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 HNAA2018052100005Inverter · inoperativeFLOOR EMERGENCY LIGHTS INOPERATIVE AT THE EMERGENCY EXIT. R & R THE INVERTER IAW AMM 33-50-11.SDR SIMA2018052119008Light · inoperativeDURING A PS-1 CHECK, FOUND THE EMERGENCY LIGHTS INOPERATIVE, COCKPIT FLOOD LIGHT, AISLE LIGHT 1 AND EXTERNAL WING TO FUSELAGE FAIRNG LIGHT. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY HOLDER ASSY AND NR 1 EMERGENCY BATTERY CHARGER ASSY IAW AMM 33-50-04.SDR HNAA2018052100004Connector · damagedFLOOR EMERGENCY LIGHT INOPERATIVE BY SEATS 8A & 9A. REMOVED LIGHT STRIP, AND FOUND THE CONNECTOR PIN WAS NOT CONNECTED. CONNECTED THE PIN AND SECURED LIGHT.SDR ASOA2018052385133Controller · faultyWHEN PASSING FROM 9000 FT DURING DESCENT, CABIN RATE WENT TO -1800 AND CABIN DELTA P WENT TO ZERO. MX FOUND THE GROUND CONNECTION VALVE STUCK OPEN AND GROUND CONNECTOR VALVE DUCT BLOWN. SECURED THE DUCT, ADJUSTED VALVE AND REMOVED AND REPLACED THE AUTO PRESSDR SIMA2018052118004Sign · inoperativeEMERGENCY EXIT SIGN ON THE AFT GALLEY WALL WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-14-000-801-A, AND 33-50-14-400-801-A. OPS CHECKED GOOD.SDR SIMA2018052118002Inverter · inoperativeFLOOR EMERGENCY LIGHT STRIPS AT ROWS 8 - 9 AND ROWS 10 - 11, AND RT AND LT OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED THE INVERTER ASSY NR 5 IAW MM 33-50-11. OPS CHECKED GOOD .SDR SIMA2018052118001Flashlight · inoperativeFWD FA FLASHLIGHT INOPERATIVE. R & R THE FWD FA FLASHLIGHT, OPS CHECKED GOOD IAW AMM 33-50-16.SDR SIMA2018052117002Coupler · failedDURING CLIMB OUT, A BLEED 1 VALVE FAIL AND PACK 1 VALVE FAIL ILLUMINATED ON EICAS. FOUND A BLOWN COUPLING ON THE NR 1 A/C PACK NEXT TO THE DUAL TEMP CONTROL VALVE. R & R THE COUPLING, OPS AND LEAK CHECKED GOOD IAW AMM 21-60-01, AND 21-50-00.SDR HNAA2018052100003Unknown · odorA BURNING MATCH ODOR IN THE COCKPIT AND AT ROWS 4 - 6 FOR APPROXIMATELY 1 MINUTE DURING DESCENT, AROUND 20K FT. NOTHING ABNORMAL NOTED. CONDITION DID NOT RETURN REST OF FLIGHT. DROPPED PSU PANELS AT ROWS 4 - 6, INSPECTED AREA AND FOUND NO DISCREPANCIES. OKSDR HNAA2018052100002Unknown · smokeDURING START, AND TAXI, CREW SAW PUFFS OF WHITE SMOKE. INSPECTED THE NOSE E/E BAY, NO OBVIOUS DEFECTS NOTED. INSPECTED THE NOSE HYD SERVICE AREA, NO OBVIOUS DEFECTS NOTED. CREW GROUND RAN THE ACFT FOR 5 MINS NO EVIDENCE OF WHITE SMOKE. OK FOR SERVICE.SDR SIMA201805176003Computer · malfunctionedSPS ADVANCE CAUTION ON EICAS AFTER ROTATION RAN QRH PROCEDURE AND RETURN TO DEPARTURE. REMOVED AND REPLACED THE STALL PROTECTION COMPUTER, OPS CHECKED GOOD IAW AMM 27-36-02 & W/C 27-700-20.SDR ASOA201805167082Skin · damagedDURING A C CHECK, FOUND THE RUDDER 2 LOWER LT SIDE WITH A HOLE