TY132Gusset · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET UNDER THE GALLEY FLOOR. MAINTENANCE REMOVED AND REPLACED THE AFT GUSSET IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 18, 2003 · N13956 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03TY131Sill · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD SERVICE DOOR SILL. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB GST NR 1907/20A AND EMB CPM 51-21-04, 05, 06. THE REPAIR WAS SATISFACTORY, THE AIRCRAFT WILL BE RELEASED UPON COMPLETIOAug 18, 2003 · N13956 · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA03TY130Seat Track · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LW3. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB MM 53-01-06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 18, 2003 · N13956 · Emb EMB145 · Fuselage, Seat/Cargo Attach FittingsSDR C2XA03TY129Seat Track · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON SEAT TRACK LW1. MAINTENANCE REMOVED AND REPLACED THE TRACK IAW EMB MM 53-01-06, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Aug 18, 2003 · N13956 · Emb EMB145 · Fuselage, Seat/Cargo Attach Fittings
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