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 HNAA2018061900123Pressure Switch · malfunctionedTAKE OFF CONFIG WARNING ON ROLL OUT. NO AURAL WARNINGS. NO OTHER EICAS OR CMC MESSAGE. TROUBLESHOT THE TAKE OFF CONFIGURATION WARNING DISCREPANCY. R & R THE AWU IAW 31-51-01-000-801A AND R & R THE EMERGENCY PARK BRAKE PRESSURE SWITCH IAW 32-44-07-00-801A.SDR HNAA2018061900122Relay · failedT/O CONFIG WARNING, ABORT T/O. R&R RELAY K0212 IAW 21-51-00-810-804-1.SDR ASOA2018062716338Skin · crackedDURING A -C- CHECK, FOUND A CRACK ON THE SKIN AT FRAME 75, STRINGER 2R. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-31-01.SDR SIMA201806186002Seal · tornFLIGHT ATTENDENT REPORTED A WHISTLING SOUND COMING FROM THE MAIN CABIN DOOR DURING THE DECENT. FOUND TWO TEARS IN THE AIRFRAME SEAL. REPAIRED IAW AMM 53-21-01, PRESSURIZED TO 4.5, NO NOISE OR SQUEAL NOTED. OPS CHECKED GOOD.SDR ASOA201807133045Fitting · crackedDURING C CHECK INSPECTION FOUND SHEAR CLIP ON LEFT SIDE OF FRAME 80 HAS .900" CRACK AT THE RADIUS. MAINTENANCE REPLACED THE SHEAR CLIP AT FRAME 80, STR 5L-6L.SDR ASOA2018062541033Battery Pack · dischargedDURING MAINTENANCE INSPECTION, AN EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA2018061850001Bulb · inoperativePAX DOOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-10. OPS CHECKED GOOD.SDR SIMA201806185004Flashlight · inoperativeFA FLASHLIGHT INOPERATIVE. R & R THE FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.SDR SIMA201806185002Flashlight · inoperativeTHE FORWARD FA FLASHLIGHT WAS INOPERATIVE. INSTALLED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.SDR SIMA201806185005Roller · lack of lubeMAIN DOOR HARD TO OPEN & CLOSE. CLEANED AND LUBRICATED MAIN DOOR FRAME ROLLERS IAW AMM 52-18-00, OPS CHECKED GOOD.SDR ASOA201807133041Beam · corrodedDURING C CHECK CARGO DOOR LOWER FRAME (BEAM) WAS FOUND HEAVELY CORRODED. MAINTENANCE REPLACED THE CARGO DOOR LOWER FRAME (BEAM) IAW SRM 51-40-02.SDR SIMA20180614002Light · inoperativeRT EXTERNAL OVERWING EMERGENCY LIGHT WILL NOT ILLUMINATE. R&R RT EXTERNAL OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-10 OPS CK GOOD.SDR ASOA2018061544032Acm · inoperativeTHE CREW REPORTED THAT ON ARRIVAL, THEY COULD SEE AND SMELL SMOKE IN THE COCKPIT, WITH A LOUD NOISE FROM THE BELLY. LANDED WITHOUT INCIDENT. INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ACM, OPS TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVESDR ASOA201807133040Skin · wornDURING C CHECK INSPECTION FOUND INNER SKIN OF THE MAIN DOOR AT COCKPIT PARTION UPPER HOLE WORN. MAINTENANCE REPAIRED IAW SRM 53-21-02.SDR HNAA2018070600140Crossbeam · corrodedGALLEY CROSSBEAM AT FRAME 20 CORRODED. INSTALLED 3 NUTPLATES ON GALLEY CROSSBEAM AT FRAME 20 IAW SRM 51-40-09.SDR HNAA2018070600139Fitting · corrodedTWO LT APU FIRE WALL SHEER CLIPS INSIDE 312AR HAVE SURFACE CORROSION. REMOVED AND REPLACED TWO APU FIRE WALL SHEER CLIPS INSIDE 312AR IAW SRM 51-40-02.SDR SIMA20180612006Floor Support · corrodedCENTER OMEGA BEAM BETWEEN FRAMES 58-59 IS CORRODED. COMPLETED REPAIR TO CENTER OMEGA BEAM BETWEEN FRAMES 58-59 IAW EO-EM-53MR-1518 R3 PART B.SDR SIMA20180612005Skin · canningRT CENTRAL FUSELAGE I LOWER SKIN DENTS PERMANENT REPAIR ERS-EM-53DF-2832 PTC. ERS-EM-53DF-2832 WAS NO LONGER REQUIRED DUE TO OIL CANNING. ACCOMPLISHED PERMANENT REPAIR IAW ERS-EM-53MR-3304.SDR SIMA201806132003Unknown · unknownAFTER TAKEOFF, A LOUD BANGING SOUND WAS HEARD AND FELT ON THE LEFT FORWARD SIDE OF THE NOSE. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. NORMAL LANDING. INSPECTED IAW 51-10-02, NO AREAS OF DAMAGE FOUND, THE DOOR OPERATED NORMAL.SDR SIMA201806132002Shear Tie · crackedSHEAR TIE AT FRAME 65 BETWEEN STRINGERS 18L AND 19L WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.SDR SIMA20180612001Flashlight · inoperativeAFT FA FLASHLIGHT INOP. REMOVED AND REPLACED AFT FA FLASHLIGHT IAW AMM 25-60-11. OPS CHECK GOOD.SDR SIMA20180611008Doubler · damagedREPAIR PYLON DOUBLER AT FRAME 73 BETWEEN STRINGERS 8 L AND 9L. REMOVED PYLON DOUBLER AT FRAME 70 TO 74 IAW SRM 51-40-02 FABRICATED DOUBLER FROM 2024 T3 0.063 IAW ENGINEERING DRAWING 145-25898. LOCATED, DRILLED, ALODINED AND PRIMED DOUBLER IAW SRM 51-20-03, 51-SDR SIMA20180611009Display · failedPFD 2 SCREEN FAILED INTERMITTENTLY. SWAPPED MFD 2 TO PFD2. REMOVED AND REPLACED PFD2 IAW AMM 34-22-01. OPS CHECKED GOODSDR SIMA20180611005Unknown · odorFUMES IN COCKPIT & FORWARD CABIN SIMILAR TO DIRTY GYM BAG WITH HINT OF OIL NO EICAS INDICATIONS DURING DESCENT AND LEVEL OFF WHILE INCREASING POWER TO MAINTAIN SPEED GOT WORSE WITH INCREASE IN POWER BOTH PACKS POWERED BY THEIR RESPECTIVE BLEED NOTHING ASSOCIATSDR SIMA20180611004Skin · damagedPAX DOOR OUTER SKIN LOWER AFT EDGE WAS GOUGED AND CHAFED. REMOVED GOUGE AND CHAFE BY MEANS OF MECHANICAL BLENDING IAW SRM 51-10-03. DAMAGE WAS LESS THAN 4D MIN DISTANCE FROM RIVET LINE . PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDTM 51-00-00-916-801-A00SDR SIMA20180611003Floor Support · corrodedCORROSION UNDER GUSSET AT FRAME 20 AND RT OMEGA BEAM. REMOVED CORROSION UNDER THE GUSSET IAW SRM 51-10-03, FOUND TO BE OUT OF LIMITS PER SRM 53-21-10, SI FIG 10, ITEM 15. CUT OUT DAMAGED AREA IAW SRM 53-21-10. PERFORMED HFEC INSP OF CUT OUT IAW NDTM 51-00-SDR SIMA20180611002Rib · crackedCRACK IN THE LT RIB 5 OTB OF THE MLG. REPAIRED IAW EO EM-57MR-594, REV 1.SDR SIMA20180611001Skin · crackedCRACK APPROXIMATELY 0.25 LONG FOUND IN FUSELAGE SKIN BY HFEC, AT FRAME 75, APPROXIMATELY 1 INCH BELOW STRINGER 2L. CUT OUT THE CRACK IAW SRM 53-31-01, ITEM 11, FIG 219, SHEET 2. PERFORMED HFEC INSPECTION ALONG AREAS OF DAMAGE REMOVAL IAW NDTM 51-00-00-916-SDR HNAA2018070600138Structure · corrodedSERVICE DOOR LOWER FWD NUT PLATE HOLE CORROSION. PERFORMED HFEC INSPECTIONS AND UT THICKNESS IAW EASI NDTM NO CRACK NOTED. BLENDED SERVICE DOOR LOWER FWD NUT PLATE HOLE TO REMOVE CORROSION IAW SRM 51-10-03, BLENDED AREA ACCEPTED AS IS IAW EO1-52-18-0239 AND ETSDR HNAA2018070600137Door Frame · corrodedCARGO DOOR FWD UPPER TWO NUTPLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC INSPECTION AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLES, FILLERS AND SHIM ON 2 LOWER NUTPLATE HOLES ON CARGO DOOR FWD FRAME IAW SRM 52-30-04. REPAIREDSDR HNAA2018070600136Structure · corrodedCARGO DOOR FWD LOWER NUT PLATE HOLES HAVE SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM, NO DEFECTS NOTED. CARGO DOOR FWD LOWER NUT PLATE PROFILE IAW SRM 51-40-02.SDR HNAA2018070600133Structure · corrodedCARGO DOOR NUT PLATE HOLE HAS SURFACE CORROSION. PERFORMED HFEC AND UT THICKNESS IAW EASI NDTM NO DEFECTS NOTED. R&R CARGO DOOR UPPER SURFACE ANGLE PROFILE IAW SRM 51-40-02.SDR SIMA201806180002Skin · crackedRUDDER 2 RT TRAILING EDGE HAD PULLED