Embraer EMB-145EP

Service difficulty reports · 2,197

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 = 'EMB145EP'
  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 V0XR201005030013Sill · corroded(V0XR) SERVICE DOOR SILL IS CORRODED BEYOND LIMITS. R & R SILL.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030012Sill · corroded(V0XR) LT SILL AT FR 18-23 LY 780.0 IS CRACKED BEYOND LIMITS. R & R SILL.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030011Structure · cracked(V0XR) RT SIDE BOTTOM PART OF VERTICAL AT FR 77 STG 01L IS CRACKED BEYOND LIMITS. R & R SHAPE L, W/C 3058.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201005030009Angle · cracked(V0XR) ANGLE AT FR 14 LY 780.0 IS CRACKED BEYOND LIMITS. R & R ANGLE.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030007Floor Support · corroded(V0XR) SCALLOPED FLOOR SUPPORT ANGLE AT FR 18 LY 479.0 - RY 780.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ANGLE. W/C 1082May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030008Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE AT FR 23 Y0.0 - RY 780.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ANGLE. W/C 1082May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030006Channel · corroded(V0XR) CTR HAT CHANNEL BEAM AT FR 16-25 Y0.0 IS CORRODED BEYOND LIMITS. R & R HAT CHANNEL BEAM. W/C 1081.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030005Gusset · corroded(V0XR) GUSSET AT FR 16.5-18 LY 479.0 - Y0.0 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED GUSSET.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030003Gusset · corroded(V0XR) GUSSET AT CTR BEAM FR 18-23 RY Y0.0 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1067.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030002Doubler · corroded(V0XR) DOUBLERS FOR RT BEAM FR 20-22 RY 479.0 ARE CORRODED BEYOND LIMITS. R & R DOUBLERS. W/C 1066May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030001Sill · corroded(V0XR) RT SILL AFT OF SERVICE DOOR FR 22-23 RY 780.0 IS CORRODED BEYOND LIMITS. R & R SILL. W/C 1063.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH164Fitting · crackedSHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6R-7R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 2, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH163Fitting · crackedSHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6L-7L. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 STRINGER 6L-7L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 2, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004300004Profile · corroded(V0XR) PROFILE AT FR 22 FROM OMEGA BEAM TO RY 780.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1117.Apr 30, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004300003Channel · corroded(V0XR) CTR HAT CHANNEL BEAM AT Y0.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1083.Apr 30, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004300002Profile · corroded(V0XR) PROFILE AT FR 17-18 OUTBOARD OF LY 479.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1078.Apr 30, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004300001Profile · corroded(V0XR) PROFILE AT FR 17 LY 479.0 -780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1077.Apr 30, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004290003Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE AT LY 479.0 FR 19-20 IS CORRODED BEYOND LIMITS. R & R ANGLE. W/C 1071.Apr 29, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004290002Floor Support · corroded(V0XR) OMEGA BEAM AT FR 20 RY 479.0 IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1070.Apr 29, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004290001Sill · corroded(V0XR) RT SILL FWD OF SERVICE DOOR FR 17-20 RY 780.0 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1065.Apr 29, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004280005Seat Track · corroded(V0XR) LT UPPER SEAT TRACK FR 17-23 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK. W/C 2106.Apr 28, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004280004Seat Track · corroded(V0XR) RT UPPER SEAT TRACK FR 23-30 IS CORRODED BEYOND LIMITS. R AND R RT SEAT TRACK. W/C 1095.Apr 28, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004270009Gusset · corroded(V0XR) RT GUSSET AT RY- 479.0 FR 59-61 IS CORRODED BEYOND LIMITS. R & R GUSSET. W/C 1087.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270007Seat Track · corroded(V0XR) LT UPPER SEAT TRACK AT FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1091.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004270008Seat Track · corroded(V0XR) LT UPPER SEAT TRACK AT FR 23-30 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1092.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004270001Profile · corroded(V0XR) CORRECTION TO NR5 SPECIFIC PART OR STRUCTURE CAUSING DIFFICULTY: PROFILE AT FR 16 LY-479.0 -LY 780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1076.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270005Profile · corroded(V0XR) LT PROFILE AT FR 61 IS CORRODED BEYOND LIMITS. R & R LT PROFILE. W/C 2103.