Embraer EMB-145LR
Service difficulty reports · 36,797
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 = 'EMB145LR' 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 = 'EMB145LR' 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 SIMA201812110004Unknown · odorSTRONG CHEMICAL ODOR IN COCKPIT AND CABIN ON DESCENT ENGINES WERE AT IDOL WHEN ODOR WAS FIRST SMELLED.-C/A-PERFORMED ENGINE RUNS AS PER ETN-EM-72-034. NO ODOR DETECTED AT ANY ENG. SETTING. AIRCRAFT O.K. FOR SERVICE.SDR RAIA201812090002Skin · crackedRT ELEVATOR UPPER SKIN IS CRACKED AROUND HINGE NR 2 CUTOUT AT YH-1310. REPAIRED CRACKED SKIN ON RT ELEVATOR AT YH-1310.SDR RAIA201812090001Skin · crackedLT ELEVATOR UPPER SKIN IS CRACKED AROUND HINGE NR 2 CUTOUT AT YH-1310. REPAIRED CRACK SKIN AT YH-1310.SDR SIMA2018121209003Brake · overheatedHIGHSPEED ABORT DUE TO BRAKE OVERHEAT ABORT AT 129KTS-C/A-PERFORMED MAIN BRAKE SYSTEM FUNCTIONAOL CK AND PHYSICAL CK OF MAIN TIRES AND BRAKES IAW EMB145 AMM 32-41-00. NO DEFECTSNOTED. DEFERED PER MEL 32-2. ALL MTX ACTIONS C/WSDR SIMA2018121009001Connector · looseBLD 1 LEAK IN FLIGHT QRH PROCEDURES COMPLIED WITH MESSAGE EXTINGUISHED.-C/A-INSPECTED PACK 1 FOR LOOSE DUCTING/CLAMPS. NO DEFECTS NOTED IAW EMB 145 AMM 21-20-04. FOUND #1 ENG BLEED VALVE CONNECTOR LOOSE. RESECURED CONNECTOR IAW EMB 145 AMM 36-11-05. NO DEFETCSSDR RAIA2018122810003Angle · crackedR/H OVERWING FAIRING "L" ANGLE IS CRACKED AT FRAME 47....REMOVED AND REPLACED "L" ANGLE AT FRAME 47.SDR RAIA2018121780002Floor Support · crackedCENTER OMEGA BEAM BETWEEN FR 20 & 21 L ANGLE IS CRACKED. R&R CENTER OMEGA BEAM BETWEEN FR 20 & 21.SDR SIMA201812108001Battery Pack · failedDURING PS-1 CHECK, FOUND LEFT AND RIGHT EXTERIOR OVER THE WING EMERGENCY LIGHTS OUT.-C/A-CHANGED #4 EMERGENCY BATTERY IAW AMM TASK 33-50-04 DID NOT FIX ISSUE. OVER WING LH AND RH EMERGENCY LIGHTS DEFERRED PER MEL 33-29 AUTH 120313D-C. EMERGENCY LIGHTING BATTERSDR SIMA201812108002Light · inoperativeSERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVD AND REPLACED SERVICER DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09-000-801 AND 33-50-09-400-801 OPS CHECK GOODSDR RAIA2018122270001Floor Support · damagedL/H CENTER OMEGA BEAM LOWER SUPPORT ANGLE IS DAMAGED AT FR 48 & 49....REMOVED AND REPLACED L/H CENTER OMEGA BEAM LOWER SUPPORT AT FR 48 & 49.SDR SIMA2018121407006Skin · crackedCARGO DOOR HANDLE CUTOUT CRACKED AT AFT UPPER CORNER-C/A-REPAIRED CARGO DOOR HANDLE CUOUT CRACK AT AFT UPPER CORNER IAW ERS-EM-52MR-936SDR HNAA2018121200315Trim System · malfunctionedON CLIMB OUT FO PITCH TRIM FAILED FOLLOWED BY PTRIM MAIN INOP AND PTRIM BACK UP INOP. RAN QRH BACK SYS MOMENTARY CAME BACK ONLINE CYCLED MAIN AND BACK UP CUT OUT. CND