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 SIMA20180317001Sign · inoperativeEMERGENCY EXIT SIGN BY SEAT 3BC FWD BULKHEAD INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-13. OPS CHECKED GOOD.SDR ASOA201803174016Acm · failedAIR RETURN DUE TO SMOKE AND HAZE IN THE COCKPIT. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT ACM, OPS TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20180317012Display · faultyTHE CREW REPORTED STRONG ODOR IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE ODOR TO BE COMING FROM THE CAPTAIN`S MFD. THE MFD WAS REPALCED AND OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR SIMA20180316001Inverter · inoperativeEMERGENCY LIGHT EXIT LOCATOR OVERWING FWD CEILING, INOPERATIVE IAW A PS-1 CHECK. FOUND EMERGENCY LIGHT DC/AC INVERTER NR 6 SUSPECTED TO BE BAD. R & R THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.SDR RAIA201803150001Bulb · inoperativeRIGHT EMERGENCY DOOR FLOOD LIGHT IS INOPERATIVE. R & R THE FLOOD LIGHT BULB, OPS CHECKED GOOD.SDR HNAA2018031600060Indicator · malfunctionedDURING CRUISE ALTITUDE, THE STBY ALTIMETER WAS INDICATING 1800 FEET LOWER THAN ADC AND THE STBY AIRSPEED INDICATOR WAS 25 KNOTS SLOWER THAN ADC. R & R THE STANDBY ALTIMETER IAW AMM 34-11-01. OPS CHECKED GOOD.SDR ASOA201803157033Stringer · crackedSTRINGER 2L CRACKED AT FRAME 75. CUT OUT CRACKED PORTION OF STRINGER INSTALLED FILLER AND DOUBLER IAW SRM 53-00-03. AIRCRAFT STILL IN C CHECK.SDR SIMA20180314008Battery · dischargedLT AND RT OVERWING EMERGENCY LIGHTS INOP. R&R NR 4 EMERGENCY BATTERY IAW WORK CARDS 33-700-19 AND 33-700-17 OPS CHECK GOOD AT THIS TIME END.SDR ASOA201803147032Stringer · crackedSTRINGER 2R CRACKED AT FRAME 75. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW ETD 2018-145-018888. AIRCRAFT STILL IN C CHECK.SDR SIMA20180313007Light · inoperativeEMERGENCY EXIT LIGHT ABOVE EMERGENCY EXIT ROW INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A, AND 33-50-08-400-801-A.. OPS CHECKED GOOD.SDR SIMA20180312004Flashlight · intermittentFWD CABIN FLASHLIGHT SWITCH INTERMITTANT. R & R THE FLASHLIGHT IAW AMM 33-50-16-000-801-A, AND 33-50-16-400-801-A. OPS CHECKED GOOD.SDR SIMA20180312001Charger · inoperativeLT AND RT OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. REMOVED AND REPLACED THE NR 4 BATTERY AND CHARGER ASSEMBLY IAW FIM 33-50-00-810-804-A, AND AMM 33-50-10. OPS CHECKED GOOD,SDR SIMA20180312003Light · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10, OPS CHECKED GOOD.SDR SIMA20180312002Lamp · inoperativeGALLEY DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. NO FURTHER DISCREPANCIES FOUND.SDR RAIA201803100001Door Sill · corrodedSERVICE DOOR CENTER SILL HAS MULTIPLE AREAS OF CORROSION. R & R SERVICE DOOR SILL.SDR SIMA20180310002Angle · crackedAFT ANGLE THAT ATTACHES TO AFT FLOOR SUPPORT UNDER FLOORBOARD 271FF WAS FOUND CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02.SDR SIMA20180309002Structure · corrodedCARGO DOOR FRAME FORWARD L SHAPE HAS CORROSION ON THE BOTTOM EDGE. REPAIRED THE DOOR FRAME FWD L SHAPE IAW SRM 53-31-04.SDR SIMA20180309001Door Sill · corrodedCARGO DOOR SILL IS CORRODED. REMOVED AND REPLACED THE CARGO DOOR SILL IAW SRM 51-40-02.SDR RAIA201803090001Wire · brokenCAPTAIN`S EMERGENCY FLASHLIGHT HAS A BROKEN WIRE. REPAIRED