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 SIMA20120512003Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FOR THE RIGHT FORWARD EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT SDR ASOA20120511046Acm · smokeTHE CREW REPORTED A BURNING RUBBER ODOR IN COCKPIT FOLLOWED BY WHITE HAZE AND SMOKE. SMOKE STOPPED WHEN PACK NR 1 WAS DESELECTED. MX REPLACED THE NR 1 ACM. OPS CHECKS WERE GOOD.SDR SIMA20120511002Flashlight · inoperativeDURING B INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT CABIN FLASHLIGHT AND BATTERY IAW EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT SDR CHQA20120511148Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE RIGHT OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20120510025Shear Tie · corrodedDURING MAINTENANCE INSPECTION FOUND FRAME 65 HAS OUT OF LIMITS WITH CORROSION AT LOWER STIKER PLATE NUTPLATES. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER PER ETD 2012-145-006915. AIRCRAFT RETURNED TO SERVICE.SDR CHQA20120510147Hydraulic System · lowCREW REPORTED THAT THEY RECEIVED A HYDRAULIC 1 LOW QUANTITY MESSAGE IN FLIGHT. AFTER RECEIVING THE MESSAGE THEY RECEIVED A HYDRAULIC SYSTEM 1 FAIL MESSAGE. THE CREW PERFORMED AN ABNORMAL FREE FALL LANDING GEAR EXTENSION DUE TO THE HYDRAULIC SYSTEM 1 FAILURESDR SIMA20120510024Inverter · inoperativeDURING B INSPECTION FOUND THE RIGHT WALL EMERGENCY LIGHT BY ESCAPE HATCH INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11 IAW W/C 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE ASDR SIMA20120510022Light · inoperativeDURING B INSPECTION FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LAMP IAW EMB 145 AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE SDR SIMA20120510021Flashlight · inoperativeDURING B INSPECTION FOUND THE FORWARD CABIN RECHARGEABLE FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TOSDR RAIA201205100002Unknown · malfunctionedDURING DESCENT INTO KSTL, THE A/C HAD A FLAP LOW SPEED MSG. THE CREW PERFORMED AN EMERGENCY LANDING. MAINTENANCE REMOVED AND REPLACED A FLAP MOTOR AND THE FLAP ELECTRONIC CONTROL UNIT WITH A NO FIX. MAINTENANCE THEN DEFERRED FLAP CHANNEL 1, OPS CHECK GOOD.SDR SIMA20120509005Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE FORWARD ENTRY CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING LAMP IAW 33-50-06-000-801-A AND 33-50-06-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRASDR SIMA20120509004Cradle · brokenDURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT’S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLASHLIGHT CRADLE ASSEMBLY IAW 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS SDR SIMA20120508006Cradle · brokenDURING MAINTENANCE INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S AND THE FORWARD FLIGHT ATTENDANT’S FLASHLIGHT CRADLE AS REQUIRED IN REF WITH WC 33-700-20. THE OPERATIONAL SDR ASOA20120507071Skin · puncturedA SMALL PUNCTURE IN THE SKIN AT FRAME 10 NEAR STRINGER 14 NEXT TO THE TAT PROBE. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED SKIN, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20120508144Valve · missingCREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN AUTO MODE OR IN MANUAL MODE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE EXTERIOR GROUND AIR CONNECTION VALVE FLAPPER MISSING. THE GROUND AIR CONNECTION VALVSDR ASOA20120508036Acm · seizedCREW REPORTED BRIEF EICAS MESSAGE BLEED NR 2 OVERTEMP, ILLUMINATED AND CLEARED. FOLLOWED BY EICAS MESSAGE PACK NR 2 CLOSED AND BLEED NR 2 CLOSED AFTER RESETTING BOTH BLEED AND PACK NR 2 STRONG BURNING ODOR OCCURRED. MX INSPECTED AND FOUND NR 1 PACK SEIZED ANSDR RAIA201205080001Glowstrip · looseFLIGHT CREW FOUND EMERGENCY EXIT 12A FLOOR PHOTO ILLUMINESCENT STRIP LOOSE DURING POST FLIGHT INSPECTION. MAINTENANCE RE-SECURED THE EMERGENCY FLOOR PHOTO ILLUMINESCENT STRIP AT 12A, OPS CHECK GOOD.SDR SIMA20120508003Flashlight · defectiveON