DISCREPANCY ON GROUND. R&R HSCU AS MX PRECAUTION OPS CHECK GOOD REF AMM 27-40-00 AND 27-40-01SDR SIMA201812107002Clamp · leakingON CLIMB OUT NOTICED AIRCRAFT NOT PRESSURIZING. THAT WAS FOLLOWED BY BLD 1 VLV CLSD & PACK 1 VLV CLSD MSG ADVISORY. RESET THEM BUT MESSAGES KEPT COMIMG BACK WITH RUSH OF AIR EACH TIME-C/A-REMOVED AND REPLACED COUPLING AND CLAMP ON DUAL TEMP VALVE DUCT IAW ETN-SDR SIMA201812107004Lamp · inoperativeSERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A & 33-50-09-400-801-A OPS CHECK GOOD AT THIS TIME NO FURTHER DEFECTS NOTED ENDSDR ASOA2018121073071Engine · leakingTHE CREW REPORTED ON CLIMBOUT AT 6000 FEET LAV SMOKE WARNING ON EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE #1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR RAIA201812060001Fitting · corrodedL ANGLE CLIP HAS SIGN OF CORROSION UNDER RAMP ON FRAME 20. R&R L ANGLE CLIP.SDR SIMA201812076002Anti-Ice Valve · failedAFTER PERFORMING ICE DET TEST IN THE AIR, E1 "OPEN" INSCRIPTION LIGHT EXTINGUISHED...WHICH IS REQ TO BE ILLUMINATED PER MEL 30-11.-C/A-REMOVED AND REPLACED #1 ENGINE ANTI ICE VALVE IAW EMB 145 AMM 30-21-01. AND PERFORMED OPERTIONAL CHECK IAW EMB 145 AMM 30-00-SDR HNAA2018120700312Warning Message · illuminatedPDIS 641 52-30 1723121 06DEC18 FWA ASSGN
BAGG DOOR OPEN DURING TAKEOFF ROLL. AND ABORTED TAKE OFF.
HISTORY: NOV 28
MEL 06DEC18 16:00 FWA C34017 52-3-2
BAGGAGE DOSDR HNAA2018120700311Landing Gear · false indicationPDIS 695 32-61 1864742 06DEC18 PHL CLOSE
L/G DISAGREE AFTER GEAR WAS RETRACTED. QRH C/W AND MESSAGE EXTINGUISHED. RETURNED TO PHL
FACT 06DEC18 18:07 PHL
PERFORMED L/G RETRACT/EXTENSIOSDR ASOA2018120763069Control Panel · faultyTHE CREW REPORTED @1000' LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR PANEL AMD OPERATIONAL CHECKS WERE GOOD.SDR RAIA201812100005Gusset · corrodedCENTER GUSSET AT FRAMES 29-35 HAS CORROSION. REMOVED AND REPLACED CENTER GUSSET AT FRAMES 29-35.SDR RAIA201812050004Angle · corrodedCARGO DOOR Z ANGLE IS CORRODED. REMOVED AND REPLACED CARGO DOOR Z ANGLE.SDR RAIA201812050003Angle · bentCARGO DOOR AFT RAMP ANGLE IS BENT. REMOVED AND REPLACED CARGO DOOR AFT RAMP ANGLE.SDR RAIA201812050002Angle · bentCARGO DOOR FWD RAMP ANGLE IS BENT AND ATTACHING UPPER AND LOWER SUPPORT ANGLES ARE BENT. REMOVED AND REPLACED CARGO FWD RAMP ANGLE AND UPPER AND LOWER SUPPORT ANGLES.SDR SIMA2018122105015Skin · cracked1/4 INCH DIAGONAL CRACK ( TOP L TO BOTTOM R) FOUND IN FUSELAGE SKIN AT FRAME 75 JUST ABOVE STRINGER 2L. 1" AREA OF PAINT REMOVED AND AREA DYE PEN'D FOR BETTER VISIBILITY AND LOCATION OF CRACK. AREA AROUND FLAW TAPED OFF.-C/A-REPAIRED CRACK IN FUSELAGE SKIN AT SDR SIMA2018121705014Support Angle · crackedRH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1/2" CRACK.