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 OEJA202504070001Unknown · odorON 04/04/2025 AT 12:15PM, LEGACY600 TAKING OFF FORM KVRB 12R, CREW EXPERINCED SMOKE IN THE COCKPIT COMING FROM THE AIR VENTS. CREW IMMEDITATELY ABORTED TAKE OFF AND RETURNED TO THE FBO, CREW THEN NOTIFIED MAINTENANCE CHIEF. TROUBLESHOT THE ISSUE, AND RESOLVED Apr 4, 2025 · N905FL · Emb EMB145ER · Air Distribution SystemSDR ASOA2018051605126Transducer · faultyCREW REPORTED BRAKES WERE SLOW TO REPOND ON LANDING ROLLOUT FOR LANDING. BRAKING WAS NORMAL ON BOTH SIDES ON TAXI TO GATE. REMOVED AND REPLACED THE NR 3 WHEEL SPEED TRANDSDUCER IAW MM 32-41-03. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 12, 2018 · N13988 · Emb EMB145ER · Landing Gear Brake SystemSDR HNAA2017092000321Light · inoperativeLEFT SIDE EMERGENCY EXIT DOOR UPPER LIGHT NOT ILLUMINATING. R&R EMERGENCY LIGHT AT LT EXIT DOOR IAW AMM TASK 33 50-14-000/400-801-A. P/N OFF 7444-9.Sep 18, 2017 · N609 · Emb EMB145ER · Emergency LightingSDR HNAA2017092000320Inverter · inoperativeROW 3B EMERGENCY EXIT LIGHT NOT ILLUMINATING. R&R EMERGENCY LIGHT DC/AC INVERTER IAW AMM TASK 33-50-11-000/400-801-A. P/N OFF INVERTER 7824-1Sep 18, 2017 · N609 · Emb EMB145ER · Emergency LightingSDR HNAA2017092000323Connector · brokenSERVICE DOOR EMERGENCY LIGHT INOP. FOUND CONNECTOR ON EMERGENCY SERVICE DOOR LIGHT BROKEN. R&R CONTACT + MALE CONNECTOR IAW SWPM 20-21-00. OPS CHECK GOOD OK FOR SERVICE.Sep 16, 2017 · N604 · Emb EMB145ER · Light System WiringSDR HNAA2017092000322Knob · missingLAV DOOR EMERGENCY KNOB MISSING. INSTALLED NEW EXTERNAL LAV KNOB IN REF TO AMM 25-40-02-000/400-801-A. OK FOR SERVICE.Sep 15, 2017 · N632 · Emb EMB145ER · LavatoriesSDR V0XR2015091000002Skin · corrodedCORROSION FOUND ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN BETWEEN FRAMES 12-13 AND STRINGERS 2021R. REPAIRED IAW ETD-2015-145-070110, REV C, REPAIR B AND EO-EMB145-53-013-R2.Sep 10, 2015 · N809HK · Emb EMB145ER · Fuselage Main, Plate/SkinSDR V0XR2015091000001Skin · corrodedCORROSION AND PIN HOLES IN SKIN AT FR 13-14, STR 16-17R. REPAIRED CORROSION DAMAGE BY CUTTING THE SKIN BETWEEN FRAME 13-14, STR 16-17R AND INSTALLING A NEW SKIN SECTION AND DOUBLER, TRIPLE IAW ETD2015-145-07011 AND EO EMB145-53-013 R2. THIS REPAIR IS CONSIDESep 10, 2015 · N809HK · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20140625144Frame · crackedDURING C-CHECK, FRAME 66 WAS FOUND TO BE CRACKED AT STRINGER 16R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 25, 2014 · N14933 · Emb EMB145ER · Fuselage Main, FrameSDR ASOA20140624135VHinge Fitting · wornDURING C-CHECK THE TOP MOUNTING HINGE ON THE VERTICAL STABILIZER FOR RUDDER, FOUND TO BE WORN. MAINTENANCE R & R THE HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 24, 2014 · N13936 · Emb EMB145ER · Rudder StructureSDR ASOA20140622134VFloor Support · corrodedDURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, FIGURE 202, SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 23, 2014 · N14933 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20140413043Door Frame · crackedCARGO DOOR AFT FRAME LOWER INSIDE CORNER HAS A CRACKED NUTPLATE. REPAIRED IAW EC5230-01326. ACFT APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · Cargo/Baggage DoorsSDR ASOA20140413042Firewall · crackedDURING C-CHECK, APU FIREWALL CRACKED AT UPPER LT MOUNT. REPAIRED IAW EC5330-02578, REV B. ACFT APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · APU Cowling/ContainmentSDR ASOA20140413041Housing · wornDURING C-CHECK, HORIZONTAL STAB HINGE FITTING HOUSINGS IS OUT OF LIMITS. REPAIRED IAW SRM 55-30-02. ACFT APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20140413040VFloor Support · corrodedDURING C-CHECK, CENTER OMEGA BEAM CORRODED ON LOWER SIDE AT FRAME 59. MAINTENANCE PERFORMED REPAIR IAW EC5310-01473. ACFT APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20140413039Shear Tie · corrodedSHEAR TIE CORRODED, AT FRAME 65, STRINGER 17L. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Internal Mounting StructureSDR ASOA20140413038Beam · corrodedDURING C-CHECK, CARGO LOWER BEAM FROM FRAMES 65-68 HAS CORROSION. MAINTENANCE R & R LOWER BEAM IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 13, 2014 · N14930 · Emb EMB145ER · Fuselage Main, StructureSDR ASOA20140318054Channel · corrodedC-CHECK, THE CENTER OMEGA BEAM GUSSET WAS CORRODED AT NUTPLATES AT FRAME 16. MAINTENANCE REMOVED THE CORROSION AND FABRICATED A NEW REPAIR IAW EC 5320-01215, REV ORIGINAL.Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20140318053TChannel · corrodedDURING C-CHECK, THE RT SIDE OMEGA BEAM TOPCAP WAS FOUND CORRODED AT FRAME 59. MAINTENANCE R & R THE RT SIDE OMEGA BEAM GUSSET AT FRAME 59 IAW SRM 51-40-02Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20140318052TShear Tie · crackedDURING C-CHECK, LT CENTER FUSELAGE FRAME 46 HAS A SHEAR TIE CRACKED. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02.Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Internal Mounting StructureSDR ASOA20140318051Floor Support · crackedC-CHECK, THE LT FLOOR SUPPORT SPLICE WAS FOUND CRACKED AT FRAMES 23 AND 24. MAINTENANCE R & R IAW SRM 51-40-02.Mar 18, 2014 · N14939 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20140311025Seal · debondedEXPERIENCED CABIN DEPRESSURIZATION AT ALTITUDE AND THEN DIVERTED. MAINTENANCE FOUND CARGO DOOR RUBBER TRIM SEAL DEBONDED AND HANGING OUT IN THE AIRSTREAM. REINSTALLED CARGO DOOR RUBBER TRIM SEAL IAW AMM 52-30-02. PERFORMED LEAK CHECK ON PRESSURIZATION AND OMar 11, 2014 · N14938 · Emb EMB145ER · Cargo/Baggage DoorsSDR ASOA20140101003Mount · crackedDURING C-CHECK NR 1 ENGINE FWD LOWER ENGINE MOUNT YOKE CRACKED.Jan 1, 2014 · N22971 · Emb EMB145ER · Engine Mount SectionSDR ASOA20140101002Frame · dentedDURING C-CHECK FRM 74 IS DENTED AT STR 14L-15L. MAINTENANCE PERFORMED REPAIR OF FRAME 74 AT STR 14L-15L IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Jan 1, 2014 · N22971 · Emb EMB145ER · Fuselage Main, FrameSDR ASOA20131218294VHinge Fitting · wornDURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING NR 4 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218293Hinge Fitting · wornDURING C-CHECK THE HORIZONTAL STAB HINGE PIN FITTING, NR 3 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218292Hinge Fitting · wornDURING C-CHECK, THE HORIZONTAL STAB HINGE PIN FITTING NR 2 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218291VHinge Fitting · wornDURING C-CHECK, HORIZONTAL STAB HINGE PIN FITTING NR 1 WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REPAIRED THE FITTING IAW EC5510-01229 REV. A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Horizontal Stabilizer StructureSDR ASOA20131218290Skin · crackedDURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-80 AND STRINGERS 3-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02840. