Embraer EMB-135LR
Service difficulty reports · 2,545
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 = 'EMB135LR' 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 = 'EMB135LR' 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 SIMA200212157Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 19. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1348/02, AND STANDARD SRM PRACTICESDR SIMA200212149Floorbeam · corrodedTHIS IS A LEVEL 2 FINDING, CORROSION GALLEY CENTRAL BEAM GUSSET. BLENDED CORROSION, PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M)SDR SIMA200212150Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION ON FORWARD DIGITAL. BLENDED CORROSION PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M)SDR SIMA200212151Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ON AFT DIGITAL. BLENDED, PERFORMED NDT, RESTORED SURFACE PROTECTION. (M)SDR SIMA200212153Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION ON CENTER BEAM AT FRAME 19. INSTALLED SERVICEABLE CENTER BEAM IAW EMB GST-1348/02. (M)SDR SIMA200212154Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION SERVICE DOOR CENTER SILL. REPAIRED CORRODED SERVICE DOOR SILL IAW EMB GST-1348/02. (M)SDR SIMA200212155Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION ON SERVICE DOOR FORWARD SILL. REPAIRED CORRODED FORWARD SILL IAW EMB GST 1348/02. (M)SDR SIMA200212152Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION ON DIAMOND GUSSET AT FRAME 20. BLENDED CORROSION, PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB GST-1348/01. (M)SDR C2XA02CL104Connector · meltedCLE FLIGHT 3149 THE CREW REPORTED A BURNING RUBBER SMELL WHEN THE APU WAS STARTED. INSPECTED AND FOUND THE SMELL WAS ORIGINATED FROM A MELTING CONNECTOR ON THE COFFEE HOT JUG. THE COFFEE HOT JUG WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.SDR C2XA02CL103Valve · leakingCLE FLIGHT#3316 THE CREW REPORTED A STRONG FUEL SMELL IN THE AIRCRAFT WHEN THE APU IS STARTED.MAINTENANCE REPLACED THE APU AIRBLEED VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR SIMA200212108Sill · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING. FABRICATED A REPAIR DOUBLER. REPAIRED IAW EMB GST-1254/02, ITEM 4 AND STANDARD SRM PRACTICES. (M)SDR SIMA200212107Skin · corrodedDURING AN MBV INSPECTION OF AIRCRAFT, FOUND FOUR GROUPS OF GOUGES ON THE LEFT FORWARD FUSELAGE BETWEEN FRAMES 12 AND 13, ALONG STRINGER 16L. BLENDED GOUGES PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLSDR C2XA02CL101Receptacle · burnedCLE FLIGHT 2955 THE FLIGHT ATTENDANT REPORTED A SMOKE SMELL IN THE GALLEY IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT COFFEE WARMER AND THE CONNECTOR RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. COFFEE WARMER (P/N 1095A).SDR SIMA200212105Beam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON CENTER BEAM AT FRAME 20. REMOVED CORRODED BY CUT OUT. FABRICATED TWO DOUBLER ANGLES, A FILLER, AND A U-SHAPE DOUBLER CHANNEL. REPAIRED IAW EMB145 (SRM145/1142, CHAPTER 53, REV 17) 53-21-10, AND SDR SIMA200212106Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1141, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTISDR SIMA200212156Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE AND FILLER. REPAIRED IAW EMB 145 SRM 145/1142, CHAPTER 53, REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M)SDR C2XA02CL097Lever · failedTHE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AFTER