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 RAIA201007060002Seal · lack of lubeFLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR SEAL. DOOR OPS CHECKED GOOD.Jul 6, 2010 · N807HK · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA201006200001Light · inoperativeDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR EMERGENCY INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EMERGENCY LIGHT BULB. SYSTEM OPS CHECKED GOOD.Jun 20, 2010 · N807HK · Emb EMB145EP · Emergency LightingSDR C2XA10IA179Light · inoperativeIAH - DURING MAINTENANCE INSPECTION THE NR 4 AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AISLE PATH LIGHT STRIP ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IAH MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE Jun 18, 2010 · N13929 · Emb EMB145EP · Emergency LightingSDR C2XA10IA177Battery · overheatedIAH - FLIGHT 3121, THE CREW REPORTED A BATTERY TWO OVER-TEMP ON DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR REJun 18, 2010 · N14930 · Emb EMB145EP · Battery/Charger SystemSDR C2XA10SH201Warning Light · false activationFLT 2213 DIVERT - E1 BLEED LK MSG-E1 COMMANDED SHUTDOWN INFLT. MAINTENANCE DOWNLOADED DFDR AND CMC - NO FAULTS FOUND, RAN AC, NO LEAKS. PERFORMED BLEED OPERATIONAL CHECKS IAW EMB-145 AMM 36-00-00 AND 36-11-09, ALL OPERATIONAL CHECKS GOOD. TEST FLIGHT GOOD. Jun 11, 2010 · N14945 · Emb EMB145EP · Pneumatic Distribution SystemSDR C2XA10IA169Adc · faultyFLIGHT 2734 - DURING CRUISE AT 36,000 FEET THE CAPTAIN'S AIRSPEED INDICATION STUCK AT 215 KIAS FOR 10 TO 15 MINUTES. AT THAT TIME THE STANDBY AND FIRST OFFICER'S AIRSPEED INDICATIONS WERE OPERATING NORMALLY. UPON DESCENT THE CREW LOST THE CAPTAINS AND FIRST Jun 7, 2010 · N13989 · Emb EMB145EP · Air Data ComputerSDR C2XA10SH199Skin · crackedSHV - DURING C CHECK IT WAS FOUND THAT THE VERTICAL STABILIZER INTERNAL FITTING WAS FRETTING WITH THE AFT FUSELAGE SKIN AT FRAME 75 BY STRINGER 1L. THE FRETTING CAUSED THE SKIN TO CRACK AND WAS DETECTED USING EDDY CURRENT. MAINTENANCE PERFORMED A DOUBLER REPJun 7, 2010 · N14942 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR C2XA10SH198Attach Bracket · wornSHV - DURING C CHECK THE LT SPEED BRAKE CENTER ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 7, 2010 · N14942 · Emb EMB145EP · SpoilersSDR C2XA10SH197Attach Bracket · wornSHV - DURING C CHECK THE LT GROUND SPOILER ACTUATOR ATTACH BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHING. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC5750-01415. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 7, 2010 · N14942 · Emb EMB145EP · SpoilersSDR C2XA10SH196Beam · corrodedSHV - DURING C CHECK THE PILOTS WINDSHIELD CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT SCREW HOLES 41, 43, 45, 49. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A BUSHING REPAIR IAW EC5310-01515. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 7, 2010 · N14942 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH195Floor Support · corrodedSHV - DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 7, 2010 · N14942 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH194Skin · crackedSHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENER AT FRAME 75 BETWEEN STRINGERS 1-2R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-02146. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 7, 2010 · N14942 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA201006060001Connector · looseDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE EMERGENCY FLOOR LIGHTS AT SEAT LOCATION 18A DID NOT ILLUMINATE. MAINTENANCE INSPECTED AND RE-CONNECTED THE EMERGENCY LIGHT CONNECT0R AT 18A. SYSTEM OPS CHECKED GOOD.Jun 6, 2010 · N808HK · Emb EMB145EP · Light System WiringSDR C2XA10SH189Beam · corrodedSHV-DURING C CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC 5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 2, 2010 · N14942 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10IA165Skin · corrodedIAH - DURING MAINTENANCE INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 72 & 73 AT STRINGER 21R. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN PANEL, OPERATIONAL CHECKS COMPLETED WITHOUT DEFECT. AIRCRAFT WAS APPROVED FOR RETURJun 1, 2010 · N17928 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA201005310001Seal · lack of lubeDURING PRE-FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND LUBRICATED THE PASSENGER DOOR SEAL. PASSENGER DOOR OPS CHECKED GOOD.May 31, 2010 · N806HK · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA2010052300001Roller · lack of lubeFLIGHT CREW REPORTED, UNABLE TO OPEN THE PAX DOOR FROM THE OUTSIDE. MAINTENANCE INSPECTED AND LUBED THE PAX DOOR ROLLERS AND REMOVED DEBRIS FROM THE DOOR. PAX DOOR OPS CHECKED GOOD.May 23, 2010 · N805HK · Emb EMB145EP · Passenger/Crew DoorsSDR C2XA10IA160Indicator · defectiveCRP - FLIGHT 2894, DURING CLIMB THE CREW REPORTED THAT THE NUMBER ONE FUEL QUANTITY INDICATOR DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY REPEATER OPERATIONALLY TESTED THE FUELMay 23, 2010 · N15948 · Emb EMB145EP · Fuel Quantity IndicatorSDR RAIA2010052200001Light · inoperativeDURING PREFLIGHT INSPECTION THE FLIGHT CREW REPORTED THE AIR STAIR DOOR EMERGENCY LIGHT AS BEING INOPERATIVE. MAINTENANCE DEFERRED THE AIR STAIR DOOR EMERGENCY LIGHT PER MEL 33-50-00-1.May 22, 2010 · N808HK · Emb EMB145EP · Emergency LightingSDR C2XA10IA161Control Lever · defectiveIAH - FLIGHT 2959, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT COMING OUT OF MOB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAMay 21, 2010 · N15926 · Emb EMB145EP · Landing Gear SelectorSDR RAIA2010051900001Light · inoperativeDURING THE PREFLIGHT INSPECTION, THE FLIGHT CREW REPORTED THE COCKPIT CEILING EMERGENCY LIGHT AS BEING INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND REMOVED AND REPLACED THE BULB. SYSTEM OPS CHECKED GOOD.May 19, 2010 · N806HK · Emb EMB145EP · Emergency LightingSDR CHQA201000099Connector · misinstalledTHE CREW REPORTED THAT ON LANDING IN CMH THE BRAKES WERE NOT AS EFFECTIVE AS NORMAL. DURING POST FLIGHT INSPECTION THE LEFT OUTBOARD TIRE WAS FLAT SPOTTED AND BLOWN. MAINTENANCE INSPECTED THE LEFT GEAR AND FOUND THE WHEEL SPEED TRANSDUCER CONNECTORS FOR THE May 19, 2010 · N978RP · Emb EMB145EP · Landing Gear System WiringSDR CHQA201000098Tire · low pressureTHE CREW REPORTED THAT ON LANDING IN LGA THE AIRCRAFT HAD POOR BRAKING AND DRIFTED TO THE RIGHT AT HIGH SPEED. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. UPON POST FLIGHT INSPECTION THE LEFT OUTBOARD TIRE WAS LOW. MAINTENANCE REPLACED BOTH TIRES ON TMay 19, 2010 · N978RP · Emb EMB145EP · TireSDR C2XA10SH178Floor Support · corrodedSHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 54. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH177Floor Support · corrodedSHV - DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH176Floor Support · corrodedSHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA10SH175Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 19, 2010 · N14938 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2010051800001Door · lack of lubeDURING POST FLIGHT INSPECTION THE FLIGHT ATTENDANT REPORTED THE MAIN PAX DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBED THE MAIN PAX DOOR. OPS CHECKED GOOD.May 18, 2010 · N806HK · Emb EMB145EP · Passenger/Crew DoorsSDR C2XA10IA153Light · overheatedIAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14937 · Emb EMB145EP · Passenger Compartment LightingSDR C2XA10IA151Hose · unknownIAH - DURING MAINTENANCE INSPECTION A BURNING SMELL WAS NOTED AT SEAT 11A AREA. MAINTENANCE REMOVED AND REPLACED SIDEWALL LIGHTS FROM 10A-12A, AND GASPER HOSE AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14937 · Emb EMB145EP · Air Distribution SystemSDR C2XA10IA150Ballast · overheatedIAH - DURING POST FLIGHT INSPECTION, AN ELECTRICAL SMELL MID CABIN WAS REPORTED WITH NO SMOKE OBSERVED. MAINTENANCE REMOVED AND REPLACED THE BALLAST AT 11A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14937 · Emb EMB145EP · Passenger Compartment LightingSDR C2XA10SH174Skin · crackedSHV - DURING C-CHECK THE LT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2L-7L. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED FASTENERS IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR C2XA10SH173Skin · crackedSHV - DURING C-CHECK THE RT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED HOLES IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR C2XA10SH172Frame · crackedSHV - DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L RIGHT BELOW THE LT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, FrameSDR C2XA10SH171Frame · crackedSHV - DURING C-CHECK FRAME 10 AT STRINGER 10R WAS FOUND TO BE CRACKED RIGHT BELOW THE RT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14938 · Emb EMB145EP · Fuselage Main, FrameSDR C2XA10SH170Yoke · crackedSHV - DURING C-CHECK THE RT ENGINE FORWARD LOWER YOKE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED YOKE IAW EC 5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 18, 2010 · N14938 · Emb EMB145EP · Nacelle/Pylon, Attach FittingsSDR C2XA10IA144Skin · crackedIAH - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 12, 2010 · N13929 · Emb EMB145EP · Fuselage Main, Plate/SkinSDR RAIA2010051000002Roller · dirtyDURING PREFLIGHT THE FLIGHT CREW REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND CLEANED THE PASSENGER DOOR ROLLERS AND SEALS OF DEBRIS. PASSENGER DOOR OPS CHECKED GOOD.May 10, 2010 · N801HK · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA2010051000001Unknown · odorDURING DESCENT THE FLIGHT CREW REPORTS SMOKE SMELL IN CABIN. MAINTENANCE INSPECTED BLEED AIR DUCTS AND CABIN LIGHT FIXTURES. MAINTENANCE PREFORMED OPS CHECK OF BLEED AIR SYSTEM. BLEED AIR SYSTEM OPS CHECKED GOOD, COULD NOT DUPLICATE PROBLEM.May 10, 2010 · N803HK · Emb EMB145EP · Air Distribution SystemSDR C2XA10IA143Skin · crackedIAH - DURING MAINTENANCE INSPECTION THE LEFT UPPER WING SKIN WAS FOUND TOP BE CRACKED AT THE SPEED BRAKE CENTER HINGE POINT CUTOUT. MAINTENANCE PLACED THE ITEM ON DEFERRED MAINTENANCE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSTALLEDMay 9, 2010 · N17928 · Emb EMB145EP · Wing, Plate/SkinSDR V0XR201005030023Bolt · corroded(V0XR) NR 1 RUDDER ACTUATOR CTR ATTACHMENT BOLTS ARE CORRODED BEYOND LIMITS. R & R ACTUATOR BOLTS.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201005030022Strip · crackedRT WING TO FUSELAGE FAIRING STRIP X=12473.0 - X=13893.0 IS CRACKED. REMOVED AND REPLACED STRIP. W/C 2135May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030021Strip · cracked(V0XR) LT WING TO FUSELAGE FAIRING STRIP X=14967.0 - X=16143.5 IS CRACKED. R & R STRIP. W/C 2132.May 3, 2010 · N805HK · Emb EMB145EP · Aerodynamic FairingsSDR V0XR201005030020Guide · broken(V0XR) RIGHT NR 2 CABLE GUIDE SUPPORT AT FR 25 IS BROKEN. R & R CABLE GUIDE.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030019Guide · broken(V0XR) LEFT NR 4 CABLE GUIDE BROKEN. R & R CABLE GUIDE.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030018Guide · broken(V0XR) LEFT NR 2 CABLE GUIDE BROKEN. R & R CABLE GUIDE. W/C 1118.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Main, StructureSDR V0XR201005030017Floor Support · corroded(V0XR) BEAM FR 20 BETWEEN LT OMEGA BEAM AND CTR OMEGA BEAM IS CORRODED BEYOND LIMITS. R & R BEAM. W/C 1102.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030016Angle · corroded(V0XR) ANGLE FR 23 AT RY 780.0 IS CORRODED BEYOND LIMITS. R & R ANGLE.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030015Channel · corroded(V0XR) RT HAT CHANNEL BEAM FR 16-25 AT RY 479.0 IS CORRODED BEYOND LIMITS. R & R BEAM.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous StructureSDR V0XR201005030014Floor Support · corroded(V0XR) FLOOR SUPPORT ANGLE FR 18-20 AT Y0.0 IS CORRODED BEYOND LIMITS. R & R ANGLE.May 3, 2010 · N805HK · Emb EMB145EP · Fuselage Miscellaneous Structure
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