IN THE SKIN AND A DESCENDING CRACK EXTENDING APPROXIMATELY 1.5 INCHES FROM THE HOLE. REPAIRED IAW ETD2018-145-048501.SDR ASOA201805167081Skin · crackedDURING A C CHECK, FOUND THE LT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 1L TO 2L, VERIFIED BY SOP 5711, NDT. REPAIRED IAW SRM 53-31-01.SDR ASOA201805167080Skin · crackedDURING A C CHECK INSPECTION, FOUND THE RT FUSELAGE SKIN AT FRAME 75, STRINGER 1R CRACKED. VERIFIED WITH NDT.SOP 5711. REPAIRED THE SKIN IAW SRM 53-31-01.SDR ASOA201805057084Window Post · crackedCRACK ON LT LATERAL POST WINDSHIELD POST. INSTALLED REPAIR TO LT LATERAL POST FOR COCKPIT WINDSHIELD IAW EC/TC SB145-53-0079R1.SDR HNAA2018052100097Warning System · false activationBLEED 2 VALVE FAIL MSG IN FLIGHT WITH ICING CONDITIONS. CREW RAN QRH. GROUND RAN AC AND PERFORMED OPS CHECK OF BLEED VALVES IAW AMM 36-11-05. OPERATIONAL CHECK GOOD. OK FOR SERVICE.SDR SIMA201805165003Bulb · inoperativeRIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD IAW AMM 33-50-00.SDR ASOA20805057083Frame · crackedCOCKPIT FRAME IS CRACKED BETWEEN FRAME 13, STRINGER 8L-10L. CUTOUT DAMAGED SECTION AND INSTALLED REPAIR DOUBLER TO FRAME 13 STRINGER 8L AND 10L PER SRM 53-00-04.SDR HNAA20180521001Light · inoperativeFLOOR EMERGENCY LIGHT INOPERATIVE BY THE EMERGENCY EXIT DOOR. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.SDR SIMA201805154001Unknown · odorODOR OF SMOKE IN THE COCKPIT. COMPLIED WITH A THREE MINUTE HIGH POWER RUN IAW MM 72-00-00. NO ODOR NOTED. FCF FOUND SATISFACTORYSDR SIMA201805140002Handle · unsecureMAIN ENTRY DOOR UNABLE TO OPEN WITH DOOR HANDLE, DOOR HANDLE NOT SECURE. SECURED THE DOOR HANDLE IAW AMM 52-10-01, OPS CHECKED GOOD, NO DEFECT NOTED.SDR SIMA201805143001Light · inoperativeRIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED GOOD IAW AMM 33-50-00.SDR HNAA2018052500114Unknown · odorDURING CRUISE, CREW BEGAN TO SMELL AN UNUSUAL ODOR ACCOMPANIED BY RADIO STATIC. ODOR AND STATIC DISAPPEARED AFTER LEAVING PRECIP. FA DID NOT NOTE THE ODOR IN THE CABIN. PERFORMED ENGINE RUN, CAN NOT DUPLICATE ODOR IN THE FLIGHT DECK. AIRCRAFT OKAY FOR SERVICSDR SIMA201805142004Roller · lack of lubeMAIN CABIN DOOR HARD TO OPEN. LUBRICATED THE PAX DOOR ROLLERS IAW AMM 52-11-00, PERFORMED A DOOR ACTUATING HANDLE TEST IAW AMM 52-18-00, EM-52-029. OPS CHECKED GOOD. THE DOOR OPENS AT 35 LBS.SDR SIMA2018051400005Lamp · inoperativeOVERWING EMERGENCY LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. R & R THE OVERWING EMERGENCY LIGHT LAMP IAW 33-50-07-000-801-A, AND 33-50-07-400-801-A. OPS CHECKED GOOD.SDR SIMA2018051400002Flashlight · odorODOR OF SMOKE IN THE COCKPIT. PERFORMED AN ENGINE RUN IAW MM 72-00-00, AND APU RUNS. FOUND THE ODOR COMING FROM FIRST OFFICER`S SIDE