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270004Partition · corroded(V0XR) RT LOWER PARTITION AT FR 61 IS CORRODED BEYOND LIMITS. R & R RT PARTITION. W/C 2102.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270003Sill · corroded(V0XR) RT SILL AT FR 61-65 IS CORRODED BEYOND LIMITS. R & R RT SILL. W/C 1089.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270002Gusset · corroded(V0XR) CORRECTION TO NR3 MAJOR EQUIPMENT IDENTITY: CTR GUSSET AT FR 59-61 Y.0.0 IS CORRODED BEYOND LIMITS. R & R CTR GUSSET. W/C 1088.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004270006Structure · corroded(V0XR) LT DIGITAL AT LY-479.0 FR 18-23 IS CORRODED BEYOND LIMITS. R & R LT DIGITAL. W/C 1061.Apr 27, 2010 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR C2XA10IA135Skin Panel · crackedIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BETWEEN THE CAPTAINS DV WINDOW AND WINDSHIELD. MAINTENANCE PERFORMED A DOUBLER REPAIR, LEAK CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SApr 26, 2010 · N16927 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR C2XA10IA133Light · out of adjustLRD - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW TWELVE TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 26, 2010 · N15948 · Emb EMB145EP · Emergency LightingSDR C2XA10IA132Connector · dirtyLRD - FLIGHT 2616, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE LAST THREE AISLE PATH LIGHT STRIPS AFT OF ROW 12 WERE INOPERATIVE. CONTRACT MAINTENANCE CLEANED THE CONNECTOR ON THE EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS. Apr 26, 2010 · N14937 · Emb EMB145EP · Light System WiringSDR V0XR201004260007Seat Track · corroded(V0XR) RT UPPER SEAT TRACK AT FR 30-36 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1096.Apr 26, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004260006Seat Track · corrodedLT UPPER SEAT TRACK AT FR 36-46 IS CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1093.Apr 26, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR V0XR201004260005Profile · corroded(V0XR) PROFILE AT FR 22 LY 479.0 - LY 780.0 IS CORRODED BEYOND LIMITS. R & R PROFILE. W/C 1062.Apr 26, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201004260004Seat Track · corroded(V0XR) RT UPPER SEAT TRACK FR 52-57 CORRODED BEYOND LIMITS. R & R SEAT TRACK. W/C 1099.Apr 26, 2010 · N805HK · Emb EMB145EP · Fuselage, Seat/Cargo Attach FittingsSDR C2XA10SH158Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM FRAME 23 IAW EMB-145 SRM 53-21-10, SRM 51-40-02 AND SRM 51-30-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH157Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 54. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM SUPPORT AT FRAME 54 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIApr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH155Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 49. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CROSSBEAM AT FRAME 49 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH154Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 44. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH153Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 44. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 44 IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH152Fitting · crackedSHV - DURING C-CHECK NR 2 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF A CRACK. MAINTENANCE REMOVED AND REPLACED NR 2 ENG YOKE FWD LWR FITTING MOUNT IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach FittingsSDR C2XA10SH151Fitting · crackedSHV - DURING C-CHECK NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING MOUNT VISUAL INDICATION OF CRACK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE FWD LOWER PYLON FWD YOKE FITTING IAW EC5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon, Attach FittingsSDR C2XA10SH150Bracket · damagedSHV - DURING C-CHECK LT AILERON PCA BRACKET I/B FLANGE HAT BUSHINGS MISSING AND HOUSING IS DAMAGED. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · AileronsSDR C2XA10SH149Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AT FRAME 39 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH148Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 3 LOCAL) AT CARBON CROSSBEAM AT FRAME 39. MAINTENANCE PERFORMED REPAIR AT LT OMEGA BEAM FRAME 38-39 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH147Inlet · corrodedSHV - DURING C-CHECK RT INLET HAS SEVERAL NUT PLATE HOLES THAT ARE CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT INLET NUT PLATE HOLES IAW EC5420-01158. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Apr 25, 2010 · N14947 · Emb EMB145EP · Nacelle/Pylon Miscellaneous StructureSDR C2XA10SH146Floor Support · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT CARBON CROSSBEAM AT FRAME 33. MAINTENANCE INSTALLED DOUBLER ON CENTER OMEGA BEAM AT CARBON CROSSBEAM AREA FRAME 33-34 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEApr 25, 2010 · N14947 · Emb EMB145EP · Fuselage Miscellaneous Structure
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