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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C2XA09TY176Floor Support · corrodedTYS - CORROSION WAS FOUND ON THE TOPCAP AT FRAME 20. MAINTENANCE REPLACED THE TOPCAP IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY174Sill · corrodedTYS - CORROSION WAS FOUND AROUND A NUT PLATE ON THE SERVICE DOOR AFT SILL. MAINTENANCE BLENDED OUT THE CORROSION, FABRICATED AND INSTALL A DOUBLER IAE EMB 145 SRM 53-21-10. ALL WORK WAS DONE AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY169Fitting · chafedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND CORROSION ON FRAME 75 VERTICAL STAB FITTING, 4 BOLT HOLES HAD SOME CORROSION. MAINTENANCE REMOVED THE FITTING AND REAMED THE FOUR HOLES AND BUSHINGS INSTALLED. THEN REINSTALL THE FITTING IAW EC 55SDR C2XA09TY173AHinge · corrodedLEFT AND RIGHT HORZ STAB HINGE PINS PITTED AND HAVE CORROSION. REPLACED HINGE PINS.SDR C2XA09IA185Metering Unit · malfunctionedMFE - FLIGHT 2627, THE CREW REPORTED THAT E2 WOULD NOT ADVANCE 85 PERCENT N2 OR 90 PERCENT N1 AND ITT WAS SPIKING ERRONEOUSLY BETWEEN 300-500 DEGREES, WITH AN EICAS CHECK MESSAGE ON MFD WITH BOTH IGNITERS ON FOR E2. THE ISSUE RESOLVED ITSELF AFTER TWO MINUTESSDR RAIA2009072100005Anti-Ice Valve · malfunctionedDREW REPORTED THAT THE NR 2 ENGINE ANTI-ICE VALVE DOESN'T SHOW OPEN. MAINTENANCE DEFERRED THE NR 2 ENGINE ANTI-ICE VALVE PER THE MEL.SDR C2XA09TY171Fitting · crackedCRACKED SHEAR CLIP AT FRM 10 JUST BELOW DV WINDOW. REMOVED CRACKED SHEAR CLIP, PARTIAL CRACKED FRM AND GUSSET AT FRM 10 JUST BELOW DV WINDOW. INSTALLED NEW SECTION OF FRM 10, REINSTALLED CONNECTING GUSSET. REPLACED SHEAR CLIP.SDR C2XA09TY170Sign · inoperativeSERVICE DOOR EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN IAW EMB 145 AMM 33-50-09. OPS CHECK GOOD.SDR RAIA2009072100001Light · inoperativeDURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT ON THE STAIRS WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE LIGHT ASSEMBLY. LIGHT OPS CHECKED GOOD.SDR C2XA09IA181Light · inoperativeDURING ROUTINE INSP, RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH194Battery · overheatedDURING C-CK, NR 2 BATTERY OVERHEATED AND HAD THERMAL RUNAWAY. REMOVED AND REPLACED NR 2 BATTERY IAW AMM 24-36-01. ACFT WAS INSPECTED AND NO OTHER DAMAGED WAS NOTED. ACFT WAS APPROVED FOR CONTINUED SERVICE.SDR C2XA09IA180Proximity Switch · inoperativeIAH - FLIGHT 2703 - DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER, SDR C2XA09IA080AProximity Sensor · inoperativeDURING CLIMB THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE LT MAIN GEAR WOW PROXIMITY SWITCH ON THE SHOCK ABSORBER, OPERATIONALLY TESTED WITH NO DEFECTS, AND SDR C2XA09TY161Sill · corrodedACFT CURRENTLY IN A C-CHECK STATUS AND CORROSION WAS FOUND UNDER THE SVC DOOR THRESHOLD PLATE AROUND THE NUT PLATES. MX REMOVED AND REPLACED SVC DOOR THRESHOLD SILL IAE SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR C2XA09TY156Sill · corrodedACFT IN C-CHECK AND THE RT FLOOR SILL WAS FOUND CORRODED BETWEEN FR 24 THRU FR 30. MX REMOVED AND REPLACED THE FLOOR SILL IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR RAIA2009071700004Battery Pack · dischargedDURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL OF THE CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK. SUBSEQUENT OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WAS GOOD.SDR C2XA09IA178Light · inoperativeIAH - FLIGHT 2115 - DURING POST FLIGHT INSPECTION THE LEFT FORWARD WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA09TY149Door Frame · corrodedCORROSION ON AFT LOWER END OF SERVICE DOOR CUT OUT FRAME. DOUBLER WAS MADE FROM A SPARE FRAME AND INSTALLED IAW EC 5310-01373.SDR C2XA09TY147Cap · corrodedRT LAV TOP CAP HAS CORROSION. BLENDED MINOR CORROSION, ALODINED, PRIMED, AND PAINTED.SDR C2XA09TY146Web · crackedNR 1 ENGINE FWD/LWR YOKE WEBBING CRACKED. REMOVED AND REPLACED NR 1 ENGINE FWD/LWR YOKE WEBBING. CLOSEDSDR C2XA09TY145Cap · corrodedLT LAV TOP CAP CORRDED, WITHIN LIMITS, BLENDED, ALODINED, PRIMED, AND PAINTED.SDR C2XA09TY144Sill · corrodedCORROSION ON LT FLOOR SILL AT FRM 43. REMOVED AND REPLACED LT FLOOR SILL.SDR C2XA09TY143Sill · corrodedRT FLOOR SILL CORRODED BETWEEN FRM 29-35. FLOOR SILL WAS REMOVED AND REPLACED.SDR C2XA09TY142Sill · corrodedCORROSION ON LT FLOOR SILL FROM FRM 18-23. FLOOR SILL WAS REMOVED AND REPLACED.SDR C2XA09TY141Floor Support · corrodedCORROSION ON CENTER OMEGA BEAM AND STEP UP AT FRM 18. CORROSION WITHIN LIMITS. BLENDED OUT, ALODINED, PRIMED, AND PAINTED.SDR RAIA2009070900001Carbon Seal · wornFLT 7939 - IAD - DURING DESCENT THE NR 2 ENGINE OIL PRESSURE DROPPED TO 15-20 PERCENT AND SHUT THE ENGINE DOWN. MAINTENANCE INSPECTED AND FOUND AN OIL LEAK BEHIND NR 2 GEN AT MAGNETIC/MECHANICAL CARBON SEAL. REMOVED AND REPLACED THE CARBON SEAL FOLLOWED BY SDR C2XA09IA173Check Valve · leakingCREW REPORTED A BLEED 2 LEAK IN CLIMB. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR 2 ESDR C2XA09IA172Clamp · looseCREW REPORTED A BLEED 2 LEAK IN CLIMB. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR SDR C2XA09IA171O-Ring · failedCREW REPORTED A BLEED 2 LEAK IN CLIMB. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE BLEED 2 O-RINGS IN THE BELLY AREA, REPLACED THE AIR START GROUND CONNECTION CHECK VALVE, AND RESECURED THE CLAMPS ON THE NR 2 ESDR C2XA09TY137ASocket · brokenEMERGENCY LIGHT IN THE MAIN DOOR AND THE SERVICE DOOR INOP. REMOVED AND REPLACED THE LIGHT SOCKETS IAW EMB AMM 33-50-06. OPS CHECK GOOD.SDR C2XA09TY173Sill · corrodedCORROSION ON LT FLOOR SILL FROM FRM 18-23. REPLACED SILL.SDR RAIA2009070700003Light · blownPRE FLT - STL - CREW REPORTED THAT THE EMERGENCY LIGHT AT THE MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND FOUND THAT THE BULB WAS BLOWN. THE BULB WAS REMOVED AND REPLACED AND THE EMERGENCY LIGHTS OPS CHECKED GOOD.SDR C2XA09IA168Electronic Unit · inoperativeIAH - FLIGHT 2605 - THE CREW REPORTED A LANDING GEAR DISAGREE ON CLIMBOUT AND THE 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 SDR C2XA09TY132Skin · damagedTYS - FOUND LIGHTNING STRIKE DAMAGE AT FRAME 38 AND STR 15L. MAINTENANCE REMOVED AND REPLACED BURNED RIVET IAW SRM 51-40-02 AND PAINTED IAW CPM 51-21-06. PRESSURIZATION CHECKS GOOD AND WAS RELEASED.SDR C2XA09TY131Skin · damagedTYS - AIRCRAFT HAD A