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20131218289Hinge Fitting · wornDURING C-CHECK, THE RUDDER II UPPER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Rudder StructureSDR ASOA20131218288Hinge Fitting · wornDURING C-CHECK, THE LT SPEED BRAKE CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · SpoilersSDR ASOA20131218287Frame · crackedDURING C-CHECK, LEFT FRAME 10 SEGMENT WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. R & R FRAME SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, FrameSDR ASOA20131218286Stringer · crackedDURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 14. R & R STRINGER SEGMENT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20131218285Floor Support · corrodedDURING C-CHECK, RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20131218284Support · corrodedDURING C-CHECK, LAVATORY WASTE DRAIN SUPPORT ASSY WAS FOUND TO BE CORRODED. R & R SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20131218283Sill · corrodedDURING C-CHECK, SERVICE DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-02. ACFT APPROVED FOR RETURN TO SERVICE.Dec 18, 2013 · N15932 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20131125447Bracket · wornAIRCRAFT IS IN C-CHECK WHEN INSPECTION FOUND THE RT GROUND SPOILER INBD HINGE FITTING AT THE WING SPAR AREA INBD/OTBD BUSHIONS MIGRATED AND OBLONG THE FITTING. MAINTENANCE R & R THE THE RT GROUND SPOILER FITTING IAW AMM 20-10-01. ALL WORK ACCOMPLISHED AND WINov 25, 2013 · N17928 · Emb EMB145ER · SpoilersSDR ASOA20130610173Tire · failedFLIGHT 4358. RT MLG NR 3 TIRE BLEW OUT AT V1 DAMAGING OTHER ITEMS. R & R NR 3 TIRE.Jun 10, 2013 · N14937 · Emb EMB145ER · TireSDR ASOA20130423156Skin · corrodedDURING C-CHECK, THE CENTER FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-15 AND STRINGERS 19R-20L. MX R & R THE SKIN IAW EC5330-02761. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 12, 2013 · N16944 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20130423153Frame · crackedDURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE PILOTS DV WINDOW AT STRINGER 9L. MX R & R THE CRACKED FRAME SECTION IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.May 11, 2013 · N16944 · Emb EMB145ER · Fuselage Main, FrameSDR ASOA20130421138Skin · corrodedDURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 20R-20L. MX R & R THE SKIN IAW EC5320-01787. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20130421137Stringer · corrodedDURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20130421136Stringer · corrodedDURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MX R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Main, Longeron/StringerSDR ASOA20130421135VSill · corrodedDURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Apr 20, 2013 · N15948 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20130226089Skin · corrodedDURING C-CHECK THE COCKPIT BELLY SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 18R-19L. MX R & R THE SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Mar 7, 2013 · N14943 · Emb EMB145ER · Fuselage Main, Plate/SkinSDR ASOA20130226088Beam · corrodedDURING C-CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 BETWEEN STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Main, StructureSDR ASOA20130226087Shear Tie · corrodedDURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Internal Mounting StructureSDR ASOA20130226086Shear Angle · corrodedDURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20130226085Shear Angle · crackedDURING C-CHECK THE RIB 1 SHEAR CLIP FROM FRAMES 40-45 WAS FOUND TO BE CRACKED. MX R & R THE SHEAR CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 26, 2013 · N14943 · Emb EMB145ER · Fuselage Miscellaneous StructureSDR ASOA20130131257TSkin · crackedACFT WAS FOUND WITH A 6MM CRACK FOR RIVET EDGE ON THE LT SKIN AT FRAME 75 BELOW STRINGER 2. MX INSTALL A SMALL PATCH TO THE FUSELAGE SKIN AT FRAME 75, STRINGER 2L IAW EC 5330-02353. PRESSURE CHECKED GOOD AND WAS RELEASED TO SERVICE.Jan 31, 2013 · N15941 · Emb EMB145ER · Fuselage Main, Plate/Skin
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