FLASHLIGHT. REMOVED AND REPLACED THE FLASHLIGHT. NO ODOR NOTEDSDR ASOA201805114029Hinge Fitting · failedTHE CREW REPORTED A LOW FREQUENCY VIBRATION THROUGH THE AIRFRAME. THE AIRCRAFT LANDED AT JAN WITHOUT INCIDENT. MX INSPECTED THE AIRCRAFT AND FOUND THAT ALL OF THE RUDDER TWO HINGE FITTINGS TO BE DAMAGED WITH THE UPPER FITTING TO BE SHEARED. REMOVED AND REPLSDR SIMA2018051400003Smoke Detector · failedDURING A FIRE DETECTOR TEST, THE CARGO SMOKE FAIL. REMOVED AND REPLACED CARGO BAY FWD SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECKED GOOD IAW AMM 26-15-00.SDR HNAA2018052500113Unknown · odorACRID SMOKE ODOR IN THE FLIGHT DECK AND FORWARD CABIN. NO VISUAL SIGNS OF SMOKE. VISUALLY INSPECTED AVIONICS NOSE BAY AND AROUND WINDSHIELDS, FOUND NO EVIDENCE OF BURNING. DURING GROUND RUN FOR RADAR, NO EVIDENCE OF SMOKE. OK FOR SERVICE.SDR SIMA2018052309006Trunnion · crackedLEFT WING MLG AFT UPPER TRUNION WAS CRACKED AT THE OUTBOARD LOWER RADIUS. COMPLIED WITH ERS-EM-57MR-965.SDR SIMA2018051409002Unknown · odorCLIMBING THROUGH 10,000 FT, A STRONG ODOR OF SMOKE IN THE CABIN AND COCKPIT. RETURNED TO DEPARTURE. AFTER LANDING THE NR 1 PACK OVERHEAT EICAS MESSAGE PRESENTED. REMOVED AND REPLACED THE NR 1 ACM IAW AMM 21-51-03. OPS AND LEAK CHECKED GOOD. COMPLIED WITH SDR SIMA2018051409004Battery Pack · failedFLOOR EMERGENCY LIGHT, WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD.SDR SIMA2018061158006Rib · crackedCRACKED, LEFT RIB 5, OTBD OF MLG. REPLACED THE LT WING RIB IAW EO EM-57MR-594.SDR ASOA2018F00002Light · inoperativeRIC FLIGHT 5529 DURING SCHEDULED MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN AT ROW 15 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN BULB WITH OPERATIONAL CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR HNAA2018052500109Actuator · leakingDURING FLIGHT, NOTICED A RAPID DEPETION OF THE NR 1 HYD SYSTEM QUANTITY WITH AN EICAS MESSAGE. R & R GROUND SPOILER ACTUATOR IAW AMM 27-62-01-400-801-A. REPLENISHED TH EHYDRAULIC SYSTEM.SDR HNAA2018052500108Inverter · inoperativeEMREGENCY EXIT SIGN ABOVE THE SERVICE DOOR DID NOT ILLUMINATE. R & R THE INVERTER IAW AMM 33-50-11. OPS CHECKED GOODSDR HNAA2018052500107Bleed Valve · failedNR 2 BLEED VALVE FAILED EICAS MESSAGE DISPLAYED DURING TAKEOFF ROLL AFTER POWER LEVELS WERE ADVANCED. ABORTED THE TAKEOFF.SDR HNAA2018052500106Fan · failedBOTH BLEEDS OVERTEMP WARNINGS AT 16K, AFTER ICE PROTECTION HAD BEEN ON FOR 5 MINUTES. APU WAS NOT ON. REMOVED AND REPLACED THE NR 1 & 2 THERMOSTAT FAN A/C AND THERMOSTAT MOUNT TUB ASSY IAW SB 145-36-0028.SDR HNAA2018052500105Bleed Valve · malfunctionedNR 1 BLEED VALVE FAILED EICAS MESSAGE DURING TAKE OFF. REJECTED THE TAKE OFF. R & R THE NR 1 BLEED VALVE IAW AMM MPP 