Embraer EMB-145LR
Service difficulty reports · 36,799
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 SIMA20140723010Skin · crackedAFT FUSELAGE LT SKIN CRACKED AT FASTENER FRAME 75 STRINGER 2L. DAMAGED SECTION OF SKIN AT FRAME 75 STRINGER 2L AREA WILL BE CUT OUT, DOUBLER & FILLER WILL BE INSTALLED USING ETD2014-145-062647, SEE NRTC E399825.SDR SIMA20140723009Spar · corrodedRIGHT WING SPAR 3 HAS CORROSION ON AFT SIDE ON LG HARNESS PASS THROUGH CUT OUT. BLENDED AS REQUIRED TO REMOVE CORROSION FROM RT WING SPAR 3 AFT SIDE ON LG HARNESS PASS THROUGH CUT OUT IAW SRM 51-10-03. UT CHECK INDICATES 0.228 INCHES REMAINING THICKNESS, DAMSDR SIMA20140723008Door · corrodedLEFT EMER EXIT CORRODED UNDER LOWER BONDING TAB MARKED. REPAIRED LT EMER EXIT UNDER LOWER FWD GUIDE IAW ERS-EM-5200-187.SDR SIMA20140723007Gusset · corrodedRIGHT OMEGA BEAM GUSSET CORRODED AT FRAME 61, 60 & 59 MARKED. R & R RT OMEGA BEAM GUSSET AT FRAME 61, 60 & 59 IAW SRM 51-40-02.SDR SIMA20140723006Support · crackedRIGHT HAT BEAM INBD SUPPORT CRACKED BETWEEN FRAME 47 & 48 MARKED. R & R RT HAT BEAM INBD SUPPORT IAW SRM 51-40-02.SDR SIMA20140723005Skin · crackedREAR ELECTRONICS COMPARTMENT ACCESS HATCH FRAME IS CRACKED BELOW PIN ATTACHMENT BRACKET. FABRICATED & INSTALLED REPAIR DOUBLER & FILLER IAW ERS-EM-52MR-176.SDR SIMA20140723004Pump · failedHYD 2 LOW QTY ADVISORY IN FLIGHT, ABOUT 20 - 30 MINUTES LATER HYD 2 PUMP FAIL MSG. POST FLIGHT SHOWS HYD FLUID COATING INSIDE NR 2 WW. R & R NR 2 ENG DRIVEN PUMP IAW AMM 29-10-03. RAN ENGS LEAK & OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.SDR SIMA20140723001Seal · damagedFLIGHT ATTENDANT STATED THAT A LOUD SQUEAL WAS COMING FROM THE SERVICE DOOR & THAT SHE COULD SEE LIGHT ABOVE THE DIAMETER OF A NICKEL BETWEEN THE DOOR SEAL & THE DOOR FRAME AT THE UPPER RT CORNER OF THE DOOR. PRESSURIZATION INDICATION NORMAL AT 300 FEET MSL DSDR SIMA20140723002Computer · malfunctionedSPS 2 INOPERATIVE ON EICAS UPON LANDING STICK SHAKER ACTIVATED. R & R STALL PROTECTION COMPUTER IAW AMM 27-36-02. OPERATIONS CHECKED GOOD.SDR CHQA20140722235Tire · separatedTHE LT INBD TIRE SEPARATED ON TAKEOFF. DECLARED AN EMER & DIVERTED THE ACFT FROM ITS INTENDED FLIGHT PLAN. THE ACFT LANDED WITHOUT FURTHER INCIDENT. PERFORMED THE TREAD SEPARATION INSPECTION & CONFIRMED THE LT INBD TO BE AT FAULT. THE LT INBD TIRE, THE LT SDR ASOA20140722081Start Valve · faultyTHE CREW REPORTED ON CLIMB OUT OF STL, AFTER SWITCHING TO ENGINE BLEEDS THEY NOTICED A STRONG ODOR SIMILAR TO "BURNED FIREWORKS". MX PERFORMED A GENERAL VISUAL INSPECTION OF NR 1 PACK SYS, PERFORMED HIGH POWER RUNS, AND PERFORMED A VISUAL INSPECTION OF THE RESDR SIMA20140722010Skin · dentedRUDDER 2 LT SIDE EXTERNAL SKIN HAS TWO DENTS APPROXIMATELY 8 INCHES BELOW PANEL 327BL & 7 INCHES FROM TE. ACCOMPLISHED REPAIR OF RUDDER 2 LT SIDE EXTERNAL SKIN DENTS IAW ERS-EM-55MR-135. FOUND DURING RUDDER MAIN CONTROL FEEDBACK PATH.SDR SIMA20140722007Warning System · false activationMASTER CAUTION AFTER ABORTED TAKEOFF, E1-2 EXCEEDANCE, WITH THE THRUST LEVERS IN THE DETENT BOTH ETTS WENT TO ABOVE 920 DURING THE ABORTED TAKEOFF. WE WERE DOING AN ALT TO 1 TAKEOFF WITH TEMP SET TO 25, MAX ACFT SPEED WAS 80 KTS LOW SPEED ABORT. PERFORMED A SDR SIMA20140722008Inverter · inoperativeSEAT 12A UPPER EMER EXIT