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 ASOA20130215082Shear Angle · corrodedDURING C-CHECK SHEAR CLIP AT FRM 65 CORRODED (LOCAL LEVEL 2) AT CARGO LOWER CUT OUT. MX R & R SHEAR CLIP AT FRM 65 CARGO LOWER CUTOUT IAW EMB-145, SRM 51-40-02 AND EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130215081Beam · corrodedDURING C-CHECK BAGGAGE DOOR MAIN BEAM CORRODED (LOCAL LEVEL 2) FRMS65-68. MX R & R BAGGAGE DOOR MAIN BEAM AT FRMS 65-68 IAW CPM 51-26-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130215080Bracket · corrodedDURING C-CHECK, NUTPLATE BRACKET CORRODED (LOCAL LEVEL 2) AT UPPER FWD CORNER BAGGAGE DOOR CUTOUT FRM 65. MX PERFORMED REPAIR AND REMOVED CORROSION ON BRACKET AROUND NUTPLATE HOLE AT FRM 65 UPPER FWD CORNER BAGGAGE DOOR CUTOUT AT FRM 65 IAW CPM 51-21-06 AND ESDR ASOA20130215079VSill · corrodedDURING C-CHECK, SERVICE DOOR CENTER SILL CORRODED. MX R & R SERVICE DOOR SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201302150101Wire Harness · faultyTHE CREW REPORTED A ELECTRICAL BURN ODOR COMING FROM SEAT 1A AREA. MX INSPECTED AND FOUND LIGHT SOCKET SHORTED OUT AT LOCATION SIDEWALL PANEL ABOVE SEAT 1A. THE POWER SUPPLY BALLAST WAS DISCONNECTED. THE LT SIDEWALL LIGHT HARNESS ASSY WAS REPLACED AT SEAT SDR SIMA20130215007Roller · out of adjustDURING MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND FWD UPPER MAIN DOOR ROLLER TO BE OUT OF ADJUSTMENT, ADJUSTED IAW AMM 52-18-00-820-805-A. PERFORMED LOAD TEST OF MAIN PASSENGER DOOR FOUND TO OPEN WITH 30LB OF FORCE, CHECKED GOODSDR ASOA20130215010Battery Pack · weakDURING MX INSPECTION, THE CAPTAINS FLASHLIGHT WAS FOUND TO BE DIM AND WOULD NOT TAKE A CHARGE. MX R & R THE CAPTAIN'S FLASHLIGHT BATTERY PACK WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130215078VSkin · corrodedDURING C-CHECK LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION (LOCAL LEVEL 2) FROM LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN AROUND RIVETS IAW EC5530-01116 REV F. SDR ASOA2013021577Skin · corrodedDURING C-CHECK RT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION ON RT HORIZ STABILIZER L/E IAW EC5530-01116, REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130215076VSkin · corrodedDURING C-CHECK CORRODED CARGO DOOR INNER SKIN AROUND NUT PLATE HOLES. MX PERFORMED REPAIR AT CARGO DOOR INNER SKIN AROUND NUTPLATE HOLES IAW EC5320-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130214075Rivet · looseDURING C-CHECK WORKING RIVET AT FR 79, STR 9R. MX PERFORMED REPAIR TO WORKING RIVET FR 79, STR 9R IAW EC5330-02699. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130214074VSkin · nickedDURING C-CHECK FWD LOWER INNER CARGO DOOR SKIN HAS NICK. MX PERFORMED REPAIR AT FWD LOWER INNER CARGO DOOR SKIN IAW EC5320-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20130215001Mechanism · dirtyON FLIGHT 3577 THE FLIGHT ATTENDANT REPORTED THE PASSENGER ENTRY DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED, INSPECTED AND LUBRICATED DOOR MECHANISM AND SEAL, PERFORMED OPERATIONAL CHECK OF DOOR IAW 52-18-00. THE AIRCRAFT WAS RETUSDR ASOA20130214073Frame · crackedDURING C-CHECK FRAME 10L CRACKED. MX R & R FRAME 10L IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130214072Frame · crackedDURING C-CHECK FRAME 10R CRACKED. MX R & R FRAME 10R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130215261Floor Support · corrodedCORROSION AROUND NUTPLATE AT FRAME 20, STRINGER 16R. BLENDED CORROSION, FABRICATED DOUBLER AND INSTALLED.SDR CHQA20130214050Light · inoperativeDURING INSPECTION, THE FIRST EMERGENCY LIGHT FLOOR PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT PROXIMITY STRIP AT ROWS 1 AND 2. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CHQA20130213049Electronic Unit · faultyCREW REPORTED THAT AFTER TAKEOFF, DURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED. THE OTHER GEAR HAD GREEN INDICATIONS AND SHOWED UP AND LOCKED. THE CREW ALSO RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THEY FOLLOWED THE SDR SIMA20130214008Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE ABOVE WING LEFT EMERGENCY LAMP INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130214004Roller · lack of lubeON FLIGHT 3959 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN PASSENGER DOOR ROLLERS PER AMM 52-18-00. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130214002Handle · lack of lubeON FLIGHT 4323 THE FLIGHT ATTENDANT REPORTED THE MAIN ENTRY DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBED MAIN DOOR EXTERNAL HANDLE. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 52 18 00. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA20130213051Wire Harness · faultyCREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER ROTATION AND REPORTED THAT THE LANDING GEAR DID NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS. OPERATIONAL SDR SIMA20130214001Pump · malfunctionedON FLIGHT 3571 THE CREW REPORTED THAT DURING CRUISE THEY RECEIVED A HYD SYS 1 FAIL EICAS MESSAGE. THE CREW RAN CHECKLIST AND MONITORED THE SITUATION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED SDR SIMA20130213003Sign · inoperativeDURING B INSPECTION FOUND THE EMERGENCY EXIT SIGN AT ROW 3BC WILL NOT COME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 3BC IAW EMB145 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNEDSDR SIMA20130212005Wire · brokenDURING B INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING STRIP AT PANEL 241BF HAS BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRASDR CHQA20130212048Coupling · brokenCREW REPORTED THEY RECEIVED THE BLEED 1 VALVE FAIL MESSAGE IN FLIGHT. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE COUPLING TO TEMPERATURE CONTROL VALVE AND OPERATIONAL CHECKS WERESDR CHQA20130212047Battery · dischargedDURING INSPECTION MAINTENANCE FOUND LEFT FUSELAGE FORWARD EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND NO FURTHER DEFECTS WERE NOTED.SDR ASOA20130212009RBattery Pack · inoperativeDURING ROUTINE MX INSPECTION, THE GALLEY AND MAIN DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA201302120001Linkage · lack of lubeDURING POST FLIGHT INSPECTION THE FLIGHT CREW REPORTED THE PASSENGER DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE INSPECTED AND LUBED THE PASSENGER DOOR HANDLE LINKAGE. DOOR OPS CHECKED GOOD.SDR SIMA20130211008Trunnion · crackedDURING MAINTENANCE INSPECTION WHILE DOING INSTALLATION OF THE RIGHT WING RIB 5QC FOUND THE RIGHT MAIN LANDING GEAR AFT TRUNNION CRACKED AT HI-LOK HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE FOR HMBV INSPECTION. REMOVED AND REPLACED THE RIGHT AFT TRUNNION IAWSDR SIMA20130211006Flashlight Assy · failedFLIGHT 3282, FLIGHT ATTENDANT AND PASSENGERS REPORTED ODOR OF SMOKE AROUND SEATS 15 -17. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND ELECTRICAL ODOR COMING FROM AFT FLASHLIGHT. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW AMM 33-SDR SIMA20130211004Flashlight · inoperativeON FLIGHT 2755 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CAPTAIN’S FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130211002Controller · malfunctionedON FLIGHT 3307 THE CREW REPORTED THAT ON FINAL APPROACH THEY NOTICED STRONG ELECTRICAL FUMES IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND ELECTRICAL SMELL COMING FROM AUTOFLIGHT GUISDR SIMA20130211001Holder · looseON FLIGHT 3423 THE FLIGHT ATTENDANT REPORTED THE FLASHLIGHT HOLDER WAS LOOSE AND WOULD NOT HOLD FLASHLIGHT AGAINST CONTACTS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER IAW AMM 33-50-16. THE OPERATIONAL CHECK WSDR SIMA20130210003Flashlight · inoperativeON FLIGHT 2939 THE FLIGHT ATTENDANT REPORTED THE AFT FLASHLIGHT WOULD NOT CHARGE AND RED CHARGE LIGHT WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT AFT FLASHLIGHT IAW AMM 33-50-16 THE OPERATIONAL CHECKSDR SIMA20130210002Frame · gougedDURING MAINTENANCE INSPECTION FOUND FRAME 65 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2077. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130210001Frame · gougedDURING MAINTENANCE INSPECTION FOUND FRAME 70 GOUGED AT STRINGER 13 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO EM-53MR-2075. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130209005Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY AT NR 4 POSITION IAW EMB AMM 33-50-64. THE OPERATIONAL CHECK WAS GOOD. THE AIRSDR SIMA20130209004Flashlight · damagedDURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS SDR SIMA20130209001Battery · dischargedDURING B INSPECTION FOUND THE LEFT & RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LAMPS IAW AMM 33-50-07. PART # 1317 AND 30-2510-3. NO FIX. REMOVED AND SDR ASOA20130126071Door Frame · corrodedDURING C-CHECK THE RT PAX EMERGENCY EXIT DOOR BOTTOM FRAME WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5220-01047. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130126070VFloor Support · corrodedDURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130126069VFrame · crackedDURING C-CHECK, FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE R/H CREW ESCAPE HATCH CUTOUT BETWEEN STRINGERS 9R-10R. MX R & R THE CRACKED FRAME SEGMENT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130126068VFrame · crackedSHV-DURING C-CHECK FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE LT CREW ESCAPE HATCH CUTOUT BETWEEN STRINGERS 9L-10L. MX R & R THE CRACKED FRAME SEGMENT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20130208011Stringer Splice · corrodedDURING MAINTENANCE INSPECTION FOUND SPLICE STRINGER 18R CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW STRINGER AT 18R BETWEEN FRAMES 14 & 14 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130208010Stringer · corrodedDURING MAINTENANCE INSPECTION FOUND STRINGER 18 R IS CORRDED BETWEEN FRAMES 13 & 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW STRINGER AT 18R BETWEEN FRAMES 13 & 14 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130208009Skin · corrodedDURING MAINTENANCE INSPECTION FOUND THE INTERNAL BELLY SKIN BETWEEN FRAMES 13 AND 14 TO HAVE CORROSION DAMAGE FROM STRINGER 17R TO 20L. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGED SKIN IAW EO EM-53MR-2074 REV 1. THE AIRCRAFT WAS RETURNED TO SERVSDR SIMA20130208008Fitting · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT MAIN LANDING GEAR AFT TRUNNION FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR TRUNNION IAW EO EM-57 NR-666. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130208007Skin · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT FUSELAGE SKIN AT FRAME 75 HAS A CRACK AT STRINGER 2 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FUSELAGE SKIN IAW EO EM-53-MR-2070. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130208006Rib · crackedDURING MAINTENANCE INSPECTION FOUND THE RIGHT WING RIB 5 CRACKED AT LOWER AFT LIGHTING HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT RIB 5 IAW EO EM-57 MR-595. THE AIRCRAFT WAS RETURNED TO SERVICE.
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