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.
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
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 C2XA05SH031Floor Support · corrodedSHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 46 TO FRM 52. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM FRM 46 TO FRM 52 IAW EC 5320-01231. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05BT029Sign · inoperativeEWR - CO2338, DURING SERVICE AND ROUTINE CHECK MAINTENANCE FOUND THE LEFT EMERGENCY EXIT SIGN WINDOW EXIT DOES NOT ILLUMINATE. REMOVED AND REPLACED LEFT EMERGENCY EXIT SIGN WINDOW EXIT IAW EMB AMM NR 33-50-13, OPS CHECKED GOOD.SDR C2XA05BT027Odor · detectedCREW REPORTED, BURNING ODOR COMING FROM RELAY BOX UNDER GEAR PINS. MAINTENANCE PERFORMED VISUAL INSPECTION OF LEFT HAND POWER DISTRIBUTION PANEL, NO ARCING OR BURNED AREAS NOTED. FOUND FORWARD COOLING AIR DUCT DISCONNECTED, RECONNECTED DUCT AND APPLIED POWERSDR C2XA05CL033Sign · inoperativeCLE - THE CREW REPORTED THE EMERGENCY EXIT SIGN DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN AND THE OPERATIONAL TESTS WERE GOOD.SDR C2XA05CL031Lamp · inoperativeCLE - DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT LOCATED ON THE PAX DOOR DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REPLACED THE LIGHT BULB AND THE OPERATIONAL TEST WAS GOOD.SDR C2XA05IA064Relay · failedIAH - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL ON TAKEOFF AND A WEIGHT ON WHEEL FAILURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0453 & K0352, OPERATIONALLY CHECKED WITH NO DEFECTS, THE SDR C2XA05IA063Control Unit · inoperativeCRP - THE CREW REPORTED THAT DURING TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CRP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, ANSDR C2XA05CL028Odor · detectedPIT FLT 2864, THE CREW REPORTED AN ELECTRICAL BURNING ODOR. CLEVELAND SENT A MAINTENANCE CREW TO INSPECT AND TROUBLESHOOT THE ODOR, THE MAINTENANCE CREW FOUND A MAGAZINE BLOCKING THE HEATING VENT AND COULD NOT DUPLICATE THE REPORTED CONDITIONS.SDR C2XA05IA061Control Unit · inoperativeDFW - DURING TAXI, THE CREW REPORTED THAT THE BRAKES WERE SPONGY, AND CHATTERING. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE BRAKE CONTROL UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05CL026Light · inoperativeDURING ROUTINE MAINTENANCE IN CLEVELAND THE EMERGENCY LIGHT ON THE SERVICE DOOR DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL TESTS WERE GOOD.SDR C2XA05CL025Sign · malfunctionedDURING ROUTINE MAINTENANCE IN CLEVELAND THE EXIT SIGN ON THE RIGHT FORWARD BULKHEAD (FORWARD OF SEAT 3B) DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE CYCLED THE EMERGENCY LIGHT CIRCUIT BREAKER AND THE OPERATIONAL TEST WAS GOOD.SDR C2XA05RI007Lamp · burned outRIC - DURING SCHEDULED MAINTENANCE, THE RIGHT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECK GOOD. A/C RELEASED TO SERVICE.SDR CA050425001Turbine Blades · failed(CAN) FOLLOWING A LOUD BANG, UNCOMMANDED IN FLIGHT SHUTDOWN, ENGINE FOR INVESTIGATION. STRIP REVEALED THAT ONE HPT BLADES HAS FAILED AT ROOT. REQUESTED FOR FAILED MATERIAL TO BE RETURNED FOR FAILURE ANALYSIS.SDR C2XA05IA055Connector · dirtyIAH - FLIGHT 2638, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE CLEANED THE ELECTRICAL CONNECTORS, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA05BT021Sign · malfunctionedBTV - MX DURING CABIN INTERIOR CHECK EMERGENCY EXIT SIGN AT 12A INOP. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING IAW EMB-145 MM 33-50-00. NO FAULT FOUND.SDR C2XA05IA053Engine · failedOKC - FLIGHT 3453, THE CREW REPORTED AN ENGINE NR 1 INFLIGHT FAILURE, LOUD BANG FOLLOWED BY UNCOMMANDED SHUTDOWN. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITSDR C2XA05SH023Light · inoperativeSHV - DURING A SERVICE/ROUTINE CHECK THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB 145 AMM 33-50-10. THE ENSUING OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS APPROVESDR C2XA05CL019Outflow Valve · failedCLE - THE CREW REPORTED, LOST ALL PRESSURIZATION WHILE CRUISING AT 22,000 FT. THE CREW MADE AN EMERGENCY DESCENT. THE CREW WAS ABLE TO REGAIN CONTROL OF PRESSURIZATION USING MANUAL CONTROL, AND LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACESDR RAI00504004Pressure Switch · leakingDAY - STRONG FUEL SMELL IN THE COCKPIT, AFTER TAKEOFF. MAINTENANCE INSPECTED AIRCRAFT FOUND APU FUEL PRESS SWITCH LEAKING. DEFERRED APU PER MEL 49-00-00.SDR C2XA05IA051Control Unit · faultyDURING CLIMB THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. THE CREW PERFORMED AN OVER-RIDE TO RETRACT GEAR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU). THE GEAR OPESDR RAIA00503013Tube · leakingFLT 3588 - RIC - ENGINE NR 2 FIRE WARNING. MAINTENANCE REMOVED AND REPLACED NR 2 HP BLEED TUBE.SDR C2XA05TY031Floor Support · corrodedTYS DURING A C-CHECK INSPECTION THE CENTER AISLE SUPPORT STRUCTURE ON THE LEFT SIDE WAS FOUND WITH CORROSION FROM FRAME 20 TO 60. MAINTENANCE REMOVED AND REPLACED THE CENTER OMEGA BEAM ASSEMBLY FROM FR 20 TO 29 AND BLENDED FROM 29 THRU 60 AND WAS FOUND WITHINSDR C2XA05TY030Fitting · looseDURING A SCHEDULED C-CHECK INSPECTION, THE NR 1 RUDDER TO VERTICAL STABILIZER LOWER HINGE FITTING ATTACH POINT BUSHING WAS FOUND TO BE MIGRATED AND LOOSE. THE DEFECTIVE BUSHING WAS REMOVED; THE FITTING HOLE WAS DIMENSIONALLY CHECKED AND FOUND TO BE WORN. MAISDR C2XA05RI006Valve · failedRIC - FLIGHT CREW REPORTED BLEED NR 2 VALVE CLOSED MSG ON EICAS DURING ICE CONDITIONS. CREW PERFORMED AIR RETURN TO RIC. MX PERFORMED TROUBLESHOOTING AND REMOVED AND REPLACED ENGINE NR 2 ANTI-ICE VALVE, ENGINE NR 2 HIGH STAGE PRESS SW AND RELAY K1088. ALL OSDR C2XA05TY029Frame · damagedTYS, DURING A SCHEDULED INSPECTION THE LOWER SKIN SUPPORT BRACKET BETWEEN STR 21L AND 21R ON FR21 HAS ELONGATED HOLES. MAINTENANCE PERFORMED REPAIR WITH TWO INTERNAL L ANGLE DOUBLERS ON FR 21 BETWEEN STR 21L AND 21R. ALODINED, PRIMED AND INSTALLED IAW EC5310SDR C2XA05TY028Fitting · corrodedTYS, DURING A SCHEDULED INSPECTION FRAME 75, SPAR 1 FITTING SHOWS SIGNS OF FRETTING. MAINTENANCE REMOVED THE FITTING, BLENDED CORROSION ON INNER SKIN SURFACE, DYE PENATRANT TESTED THE AREA, TREATED FOR CORROSION, DRILLED AND INSTALLED A NEW FITTING IAW EC5310SDR C2XA05CLO15Inverter · inoperativeCLE FLIGHT 2322 THE CREW REPORTED THE MID CABIN EMERGENCY LIGHTS NOT ILLUMINATING DURING PREFLIGHT TEST. MAINTENANCE REPLACED THE CENTER CABIN EMERGENCY LIGHTING INVERTER AND OPERATIONAL CHECKS GOOD.SDR C2XA05IA045Fuse · blownIAH - FLIGHT 3341, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. DURING PSDR C2XA05IA044Battery Pack · dischargedIAH - FLIGHT 2057 DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EXIT SIGNS OVER THE GALLEY, ROW 2B, AND THE FLT ATTENDANTS SEAT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKESDR C2XA05IA039Battery Pack · dischargedIAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOSDR C2XA05IA038Battery Pack · dischargedIAH - FLIGHT 2057, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROSDR C2XA05IA040Wire Harness · inoperativeLFT - FLIGHT 2903, THE CREW REPORTED ON DESCENT THAT THERE WAS NO DOWN AND LOCK INDICATION ON THE RT MAIN LANDING GEAR. THE CREW DECLARED AN EMERGENCY, AND LANDED AT LFT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WIRE HARNESS FOR THE UPLOCK PROXISDR C2XA05RI002Bulb · looseRIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR OVERHEAD EMERGENCY LIGHT (ONE BULB) NOT WORKING. MAINTENANCE REPOSITION BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA05CL012Check Valve · inoperativeCLE FLIGHT 2150, CREW REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE NOSE LANDING GEAR CHECK VALVE. ALL OPERATIONAL CHECKS WERE GOODSDR C2XA05SH010Frame · gougedSHV - DURING C-CHECK, SEVERAL GOUGES FOUND ON LEFT HAND EMERGENCY EXIT DOOR LOWER INTERNAL FRAME.SDR C2XA05SH008Floor Support · damagedSHV - DURING C-CHECK, THE LT OMEGA BEAM AT FRAME 48 HAS DAMAGED SEAT TRACK SCREW HOLE.SDR C2XA05SH009Skin · gougedSHV - DURING C-CHECK, GOUGES WERE FOUND ON THE EXTERNAL FUSELAGE SKIN AT FRAME 40.SDR C2XA05TY016Skin · corrodedTYS, DURING A SCHEDULED INSPECTION THE FUSELAGE SKIN INSIDE SURFACE AT THE POTABLE WATER MANIFOLD MOUNT, CORRODED. REMOVED THE CORROSION, ALODINED, FABRICATED NEW REPAIR DOUBLER AND INSTALLED, PAINTED AND PRESSURE CHECKED I/A/W-EC5330-01435.SDR C2XA05TY014Skin · crackedTYS, DURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN WAS FOUND CRACKED AT FS 75. MAINTENANCE MEASURED DAMAGED AREA, CUT OUT, FABRICATED A DOUBLER AND INSTALLED I/A/W-EC5310-01320 AND IC2005-145/0271.SDR C2XA05TY013Rivet · looseTYS, DURING A SCHEDULE INSPECTION, SMOKING RIVETS WHERE FOUND ON THE BASE OF THE VERTICAL STAB (LEFT AND RIGHT SIDES). MAINTENANCE REMOVED THE OLD RIVETS, FABRICATED AND INSTALLED DOUBLERS, (4 ON EACH SIDE) I/A/W-EC5510-01109, EMB145-SRM-51-40-02, IC2005-145/SDR C2XA05TY010Spar · crackedTYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRCRAFT RETURNED TO SERVICE.SDR C2XA05BT010Control Lever · faultyCREW REPORTED, LANDING GEAR LEVER/DISAGREEMENT WARNING ON RETRACTION, NOSE GEAR RED HATCHED INDICATION. PERFORMED CHECKLIST, RECYCLED GEAR, GEAR INDICATED NORMAL AFTER RECYCLE. EXTENDED NORMALLY FOR AIR-RETURN LANDING IN NEWARK. MAINTENANCE REMOVED AND REPLSDR C2XA05BT009Light · faultyEWR---CO2383, CREW REPORTED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT HOUSING IAW EMB145 AMM NR 33-50-10, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR RAIA00501054Precooler · failedPIT- NR 2 BLEED OVERTEMP UPON ENTERING ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED NR 2 PRECOOLER.SDR C2XA05BT007Sign · looseYUL- CO3442, CREW REPORTED, BULKHEAD EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE RECONNECTED LOOSE CONNECTOR AT EMERGENCY EXIT SIGN, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR RAIA00501056Valve · failedPIT - NR 1 AND NR 2 BLEED OVERTEMP DURING CLIMB IN ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED FAN AIR VALVES.SDR C2XA05TY007Bearing · wornTYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VERTICAL BEARING HOUSING AND INSTALL NEW BUSHINGS IAW EC5510-01108. ALL WORK WAS ACCOMPLISHED AND OSDR C2XAO5TY006Floor Support · corrodedTYS - DURING A SCHEDULED 4C INSPECTION, THE LT OMEGA BEAM BETWEEN FS 22 AND FS 23 HAS A BLENDED AREA BELOW LIMITS NEXT TO A NUTPLATE. MAINT CUTOUT THE EFFECTED AREA, FAB`D A SPLICE REPAIR FROM A NEW PART AND FAB`D AN INTERNAL ANGLE, DRILL, ALODINED, PRIMED ANSDR C2XA05SH011Battery Pack · inoperativeDURING SERVICE ROUTINE, LT OVERWING EMERGENCY LIGHT AND 3RD CEILING PANEL EMERGENCY LIGHT DO NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED NR 1 BATTERY AND BATTERY PACK FOR EMERGENCY LIGHT ON LT FWD OVERWING AND 3RD CEILING PANEL IAW EMB 145 AMM 33-50-11. SDR C2XA05IA011Connector · looseTHE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE RESECURED A LOOSE CONNECTOR ON THE AFFECTED LIGHT, OPS CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED A
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