SIGN INOPERATIVE. TROUBLE SHOT & FOUND EMER LIGHT DC & AC INVERTER. R & R INVERTER IAW AMM 33-50-11-000-801-A & 33-50-11-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20140722004Coupler · failedON TAKEOFF PASSING THROUGH 8000 FT GOT BLEED 2 LEAK. COMPLIED WITH EPC EMER PROCEDURES. BLEED 2 LEAK SECURED & RETURNED. PERFORMED LEAK CHECK OF NR 2 BLEED SYS IAW AMM 36-11-09. REPLACED GND CONNECTION COUPLING IAW AMM 36-10-02. OPERATIONS CHECKED GOOD IASDR ASOA20140722058Acm · seizedTHE CREW REPORTED WHITE SMOKE IN THE COCKPIT. MAINTENANCE INSPECTED AND FOUND NR 2 PACK ACM WAS SEIZED. MAINTENANCE REPLACED THE NR 2 PACK ACM. OPS CHECKS WERE GOOD.SDR SIMA20140721002Duct · leakingCLIMBING THROUGH 6000 FT, NR 1 BLEED LEAK EICAS MESSAGE PRESENTED. COMPLETED EPC & AOM 1 PROCEDURES. MESSAGE TOOK ABOUT 2 1/2 MINUTES TO CLEAR, BUT CLEARED. DIVERTED & RETURNED. REMOVED AND REPLACED LT PACK VALVE AND Y-DUCT IAW AMM 21-51-01 AND FLEX DUCSDR SIMA20140721008Connector · looseSERVICE DOOR EMER EXIT SIGN INOPERATIVE. TROUBLE SHOT EMER LIGHT IAW FIM 33-50-00-810-804-A. FOUND CONNECTOR LOOSE, ATTACHED CONNECTOR IAW AMM 33-50-09-400-802-A. OPERATIONS CHECKED GOOD.SDR SIMA20140721007Connector · looseSERVICE DOOR OVERHEAD EMER LIGHT INOPERATIVE. TROUBLE SHOT EMER LIGHT IAW FIM 33-50-00-810-804-A. FOUND CONNECTOR LOOSE, ATTACHED CONNECTOR IAW AMM 33-50-09-400-802-A. OPERATIONS CHECKED GOOD.SDR SIMA20140721009Light · inoperativeSERVICE DOOR EMER LIGHT INOPERATIVE. R & R EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.SDR SIMA20140721011Cradle · brokenFLIGHT ATTENDANTS EMER FLASHLIGHT CRADLE BROKEN. R & R IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.SDR RAIA201407200002Floor Support · corrodedRIGHT GUSSET HAS CORROSION AT FROM FRAMES 59-61. MAINTENANCE REPLACED RT GUSSET.SDR RAIA201407200001Floor Support · corrodedCENTER OMEGA BEAM IS CORRODED AT FRAME 20. MAINTENANCE REPLACED CENTER OMEGA BEAM.SDR SIMA20140720006Wire · brokenCEILING EXIT SIGN NEAR GALLEY IS INOPERATIVE. FOUND WIRE BROKEN ABOVE RT GALLEY BETWEEN CONNECTOR P8525 NAD SP9008. REPAIRED WIRE IAW SWPM 20-21-00 & WM 33-50-50. OPERATION CHECKED GOOD IAW AMM 33-50-00.SDR SIMA20140720004Heater · unknownNR 1 WINDSHIELD HEAT FAILED IN FLIGHT. REMAINED AFTER AOM VOL 1 PROCEDURE COMPLETED. PERFORMED OPS CHECK OF WINDSHIELD HEATING SYS IAW AMM 30-42-00. OPS CHECKED GOOD.SDR SIMA20140720003Flashlight · defectiveTHE FLASHLIGHT BEHIND THE CAPTAIN SEAT IS VERY DIM & SMELLS LIKE BURNING. R & R ASSEMBLY IAW 33-50-05 AMM. OPERATIONS CHECKED OK.SDR SIMA20140720001Icu · failedADC 1 & 2 FAIL WITH AP FAIL & AIRSPEED & ALT PRESELECT FAIL VERT SLOPE OFF. R & R REPLACED 2 ICU IAW AMM 23-00-01. OPERATIONS CHECKED GOOD & PERFORMED FNC OF ADC 1 & 2 IAW AMM 34-15-00. OPERATIONS CHECKED GOOD.SDR SIMA20140720002O-Ring · damagedBLD 1 LEAK INDICATION ON EICAS DURING EN ROUTE CLIMB THRU 10000 MSC RAN A011 CHECK LIST BLD LEAK INDICATION EXTINGUISHED AFTER APPROX 3 MINUTES. R & R ORING IAW ETN EM 36-048 ON BLD DUCT LOCATION 28, 17, 15, 9 & 7 IAW AMM 36-11-09. GND RAN OPERATIONS CHECK NSDR RAIA201407190008Floor Support · corrodedCENTER OMEGA BEAM GUSSET HAS MULTIPLE SPOTS OF CORROSION FROM FRAMES 18 TO 23. MAINTENANCE REPLACED CENTER OMEGA BEAM GUSSET.SDR RAIA201407190007Doubler · corrodedRIGHT AFT