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 SIMA20140831004Skin Panel · dentedHAIL DAMAGE EVENT REPLACE FWD FUSELAGE 1 RT SKIN PANEL. R & R IAW SRM 51-40-02, ETN-EM-53-206 & ETN-EM-53-262.SDR SIMA20140831003Tee Fitting · crackedBLEED 1 LEAK INFLIGHT. TRANSFERRED TO NRWC 603-DFW-01980. SEE NRWC 603-DFW-01980 FOR WORK PERFORMED. REPLACED TEE DUCT ASSEMBLY IN CARGO, NO LEAKS NOTED. INSPECTED & FOUND TEE FITTING IN CARGO ON LT UPPER BLEED DUCTS CRACKED. REMOVED TEE FITTING IAW AMM 3SDR ASOA20140831075Fire Loop · failedTHE CREW REPORTED NR 1 ENGINE FIRE DETECTOR FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE PYLON FIRE LOOP. OPS CHECKED GOOD.SDR SIMA20140831001Unknown · malfunctionedAD 2 AIRSPEED & ALT WAS OFF DUE TO WATER OR ICE ON THE STATIC PORTS. CLEARED ON DESCENT. INSPECTED PITOT DRAIN HOSE FOR WATER IAW AMM 34-13-00 & PERFORMED OPERATIONS CHECK OF ADC 2. ADC 2 CHECKS NORMAL IAW AMM 34-15-00.SDR SIMA20140830011Skin · gougedPASSENGER DOOR SKIN GOUGED AFT LOWER EDGE. REPAIRED IAW ERS-EM-5200-203. SEE WIP & TASK ENTRIES FOR DETAILS.SDR SIMA20140830010Gusset · corrodedLAVATORY RT BEAM GUSSET HAS CORROSION SPOTS. COMPLIED WITH ERS-EM-5300-713 LAVATORY RT CORROSION REPAIR.SDR SIMA20140830012Support Bracket · crackedFORWARD CARGO DOOR LIFTING MECHANISM SUPPORT BRACKET IS CRACKED. R & R FWD CARGO DOOR LIFTING LOWERING MECHANISM SUPPORT BRACKET IAW SRM 51-40-02 & IAW INFORMATION CONTAINED IN EO-GN-5100-003 R6 & ETN -EM-51-091 R3 SEE TURNOVER FOR DETAILS.SDR SIMA20140830009Profile · crackedPERFORM PERMANENT REPAIR ON 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART C. REMOVED DAMAGED LT WW PROFILE & INSTALLED SERVICEABLE PROFILE AT LT AFT WING STUB IAW ERS ERS-EM-57DF-082 PART C.SDR SIMA20140830008Structure · crackedFORWARD AVIONICS BAY FLOOR CRACKED AT RT END OF NLG UPLOCK BOX AFT CROSS MEMBER. REPAIRED FWD AVIONICS BAY FLOOR AT RT END OF NLG UPLOCK BOX AFT CROSS MEMBER IAW ERS-EM-5300-718.SDR SIMA20140830007Gusset · corrodedLAVATORY CTR BEAM GUSSET HAS CORROSION. COMPLIED WITH ERS-EM-5300-713 LT CTR BEAM GUSSET CORROSION REPAIR.SDR SIMA20140830006Skin · crackedLEFT UPPER FUSELAGE SKIN HAS SMALL CRACK JUST AFT OF FRAME 75 & ABOVE STRINGER 2L APPROX 3/8 INCH IN LENGTH. EASI 6581 USED. FREQ=400, LPF =100, V GAIN=74, H GAIN=63. REPAIRED IAW ERS-EM-53MR-727. SEE WIP & TASK ENTRIES FOR DETAILS.SDR SIMA20140830005Check Valve · failedEMERGENCY LINE CHECK VLV OF THE EMER PARKING BRAKE SYS FAILS OPERATIONS CHECK. R & R EMER LINE CHECK VLV OF THE EMER PARKING BRAKE SYS IAW AMM 32-44-08. LEAK CHECKED GOOD. TORQUE WRENCH 4484.SDR SIMA20140830003Support · crackedRIGHT HAT BEAM SUPPORT CRACKED OVER THE WING BOX BETWEEN FRAME 47 & 48. R & R RT HAT BEAM SUPPORT OVER THE WING BOX IAW SRM 53-23-02.SDR SIMA20140830004Structure · crackedPERFORM REPETITIVE INSPECTION ON 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART B. ACCOMPLISHED PERMANENT REPAIR OF 3 1/2 INCH CRACK IN LT AFT WING STUB IAW ERS-EM-57DF-082 PART C. REFER TO NRTC E403463 FOR DETAILS. TDMI 928T5714 RESTORED. RSDR SIMA20140830002Skin · damagedRIGHT LOWER OTBD ELEVATOR WING TIP SKIN HAS ELONGATED HOLES. PERFORMED REPAIR ON RT ELEVATOR LOWER OTBD WING TIP SKIN IAW ERS-EM-55MR-161.SDR RAIA201408300002Bleed Valve · failedNR 2 BLEED VALVE FAILED DURING CLIMB AND RETURNED TO BLOCK. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE HIGH STAGE VALVE, OPS CHECKED GOOD.SDR RAIA201408300001Bulb · inoperativeRIGHT EMERGENCY DOOR EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED BULB, OPS CHECKED GOOD.SDR ASOA20140830267Bracket · wornDURING C-CHECK, THE RT AILERON PCA BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140830266Attach Bracket · wornDURING C-CHECK, THE TOP RUDDER ATTACH BRACKET ON THE VERTICAL STABILIZER WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20140829255Floor Support · corrodedDURING INSPECTION THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 59 & 60. THE BEAM WAS REPLACED IAW ETD 2014-145-073053.SDR CHQA20140829253Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM AT FRAME 20. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.SDR SIMA20140829001Solenoid Valve · failedLANDING GEAR DISAGREE ON CLIMB OUT. AOM PROCEDURES FOLLOWED. TRANSFERRED TO NRWC 630-DFW-01943. R & R LG SOLENOID VLV IAW AMM 32-33-04. OPERATIONS CHECKS & LEAK CHECKS GOOD.SDR SIMA20140829002Unknown · malfunctionedRUDDER SYS 1 - 2 FAIL INFLIGHT. FOLLOWED FIM PROCEDURES. PERFORMED OPERATIONAL CHECK OF RUDDER SYS IAW AMM 27-25-00 NO FAULTS FOUND. COULD NOT DUPLICATE.SDR SIMA20140828007Attach Bracket · crackedRIGHT WING TO FUSELAGE PANEL LOWER ATTACH BRACKET AT FRAME 46 IS CRACKED. CRACK APPROX 1 INCH LONG. REMOVED & INSTALLED NEW RT WING TO FUSELAGE PANEL LOWER ATTACH BRACKET AT FRAME 46 IAW SRM 51-40-02 & ETN-EM-53-142 & APPLIED ANTI-MICROBIAL COATING IAW AMM 2SDR SIMA20140828006Plate · corrodedSERVICE DOOR SILL PLATE IS CORRODED. R & R SERVICE DOOR SILL PLATED IAW SRM 51-40-02.SDR SIMA20140828005Floor Support · crackedRIGHT OTBD OMEGA BEAM SUPPORT CRACKED BETWEEN FRAME 47 - 48. R & R RT OMEGA BEAM & SUPPORT IAW SRM 53-23-02 & 51-40-0. SHEAR CLIP PN 140-04213-609.SDR CHQA20140828252Skin · chafedDURING INSPECTION THE CARGO DOOR INNER SKIN WAS FOUND TO HAVE CHAFE MARKS ON THE LOWER AFT END. THE SKIN WAS REPLACED IAW SRM 51-40-02.SDR SIMA20140828004Yoke · crackedDURING MBV INSPECTION, QA FOUND LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE CRACKED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION & WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. R & R LT PYLON LOWER FWD ENG MOUNT SUPPORT YOKE IAW EO EM-54MR-386. ACFT SDR RAIA201408280001Bulb · inoperativeLEFT EMERGENCY DOOR EXIT LIGHT INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED BULB, OPS CHECK GOOD.SDR SIMA20140828003Inverter · inoperativeEMERGENCY LIGHTING FLOOR STRIPS 2 & 3 WILL NOT ILLUMINATE. R & R NR 3 INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD.SDR SIMA20140828001Spar · crackedLEFT WING SPAR 3 CRACKED AT MLG PROXIMITY HARNESS ROUTING HOLE. ACCOMPLISHED LT WING SPAR III PERMANENT REPAIR IAW ERS-EM-57MR-222.SDR SIMA20140828002Spar · crackedRIGHT WING SPAR 3 CRACKED AT MLG PROXIMITY HARNESS ROUTING HOLE. ACCOMPLISHED RT WING SPAR III PERMANENT REPAIR IAW ERS-EM-57MR-219.SDR ASOA20140828265Beam · 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 ASOA20140828264Floor Support · corrodedDURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-60. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01969. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20140827254Firewall · crackedDURING INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED UNDER THE UPPER LT SUPPORT ROD. THE APU FIREWALL WAS REPAIRED IAW SRM 53-32-13.SDR ASOA20140827073Deflector · misinstalledDURING ROUTINE MAINTENANCE, THE RT OVERWING EMERGENCY EXIT WOULD NOT OPEN. CATHES ON SIDEWALL DEFLECTOR. FURTHER INSPECTION FOUND THE SIDE WALL DEFLECTOR WAS INSTALLED IN THE WRONG LOCATION. MAINTENANCE REPOSITIONED THE SIDE WALL DEFLECTOR AND OPS CHECKS WERSDR SIMA20140827004Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2L. PERFORMED PERMANENT REPAIR OF LT FUSELAGE SKIN IAW ERS-EM-53MR-700.SDR SIMA20140827003Uplock · failedDURING TAKEOFF, ON GEAR RETRACTION A LOUD NOISE STARTED FROM THE FRONT OF THE ACFT. FEW SECONDS LATER ON EICAS GEAR INDICATION OF THE RT MAIN GEAR CYCLED BETWEEN UP INDICATION & TRANSIT INDICATION CONTINUOUSLY. CAUTION MSG DAU 1 WARN MISCOMP APPEARED ON EICASDR SIMA20140827002Roller · lack of lubeFLIGHT ATTENDANT REPORTS THAT MAIN DOOR IS HARD TO OPEN. CLEANED & LUBRICATED MAIN DOOR ROLLERS IAW AMM 53-21-02. ALSO PERFORMED PULL TEST OF DOOR HANDLE IAW AMM 52-18-00-820-801-A & DYNAMETER READING IS 43 LBS. NO FURTHER ACTION REQUIRED.SDR SIMA20140826010Skin · damagedHAIL DAMAGE EVENT REPLACE CTR FUSELAGE IV TOP SKIN. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 51-40-02, 51-20-01, ETN EM-53-265 & ETN-EM-51-118.SDR CHQA20140826256Doubler · corrodedDURING INSPECTION THE LT OMEGA BEAM REPAIR DOUBLER ON THE INBD SIDE WAS FOUND TO BE CORRODED AT FRAME 20. THE REPAIR DOUBLER WAS REPLACED IAW SRM 53-00-10.SDR CHQA20140826250Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE CTR OMEGA BEAM SEAT TRACK FROM FRAME 25 - 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.SDR CHQA20140826249Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON THE LT OMEGA BEAM SEAT TRACK FROM FRAME 25 THROUGH FRAME 30. THE SEAT TRACK WAS REPLACED IAW AMM 53-01-06.SDR SIMA20140826009Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-701.SDR SIMA20140826006Acm · failedCLIMBING THROUGH FL 190 SMOKE & FUMES IN THE CABIN & COCKPIT. LOUD NOISE HEARD AROUND ROW 10 & 11 ON LT SIDE OF ACFT. WHEN ISOLATING THE PROBLEM SMOKE & FUMES SEEMED TO GO AWAY WHEN DESELECTING PACK 1. NUMBER 1 PACK VERIFIED INOPERATIVE & DEFERRED IAW MEL 2SDR SIMA20140826008Inverter · inoperativeEXIT LAMP 1A INOPERATIVE. R & R NR 1 EMER LIGHT INVERTER IAW AMM 33-50-11. OPERATIONS CHECKED GOOD IAW WC 33-700-17.SDR SIMA20140826004Wire · brokenNUMBER 1 EMER LIGHT STRIP HAS BROKEN WIRE. R & R NR 1 EMER LIGHT STRIP IAW AMM 33-50-12.SDR SIMA20140826001Skin · crackedRIGHT FUSELAGE SKIN CRACKED AFT OF FRAME 75 ABOVE STRINGER 2R. CRACK APPROX LENGTH 9/16 INCHES. PERFORMED REPAIR TO RT FUSELAGE SKIN AFT FRAME 75 & STRINGER 2R IAW ERS-EM-53MR-697.SDR SIMA20140826003Skin · crackedLEFT FUSELAGE SKIN CRACKED AFT OF FRAME 75, ABOVE STRINGER 2L. CRACK APPROX LENGTH 3/8 INCHES. PERFORMED REPAIR AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-698.SDR ASOA20140826072Light · inoperativeDURING ROUTINE MAINTENANCE THE AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. 2ND MOST AFT. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD.
Back to Embraer EMB-145LR