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 C2XA03CL015Uplock · defectiveCLE FLIGHT 2217 THE CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY AND BOTH UPLOCK PROXIMITY SENSORS. OPERATIONAL CHECKS WERE GOOD. PROXIMITY SENSOR P/N 8-527-01 AND S/N'S OFF WERE 5105 AND15960.SDR C2XA03TY004Attach Fitting · damagedDURING A SCHEDULED 3-C INSPECTION THE RT AILERON PCA ATTACH FITTING WAS FOUND DAMAGE AND THE BOLT FROZEN. MAINTENANCE REMOVED AND REPLACED THE RT HAND AILERON PCA ATTACH FITTING, PRIMED AND PAINTED IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELSDR C2XA03CL011Manifold · crackedDURING INSPECTION MAINTENANCE FOUND THE #2 ENGINE BLEED DUCT MANIFOLD CRACKED APPROX. 4.5 INCHES.THE DUCT IS LOCATED AT THE 14 STAGE BLEED VALVE AT THE TOP OF THE ENGINE.MAINTENANCE REPLACED THE 14TH STAGE CUSTOMER BLEED DUCT MANIFOLD.OPERATIONAL CHECKS WERE GSDR C2XA03CL009Switch · contaminatedCLE FLIGHT#2408 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF FOLLOWED BY ENGINE 1-2 REV. DISAGREE.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR AIR/GROUND PROXISDR C2XA03BT007Harness · shortedCREW REPORTED NR 1 ENGINE UNCOMMANDED SHUTDOWN ON APPROACH TO SYR, CONTINUED INTO SYR, LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED NR 1B FADEC ENGINE HARNESS IAW RR AE3007 MM #71-00-00 AND REMOVED AND REPLACED FADEC NR 1B DUE TO SHORSDR C2XA03BT004Actuator · faultyEWR---CO3628, CREW REPORTED, "LEFTHAND MAIN GEAR WOULD NOT RETRACT." MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED #1 MAIN LANDING GEAR UNLOCK ACTUATOR IAW #32-33-09 (REFERENCE M-602 #430342). OPS.CHECKED GOOD.. AIRCRAFT RETURNED TO SERVICE.SDR C2XA03CL008Odor · detectedSYR FLIGHT 2479 THE CREW REPORTED UPON APU START THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. THE ODOR DISSIPATED ON SHUTDOWN. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00.SDR C2XA03BT003Proximity Switch · faultyCREW REPORTED, LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS ON TAKEOFF FROM NEWARK. AIRCRAFT AIR RETURNED TO EWR, LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 MM 32-63-01. OPS CHECKED GOOD. SDR C2XA03CL003Selector · inoperativeCLE FLIGHT 3014 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT UNLESS THE DOWNLOCK RELEASE BUTTON WAS PRESSED. MAINTENANCE REPLACED THE LANDING GEAR LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA03CL002Tube · leakingCLE FLIGHT 3091 THE CREW REPORTED BLEED 1 LEAK INDICATION ON EICAS,THEN RETURNED TO CLE .AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PYLON BLEED TUBE ASSEMBLY AND IT LEAK CHECKED GOOD.SDR RAIA00212371Warning System · activated5305-PIT- APU BLEED VALVE FAULT INDICATION. MAINTENANCE DEFERRED PER MEL 49-52-02.SDR C2XA02CL252Bulb · inoperativeDURING ROUTINE MAINTENANCE THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE REPLACED THE RIGHT EMERGENCY LIGHT BULB.OPERATIONAL CHECKS WERE GOOD.SDR C2XA02SH152Rib · crackedSHV- DURING C-CHECK RIB FOUND CRACKED ON RUDDER NUMBER 1 AT LOWER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH150Support · damagedSHV - DURING C-CHECK RUDDER 1 CENTER HINGE POINT LOWER LEADING EDGE SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH149Support · damagedSHV- DURING C-CHECK RUDDER NUMBER 1 CENTER HINGE POINT UPPER LEADING EDGE SKIN SUPPORT WAS FOUND BENT. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH156Frame · gougedSHV DURING C CHECK FRAME 81 WAS FOUND GOUGED AT BOTTOM CENTER. MAINTENANCE REMOVED DAMAGED SECTION AND REPAIRED FRAME 81 IAW CONTINENTAL EXPRESS EC 5310-01223. