Embraer EMB-145EP

Service difficulty reports · 2,197

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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 RAIA2009081700001Duct · brokenCREW REPORTED THAT THE NUMBER 1 PACK WAS PRODUCING A ABNORMAL SMELL AND WAS WEAK FOR PRESSURIZATION. MAINTENANCE REMOVED AND REPLACED A DUCT AND SEVERAL CLAMPS AT THE NUMBER 1 PACK. OPS AND LEAK CHECKED GOOD.Aug 11, 2009 · N807HK · Emb EMB145EP · Air Distribution SystemSDR C2XA09TY214Door Frame · corrodedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION AT FRAME 22 AT THE SERVICE DOOR CUTOUT. MAINTENANCE CUT OUT THE DAMAGE SECTION AND REPLACED. COLD WORK THE TWO HOLES FOR THE DOOR STOPS IAW EA 5310-01054. ALL WORK WAS ACCOMPLISHED AND WILL BE RAug 7, 2009 · N14933 · Emb EMB145EP · Fuselage Main, StructureSDR C2XA09TY213Sill · corrodedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE SERVICE DOOR SILL CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-07. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED Aug 7, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09IA199Wire · brokenIAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROWS 16 & 17 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEAug 6, 2009 · N14942 · Emb EMB145EP · Light System WiringSDR C2XA09IA198Wire · brokenIAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 & 9 WAS FOUND TO HAVE BROKEN WIRES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 6, 2009 · N14942 · Emb EMB145EP · Light System WiringSDR C2XA09SH280Floor Support · corrodedSHV - DURING C-CK, RT OMEGA BEAM HAS CORROSION AT FR 22. REPAIRED RT OMEGA BEAM IAW EC 5320-01467. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 5, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2009081000003Control Lever · faultyDURING CLIMB AFTER TAKEOFF, CREW REPORTED THAT THE LANDING GEAR HANDLE WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER AND THE SYSTEM OPS CHECKED GOOD.Aug 4, 2009 · N804HK · Emb EMB145EP · Landing Gear SelectorSDR C2XA09TY212Firewall · crackedTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND A CRACK IN THE APU FIREWALL. MAINTENANCE REMOVED AND REPLACED THE FIREWALL IAW EMB 145 SRM 51-40-02 AND IC 2009-145/06143. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Aug 4, 2009 · N14933 · Emb EMB145EP · Fuselage Main, BulkheadSDR RAIA2009081000001Wire · looseDURING PRE FLIGHT INSPECTION, CREW REPORTED THAT THE AFT OVERHEAD AISLE EMERGENCY LIGHT AS BEING INOPERATIVE. MAINTENANCE RESECURED A LOOSE WIRE TO THE LIGHT ASSEMBLY.Aug 3, 2009 · N802HK · Emb EMB145EP · Light System WiringSDR C2XA09SH261Battery · dischargedSHV - DURING C-CHECK PROXIMITY LIGHT 3 AND 4 FAILED OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED NUMBER 3 EMERGENCY LIGHT BATTERY IAW EMB-145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Emergency LightingSDR C2XA09SH260Hinge · wornSHV - DURING C-CHECK MAIN DOOR LOWER HINGE LOCK PIN HAS MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED MAIN DOOR LOWER HINGE IAW EMB-145 AMM 52-18-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Passenger/Crew DoorsSDR C2XA09SH259Hinge · wornSHV - DURING C-CHECK LT AILERON OUTBOARD HINGE POINT HAS MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED LT AILERON O/B HINGE POINT IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · AileronsSDR C2XA09SH258Floor Support · corrodedSHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FRAME 17-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09SH257Support Bracket · crackedSHV - DURING C-CHECK FRAME 10 SUPPORT BRACKET CRACKED JUST UNDER LEFT DV WINDOW LOWER CUTOUT FRAME. MAINTENANCE REMOVED AND REPLACED SUPPORT BRACKET AT FRAME 10 LT IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09SH256Channel · crackedSHV - DURING C-CHECK FRAME 10 CRACKED AT STRINGER 13L. MAINTENANCE REMOVED AND REPLACED CHANNEL AT FRAME 10 STRINGER 13L IAW EMB-145 SRM 51-40-02 AND CPM 51-21-05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09SH255Doubler · corrodedSHV - DURING C-CHECK RT DOUBLER AT FRAME 61 CORRODED (LEVEL 2 LOCAL) AT RIVET HOLES (BEHIND CARBON CROSS BEAM). MAINTENANCE REMOVED AND REPLACED RT DOUBLER AT FRAME 61 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09SH254Buttstrap · corrodedSHV - DURING C-CHECK LT OMEGA BEAM BUTTSTRAP HAS CORROSION (LEVEL 2 LOCAL) FRAME 46-53. MAINTENANCE REMOVED AND REPLACED LT OMEGA BEAM BUTTSTRAP FRAME 46-53 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09SH253Fitting · crackedSHV - DURING C-CHECK LEFT O/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT O/B LEADING EDGE SPLICE SHEAR CLIP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Wing Miscellaneous StructureSDR C2XA09SH252Fitting · crackedSHV - DURING C-CHECK LEFT I/B LEADING EDGE SPLICE SHEAR CLIP CRACKED. MAINTENANCE REMOVED AND REPLACED LEFT I/B LEADING EDGE SPLICE SHEAR CLIP IAW SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Wing Miscellaneous StructureSDR C2XA09SH251Hinge · wornSHV - DURING C-CHECK LT GROUND SPOILER CENTER HINGE O/B FITTING I/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER CENTER HINGE IAW EMB-145 AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · SpoilersSDR C2XA09SH250Bracket · wornSHV - DURING C-CHECK LT GROUND SPOILER I/B HINGE O/B HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED LT GROUND SPOILER I/B BRACKET IAW EMB-145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · SpoilersSDR C2XA09SH249Hinge · damagedSHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE O/B HOLE OF ATTACHMENT BRACKET ON WING DAMAGED. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER HINGE IAW EMB-145 AMM 20-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · SpoilersSDR C2XA09SH248Sill · corrodedSHV - DURING C-CHECK CENTER SERVICE DOOR SILL IS CORRODED (LEVEL 2 LOCAL) IN VARIOUS SPOTS. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 3, 2009 · N16927 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY211Angle · crackedGALLEY CENTER AISLE LT RAMP ANGLE CRACKED. REMOVED AND REPLACED RAMP ANGLE.Aug 3, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2009080600006Inverter · inoperativeCREW REPORTED THAT THE EMERGENCY EXIT LIGHT ON THE BULKHEAD AT SEAT 3BC WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER FOR THE EMERGENCY EXIT LIGHT. FOLLOW ON OPERATIONAL CHECK WAS GOOD.Aug 2, 2009 · N807HK · Emb EMB145EP · Emergency LightingSDR C2XA09TY210Fitting · crackedSHEAR CLIP CRACKED AT FRM 77 STR 1R. REMOVED AND REPLACED CRACKED SHEAR CLIP.Aug 2, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2009080600005Connector · dirtyCREW REPORTED THAT THE FORWARD BULKHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR TO THE NR 3 INVERTER AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD.Aug 1, 2009 · N807HK · Emb EMB145EP · Light System WiringSDR C2XA09TY209Bracket · crackedBRACKET CRACKED AT FRM 81 TO STR 8R. REMOVED AND REPLACED SHEAR CLIP.Jul 31, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY208Fitting · crackedSHEAR CLIP CRACKED AT FRM 81 TO STR 8L. REMOVED AND REPLACED SHEAR CLIP.Jul 31, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY207Floor Support · corrodedGALLEY AREA CENTER OMEGA BEAM TOP CAP HAS SMALL AREAS OF CORROSION. CENTER TOP CAP WAS REMOVED AND REPLACED.Jul 31, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY199Sill · corrodedTYS - A/C IN C-CHECK WHEN INSPECTION FOUND THE LEFT FLOOR SILL CORRODED FROM FRAME 23 TO FRAME 29 (SSI 53-20-11). MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS WHICH WERE OUTSIDE THE MFG'S LIMITS. ALL WORK WAS DONE IAW EMB 145 SRM 51-20-03 AND 51-40-02. Jul 30, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY197Bearing Cap · corrodedTYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND CORROSION ON THE RIGHT FORWARD MAIN LANDING GEAR BEARING CAP WITH DEEP PITTING. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB 145 AMM 32-20-01-400-801-A, SSI REFERENCE 57-26-94. ALL WORK WAS ACCOJul 30, 2009 · N14933 · Emb EMB145EP · Main Landing GearSDR C2XA09TY206Bearing Cap · corrodedRIGHT AFT MAIN LANDING GEAR BEARING CAP HAS DEEP PITTING CORROSION. REMOVED AND REPLACED CAP.Jul 29, 2009 · N14933 · Emb EMB145EP · Main Landing GearSDR C2XA09TY203Angle · corrodedGALLEY CENTER AISLE RT RAMP ANGLE CORRODED BEYOND LIMITS AT CARBON CROSS BEAM. REMOVED AND REPLACED RAMP ANGLE.Jul 29, 2009 · N14933 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY201Case · corrodedNR 2 ENG FAN CASE FWD FLANGE HAS CORROSION IN BOLT HOLES. REMOVED CORROSION FROM 12 HOLES