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 CHQA20130403120Frame · crackedDURING INSPECTION, A DENT WAS FOUND ON FRAME 72 ON THE LEFT SIDE ABOVE STRINGER 14L. A HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND THE FRAME TO BE CRACKED. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-006047.SDR SIMA20130403003Duct · damagedFLIGHT 3577, NR 1 ENGINE BLEED LEAK WHILE CLIMBING THRU 1000 FT. DECLARED AN EMERGENCY AND FOLLOWED AOM EMERGENCY PROCEDURES. INDICATION EXTINGUISHED 2.5 MINTUES AFTER BLEED VALVE WAS CLOSED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HORIZITAL DUCT SDR CHQA20130403104Controller · malfunctionedCREW REPORTED THAT THE AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION DURING FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED THAT THE MANUAL PRESSURIZATION SYSTEM WAS OPERATIVE AND DEFERRED THE AUTO PRESSURIZATION SYSSDR SIMA20130403008Battery · dischargedDURING B INSPECTION FOUND THE EMERGENCY LIGHTS AT COCKPIT CEILING, FORWARD CEILING IN CABIN AND EXIT FORWARD LEFT WING LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW AESDR SIMA20130403007Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB 145 AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. NOSDR SIMA20130403004Skin · crackedDURING MAINTENANCE INSPECTION FOUND THE SKIN CRACKED NEAR RIVET HOLE ON FRAME 75 AND BETWEEN 1R/2R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-2114. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130403002Flashlight · inoperativeON FLIGHT 3574 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW/CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA20130402123VBeam · corrodedDURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT MAIN BEAM CORRODED. FRAMES 65-68. BEAM R & R IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402122VNut Plate · corrodedDURING C-CHECK, CORROSION AROUND MAIN DOOR LOWER NUTPLATES. REPAIRED IAW EC5210-01154, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402121Torque Box · damagedDURING C-CHECK, LT NR 1 UPPER INBD TORQUE BOX BOLT HOLE DAMAGED. REPAIRED IAW EC5710-01202, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402120Nut Plate · corrodedDURING C-CHECK, SERVICE DOOR HAS CORROSION AROUND LOWER NUTPLATES. REPAIRED IAW EC5210-01154, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402119Yoke · crackedDURING C-CHECK, LT FWD LOWER ENGINE YOKE FWD FITTING CRACKED. REPAIRED IAW EC5450-01071. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402118Skin · corrodedDURING C-CHECK INTERNAL SKIN CORRODED. FRAMES 13-14, STRINGERS 20L-20R. REPAIRED IAW EC5320-01777. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402117Frame · chafedDURING C-CHECK, FRAME 60 CHAFED AT STRINGER 5L. REPAIRED IAW EC5310-01695. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402116Door Frame · corrodedDURING C-CHECK, FRAME 65 CORRODED AT NUT PLATES AT STRINGER 14-15L. R & R FRAME 65 DOUBLER IAW SRM 51-40-02 AND EC5310-01505, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR CHQA20130402123Rail · corrodedDURING INSPECTION, THE PASSENGER DOOR STEP RAILS WERE FOUND TO BE CORRODED. THE PASSENGER DOOR STEP RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130402122Rail · corrodedDURING INSPECTION, THE PASSENGER DOOR STEP RAILS WERE FOUND TO BE CORRODED. THE PASSENGER DOOR STEP RAILS WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR SIMA20130402001Flashlight · malfunctionedON FLIGHT 3585 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT ABOVE JUMP SEAT APPEARS TO NOT BE CHARGING BECAUSE THE RED LIGHT IS NOT ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET FLASHLIGHT CHARGING IAW AMM 33-30-00. THE OPERATIONAL CHECK WASDR ASOA20130402115Skin · dentedDURING C-CHECK, EXTERNAL FUSELAGE DENTED BETWEEN FRAMES 75-76, STRINGERS 17-18R. REPAIRED IAW EC5330-02731, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402114Shear Tie · corrodedDURING C-CHECK, AFT LOWER CARGO DOOR CUTOUT SHEAR CLIP CORRODED FRAME 68. MX R & R SHEAR CLIP IAW SRM 51-40-02 AND EC5320-01494. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130402113Shear Tie · corrodedDURING C-CHECK FWD LOWER CARGO DOOR CUTOUT SHEAR CLIP CORRODED FRAME 65. MX R & R SHEAR CLIP IAW SRM 51-40-02 AND EC5320-01494, REV A. ACFT APPROVED FOR RETURN TO SERVICE.SDR CHQA20130401118Frame · chafedDURING INSPECTION, A CHAFE WAS FOUND AT FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.SDR SIMA20130401006Unknown · odorON FLIGHT 2803 THE CREW REPORTED A STRONG AND PUNGENT ODOR IN THE COCKPIT DURING THE TAKEOFF ROLL. THE CREW ELECTED TO MAKE A HIGH SPEED ABORT AROUND 120 KTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH INSP 05-50-16 EMB MM NO DEFECTS NOTED. PERFOSDR SIMA20130404001Spar · crackedDURING MAINTENANCE INSPECTION FOUND THE LEFT WING SPAR 3 CRACKED AT 10 O’CLOCK AND 4 O’CLOCK POSITIONS AT MLG HARNESS 10 O’CLOCK POSITION 2.10, 4 O`CLOCK POSITION 1.50 VIABLE FROM FORWARD AND AFT SIDES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED AS PER SDR RAIA201303310002Light · inoperativeDURING SCHEDULED MAINTENANCE THE RIGHT AFT WING/FUSELAGE FARING EXTERIOR FLOOD LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT WING/FUSELAGE FARING EXTERIOR FLOOD LIGHT. SYSTEM OPS CHECKED GOOD.SDR RAIA201303310001Light · inoperativeDURING SCHEDULED MAINTENANCE FOUND THE RIGHT AFT WING/FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOP. MAINTENANCE REMOVED AND REPLACE THE BULB. SYSTEM OPS CHECKED GOOD.SDR CHQA20130331103Strut · lowCREW REPORTED THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE WITH AN ASSOCIATED ENGINE 1 AND 2 REVERSE DISAGREE MESSAGE DURING LANDING GEAR RETRACTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE NOSE LSDR SIMA20130331010Flashlight Assy · inoperativeFLIGHT 3358, CAPTAIN’S FLASHLIGHT WAS INOPERATIVE. REMOVED AND REPLACED COCKPIT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.SDR SIMA20130331009Pressure Switch · faultyON FLIGHT 4155 THE CREW REPORTED THE RUDDER SYSTEM 1 AND 2 FAILED IN CLIMB. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO CMH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER SYSTEM 2 PRESSURE SSDR SIMA20130331008Computer · malfunctionedON FLIGHT 3409 THE CREW REPORTED THAT AFTER TAKEOFF CLIMBING AT NORMAL CLIMB SPEED APROX 14,000 FT STICK SHAKER AVTIVATED NO LOSS OF AIRSPEED YAW DAMP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETUNRED TO DRO. UPON LANDING SPOILERS FAILED TO DSDR SIMA20130331007Connector · disconnectedDURING MAINTENANCE INSPECTION FOUND THE FORWARD EMERGENCY FLOOR LIGHT STRIP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RECONNECTED CONNECTOR. THE OPERATIONAL CHECK WAS NORMAL IAW EMB145 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130331004Unknown · fumesFOR FLIGHT 4093 THE CREW REPORTED FUMES IN COCKPIT AFTER ENGINE 1 START COMPLIED WITH AOM PROCEDURES. THE AIRCRAFT RETURNED TO GATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE ODOR EVENT TROUBLESHOOTING IAW ETN: ETN-EM-72-034. COULD NOT DUPLICSDR SIMA20130330005Light · inoperativeDURING B INSPECTION FOUND THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EXTERNAL EMERGENCY LIGHT BULB IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATISDR SIMA20130330004Charger · defectiveDURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY CHARGER NEEDS TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW EMB AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THSDR SIMA20130330003Battery · weakDURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT BATTERY WEAK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY IAW EMB AMM 33-50-04. REF ITEM 1 LOG PG 3084360. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURSDR V0XR20130401J0186Stringer · chafedSTRINGER 2L IS CHAFED AT FRAME 20. BLENDED OUT DAMAGE IAW SRM 51-10-03, NDT PERFORMED, NO DEFECTS NOTED, ALODINED DAMAGED AREA, FABRICATED REPAIR, ALODINED AND PRIMED FABRICATED PARTS, INSTALLED NEW FABRICATED REPAIR, DOUBLER. CLASSIFIED AS A MAJOR.SDR SIMA20130329006Rib · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT WING RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIB 5 IAW EO EM-57MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130329004Light · inoperativeDURING B INSPECTION FOUND THE SERVICE DOOR CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP AT SERVICE DOOR CEILING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-09-000-801-A AND 33-50-09-400-801-A. THE OPERASDR SIMA20130329003Light · inoperativeDURING B INSPECTION FOUND THE CABIN CENTER AISLE CEILING EMERGENCY LIGHT 2ND FROM FRONT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN CENTER AISLE CEILING EMERGENCY LIGHT LAMP 2ND FROM FRONT IAW EMB AMM TASK 33-50-08-000-8SDR ASOA20130328027Fcu · leakingTHE CREW REPORTED A VERY STRONG FUEL ODOR RT AFTER TAKEOFF AND LASTED 2-03 MINUTES. MX INSPECTED AND REPLACED THE APU FUEL CONTROL UNIT. OPS CHECKED GOOD.SDR SIMA20130328005Battery · defectiveDURING B INSPECTION FOUND THE COPILOTS FLASHLIGHT INTERMITTENTLY CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT CRADDLE ASSEMBLY AND REMOVED AND REPLACED THE FLASHLIGHT BATTERY UNIT IAW EMB145 AMM 33-50-1SDR SIMA20130328004Flashlight · inoperativeDURING B INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT WILL NOT TURN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT IAW EMB AMM 33-50-16-00-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AISDR SIMA20130328003Holder · brokenDURING B INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BASE IAW EMB 145 AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOODSDR SIMA20130328002Power Supply · inoperativeDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTS FROM ROW 12-18 FAILED AFTER A FEW SECONDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AISDR ASOA20130326107Shear Tie · corrodedDURING C-CHECK SHEAR TIE AT FRAME 68 BETWEEN STRINGER 18L-17L IS CORRODED. MX REPAIRED SHEAR TIE IAW SRM 51-20-01 AND CPM 51-21-06. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130326106Skin · corrodedDURING C-CHECK, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130326104Stringer · corrodedDURING C-CHECK, COCKPIT STRINGER 21R CORRODED. MX R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130326103Stringer · corrodedDURING C-CHECK COCKPIT STRINGER 21L CORRODED. MX REPAIRED OF STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130326102Stringer Splice · corrodedDURING C-CHECK, STRINGER SPLICE 21L CORRODED BETWEEN FRAMES 12-13. MX PERFORMED REPAIR ON STRINGER SPLICE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.SDR SIMA20130327002Guide · dirtyON FLIGHT 2758 THE CREW REPORTED THE PASSENGER ENTRY DOOR HANDLE DID NOT ROTATE FULLY MAKING IT DIFFICULT TO OPEN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED PASSENGER DOOR GUIDE/ROLLERS PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IA
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