LIGHTNING STRIKE DAMAGE AT FR 40 STR 14L. MAINTENANCE REMOVED AND REPLACED THE BURNT RIVET IAW SRM 51-40-02. PAINTED IAW CPM 51-21-06. PRESSURE CHECKS GOOD AND WAS RELEASED TO SERVICE.SDR C2XA09CL090Unknown · odorCLE - FLT 2743 - THE CREW REPORTED AN ELECTRICAL ODOR IN THE GALLEY, MOST NOTICEABLE NEAR THE COFFEEMAKER. MAINTENANCE INSPECTED AND DEFERRED SYSTEM ON NEF. SUPPLEMENT TO FOLLOW.SDR RAIA200906290003A/C Pack · malfunctionedFLT 7928 - CHS - PAC NR 1 OVERLOAD MESSAGE. MAINTENANCE DEFERRED NR 1 PAC.SDR C2XA09TY129Mount · corrodedNR 1 AND NR 2 ENG INLET BOLT HOLES SCARED AND/OR HAVE CORROSION. REMOVED DAMAGE AND CORROSION FROM BOLT HOLES ON INLET MOUNT FLANGE IAW EC5420-01158B.SDR RAIA200906290001Brake Assy · overtempFLT 8057 - ORD - BRAKE OVERTEMP MESSAGE ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED NR 1 BRAKE.SDR C2XA09IA164Control Handle · inoperativeIAH - FLIGHT 2104 - THE CREW REPORTED WHEN COMMANDED GEAR SW TO UP, GEAR DID NOT RETRACT. TEN TO FIFTEEN SECONDS LATER CREW RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS, AND THE GEAR RETRACTED, AND EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO IAH SDR RAIA200906250003Light · inoperativeDURING PRE-FLIGHT AT CID, FOUND CEILING EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT.SDR C2XA09TY126Yoke · crackedNR 1 ENGINE LOWER FWD YOKE WEBBING CRACKED. THE LOWER FWD YOKE WAS REMOVED AND REPLACED.SDR RAIA200906250002Printed Ckt Board · overheatedFLT 7933 - UNSCHEDULED LANDING AT STL. CREW REPORTED BURNING PLASTIC SMELL IN CABIN BUT NO VISIBLE SMOKE. MAINTENANCE REMOVED AND REPLACED PRINTED CIRCUIT BOARD IN GALLEY CONTROL MODULE.SDR RAIA200906250001Inverter · inoperativeDURING PRE-FLIGHT AT PHL, CREW REPORTED EMERGENCY LIGHT STRIPS 2&3 INOP. MAINTENANCE REMOVED AND REPLACED NR 3 INVERTER AND NR 3 FLOOR LIGHT STRIP.SDR C2XA09TY125Fitting · wornDURING C-CHECK FRAME 75 TO VERTICAL STAB SPAR FITTING WAS FOUND FRETTING. MX REMOVED AND REPLACED THE VERTICAL STAB SPAR FITTING IAW EC 5310-01317. ACFT STILL IN C-CHECK.SDR C2XA09TY123Skin Panel · crackedTYS DURING A CURRENT 6C INSPECTION THE LEFT LOWER WING SKIN WAS FOUND CRACKED AT THE LOWER INBOARD FLAP SHROUD O/B HOLE. MAINTENANCE REPAIRED THE LEFT LOWER WING SKIN AROUND THE LOWER INBOARD FLAP SHROUD OUTBOARD HOLE IAW EC 5710-01160. ALL WORK ACCOMPLISHEDSDR C2XA09TY130Attach Bracket · wornLT AND RT GROUND SPOILER MIDDLE ATTACH BRACKET HAS MIGRATING HAT BUSHINGS. REMOVED AND REPLACED BOTH LT AND RT BRACKETS IAW EMB 145 SRM 51-20-03.SDR C2XA09IA159Ballast · overheatedIAH - FLIGHT 2414 - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN ROW 1. MAINTENANCE REMOVED AND REPLACED THE LIGHTING BALLAST ABOVE ROW 1, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA158Selector · inoperativeIAH - FLIGHT 2967 - THE CREW REPORTED THAT THE FLAPS FAILED AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRSDR C2XA09IA156Windshield · crackedIAH - FLIGHT 2809, THE CREW REPORTED THAT THE F/O'S WINDSHIELD CRACKED ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S WINDSHIELD, OPERATIONALLY & LEAK CHECKED WITH NO DEFECTS, AND THE AIRCR
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