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 ASOA20120813111Inverter · inoperativeDURING MX INSPECTION, THE AISLE PATH LIGHTING FROM ROW 3 TO 7 WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA201208130001Proximity Switch · failedDURING CLIMBOUT OF KIAD, GEAR WENT FROM DOWN AND LOCKED TO UP AND LOCKED WITHOUT A TRANSIT INDICATION. CREW THEN RETURNED A/C TO KIAD FOR MAINTENANCE TO TROUBLESHOOT. MAINTENANCE INSPECTED AND FOUND THAT THE RIGHT MLG UPLOCK NR 2 PROX SWITCH BAD. REMOVED ANSDR ASOA20120813130Seat Track · corrodedDURING C-CHECK, FOUND THE RT WALL SEAT TRACK SUPPORT AT FRAME 50 CORRODED. MX BLENDED OUT THE CORROSION IAW SRM 51-10-03. FOUND AREA TO BE WITHIN LIMITS IAW 53-23-10. R & R ALL CORRODED FASTENERS IAW SRM 51-40-02. REMOVED ALL CORRODED NUTPLATES IAW SRM 51-SDR ASOA20120813129Bulb · burnedACFT RETURN TO THE GATE WHEN A BURNING ODOR IN THE CABIN WAS DETECTED. MX FOUND THE 2A LIGHT BURNED OUT. ACFT WAS THEN RELEASED TO SERVICE.SDR SIMA20120812004Control Unit · inoperativeFLT 4038, CREW REPORTED PITCH TRIM BACKUP INOPERATIVE MASTER WARNING AND EICAS MESSAGE PRESENTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU IAW AMM 27-40-01. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.SDR SIMA20120811001Flashlight Assy · malfunctionedFLIGHT 2830, FOUND REAR CABIN FLASHLIGHT CHARGING LIGHT NOT ILLUMINATED. THE AIRCRAFT WAS REMOVED FROM SERVICE.SDR SIMA20120810004Lamp · inoperativeDURING MAINTENANCE INSPECTION, FOUND MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.SDR SIMA20120810003Battery Pack · inoperativeDURING MAINTENANCE INSPECTION, FOUND CAPTAIN`S FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAINS FLASHLIGHT BATTERY IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.SDR SIMA20120810002Flashlight · inoperativeDURING MAINTENANCE INSPECTION, FOUND CAPTAIN`S FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACE CAPTAIN’S FLASHLIGHT. OPS CHECKED GOOD IAW AMM 33-50-16. AIRCRAFT RETURN TO SERVICE.SDR SIMA20120812002Lamp · inoperativeDURING MAINTENANCE INSPECTION FOUND EMERGENCY LIGHT OUT AT 12A PSU PANEL. THE AIRCRAFT WAS REMOVED FROM AND REMOVED AND REPLACED EMERGENCY LIGHT LAMP AS PER EMB AMM 33-50-00, OPS CHECKED GOOD. THE AIRCRAFT RETURN TO SERVICE.SDR SIMA20120813001Flashlight · inoperativeDURING MAINTENANCE INSPECTION, FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT ASSY, OPS CHECKED GOOD. THE AIRCRAFT RETURN TO SERVICE.SDR CHQA20120812260Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND BETWEEN THE MAIN PASSENGER DOOR NUT PLATES AND THE DOOR STRUCTURE. MAINTENANCE REPLACED THE LOWER CORNER PROFILE IN ACCORDANCE WITH SRM 51-40-02.SDR ASOA20120812109Battery Pack · dischargedDURING PREFLIGHT INSP THE CREW REPORTED TAHT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO IFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 EMERGENSDR ASOA20120812108Battery Pack · dischargedDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO OFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 SDR ASOA2012081402063Flashlight · inoperativeFLASHLIGHT BEHIND F/A'S SEAT ON/OFF SWITCH INOP. R & R FLASHLIGHT BY REMOVING FROM MOUNT CLIP AND INSTALL SERVICEABLE UNIT INTO MOUNT CLIPS. SDR CLOSED.SDR ASOA20120813128Lamp · inoperativeEMERGENCY DOME LIGHT AFT OF OVER-WING CEILING EXIT INOPERATIVE. REPLACED BULB OPS CHECK GOOD ACFT, RELEASED AND RETURNED TO SERVICE.SDR ASOA20120813127Skin · corrodedCORROSION OUT OF LIMITS ON INNER SKIN BAYS BETWEEN STR 20R & 21L & 22L AT FRM 13 & 14. CUTOUT CORRODED AREAS, FABRICATED 2 FILLERS AND ONE DOUBLER. ACFT STILL IN C CHECK.SDR SIMA20120809019Structure · crackedRT PYLON BOLT HOLE CRACKED. COMPLIED WITH PERMANENT REPAIR IAW EO EM-54MR-410, PART C.SDR SIMA20120809005Electronic Unit · inoperativeON FLIGHT 3556, THE CREW REPORTED THAT AFTER BECOMING AIRBORNE AFTER TAKEOFF THEY RECEIVED