BY REAMING IAW EC 7220-01066.Jul 29, 2009 · N14933 · Emb EMB145EP · Turbine Engine Air Inlet SectionSDR RAIA2009080600003Cooling Fan · out of adjustCREW REPORTED THAT DURING CRUISE, RECEIVED AN AHRS 1 OVERHEAT MESSAGE ON THE EICAS. MAINTENANCE PERFORMED AN ADJUSTMENT AND TEST OF THE AHRS COOLING FAN. NO DEFECTS WERE NOTED.Jul 28, 2009 · N806HK · Emb EMB145EP · Air Distribution FanSDR RAIA2009080600002Mechanism · lack of lubeCREW REPORTED THAT THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE DOOR OPERATING MECHANISM AND HINGES. FOLLOW-ON OPERATIONAL CHECK OF THE DOOR WAS GOOD.Jul 28, 2009 · N806HK · Emb EMB145EP · Passenger/Crew DoorsSDR RAIA2009080600001Wire · loosePRE FLT 7918 - SYR - CREW REPORTED THAT THE EMERGENCY EXIT SIGN IN FRONT OF SEAT 3A WAS INOPERATIVE. MAINTENANCE SECURED SOME LOOSE WIRES AT THE EMERGENCY LIGHT ASSEMBLY. FOLLOW-ON OPERATIONAL CHECK OF THE EMERGENCY LIGHTS CHECKED GOOD.Jul 28, 2009 · N807HK · Emb EMB145EP · Light System WiringSDR C2XA09TY193Fitting · wornRT SPEED BRAKE ACTUATOR BRACKET LOWER ATTACHMENT HAT BUSHING BORE OUT OF LIMITS. REMOVED AND REPLACED FITTING.Jul 28, 2009 · N14933 · Emb EMB145EP · Drag Control ActuatorSDR C2XA09TY187Bushing · wornTYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND THE RIGHT GROUND SPOILER, CENTER HINGE BRACKET HAT BUSHING RACE OUT OF MFG'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EMB 145 SRM 51-40-02. A/C WILL BE RELEASED AT THE END OF THE CHECK. SSJul 28, 2009 · N14933 · Emb EMB145EP · SpoilersSDR RAIA2009072800004Anti-Ice System · malfunctionedDURING CRUISE, CREW RECEIVED A WING ANTI-ICE FAIL MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE WING ANTI-ICE SYSTEM PER THE MEL.Jul 27, 2009 · N801HK · Emb EMB145EP · Airfoil Anti/De-ice SystemSDR C2XA09TY186Floor Support · corrodedTYS - A/C WAS IN A C-CHECK STATUS WHEN CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAMES 20 AND 21. MAINTENANCE REPLACED THE PREVIOUS REPAIR BY REMOVING THE PREVIOUS REPAIR AND INSTALLED A NEW RAMP ANGLE AND A NEW REPAIR FOR THE OMEGA BEAM IAW 135/145 SRM Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY185Sill · corrodedTYS - A/C WAS IN A C-CHECK WHEN CORROSION WAS FOUND IN THE FLOOR SILL AT FRAME 24 THRU 30. MAINTENANCE REPLACED THE FLOOR SILL IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY184Sill · corrodedTYS - A/C WAS IN A C-CHECK STATUS WHEN THE LEFT FLOOR SILL WAS FOUND CORRODED AT FRAME 30 THRU 35. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AT THE END OF THE CHECK.Jul 27, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR RAIA2009072800003Connector · looseCREW REPORTED THE GALLEY BULKHEAD EMERGENCY EXIT SIGN AS BEING INOPERATIVE. MAINTENANCE RESET THE ELECTRICAL CONNECTOR GOING TO THE LIGHT ASSEMBLY AFTER WHICH THE EMERGENCY LIGHT OPERATED AS PER THE AMM PROCEDURES.Jul 26, 2009 · N807HK · Emb EMB145EP · Light System WiringSDR C2XA09IA187Duct · leakingIAH - FLIGHT 2834, THE CREW REPORTED A BLEED 1 LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT BEHIND PANEL 271DLW, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAJul 24, 2009 · N15941 · Emb EMB145EP · Pneumatic Distribution SystemSDR C2XA09TY180Spar Cap · corrodedTYS - SURFACE CORROSION WAS FOUND ON THE LEFT WING SPAR ONE I/B CAP. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 57-20-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jul 24, 2009 · N14933 · Emb EMB145EP · Wing SparSDR C2XA09TY179Floor Support · corrodedTYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE FWD DIGITAL PLATE. MAINTENANCE REMOVED THE LITE CORROSION IAW EMB 135/145 SRM 51-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY178Floor Support · corrodedTYS - CORROSION WAS FOUND AROUND THE NUT PLATES ON THE PAX DOOR ENTRYWAY AT THE AFT DIGITAL PLATE. MAINTENANCE BLENDED OUT THE LIGHT CORROSION IAW EMB 135/145 SRM 53-21-10. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous StructureSDR C2XA09TY177Floor Support · corrodedTYS - CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 22. MAINTENANCE BLENDED OUT THE CORROSION IAW EMB 135/145 SRM 51-40-01 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.Jul 24, 2009 · N14937 · Emb EMB145EP · Fuselage Miscellaneous Structure
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