-C/A-REMOVED AND REPLACED RH UPPER WING-TO-FUSELAGE FAIRING SUPPORT FROM FRAME 48 TO 52 IAW SRM 51-40-02. REFER TO NRTC E684169 FOR PAINT.SDR SIMA2018121405013Support Angle · crackedLH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST FWD OF FRAME 41 HAS EVIDENCE OF 1/4" CRACK. PROCEEDING DOWNWARD FROM THE RIVET. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE JUST FWD OF FRAME 41 IAW SRM 53-23-12. SEE NRTC E683553 FOR PAINT.SDR SIMA2018121705012Support Angle · crackedLH UPPER WING TO FUSELAGE SUPPORT ANGLE. JUST AFT OF FRAME 50 HAS EVIDENCE OF 1" CRACK. -C/A-REPAIRED LH UPPER WING TO FUSELAGE SUPPORT ANGLE IAW SRM 53-23-12 AND SRM 51-40-02.SDR SIMA2018121705011Support Angle · crackedRH LOWER #4 WING TO FUSELAGE SUPPORT ANGLE. HAS 2" CRACK ON THE FWD END. -C/A-REPAIRED IAW SRM 57-20-01.SDR SIMA2018121705010Crossbeam · corrodedLH OMEGA BEAM HAS EVIDENCE OF CORROSION BY THE CROSS BEAM BETWEEN FRAMES 59-60.-C/A- IN REFERENCE TO WIP #6. COMPLETED REPAIR TO LH OMEGA BEAM AT FR 59-60 IAW EO EM-53MR-1518 PART A.SDR RAIA2018120750001Engine · warning messageE1 OIL PRESSURE DECREASED TO AMBER RANGE IN FLIGHT. (CAPTAINS SAID IT HAPPENED 40 MINUTES INTO FLIGHT AT 35K FT, E1 OIL PRESSURE DECREASED INTO AMBER RANGE BUT NEVER TURNED RED.) FOLLWED QRH FOR LOW OIL PRESSURE WITH NI EICAS MSG PRESENT. STARTED WITH 12 QUTS SDR SIMA2018121405009Frame · gougedFRAME 70 GOUGED BETWEEN STR 13R-12R INSIDE CARGO-C/A-REPAIRED FRAME 70 IAW ERS-EM-53MR-3535SDR SIMA2018121405008Trunnion · crackedRH AFT UPPER TRUNION CRACKED-C/A-REMOVED AND REPLACED RH AFT UPPER TRUNNION IAW ERS-EM-57MR-1053SDR SIMA20181205004Support Angle · crackedLT LOWER NR 1 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE AFT PREVIOUS REPAIRED SPLICE. REMOVED AND REPLACED LT LOWER NR 1 WING TO FUSELAGE SUPPORT ANGLE AFT SPLICE IAW SRM 51-40-02.SDR SIMA20181205006Support Angle · crackedLT LOWER NR 4 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE FWD END. REPAIRED IAW ETN-EM-53-142.SDR SIMA20181205005Support Angle · crackedLT LOWER NR 3 WING TO FUSELAGE SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE FWD END. REMOVED AND REPLACED LT LOWER NR 3 WING TO FUSELAGE ANGLE IAW SRM 51-40-02.SDR SIMA20181205007Support Angle · crackedLT UPPER WING TO FUSELAGE SUPPORT ANGLE. HAS 1" CRACK BETWEEN FRAMES 48-49. WILL BE REPAIRED DURING COMPLIANCE OF FRAME 50 CRACK NRTC E680918.SDR SIMA20181205003Support Angle · crackedRT CABIN OUTBD OMEGA BEAM LOWER SUPPORT ANGLE. HAS 3/4" CRACK ON THE INBD SUPPORT FWD END JUST AFT OF FRAME 47. REMOVED AND REPLACED RT CABIN OUTBD OMEGA BEAM LOWER INBD SUPPORT ANGLE IAW SRM 53-23-02 AND SRM 51-40-02.SDR SIMA20181205002Support