THE WIRE. OPS CHECKED GOOD.SDR 4VAA20180309001Trim Switch · failedAFTER TAKEOFF AND PASSING THROUGH 5000 FT, CREW EXPERIENCED A STABILIZER TRIM RUNAWAY, FOLLOWED BY A FAILURE OF THE MAIN AND STANDBY TRIMS AS INDICATED BY EICAS MESSAGES. CREW COMPLETED STABILIZER TRIM RUNAWAY, AND STABILIZER TRIM FAILURE QRC PROCEDURES. RETUSDR ASOA201803097031Skin · crackedDURING A C-CHECK, FOUND A CRACK ON THE RT TRAILING EDGE OF THE VERTICAL STAB BETWEEN THE FIRST ROLL OF BEARINGS AND THE 2ND ROLL. MAINTENANCE INSTALLED A REPAIR TO THE CRACKED AREA OF THE RUDDER TRAILING EDGE IAW EC/TC ETD 2018-145-019454.SDR ASOA201803097030Skin · crackedDURING A C CHECK, FOUND A CRACK ON THE LEFT TRAILING EDGE FLANGE OF THE VERTICAL STAB ABOVE THE PCU ACTUATORS. MAINNTENANCE INSTALLED A REPAIR TO THE AREA IAW EC/TC ETD2018-145-019454.SDR RAIA2018041900003Door Sill · corrodedCARGO DOOR LOWER SILL IS CORRODED. R & R THE CARGO DOOR LOWER SILL.SDR RAIA201803080002Shear Tie · corrodedFRAME 68, SHEAR TIE WAS FOUND CORRODED. REPAIRED THE SHEAR TIE.SDR RAIA201803080001Shear Tie · corrodedFRAME 65, SHEAR TIE IS CORRODED. R & R THE SHEAR TIE.SDR SIMA20180308011Support Bracket · crackedAFT CARGO DOOR HORIZONTAL SUPPORT BRACKET FOR LIFTING AND LOWERING MECHANISM IS CRACKED. REMOVED AND REPLACED THE SUPPORT BRACKETIAW SRM 51-40-02.SDR SIMA20180308010Attach Bracket · crackedLEFT OVERWING PANEL UPPER ATTACH BRACKET AT FRAME 48 IS CRACKED APPROXIMATELY ONE INCH. REPAIRED IAW SRM 53-23-12.SDR SIMA20180308009Bracket · crackedPAX DOOR INNER HANDLE SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED PRE-EXISTING REPAIR DOUBLER ON PAX DOOR INNER HANDLE TORQUE BOX REFERENCING EO-EM-52MR-250 FOR MATERIAL AND FASTENER INSTALLATION SPECS.SDR SIMA20180308008Bracket · crackedCARGO DOOR HOLD OPEN HANDLE BRACKET IS CRACKED. INSTALLED A NEW CARGO DOOR HOLD OPEN HANDLE BRACKET IAW SRM 51-40-02.SDR SIMA20180308007Attach Bracket · crackedLEFT OVERWING PANEL NR 2 LOWER ATTACH BRACKET IS CRACKED APPROX. 1/4 INCH. REMOVED AND REPLACED THE OVERWING PANEL LOWER ATTACH BRACKET IAW SRM 51-40-02.SDR SIMA20180308002Flap Track · defectiveFLAP FAIL AFTER TAKEOFF CLIMBING THROUGH 2500' AND DECELERATING THROUGH 200 KTS AOM 1 PROC APPLIED. REMOVED AND REPLACED RT I/B FLAP ROOT MOVABLE TRACK IAW AMM 57-52-01. INSTALLED NEW RT I/B FLAP SHROUD IAW AMM 57-56-01. REMOVED AND REPLACED RT I/B FLAP TIP MOSDR SIMA20180308005Lamp · inoperativeLEFT EXTERNAL FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A.. OPS CHECKED GOOD.SDR SIMA20180308004Ecu · failedDURING APPROACH, A FLAP FAILED MESSAGE WITH FLAPS AT 9 DEGREES. PERFORMED A VISUAL INSPECTION OF THE FLAPS AND FLAP HANDLE. FOUND BOTH TO BE AT 9 DEGREES. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02. OPS CHECKED SATISFACTORY. NO SDR SIMA20180308006Support Angle · crackedRIGHT OUTBOARD OMEGA BEAM SUPPORT BRACKET CRACKED APPROXIMATELY 3/4 INCH AT FRAME 48. REMOVED AND REPLACED THE RT OTBD OMEGA BEAM SUPPORT ANGLE IAW SRM 51-40-02.SDR SIMA20180308001Landing Gear · malfunctionedWHEN THE LANDING GEAR WAS RETRACTED, HEARD TWO LOUD BANGS AND THE AIRCRAFT STUDDERED AS GEAR WENT UP AND LOCKED . BURNED FUEL TO BELOW MAX LANDING WEIGHT, GEAR CAME DOWN NORMALLY AND LANDING UNEVENTFUL. PERFORMED SEVERAL CHECKS IAW AMM 32-30-00, RETRACTIOSDR