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH155Bracket · crackedSHV- DURING C CHECK PULLEY BRACKET INSIDE PANEL 325 LR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH154Sill · corrodedSHV DURING C CHECK SILL ON RIGHT SIDE SERVICE DOOR WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 SECTION 7 AND GST-3627/02.SDR C2XA02SH153Sill · corrodedSHV DURING C CHECK SILL FOWARD OF SERVICE DOOR WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH151Rib · bentSHV DURING C CHECK RIB WAS FOUND BENT ON RUDDER NUMBER ONE AT LOWER SIDE OF UPPER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH148Beam · corrodedSHV- DURING C CHECK CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-06. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH147Beam · gougedDURING C CHECK CENTER OMEGA BEAM WAS FOUND GOUGED AT FRAME 23. MAINTENANCE REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH146Gusset · nickedSHV DURING C CHECK GUSSET WAS FOUND NICKED ON NUMBER 2 LOWER COWLING AT STAION XN=3167.5MM. MAINTENANCE REMOVED AND REPLACED AFFECTED GUSSET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH145Stiffener · gougedSHV- DURING C CHECK NUMBER 2 LOWER COWLING STIFFENER WAS FOUND GOUGED NEAR CENTER LINE AT STAION XN=2180.0MM. MAINTENANCE REMOVED DAMAGE AREA AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH144Structure · gougedDURING C CHECK, NR 2 LOWER NACELLE STRUCTURE WAS FOUND TO HAVE A GOUGED EDGE MEMBER AT STATION XN=776.8MM. MAINTENANCE REMOVED AND REPLACED AFFECTED EDGE MEMBER IAW EMB 145 SRM. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH143Beam · corrodedDURING C CHECK, CENTER OMEGA BEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE SECTION AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH142Butt Strap · corrodedSHV- DURING C CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH141Angle · dentedSHV- DURING C CHECK ANGLE WAS FOUND DENTED ON CENTER OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.SDR C2XA02SH140Cap · gougedSHV-DURING C CHECK CROSSBEAM CAP WAS FOUND GOUGED BETWEEN CENTER AND RIGHT HAND OMEGA BEAMS AT FRAME 22. MAINTENACE REMOVED AND REPLACED AFFECTED CROSSBEAM CAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR RAIA00212360Connector · loose5295-STL- EMERGENCY PATH LIGHTING INOP AT SEAT 1A. RESECURED EMERGENCY PATH LIGHT ELECTRICAL CONNECTOR, OPS CHECK OK.SDR C2XA02BT084Light · faultyEWR---CO3533, CREW REPORTED AISLE PATH LIGHTING BETWEEN SEAT ROW 10A AND 12A INOPERATIVE....MAINTENANCE REMOVED AND REPLACED AISLE PATH LIGHTING AT THE EMERGENCY EXIT IAW EMB145 AMM #33-50-08. OPS. CHECKED SYSTEM GOOD.SDR RAIA00212354Connector · looseMX-PIT- EMERGENCY PATH LIGHTING INOP. RECONNECTED EMERGENCY PATH LIGHTING ELECTRICAL CONNECTOR, OPS CHECK OK.SDR C2XA02BT081Fire Bottle · faultyEWR---CO3359, CREW REPORTED, "EICAS MESSAGES E1/E2 EXTBTL A INOP"; OCCURRED SHORTLY AFTER LANDING. MAINTENANCE REMOVED AND REPLACED "A" FIRE EXTINGUISHER BOTTLE. AIRCRAFT TESTS GOOD IAW EMB145 MM 26-21-02. AIRCRAFT RETURNED TO SERVICE.SDR C2XA02CL245Control Handle · intermittentTHE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE CREW RECYCLED THE GEAR AND AFTER 1 MINUTE THE MESSAGE WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL LEVER. OPESDR C2XA02CL240Proximity Switch · faultyCLE FLIGHT#3085 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE RIGHT AND LEFT WOW PROXIMITY SWITCHES ON THE LEFT MAIN GEAR.OPERATIONAL CHECKS WERE GOOD.THE SDR C2XA02CL244Proximity Switch · faultyCLE FLIGHT#3031 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN THE GEAR WAS