Embraer EMB-145ER

Service difficulty reports · 1,266

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 = 'EMB145ER'
  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 C2XA04SH530Bearing Cap · corrodedDURING C-CHECK THE LEFT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02.Oct 25, 2004 · N13935 · Emb EMB145ER · Nose/Tail Landing GearSDR C2XA04SH529Bearing Cap · corrodedDURING C-CHECK RIGHT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02.Oct 25, 2004 · N13935 · Emb EMB145ER · Nose/Tail Landing GearSDR C2XA04SH523Bearing Cap · corrodedDURING C-CHECK FOUND THE LEFT MAIN GEAR AFT BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01.Oct 22, 2004 · N13935 · Emb EMB145ER · Main Landing GearSDR C2XA04SH524Bearing Cap · corrodedDURING C-CHECK FOUND THE LEFT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01.Oct 22, 2004 · N13935 · Emb EMB145ER · Main Landing GearSDR C2XA04SH525Bearing Cap · corrodedDURING C-CHECK FOUND THE RIGHT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED BEARING CAP IAW 32-10-01.Oct 22, 2004 · N13935 · Emb EMB145ER · Main Landing GearSDR C2XA04SH526Bearing Cap · corrodedDURING C-CHECK THE RIGHT MAIN GEAR AFT BEARING CAP FOUND PITTED. REPLACED THE BEARING CAP IAW 32-10-01.Oct 22, 2004 · N13935 · Emb EMB145ER · Main Landing GearSDR C2XA04SH527Frame · crackedDURING C-CHECK EDDY CURRENT INSPECTION OF MAIN PASSENGER DOORSTOP BOLT HOLE AT FRAME 18 AND STRINGER 14 REVEALED A CRACK. OVERSIZED HOLE REINSPECTED AND NO CRACKS NOTED IAW EC5310-01297.Oct 20, 2004 · N13935 · Emb EMB145ER · Fuselage Main, FrameSDR C2XA04CL108Light · inoperativeFLIGHT NR 2805, THE CREW REPORTED THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. SIR REMAINS OPEN PENDING ADDITIONAL INFORMATIOct 20, 2004 · N14939 · Emb EMB145ER · Emergency LightingSDR C2XA04SD009Bulb · inoperativeDURING INSPECTION RIGHT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT WING EMERGENCY LIGHT BULB. OPS CHECK GOOD.Oct 19, 2004 · N15941 · Emb EMB145ER · Emergency LightingSDR C2XA04IA135Wire · looseCREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT THE EXIT ROW WAS INOPERATIVE. RESECURRED THE WIRE AT THE LIGHT. OPERATIONALLY CHECK OK. AIRCRAFT RETURNED TO SERVICE.Oct 19, 2004 · N14942 · Emb EMB145ER · Light System WiringSDR C2XA04SH517Floor Support · corrodedDURING C-CHECK THE CENTER OMEGA BEAM HAT SECTION CORRODED AT FRAME 20. REPLACED THE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE.Oct 14, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04BT106Inverter · inoperativeCREW REPORTED EMERGENCY SIGN ABOVE ROW 12 LEFT SIDE INOPERATIVE. REPLACED THE NUMBER 4 INVERTED. OPS CHECK GOOD.Oct 10, 2004 · N14939 · Emb EMB145ER · Emergency LightingSDR C2XA04IA127Control Unit · inoperativeIAH - FLIGHT 2830, THE CREW REPORTED AN AIR/GROUND FAIL IN FLIGHT AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). OPERATIONALLY Oct 3, 2004 · N12946 · Emb EMB145ER · Landing Gear Position and WarningSDR C2XA04SH513Floor Support · corrodedDURING VISUAL INSPECTION AT C-CHECK THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WERE CORRORDED. REPAIRED OMEGA BEAM USING DOUBLER REPAIR IAW 53-22-10. AIRCRAFT RETURNED TO SERVICE.Oct 3, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH510Torque Box · crackedDURING C-CHECK EDDY CURRENT INSPECTION OF THE RIGHT WING INBOARD TORQUE BOX INDICATED A CRACK AT THE FORWARD TWO HI-LOK POSITION. REAMED THE AFFECTED HI-LOK HOLES TO THE NEXT OVERSIZE IAW EMB SRM 51-40-04. AIRCRAFT RETURNED TO SERVICE.Oct 2, 2004 · N12934 · Emb EMB145ER · Wing, Fuselage Attach FittingsSDR C2XA04SH521Battery · dischargedDURING INSPECTION THE LAST THREE AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY IAW 33-50-04.Oct 1, 2004 · N12934 · Emb EMB145ER · Emergency LightingSDR C2XA04SH520Floor Support · corrodedDURING INSPECTION THE LEFT OMEGA BEAM CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159.Oct 1, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH519Floor Support · corrodedDURING INSPECTION THE LEFT OMEGA BEAM FOUND TO BE CORRODED AT FRAME 19A-23. REMOVED THE DAMAGED AREA AND INSTALLED A SPLICE REPAIR IAW EC5320-01159.Oct 1, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH507Floor Support · corrodedDURING VISUAL INSPECTION AT C-CHECK LT OMEGA BEAM AT FRAME 38 WAS CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01157 AND SRM 53-21-10.Oct 1, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04IA125Control Unit · malfunctionedIAH- FLIGHT 2225, DURING CRUISE, THE CREW REPORTED A/P FAIL & AUTO TRIM FAIL MESSAGES, WITH PITCH TRIM INDICATIONS BEING ERRATIC, WITH BOTH SYSTEMS STILL FUNCTIONING. THE CREW ALSO REPORTED CONTROLLABILITY ISSUES ABOVE 240KTS WITH ROLLING 20 DEGREES TO EITHERSep 30, 2004 · N14945 · Emb EMB145ER · Stabilizer Control SystemSDR C2XA04SH514Floor Support · corrodedDURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED AND REPLACED THE DEFECTIVE BEAM IAW SRM 51-40-02.Sep 29, 2004 · N12934 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY166Frame · chafedDURING SCHEDULED INSPECTION FRAMES 68 AND 70 AT STRINGER 13R WERE FOUND CHAFED. REPAIRED CHAFED AREAS BY BLENDING THE DAMAGED AREA IAW EC 5310-01292. AIRCRAFT RETURNED TO SERVICE.Sep 25, 2004 · N16927 · Emb EMB145ER · Fuselage Main, FrameSDR C2XA04CL099Spline · strippedTHE CREW REPORTED THE MAIN PASSENGER DOOR WOULD NOT OPEN. MAINTENANCE INSPECTED AND REPLACED THE INSIDE DOOR HANDLE. OPS CHECKED GOOD.Sep 25, 2004 · N14925 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA04SH501Floor Support · corrodedSHV - DURING C-CHECK THE LT HAND OMEGA BEAM ASSEMBLY WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 23, 2004 · N13929 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH500Floor Support · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA SHAPE WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 23, 2004 · N13929 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY165Stop · elongatedDURING SCHEDULED INSPECTION THE TWO UPPER COMMON TO MAIN DOOR STOPS AT FRAME 18 AND STRINGER 61 WERE ELONGATED. OVERSIZED HOLES, AND REWORKED PER ED5310-01291. AIRCRAFT RETURNED TO SERVICE.Sep 22, 2004 · N16927 · Emb EMB145ER · Passenger/Crew DoorsSDR C2XA04IA119Control Lever · malfunctionedLCH - FLIGHT 2705, ON DEPARTURE THE CREW REPORTED, RECEIVED AN AIR/GROUND FAILURE MESSAGE AND THE LANDING GEAR LEVER WAS STUCK IN THE DOWN POSITION. THE AIRCRAFT RETURNED TO LCH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GSep 16, 2004 · N12946 · Emb EMB145ER · Landing Gear SelectorSDR C2XA04CL091Control Lever · malfunctionedAFTER TAKEOFF FROM CLE FLIGHT CREW HAD TO CYCLE THE LANDING GEAR HANDLE TWICE TO GET THE LANDING GEAR TO RETRACT. AIRCRAFT RETURNED TO CLE LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKED GOOD.Sep 10, 2004 · N14925 · Emb EMB145ER · Landing Gear SelectorSDR C2XA04TY162Support · gougedVERTICAL STABILIZER TO HORIZONTAL STABILIZER RIGHT SPHERICAL BEARING HOUSING WAS GOUGED. REWORKED HOUSING PER EC5510-01089. AIRCRAFT RETURNED TO SERVICE.Sep 10, 2004 · N15926 · Emb EMB145ER · Horizontal Stabilizer, Attach FittingsSDR C2XA04IA118Light · looseDURING REFLIGHT INSPECTION THE CREW REPORTED THE SECOND AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION ON THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED GOOD IAW EMB-145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOSep 9, 2004 · N14943 · Emb EMB145ER · Emergency LightingSDR C2XA04CL088Bulb · burned outDURING PREFLIGHT FOR FLIGHT 2180 OUT OF CLE THE CREW DISCOVERED THE GALLEY EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN BULBS AND IT OPERATED PROPERLY. FLIGHT 2180 CONTINUED WITHOUT FURTHER INCIDENT.Sep 3, 2004 · N14939 · Emb EMB145ER · Emergency LightingSDR C2XA04IA112Inverter · inoperativeIAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED AISLE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 29, 2004 · N14938 · Emb EMB145ER · Emergency LightingSDR C2XA04SH488Floor Support · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 28, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04SH489Floor Support · corrodedDURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 28, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY160Floor Support · corrodedDURING A SCHEDULED 4C INSPECTION, THE LT OMEGA SHAPE WAS FOUND TO HAVE CORROSION NEAR FRAME 20. MX REMOVED THE CORRODED SECTION OF THE OMEGA SHAPE AND SPLICED IN A NEW SECTION IAW EC5320-01145. THE ACFT WILL BE RELEASED FOLLOWING THE COMPLETION OF THE 4C INSAug 26, 2004 · N15926 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY158Floor Support · corrodedDURING A SCHEDULED 4C INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. MX REMOVED AND REPLACED THE CENTER OMEGA BEAM IAW THE EMB SRM. ACFT PENDING RELEASE UPON COMPLETION OF 4C INSPECTION.Aug 22, 2004 · N15926 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY159Sill · corrodedDURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FLOOR SILL AT FRAME 28. THE SILL WAS REMOVED AND REPLACED IAW THE EMB SRM. ACFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION.Aug 22, 2004 · N15926 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY157Channel · corrodedDURING A SCHEDULED 4C INSPECTION THE PAX DOOR SILL U CHANNEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE PAX DOOR SILL U CHANNEL IAW THE MFG SRM. AIRCRAFT RELEASE PENDING COMPLETION OF THE 4C INSPECTION.Aug 20, 2004 · N15926 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04CL080Wire · looseCLE FLIGHT NR 2153, CREW REPORTED THAT THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR IS INOPERATIVE. MAINTENANCE INSPECTED SYSTEM AND FOUND A LOOSE CONNECTION ON THE EMERGENCY LIGHT. MAINTENANCE RESECURED THE CONNECTION. ALL OPERATIONAL CHECKS WERE GOOD.Aug 12, 2004 · N14939 · Emb EMB145ER · Light System WiringSDR C2XA04BT088Actuator · bypassingBTV LOG SQUAWK LEFT SPOILER REMAINED OPEN IN FLIGHT AFTER SPEED BRAKE LEVER WAS RETURNED TO CLOSE POSITION. THIS LEAD TO UNCOMMANDED LEFT ROLL OF AIRCRAFT ALONG WITH SPOILER FAIL MESSAGE. REMOVED AND REPLACED LEFT SPEED BRAKE ACTUATOR IAW EMB MM 27-62-02. OAug 12, 2004 · N12934 · Emb EMB145ER · Drag Control ActuatorSDR RAIA00408011Starter · inoperativeLT ENGINE WILL NOT START. MAINTENANCE REMOVED AND REPLACED NR 1 AIR TURBINE STARTER.Aug 12, 2004 · N827HK · Emb EMB145ER · Engine StarterSDR C2XA04SH485Floor Support · corrodedSHV - DURING C-CHECK THE RIGHT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 10, 2004 · N14925 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04IA096Light · burnedCRP - FLIGHT 2207, DURING POST FLIGHT INSPECTION THE CREW REPORTED A ELECTRIC BURNING SMELL COMING FROM THE FORWARD CABIN. MAINTENANCE REMOVED THE LIGHT BULB FROM ROW 6/7, AND MEL'D THE LIGHT UNDER MEL 33-20-001 CONTROL 044887, AND THE AIRCRAFT WAS APPROVED FAug 9, 2004 · N14930 · Emb EMB145ER · Passenger Compartment LightingSDR C2XA04BT086Light · malfunctionedATL LOG SQUAWK EMERGENCY LIGHTS NOT ARMED EICAS INFLIGHT. PERFORMED ADJUSTMENT TEST ON EMERGENCY LIGHT SYSTEM. OPS CHECK OK IAW EMB AMM 33-50-00.Aug 8, 2004 · N15932 · Emb EMB145ER · Emergency LightingSDR C2XA04TY142Floor Support · corrodedTYS - DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND FLOOR SUPPORT SILL AT FRAME 36 TO 41. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND FLOOR SUPPORT SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONAug 3, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY132Support · corrodedDURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE LT FORWARD FLOOR SILL SUPPORT IN THE LAV MAINT. REMOVED AND REPLACED THE FLOOR SILL SUPPORT IAW SRM 51-40-02.Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY134Channel · corrodedDURING A SCHEDULED 4C INSPECTION THE RT SIDE STEPUP BRACKET AFT OF PAX DOOR WAS FOUND CORRODED. MAINT. REMOVED AND REPLACED THE STEP UP BRACKET AND CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL 4C WORK.Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY135Sill · corrodedDURING A SCHEDULED 4C INSPECTION THE RT FLOOR SILL WAS FOUND CORRODED AT FR 70. MAINT REMOVED AND REPLACED A NEW COUNTERSUNK FLOOR SILL ALLODINED AND INSTALL IAW 135/145 SRM 51-40-02;51-40-06 AND CPM 51-21-04.Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR C2XA04TY130Support Beam · corrodedDURING A SCHEDULED 4C INSPECTION SIGNS OF CORROSION WERE FOUND ON SEVERAL NUTPLATES ON SUPPORT BEAM IN THE GALLEY. MAINT. REMOVED AND REPLACED ALL TOP CAPS IN THE GALLEY AREA IAW 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETAug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Main, StructureSDR C2XA04TY133Floorbeam · corrodedTYS - DURING A SCHEDULED 4C INSPECTION CORROSION WAS FOUND ON THE CENTER AREA OF THE FLOORBEAM AT FR 20>23. REMOVED AND REPLACED THE FLOORBEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL 4C INSPECTION.Aug 2, 2004 · N17928 · Emb EMB145ER · Fuselage Main, Floor Beam
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