TAKEOFF. MAINTENANCE REPLACED THE LANDING GEAR LEVER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA02CL091Lever · faultyCLE FLIGHT NR 3052 THE CREW REPORTED UPON GEAR RETRACTION RECEIVED A LANDING GEAR WARNING AND THE WARNING WOULD NOT CANCEL UNTIL THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WASDR C2XA02CL090Warning System · faultyCLE FLIGHT 3078 THE CREW REPORTED A LANDING GEAR WARNING AFTER TAKEOFF. THE WARNING WOULD NOT CANCEL. MAINTENANCE INSPECTED AND REPLACED THE AURAL WARNING UNIT. OPERATIONAL CHECKS WERE GOOD. MAINTENANCE ALSO PERFORMED CONTINUITY CHECK OF WIRES W001-0843-24SDR SIMA20021003Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER, FILLER, AND TWO SHIMS. WORK DONE IAW EMB145 SRM 145/1142, CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICESDR C2XA02CL088Odor · detectedTHE CREW REPORTED A STRONG ODOR OF FUEL IN CABIN WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU. NO DEFECTS WERE FOUND.THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR SIMA200209335Floor Support · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON CENTER BEAM UNDER GUSSET AT FRAME 20. REMOVED CORROSION BY CUT OUT. REPAIRED IAW EMB 145 SRM 145/1142 CHAPTER 53, REV 17 53-21-10, AND STANDARD. (M)SDR SIMA200210013Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR SILL IS CORRODED AROUND NUTPLATES, FRAME 20-22. REPAIRED CORRODED AREA IAW EMB135 GST 1067/02. (M)SDR SIMA200210012Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM RAMP SUPPORT CORRODED AT FRAME 20. REMOVED AND REPLACED RAMP IAW EMB135 SRM 51-40-02. (M)SDR SIMA200210011Gusset · corrodedABI - THIS A LEVEL 2 FINDING. AFT DIAMOND GUSSET IS CORRODED AT FRAME 22. REPAIRED CORRODED AREA IAW EMB135 GST-1067/02. (M)SDR SIMA200210010Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. CORROSION FOUND ON FORWARD CORNER OF AFT SERVICE DOOR SILL AT FRAME 22. REPAIRED CORROSION IAW EMB 135 GST-1067/02. (M)SDR SIMA200210009Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. FORWARD DIGITAL HAS CORROSION AROUND FASTENERS AT FRAME 16. REPAIRED CORROSION IAW EMB GST-1067/02. (M)SDR SIMA200210007Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD DOOR SILL HAS CORROSION AROUND NUTPLATE AT FRAME 20. REMOVED CORROSION AROUND NUTPLATE IAW EMB 135 GST 1067/02. (M)SDR SIMA200210006Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET IS GOUGED FROM FRAME 20 TO 22. UPPER SURFACE IS CORRODED AROUND FASTENERS. REMOVED AND REPLACED GUSSET IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200210005Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. OMEGA BEAM HAS CORROSION AT FRAME 20. FABRICATED A DOUBLER FILLER AND SHIMS AND INSTALLED IAW EMB135 SRM 53-21-10, 51-40-02. (M)SDR SIMA200210004Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET HAS CORROSION AROUND NUTPLATE AT FRAME 20. REMOVED AND REPLACED SERVICEABLE FORWARD DIAMOND GUSSET IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200210008Bracket · corrodedABI - THIS IS A LEVEL 2 FINDING. PASSENGER DOOR THRESHOLD ATTACHMENT BRACKETS ARE CORRODED AROUND NUTPLATE AT FRAME 16 AND 17. REPAIRED CORROSION ON PAX DOOR THRESHOLD IAW EMB 135 GST-1067/02. (M)SDR SIMA200209326Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET REMOVED CORROSION FOUND ON CENTER BEAM AT FRAME 20. CUT OUT DAMAGED AREA AND REPAIRED IAW EMB135 SRM 53-21-10. (M)SDR SIMA200209325Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET HAS CORROSION AT FRAME 20. INSTALLED NEW CENTER GUSSET IAW EMB 135 SRM 51-40-02. (M)SDR SIMA200208712Fire Warning · false activationRDU - FLT 4549 - ON CLIMB-OUT, CREW HAD CARGO COMPARTMENT SMOKE WARNING AND DISCHARGED FIRE BOTTLES. DECLARED EMERGENCY AND RETURNED TO RDU. NO FIRE NOTICED. REPLACED CARGO FIRE BOTTLES. PERFORMED SYSTEMS OPS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICESDR C2XA02CL081Module · faultyCLE FLIGHT 3029 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR SIMA200207903Sill · corrodedTHIS IS A LEVEL 2 FINDING. CORROSION SERVICE DOOR CENTER SILL. BLENDED AND RESTORED SERVICE DOOR CENTER SILL IAW EMB GST-0798/02 AND EMB135 CPM 51-14-02 AND 51-21-06. (M)SDR SIMA200207905Cap · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT NOSE LANDING GEAR STRUT LOWER BEARING CAP CORRODED. REPLACED STRUT LOWER BEARING CAP IAW EMB 135 AMM 32-20-01. (M)SDR SIMA200207904Cap · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. REMOVED AND REPLACED LEFT FORWARD BEARING CAP IAW EMB 135 AMM 32-10-01. (M)SDR SIMA200208303Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. CORROSION ON SERVICE DOOR CENTER SILL. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST 0636/02. (M)SDR SIMA200208707Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET IS CORRODED AT FRAME 20. REPLACED SERVICEABLE FORWARD DIAMOND GUSSET IAW EMB 135 SRM 51-40-06, 51-40-02. (M)SDR SIMA200208708Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR SILL CORRODED AROUND NUTPLATE AT FRAME 20. BLENDED AND TREATED CORROSION, ACCEPTED AS IS IAW GST-0925/02. (M)SDR SIMA200208709Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. RIGHT FORWARD SILL IS CORRODED AROUND THE NUTPLATES AT FRAME 18 AND 20. BLENDED AND TREATED FOR CORROSION IAW GST-0925/02. (M)SDR SIMA200208710Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET IS CORRODED AT FRAMES SO AND 22. BLENDED AND TREATED FOR CORROSION, ACCEPTED AS IS IAW GST-0725/02. (M)SDR C2XA02CL079Landing Gear · malfunctionedDAY FLIGHT 3316 CREW REPORTED THAT AFTER TAKEOFF, GOT THE LANDING GEAR LEVER DISAGREE WARNING, AND THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DAY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO TYS WHERE MAINTENANCE PERFORMED A LANDING GEAR RETRASDR C2XA02RI002Connector · looseRIC-FLT 3000 CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BOTH NOSE LANDING GEAR UPLOCK AND DOWNLOCK PROXIMITY SWITCH HARNESS CANNON PLUGS NOT PROPERLY SECURED. MASDR SIMA200207301Structure · corrodedMBV - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL. REMOVED CORROSION BY BLENDING OUT. FABRICATED A REPAIR DOUBLER 2 INCH BY 2.75 INCH, .040 INCH THICK IAW EMB GST-0800/02, ITEM 1, AND STANDARD SRM PRACTICES. (M)SDR SIMA200207303Beam · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE 18.5 INCH BY 3 INCH, AND FILLER 14 INCH BY 2.75 INCH, 050 INCH THICK, A PLATE 6.5 INCH BY 1 INCH .125 INCH THICK, ANSDR C2XA02CL076Skin · crackedDURING ROUTINE MAINTENANCE THE RUDDER II SKIN WAS FOUND CRACKED.THE CRACK WAS APROX.7 1/2 INCHES LONG AND APROX. 4 INCHES FROM THE BOTTOM.THE CRACK WAS PERPENDICULAR TO THE TRAILING EDGE.MAINTENANCE REPAIRED THE RUDDER II SKIN I/A/W CONTINENTAL EXPRESS EC5540-SDR SIMA200207209Support · corrodedABI - CENTER BEAM RAMP AND SUPPORT CORRODED. INSTALLED NEW RAMP SUPPORT IAW EMB 145 SRM 51-40-02. (M)
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