36-11-05-04. OPS CHECKED GOOD.SDR HNAA2018052500104Warning Message · false activationDURING TAKEOFF ROLL, THE SPOILERS DEPLOYED AND THE NR 1 BLEED VALVE FAILED EICAS MESSAGES DISPLAYED. INSPECTED AND DETERMINED THE SPOILER DEPLOYMENT TO BE CONSISTENT WITH NORMAL GROUND SPOILER AUTO-DEPLOY SEQUENCE. ACFT OVER 30KTS AND TL RETARDED FOR REJECTSDR HNAA2018052500102Lock Screw · looseNR 1 BLEED VALVE FAILED ON TAKEOFF ROLL. ABORTED THE TAKEOFF. INSPECTED THE NR 1 ENGINE BLEED VALVE AND FOUND THE LOCK SCREW TO BE LOOSE. TIGHTENED THE LOCK SCREW. PERFORMED AN ENGINE BLEED VALVE FUNCTIONAL OPS CHECK IAW AMM 36-11-05. CHECKED GOOD. OK FORSDR HNAA2018052500103Distribution Box · hotDURING A HIGH POWER RUN, THE ODOR OF SOMETHING BURNING IN THE COCKPIT. LEFT DISTRIBUTION BOX HOT TO THE TOUCH. RAN UP AIRCRAFT AT HIGH POWER AND INSPECTED THE LT AND RT RELAY SUPPORT PANELS AND DISTRIBUTION BOXES. PERFORMED A VISUAL INSPECTION OF AREAS. NO DSDR HNAA20180525002Screw · looseNR 1 BLEED VALVE FAILED ON TAKEOFF ROLL. ABORTED TAKE OFF. INSPECTED THE NR 1 ENGINE BLEED VALVE AND FOUND THE LOCK SCREW TO BE LOOSE. TIGHTENED THE LOCK SCREW. PERFORMED AN ENGINE BLEED VALVE FUNCTIONAL, OPS CHECKED IAW AMM 36-11-05. FUNCTIONAL/OPS CHECKSDR 2018FA0000244Inverter · inoperativeDURING SCHEDULED MX INSPECTION, THE EMERGENCY EXIT SIGN AT SEAT 18D WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN INVERTER, OPS CHECKED GOOD.SDR HNAA2018052500100Indicator · false indicationDURING TAXI OUT, THE NR 1 FUEL TANK LEVEL FLUCTUATED FROM 42 - 4600 LBS. AFTER DEPARTURE THE NR 2 TANK CONTENTS AND TOTAL FOB INDICATIONS ON MFD AND EICAS SHOWED DASHES AND FUEL 1 LOW LEVEL EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH PROCEDURES. R & R THE RSDR SIMA2018051402008Rib · crackedRIB ABOVE CAPTAINS WINDSHIELD HAS A 1/4 INCH CRACK AROUND THE NUTPLATE HOLE. REPAIRED THE RIB IAW SRM-53-12-16.SDR SIMA2018051601013Support Bracket · crackedLEFT OVERWING ROOT FAIRING L BRACKET SUPPORT ON UPPER WING SURFACE IS CRACKED. REPAIRED IAW ETN-EM-53-142.SDR SIMA2018051501001Pneumatic System · leakingBLEED 1 LEAK DURING DEPARTURE, RAN QRH, MESSAGE DID NOT EXTINGUISH AND RETURNED TO DEPARTURE. EMERGENCY DECLARED. PERFORMED OPC OF E1 BLEED AIR SYSTEM AS PER EMB145 AMM 36-00-00. OPS CHECKED GOOD. PERFORMED LEAKAGE TEST OF LT AIR BLEED SYSTEM DUCTS IAW AMM 3SDR SIMA2018051401012Bulkhead · crackedLT MLG WHEEL WELL AT THE AFT BULKHEAD WALL HAS TWO CRACKS. INSTALLED THE BULKHEAD IAW SRM 51-40-02.SDR SIMA2018051401009Support Bracket · crackedLEFT OVERWING ROOT FAIRING SUPPORT BRACKET ON THE UPPER SURFACE WAS FOUND CRACKED, JUST INBD OF THE GROUND SPOILER. REPAIRED THE SUPPORT BRACKET IAW ETN-EM-53-142
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