RIVETS, AND FOUND TO BE CRACKED .196 FROM A RIVET TO THE TRAILING EDGE. REPAIRED THE RUDDER TRAILING EDGE IAW ERS-EM-55MR-680.SDR SIMA2018061110001Lamp · inoperativeSERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A. OPS CHECKED GOOD.SDR SIMA2018061109004Skin · crackedFIVE WORKING RIVETS AT FRAME 78 BETWEEN STRINGERS 5R AND 8R. REMOVED PAINT AT FIVE WORKING RIVETS IAW SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE BELOW STRINGER 6 FOUND TO BE CRACKED. REMOVED EXISTING RIVET ASDR SIMA2018061109001Skin · crackedTHE AFT UPPER SKIN HAD NUMEROUS CRACKS. REMOVED THE AFT UPPER SKIN IAW SRM 51-40-02. LOCATED, DRILLED, COUNTERSUNK, TRIMMED AND ALODINED THE NEW SKIN IAW SRM 51-20-03, 51-40-06, AND CPM 51-21-04. INSTALLED THE SKIN IAW SRM 51-40-02.SDR SIMA2018061109002Skin · crackedFOUR WORKING RIVETS AT FRAME 79 BETWEEN STRINGERS 4R TO 7R. REMOVED PAINT AT 4 EACH WORKING RIVETS IAW EMB 145 SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE ABOVE STRINGER 6 FOUND TO BE CRACKED. REMOVED EXISTING SDR SIMA2018061109003Skin · crackedFOUR WORKING RIVETS AT FRAME 79 BETWEEN STRINGERS 4R TO 7R. REMOVED PAINT AT 4 EACH WORKING RIVETS IAW SRM 51-10-05. PERFORMED FPI TO AFFECTED FASTENERS IAW NDTM INTRODUCTION SECTION D.FIRST HOLE ABOVE STRINGER 4 FOUND TO BE CRACKED. REMOVED EXISTING RIVET ANSDR SIMA2018061109005Bulb · inoperativeDURING A PS-1 CHECK, FOUND THE LT EMERGENCY LIGHT ABOVE THE WING INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-07. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.SDR SIMA2018061508012Stringer · chafedSTRINGER 2L WAS CHAFED BETWEEN FRAMES 20 AND 21. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-3312.SDR SIMA2018061508011Bracket · corrodedTOILET WASTE VALVE SUPPORT HAD MINOR CORROSION BENEATH LANYARD FOR FILL CAP. REMOVED AND REPLACED THE TOILET WASTE VALVE SUPPORT IAW SRM 51-40-02.SDR SIMA2018061508015Floor Support · crackedLEFT OMEGA BEAM SUPPORT WAS CRACKED ON THE AFT INBD SIDE AT FRAME 50. PERFORMED A REPAIR IAW SRM 53-23-02.SDR SIMA2018061508014Skin · scratchedPAX DOOR EXTERNAL SKIN HAD SEVERAL SCRATCHES ALONG THE TRAILING EGDE. INSTALLED A FILLER, DOUBLER AND EDGE SEALED THE REPAIR IAW SRM 52-10-01, FIG 204.SDR SIMA2018061508013Frame · corrodedFRAME 22 CORRODED AT PREVIOUS BLEND JUST BELOW THE SERVICE DOOR CUTOUT AFT LOWER DOOR STOP . ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-3311.SDR HNAA2018061200121Inverter · inoperativeEMERGENCY LIGHT WAS INOPERATIVE ABOVE THE GALLEY EXIT. R & R THE EMERGENCY LIGHT INVERTER.SDR HNAA2018061200120Bulb · inoperativeSERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.SDR HNAA2018061280120Bulb · inoperativeSERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE BULB.SDR SIMA2018061108009Starter Gen · failedON GROUND POWER, APU PNEUMATICS, PACK 2 ON, GROUND RAMPERS REPORTED SMOKE OUT OF APU STARTER OUTFLOW EXHAUST. SMELL OF SMOKE IN THE FLIGHT DECK-C/A-FLIGHT CREW PLACARDED APU GEN FUNCTION MEL 2408 AUTH 060363-D MOC 056048. DEFERRAL PER MEL 49-1 AUTH # 060368DMSDR ASOA2018060871051Housing · damagedRT AND LT SPHERICAL BEARING HOUSINGS HAVE DISPLACED METAL. REPAIRED LT AND RT SPHERICAL BEARING HOUSING IN ACCORDANCE WITH SRM 55-30-02.SDR ASOA201806087105Skin · crackedRT REAR FUSELAGE SKIN AT FRAME 75, STRINGER 2R-3R CRACKED. REPAIRED FUSELAGE SKIN IN ACCORDANCE WITH SRM 53-31-01.
Back to Embraer EMB-145LR