LOWERED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN GEAR AFT PROXIMITY SWITCH.OPERATIONAL CHECKS WERE GOOD.SDR C2XA02IA248Duct · damagedFLIGHT 3789, THE CREW NOTED A FIRE INDICATION NR 2 ENGINE AFTER TAKEOFF. THE CREW SHUTDOWN NR 2 ENGINE, DECLARED EMERGENCY, AND, RETURNED TO HSV, AND, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ANTI ICE BLEED DUCT, PERFORMED A SDR C2XA02CL234Battery Pack · dischargedDURING ROUTINE MAINTENANCE THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS AND THE AFT AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE.MAINTENANCE REPLACED THE #4 EMERGENCY BATTERY PACK.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA02TY168Battery · shortedDURING A SCHEDULED SERVICE AND ROUTINE INSPECTION, THE AFT OVERWING EMERGENCY LIGHT, FLOOR STRIP LIGHTS AFT OF EMERGENCY EXITS,AND OVERHEAD EMERGENCY LIGHT WAS ALL FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND THE OPSDR C2XA02IA243Battery Pack · dischargedBNA- DURING MAINTENANCE THE MECHANIC NOTED THAT THE AFT OVERWING, AND, AFT THREE AISLE EMERGENCY LIGHT STRIPS INOP. BNA- MAINTENANCE REMOVED AND REPLACED THE #4 EMERGENCY LIGHT BATTERY PACK, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFTSDR RAIA00211316Connector · disconnectedFWD ESCAPE PATH LIGHTS INOPERATIVE. RE-SECURED FORWARD FLOOR EMERGENCY LIGHTING STRIP CONNECTOR, OPS CK OK.SDR C2XA02CL227Combustion Liner · crackedCLE FLIGHT#3280 THE CREW REPORTED A STRONG FUEL ODOR IN THE COCKPIT AFTER TAKEOFF FROM CLEVELAND.THE ODOR WAS NOTED WHEN THE PACKS WERE OPERATED FROM THE ENGINE BLEED.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED SDR C2XA02CL226Windshield · arcedMHT FLIGHT#3595 THE CREW REPORTED THE FIRST OFFICER'S WINDSHIELD HEATING ELEMENT WAS ARCHING.MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S WINDSHIELD.OPERATIONAL CHECKS WERE GOOD.SDR C2XA02IA239Pressure Switch · failedTHE CREW NOTED THAT THE RUDDER SYSTEMS NR 1 AND NR 2, INOPERATIVE. ON DEPARTURE, THE CREW DECLARED EMERGENCY. PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 RUDDER SYSTEM PRESSURSDR C2XA02IA238Pressure Switch · inoperativeIAH- FLIGHT 3558, THE CREW NOTED THAT THE RUDDER SYSTEMS #1 & #2 INOPERATIVE, ON DEPARTURE FOR (TYS), THE CREW DECLAIRED EMERGENCY, AND, PERFORMED AN EMERGENCY DESCENT. THE AIRCRAFT RETURNED TO (IAH), AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE REMOVED SDR C2XA02IA237Circuit Card · malfunctionedTHE CREW NOTED THAT THE AUTOPILOT/YAW DAMPER FAILED. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC-600. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA02SH123Beam · crackedDURING C CHECK LT OMEGA BEAM WAS FOUND TO HAVE A CRACK ON RIVET AT FRAME 22. MAINTENANCE REPAIRED CRACK ON RIVET IAW CONTINENTAL EXPRESS EC 5320-01081. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA236Battery · dischargedBNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. BNA- MAINTENANCE REMOVED AND REPLACED THE #3 EMERGENCY BATTERY,PERFORMED A OPERAIO9NAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RESDR C2XA02IA235Battery · dischargedBNA- WHILE PERFORMING MAINTENANCE THE MECHANIC NOTED THAT THE AISLE PATH EMERGENCY LIGHTS WERE JNOPERATIVE. BNA- MAINTENANCE REMOVED AND REPLACED THE #2 EMERGENCY LIGHT BATTERY. PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED SDR C2XA02CL216Firewall · crackedDURING A ROUTINE INSPECTION THE APU FIREWALL WAS FOUND CRACKED AT THE UPPER RIGHT ATTACH POINT.MAINTENANCE REPAIRED THE APU FIREWALL I/A/W GST 3249/02.THE AIRCRAFT WAS RELEASED FOR SERVICE.
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