Angle · crackedRT CABIN OUTBD OMEGA BEAM LOWER SUPPORT ANGLE. HAS 1 1/2" CRACK ON THE OUTBD SUPPORT FWD END JUST AFT OF FRAME 47. REMOVED AND REPLACED RT CABIN OUTBD OMEGA BEAM LOWER OUTBD SUPPORT ANGLE IAW SRM 53-23-02 AND SRM 51-40-02.SDR SIMA201812065001Lamp · inoperativeLH EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH EMERGENCY LIGHT IAW AMM 33-50-10 OPS CHECK GOOD.SDR ASOA201812067187Doubler · gougedGOUGE AT FRAME 51, STRINGER 19R. REPLACED REPAIR DOUBLER IAW SRM 53-24-02.SDR RAIA2018122840003Floor Support · crackedL/H OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CRACKED BETWEEN FRAME 15 & 16....REMOVED AND REPLACED L/H OMEGA BEAM UPPER DIGITAL SUPPORT AT FRAME 15 & 16.SDR SIMA201812054004Charger · failedON APPROACH THERE WAS A STRONG SMELL OF SMOKE IN THE CABIN AND COCKPIT. WE DECLARED AN EMERGENCY. AND LANDED IN MIA. THERE WAS NOT VISIBLE SMOKE.-C/A-REMOVED AND REPLACED #2 BATTERY POWER SUPPLY AND CHASSIS ASSEMBLY IAW AMM 33-50-04, EMERGENCY LIGHTING SYSTEM SDR ASOA201812067188Socket · inoperativeMAIN CABIN DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT SOCKET IAW AMM 33-50-06.SDR SIMA20181204005Battery Pack · crackedBATTERY POWER SUPPLY NR 2 BATTERY PACK FOUND CRACKED. REMOVED AND REPLACED NR 2 BATTERY POWER SUPPLY AND CHASSIS ASSEMBLY IAW AMM 33-50-04, EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK SATISFACTORY IAW AMM 33-50-00. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 10SDR SIMA201812054003Light · inoperativeDURING PS-1 CHECK FOUND LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED LH AND RH O/W SIDE CENTER FAIRING EMERGENCY LIGHT IAW 33-50-10 SUBTASK 020-004-A AND TROUBLE SHOT LIGHTS IAW EMB-145 AMM 20-20-03. FOUND LH O/W EMERGENCY LIGHT TO BE SHORTED. RAR LH OSDR ASOA201812047186Shear Tie · corrodedA/C IS IN C-CHECK WHEN INSPECTION FOUND FRAME 65 CORRODED AT THE CARGO FLOOR SILL. MAINTENANCE REPAIRED CORRODED SHEAR CLIP AT FRAME 65 AT CARGO DOOR SILL IAW SRM 53-31-04 AND FIGURE 212. LIGHT CORROSION.SDR SIMA201812053005Controller · failedAUTO PRESSURIZATION SYSTEM FAILED AT 33,000 FT.-C/A-DEFERRED AUTO PRESSURIZATION SYSTEM, M PROCEDURES COMPLIED WITH. MEL# 21-17 AUTH# 120087DM-C. .REMOVED AND REPLACED MANUAL PRESSURIZATION CONTROLLER IAW EMB AMM 21-31-02. OPS CHECK OK IAW EMB AMM 21-31-00 ANDSDR HNAA2018120500304Display · malfunctionedDURING TAXI IN TO GATE. FO'S PFD WENT BLANK ALONG WITH ELECTRICAL ODOR. SELECTED AVIONICS BUSS 2 OFF. SWAPED FO'S PFD AND MFD PER AMM 34-22-01 AND DEACTIVATED MFD PER MEL.SDR ASOA201812024069Bulb · inoperativeIAH - FLIGHT 4035, THE CREW REPORTED THAT THE REAR OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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