FLIGHT 2914 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT NOT SNUG IN CRADLE RED LIGHT DOESN’T STAY ILLUMINATED UNLESS FLIGHT ATTENDANT PUSHES ON IT IN TURBULENCE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANSDR SIMA20120508001Flashlight · inoperativeON FLIGHT 3514 THE CREW REPORTED THE CAPTAIN'S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN'S FLASHLIGHT IAW MM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA20120507035Unknown · odorCREW REPORTED A STRONG ELECTRICAL ODOR ON CLIMBOUT. FLIGHT CONTINUED. MX RAN ENGINES IAW AMM 71-00-01 AND PERFORMED OPS CHECKS OF THE APU, PACK SYS, AND PNEUMATIC SYS SUCCESSFULLY. COULD NOT DUPLICATE ANY ELECTRICAL BURNING ODOR OR DEFECTS AT THIS TIME. ACFSDR SIMA20120507006Engine · failedON FLIGHT 4164 THE CREW REPORTED THE NUMBER 2 ENGINE FAILED ON FINAL APPROACH. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NR 2 IAW MTX WC 71-000-00. THE OPERATIOSDR ASOA20120507044Charger · faultyDURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER AND EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.SDR SIMA20120507005Light · inoperativeDURING B-INSPECTION FOUND THE RIGHT HAND OVER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOSDR SIMA20120507003Light · inoperativeDURING B-INSPECTION FOUND THE EMERGENCY AISLE LIGHT INOPERABLE AT ROW 12. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LAMP AT ROW 12 IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00-700-801A. THESDR SIMA20120507002Flashlight · inoperativeON FLIGHT 4055 THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT HOLDER DOES NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNSDR SIMA20120506004Wire · separatedDURING MAINTENANCE INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT WIRE SEPARATED. MEL 25-53 AUTH# 050273-C FWD FLT ATND FLASHLIGHT. REQ MAINT ACTIONS COMPLIED WITH. REPLACED SPLICE AS REQUIRED IAW SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. MELSDR SIMA20120506002Cover · defectiveON FLIGHT 4291 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN CABIN DOOR HANDLE COVER PER STANDARD MTX PROCEDURES. THE OPERATIONAL CHECK WAS GOOD PER EMB-145 MM 52SDR SIMA20120506001Inverter · inoperativeDURING B-INSPECTION FOUND THE RIGHT WINDSCREEN EMERGENCY EXIT LOCATOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNESDR SIMA20120505001Fuse · unserviceableDURING B-INSPECTION FOUND THE SECOND AISLE AND RIGHT FORWARD FAIRING EXTERNAL EMERGENCY LIGHTS ARE INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND DEDICATED FUSE IN CIRCUIT POWERING BOTH LIGHTS TO HAVE A RESISTANCE OF 21 OHMS. GAINED ACCESS TO FUSSDR CHQA20120504156Skin · damagedDURING INSPECTION, THE RUDDER I PROTRACTOR SKIN AT THE ATTACHING NUT PLATE WAS FOUND TO BE DAMAGED. THE RUDDER I SKIN AT PROTRACTOR ATTACHING NUT PLATE WAS REPAIRED IN ACCORDANCE WITH SRM 55-40-01.SDR ASOA20120504043Fan · odorCREW REPORTED AN ELECTRICAL ODOR. INSPECTED AVIONICS BAY AND FOUND RECIRCULATION FANS INOPERATIVE. THE SYS WAS RESET AND OPS CHECKED GOOD. NO ELECTRICAL ODOR WAS FOUND.SDR SIMA20120504001O-Ring · damagedON FLIGHT 3214 IN CRUISE FLIGHT THE CREW REPORTED THEY GOT E1 BLEED LEAK EICAS MESSAGE FOLLOWED AOM E1 BLEED SHUT OFF MESSAGE CLEARED AND EMERGENCY DECLARED AND LANDED IN MAF. THE AIRCRAFT LANDED WITHOUT INCIDENT. NO OTHER PROBLEMS NOTED. THE AIRCRAFT WAS RSDR SIMA20120423010Mount Fitting · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT LOWER YOKE 1 FORWARD ENGINE MOUNT FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FITTING IAW EO-EM-54MR-386. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120503018Angle · corrodedCORROSION ON FR68 "L" SHAPE AT THRESHOLD. REPAIRED FR 68 "L" SHAPE IAW EM-53MR-1129.SDR SIMA20120503017Structure · corrodedCARGO DOOR CUT OUT FWD LOWER CORNER CORROSION AT LOWER STRIKER PLATE AND RIVETS. REMOVED CORROSION ON FWD STRIKER PLATE REF SRM 51-20-00. REMOVED STRIKER PLATE FOM.SDR SIMA20120503016Floor Support · crackedDURING SCHEDULED MAINTENANCE FOUND THE RIGHT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47 AS MARKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED OUTBOARD OMEGA BEAM SUPPORT REF 51-40-02. LOCATED AND DRILLED NEW OUTBOARD OMEGA SUPPORT AT FRAME 47. INSTALLSDR SIMA20120503015Rib · corrodedDURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR CUTOUT FORWARD LOWER CORNER CORRODED AT NUT PLATE FOR TRIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED RIB DUE TO OUT OF LIMIT CORROSION. LOCATED & DRILLED NEW RIB IAW SRM 51-40-02. THE AIRCRAFT WAS RESDR SIMA20120503014Sill · corrodedDURING SCHEDULED MAINTENANCE FOUND THE BAGGAGE DOOR SILL HAS CORROSION AT NUT PLATE (4 EACH). THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CARGO DOOR SILL, LOCATED & DRILLED NEW SILL BLENDED CORROSION ON EXISTING SILL REF SRM 51-10-03, 100 PERCENT MATERIALSDR SIMA20120503013Wire · damagedDURING SCHEDULED MAINTENANCE FOUND THE EMERGENCY LIGHT STRIP WIRES PULLED/BROKEN AT FERRULE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESOLDERED LEFT NR 1 EMERGENCY LIGHT WIRES REFERENCING EMB 145 SWPM 20-30-00. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120503012Light · inoperativeDURING B INSPECTION, FOUND THE EMERGENCY LIGHT NR 1 AND NR 7 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT NR 1 AND NR 7 IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120503011Wire · damagedDURING B INSPECTION, FOUND THE NR 3 AND NR 4 PROXIMITY LIGHT WIRING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 AND NR 4 FLOOR PROXIMITY STRIPS IAW EMB145 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETUSDR SIMA20120503010Inverter · inoperativeDURING B INSPECTION, FOUND EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120503009Battery · inoperativeDURING MAINTENANCE INSPECTION, FOUND THE RECHARGEABLE FLASHLIGHT SYSTEM NEEDS A BATTERY. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120503008Floor Support · corrodedDURING MAINTENANCE INSPECTION, FOUND THE RIGHT FLOOR SILL CORRODED BETWEEN FRAMES 39 AND 44. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORROSION REF SRM 51-10-03 NOMINAL .050 INCH REMAINING MATERIAL .032" OUT OF LIMITS OF SRM 53-23-10 FIGURE 101. REMOVSDR SIMA20120501003Light · crackedDURING B INSPECTION, FOUND THE NR 4 CABIN PROXIMITY LIGHT CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 CABIN PROXIMITY LIGHT IAW AMM 33-50-12, NRTC BOW93438. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120503007Support · crackedDURING MAINTENANCE INSPECTION, FOUND A CRACK ON RIGHT BELLY PANEL SUPPORT FORWARD OF RIGHT INBOARD FLAP TQ BOX. AIRCRAFT REMOVED FROM SERVICE. REMOVED CRACKED BELLY PANEL SUPPORT RIGHT USING REF SUM 51-40-00. FABRICATED NEW ANGLE IAW SRM 51-40-02. TREATED SDR SIMA20120503006Floor Support · crackedDURING MAINTENANCE INSPECTION, FOUND THE LEFT OUTBOARD OMEGA BEAM SUPPORT CRACKED AT FR47. AIRCRAFT REMOVED FROM SERVICE. REMOVED LEFT OUTBOARD OMEGA BEAM SUPPORT, LOCATED AND DRILLED NEW PART AND INSTALLED REF SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.SDR CHQA20120503155Support · crackedDURING INSPECTION, THE FORWARD RADIO ALTIMETER 2 BASE SUPPORT WAS FOUND TO BE CRACKED. THE FORWARD RADIO ALTIMETER 2 BASE SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20120503154Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM OUTBOARD ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAME 47 AND FRAME 48. THE LEFT OMEGA BEAM OUTBOARD ANGLE BETWEEN FRAME 47 AND FRAME 48 WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.SDR CHQA20120503153Floor Support · crackedDURING INSPECTION, THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS FOUND TO BE CRACKED BETWEEN FRAME 47 AND FRAME 48. THE RIGHT OMEGA BEAM OUTBOARD ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
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