LG AIR/GND FAIL MESSAGE AND LANDING GEAR LEVER COULD NOT BE MOVED. AFTER 10 SEC LG AIR/FAIL MSG WENT OUT. FOLLOWED AOM PROCEDURES AND THE LANDING GEAR EXTENDED NORMALSDR CHQA20120809262Frame · corrodedDURING INSPECTION, A GOUGE WAS FOUND IN FRAME 60 BETWEEN STRINGERS 4L AND 5L. MAINTENANCE REPAIRED THE DAMAGED AREA IN ACCORDANCE WITH SRM 53-00-04, 51-20-03, 21-21-04, 51-21-05, AND 51-40-02.SDR CHQA20120809261Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND IN FRAME 22 AT THE LOWER SCREW HOLE FOR THE LINER. THE CORROSION WAS REMOVED IN PER SRM 51-10-03. THE REMAINING MATERIAL (0.068") IS ACCEPTED AS PERMANENT IN ACCORDANCE WITH ETD 2012-145-011370 REVISION A.SDR CHQA20120809259Shear Plate · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 67 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE FABRICATED A NEW SHEAR CLIP DOUBLER IN ACCORDANCE WITH SRM 53-31-04 AND INSTALLED THE NEW SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L AND 7L IN ACCORDANCESDR CHQA20120809258Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE SERVICE DOOR THRESHOLD AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.SDR CHQA20120809257Rib · crackedDURING INSPECTION, A CRACK WAS DETECTED IN THE RIGHT WING RIB INBOARD TORQUE BOX FORWARD CENTER FASTENER HOLE. MAINTENANCE REAMED THE HOLE SIZE TO 0.308" DIAMETERS IN ACCORDANCE WITH SRM 51-20-03, A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH WISDR CHQA20120809256Rib · crackedDURING INSPECTION, A CRACK WAS DETECTED IN THE LEFT WING RIB INBOARD TORQUE BOX FORWARD CENTER FASTENER HOLE. MAINTENANCE REAMED THE HOLE SIZE TO 0.261 DIAMETERS IN ACCORDANCE WITH SRM 51-20-03, A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CSDR ASOA20120809110Battery Pack · dischargedDURING MX INSPECTION, VARIOUS OVERWING EMERGENCY EXIT LIGHTS/SIGNS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR CHQA20120809244Tire · separatedCREW REPORTED THAT THE LEFT INBOARD TIRE SEPARATED ON TAKEOFF CAUSING DAMAGE TO THE LEFT FLAP. THE CREW DECLARED AN EMERGENCY ON LANDING AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON FURTHER INSPECTION, A DENT WAS FOUND ON THE LEFT FUSELAGE BETWEEN FSDR ASOA20120809106Control Panel · burnedTHE CREW REPORTED A BURNING ODOR IN FLIGHT AFTER THE F/O PRESSED THE F/O'S SIDE PA BUTTON WITH NO SMOKE NOTED. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, R & R THE F/O AUDIO CONTROL PANEL, AND THE F/A AFT HANDSET AND PA AMPLIFIER AS A PRECAUTIOSDR SIMA20120809008Door · lack of lubeFLIGHT 3552, THE MAIN DOOR WAS HARD TO OPEN AND CLOSE. AIRCRAFT REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR IAW AMM 52-19-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120809001Skin · dentedDURING MAINTENANCE INSPECTION, FOUND A DENT IN THE LEFT FORWARD FUSELAGE AT FRAME 2 AND STRINGER 15 LEFT. REPAIRED IAW EO EM 53MR-1686 PART C. AIRCRAFT RETURNED TO SERVICE.SDR RAIA201208080001Flashlight · inoperativeDURING MAINTENANCE INSPECTION, FOUND THE AFT BULKHEAD EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED THE FLASHLIGHT AND OPS CHECK GOOD.SDR SIMA20120808010Sill · corrodedDURING B INSPECTION, FOUND THE CARGO DOOR SILL CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL SRM 51-40-02. TOUCHED UP PAINT IAW CPM 51-21-05 AND 51-21-06. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20120808009Support · corrodedDURING B INSPECTION, FOUND THE CARBON CROSSBEAM LEFT SUPPORT GUSSETT CORRODED IN LAV AT FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CORRODED CARBON CROSSBEAM LEFT SUPPORT GUSSET IN LAV IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RSDR SIMA20120808008Floor Support · corrodedDURING B INSPECTION, FOUND THE LAV LEFT FLOOR SUPPORT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV LEFT FLOOR SUPPORT IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120808007Gusset · corrodedDURING B INSPECTION, FOUND THE GALLEY AFT DIAMOND GUSSET TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY AFT DIAMOND GUSSET IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120808006Floor Support · corrodedDURING B INSPECTION, FOUND THE CABIN RIGHT FLOOR SUPPORT CORRODED AT FRAME 40. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOOR SUPPORT AT FRAME 40 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR ASOA20120808105HAcm · seizedAFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE CABIN AND ELECTED TO RETURN TO DEPARTURE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, MX FOUND THE SOURCE OF THE SMOKE TO BE A SEIZED NR 1 AIR CYCLE MACHINE (ACM). MX REPLACED THE ACM, PERFORMED OSDR SIMA20120808002Lamp · inoperativeDURING MAINTENANCE INSPECTION, FOUND 12C OVERHEAD EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RELAMPED. NO FURTHER DEFECTS, FOUND OPS CHECKED GOOD. AIRCRAFT RETURN TO SERVICE.SDR CHQA20120807273Spar Cap · damagedDURING INSPECTION, THE RIGHT-HAND WING FRONT SPAR LOWER CAP HOLES FOR LEADING EDGE ARE ELONGATED FROM YA-2723.00 TO YA-3815.00.THE RIGHT-HAND WING FROM SPAR LOWER CAP HOLE FOR LEADING EDGE FROM YA-2723.00 TO YA-3815.00 WERE REPAIRED IN ACCORDANCE WITH ETD 2012SDR CHQA20120807272Floor Support · corrodedDURING INSPECTION, THE CENTER FUSELAGE IV FLOOR STRUCTURE RIGHT OMEGA BEAM WAS FOUND TO BE CRACKED AND CORRODED AROUND ANCHOR NUT BETWEEN FRAME 59 AND FRAME 60. THE RIGHT OMEGA BEAM ON THE CENTER FUSELAGE IV FLOOR STRUCTURE WAS REPLACED AND INSTALLED WITH A SSDR SIMA20120807003Flashlight · missingFLIGHT 4023, FLIGHT ATTENDANT FLASHLIGHT MISSING. INSTALLED NEW FLASHLIGHT. AIRCRAFT RETURN TO SERVICE.SDR SIMA20120806023Gusset · corrodedDURING B INSPECTION FOUND THE RIGHT FLOORBEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOORBEAM GUSSET BETWEEN FRAMES 59-61. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120806022Gusset · corrodedDURING B INSPECTION FOUND THE CENTER FLOORBEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER FLOORBEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120806021Gusset · corrodedDURING B INSPECTION FOUND THE LEFT FLOORBEAM GUSSET CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOORBEAM GUSSET BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120806020Strip · crackedDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP FORWARD RAMP PANEL EXTRUSION CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP FORWARD RAMP PANEL EXTRUSION IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WASDR SIMA20120806018Wire · brokenDURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 7 HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP NR 7 IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120806017Support Angle · crackedDURING B INSPECTION FOUND FRAME 66 T-PROFILE SUPPORT ANGLE IS CRACKED AT CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME 66 T-PROFILE SUPPORT ANGLE AT CARGO DOOR SILL IAW EMB SRM 51-40-02, CPM 51-21-05, CPM 51-21-06, AESDR SIMA20120806016Support Angle · crackedDURING B INSPECTION FOUND FRAME 67 T-PROFILE SUPPORT ANGLE CRACKED AT CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FRAME 67 T-PROFILE SUPPORT ANGLE AT CARGO DOOR SILL IAW EMB SRM 51-40-02,CPM 51-21-05, 51-21-06, AEA ETN-EMSDR SIMA20120806015Sill · corrodedDURING B INSPECTION FOUND THE LEFT FLOOR SILL CORRODED BETWEEN FRAMES 59-61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLOOR SILL BETWEEN FRAMES 59-61 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120806013Gusset · corrodedDURING B INSPECTION FOUND THE RIGHT CROSSMEMBER OUTBOARD GUSSET AT FRAME 23 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT CROSSMEMBER OUTBOARD GUSSET AT FRAME 23 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.
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