HNAA2018030900055Connector · contaminatedEICAS SPOILER FAILED MESSAGE WITH SPOILER DEPLOYMENT, DURING CLIMB OUT. HAPPENED AROUND 3000 FEET, SPOILERS FELT DEPLOYED, CIRCUIT BREAKERS WERE PULLED IAW QRH. TROUBLESHOT IAW FIM 27-63-00-810-802-A AND DETERMINED TO BE TRANSITORY CONDITION. PERFORMED SDR SIMA20180307004Frame · crackedUPPER FRAME 10R IS CRACKED JUST BELOW RIGHT DV WINDOW SILL. REMOVED AND REPLACED FR 10R BELOW DV WINDOW IAW SRM 51-40-02.SDR SIMA20180307002Electronic Unit · failedFLAPS FAILED MESSAGE DURING CLIMBOUT. PERFORMED CMC DOWNLOAD. NOTED FECU FAIL MESSAGE. COMPLIED WITH FIM 27-51-00-810-803-A. REMOVED AND REPLACED FLAP ELECTRONIC UNIT IAW AMM 27-53-02. OPS CHECKED GOOD, NO FAULTS FOUND.SDR SIMA20180307003Sensor · malfunctionedFLAP FAILED ON APPROACH. REMOVED AND REPLACED THE LT FLAP VELOCITY SENSOR, OPS CHECKED GOOD.SDR RAIA201803013001Door Frame · dentedCARGO DOOR LOWER FRAME PROFILE IS DENTED. R & R CARGO DOOR LOWER FRAME PROFILE.SDR ASOA201803063010Door Sill · corrodedGALLEY SERVICE DOOR SILL CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED GALLEY SERVICE DOOR SILL IAW SRM 53-21-10.SDR HNAA2018030800054Relay · damagedINSPECTED RELAYS K1237 AND K0058 IAW FCD1-30-16-0276, FOUND EVIDENCE OF HEAT DAMAGE. R & R THE RELAYS IAW AMM 20-13-02-0001, OPS CHECKED GOOD. OK FOR SERVICE.SDR RAIA201803050002Skin · dentedPAX DOOR LOWER CENTER EXTERIOR SKIN, 6 INCHES FROM BOTTOM HAS 2 DENTS. REPAIRED THE DOOR SKIN.SDR RAIA201803040001Blanking Plate · leakingLOSS OF PRESSURIZATION AT ABOUT 19000 FT. REINSTALLED CLAMP AND BLANKING PLATE FOR THE NR 2 CONDENSER MIXER. PERFORMED AN OPS CHECK OF PRESSURIZATION CONTROL SYSTEM, NO FAULTS NOTED.SDR HNAA2018030500053Warning Message · illuminatedBLEED 2 VALVE CLOSED MESSAGE DISPLAYED ON EICAS DURING FLIGHT, CREW FOLLOWED QRH MESSAGE AND RETURNED.SDR HNAA2018030500052Proximity Switch · failedON LIFTOFF, MLG AIR GROUND FAILED AND THE NR 1 & 2 ENGINE REVERSER DISAGREE EICAS MESSAGES APPEARED AND REMAINED ON UNTIL TOUCHDOWN. R & R THE WOW PROXIMITY SWITCH HARNESS, R & R THE NOSE GEAR UPLOCK HARNESS. R & R THE NLG WOW PROXIMITY SWITCH.SDR SIMA20180302004Module · failedAFTER STARTING THE NR 1 ENGINE, THIN TRAIL OF SMOKE VISIBLE AND ODOR FROM BEHIND THE NR 2 LIGHTING PANEL. SMOKE STARTED WHEN FO CHART HOLDER LIGHT WENT OUT. FOUND THE CO PILOT`S LIGHTING CONTROL PANEL CHART HOLDER KNOB BURNED. REMOVED AND REPLACED CO PILOTSDR ASOA201803024015Charger · inoperativeDURING A MAINTENANCE INSPECTION, THE EXTERNAL EMERGENCY LIGHT ON THE LT & RT OVERWING PANELS WERE FOUND TO BE INOPERATIVE. MAINTEMNANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY, OPS TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20180301001Solenoid · failedFLIGHT ATTENDANT REPORTED A STRANGE ODOR BEHIND THE EXIT ROW IN THE CABIN. THE LIGHTS CAUSED A SPARK WHEN TURNED ON. INSPECTED WIRING FOR SIGNS OF DAMAGE, FOUND OXYGEN DOOR RELEASE SOLINOID SMELLED OF BURNED ELECTRICAL. REMOVED AND REPACED THE PSU PANEL ATSDR ASOA201903017028Skin · crackedA/C IS IN C-CHECK WHEN INSPECTION FOUND THE RIGHT AFT FUSELAGE SKIN CRACKED AT RIVET ON FRAME 75 AND STRINGER 2R. MAINTENANCE REPAIRED THE SKIN AT FRAME 75 STRINGER 2R IAW SRM 53-31-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
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