DOUBLER AT FRAME 22 CORRODED ON FORWARD NUT PLATE HOLE. MAINTENANCE REPLACED RT AFT DOUBLER.SDR RAIA201407190006Door Sill · corrodedAFT SERVICE DOOR SILL CORRODED FORWARD NUTPLATE HOLE AFT OF FR 22. MAINTENANCE REPLACED AFT SERVICE DOOR SILL AT FR 22.SDR RAIA201407190005Channel · corrodedLOWER SERVICE DOOR FRAME CHANNEL CORRODED AROUND AFT NUTPLATE HOLE FORWARD OF FR 20. MAINTENANCE REPLACED LOWER SERVICE DOOR SILL AT FR 20.SDR RAIA201407190004Door Sill · corrodedFORWARD SERVICE DOOR SILL CORRODED AROUND NUTPLATES AT FRAMES 19 AND 20. MAINTENANCE REPLACED DOOR SILL.SDR RAIA201407190003Floor Support · corrodedCENTER FLOOR SUPPORT ON CENTER OMEGA BEAM IS CORRODED AT FRAME 20. MAINTENANCE REPLACED CENTER FLOOR SUPPORT AT FR 20.SDR RAIA201407190002Floor Support · corrodedLEFT LOWER FLOOR SUPPORT ON LT OMEGA BEAM IS CORRODED AT FR 20. MAINTENANCE REPLACED LT LOWER FLOOR SUPPORT AT FR 20.SDR SIMA20140719002Heat Exchanger · crackedDURING REMOVING NR 1ACM FOUND CRACK ON NR 1 HEAT EXCHANGER. R & R NR 1 HEAT EXCHANGER IAW AMM 21-51-02.SDR SIMA20140719001Unknown · malfunctionedAT 25,000 CABIN ALTITUDE WENT TO 11,200. FOLLOWING FIM TASK 21-31-00-810-809 PERFORMED PRESSURIZATION CONTROL SYS FUNCTIONAL TEST IN THE AUTOMATIC MODE & FOUND SYSTEM OK IAW AMM 21-31-00-700-802-A.SDR SIMA20140718004Wire · brokenFIRST EMER LIGHT STRIP WIRE BROKEN. REPLACED ELEC CONNECTOR, MALE, ON THE POWER SUPPLY HARNESS ACFT SIDE TO THE FLOOR PROXIMITY STRIP LIGHT NR 1 IN THE MAIN CABIN IAW SWPM 20-21-00, 20-50-00 & 20-50-01 & IAW AMM 33-50-12 & 33-50-00, OPERATIONS CHECKED GOOD.SDR SIMA20140718003Wire · brokenNUMBER 1 EMER LIGHT STRIP HAS BROKEN WIRES. INSTALLED CONNECTOR AT NR 1 LIGHT STRIP IAW WM 91-10-02 & SWPM 20-00-03, FOR OPERATIONS CHECK SEE BOW 160456.SDR RAIA201407180001Channel · corrodedCARGO BAY ZEE CHANNEL HAS CORROSION. MAINTENANCE REPLACED CHANNEL.SDR SIMA20140718002Flashlight · inoperativeAFT CABIN BULKHEAD FLASHLIGHT INOPERATIVE. REPLACED AFT FLASHLIGHT IAW 33-50-16.SDR ASOA20140718225Floor Support · corrodedDURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 43-44. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01958. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140718224VFloor Support · corrodedDURING C-CHECK, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140718223VFloor Support · corrodedDURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140718222Floor Support · corrodedDURING C-CHECK, THE LT OMEGA BEAM AT FRAME 33-34 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140718221Beam · corrodedDURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20140717005Tube · leakingAFTER TAKEOFF DURING CLIMB OUT AT ABOUT 5000 FT A BLD 2 LEAK MSG WAS PRESENT ON EICAS WITH NO BLD LEAK LIGHT ON THE BLD 2 PB. WHILE COMPLYING WITH AOM 1 PROCEDURE A BLD 1 LEAK MSG WAS PRESENT ON EICAS WITH NO BLD LEAK LT ON THE BLD 1 PB, CONTINUED WITH BOTH BSDR SIMA20140717003Skin · crackedRIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1R & 2R IAW ERS-EM-53MR-595.SDR SIMA20140717004Skin · crackedLEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-596.SDR ASOA20140717056Power Supply · faultyDURING ROUTINE MAINTENANCE THE FWD OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.
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