Embraer EMB-135KL
Service difficulty reports · 5,598
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 = 'EMB135KL' 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 = 'EMB135KL' 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 SIMA20130505003Battery · inoperativeDURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIPS POWERED BY THE NR 3 POWER PACK WAS INOPERABLE. SUSPECT NR 5 INVERTER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT DC/AC NR 5 INVERTER IAW AMM 33-50-11. PART NUMBER 782SDR SIMA20130505002Sign · inoperativeDURING B INSPECTION FOUND THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT SIGN NEXT TO SERVICE DOOR IAW EMB 140 AMM 33-50-13. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRASDR CHQA20130504153Skin · damagedDURING INSPECTION, A TOOLING MARK ON THE INTERIOR BELLY SKIN WAS FOUND ADJACENT TO STRINGER 21L AND BETWEEN FRAMES 10 AND 11. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008436.SDR SIMA20130503005Retainer · brokenDURING B INSPECTION FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT CHARGER RETAINER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT SYSTEM IAW EMB AMM 33-50-16-000-801/33-50-16-400-801. THE OPERATIONASDR SIMA20130503002Light · inoperativeDURING B INSPECTION FOUND THE CEILING EMERGENCY LIGHT ABOVE SEAT 11C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SEAT 11C CEILING EMERGENCY LIGHT LAMP IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNSDR CHQA20130502162Frame · damagedDURING INSPECTION, AN ELONGATED RIVET HOLE WAS FOUND ON FRAME 12 BETWEEN STRINGERS 21R AND 20R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008257.SDR CHQA20130502161Support · damagedDURING INSPECTION, A MISDRILLED RIVET HOLE ON THE RIGHT CONTROL CABLE QUADRANT SUPPORT. THE SUPPORT BRACKETS AND QUADRANT SUPPORT WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03.SDR CHQA20130502143Light · inoperativeCREW REPORTED THAT THE EMERGENCY LIGHT IN THE FLIGHT DECK WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR SIMA20130502003Floor Support · corrodedDURING MAINTENANCE INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT SPECIFIED. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130502002Fitting · wornDURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON OUTBOARD PCA ATTACH LUG HAS MIGRATED HAT BUSHING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130502001Floor Support · corrodedDURING MAINTENANCE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED AT FRAME 59. THE AIRCRAFT WAS REMOVED FROM SERVICE. LEVEL OF CORROSION NOT SPECIFIED. REPAIRED OMEGA BEAM IAW EO EM-53MR-1518. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA20130501159Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501158Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE LEFT AILERON QUADRANT SUPPORT WEB AT FRAMES 12-13 AND STRINGERS 20L-21L. THE QUADRANT SUPPORT WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501157Support · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE RIGHT AILERON QUADRANT SUPPORT WEB AT FRAME 12 AND 13 AND STRINGERS 20R AND 21R. THE RIGHT QUADRANT SUPPORT WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130501156Stringer · corrodedDURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IAW SRM 51-40-02.SDR CHQA20130501151Floor Support · corrodedDURING INSPECTION, CORROSION AND CRACKS WERE FOUND ON THE FLOORBOARD SUPPORT FLANGE OF THE LEFT OMEGA BEAM BETWEEN FRAME 24 AND FRAME 25. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR SIMA20130501002Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFTSDR SIMA20130501001Roller · lack of lubeFOR FLIGHT 4182 THE FLIGHT ATTENDANT REPORTED THE MAIN PASSENGER DOOR WAS VERY HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEAN AND LUBED THE PASSENGER DOOR ROLLERS AND SEAL. STANDARD MAINTAINCE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT SDR CHQA20130430160Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21L AND 20L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR SIMA20130430006Frame · crackedDURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED BETWEEN STRINGERS 15R AND 16R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED SECTION OF FRAME, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130430004Flashlight · intermittentDURING B INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT WORKING INTERMITTENTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S EMERGENCY FLASHLIGHT ASSEMBLY IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT SDR SIMA20130429010Shear Tie · corrodedFR 68 SHEAR TIE CORRODED AFT OF CARGO DOOR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART B.SDR SIMA20130429009Shear Tie · corrodedFR 65 SHEAR TIE CORRODED IN FRONT OF CARGO DOOR SILL. REPAIRED SHEAR TIE IAW EO EM-53MR-1129, PART A.SDR SIMA20130429008Wire · brokenDURING MX INSPECTION, FOUND THE CABIN AISLE NR1 EMERGENCY LIGHT STRIP HAS BROKEN WIRES. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 PROXIMITY LIGHT STRIP IAW AMM 35-50-12. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130429007Wire · brokenDURING B INSPECTION, FOUND THE EMERGENCY EXIT OVERHEAD CEILING PANEL NR 253CLC HAS EMERGENCY LIGHT WIRE BROKEN. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED BROKEN WIRE ON CEILING PANEL NR 253CLC IAW SWPM 20-50-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNSDR SIMA20130427003Switch · brokenDURING MAINTENANCE INSPECTION, FOUND CAPTAIN'S FLASHLIGHT SWITCH BROKEN. AIRCRAFT REMOVED FORM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. NO FURTHER DEFECT NOTED. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA20130427001Mechanism · lack of lubeON FLIGHT 3341 FOUND MAIN DOOR DIFFICULT TO CLOSE SOMETIMES LEVES GAP AT TOP. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W PERFORMED LUBRICATION OF THE STANDARD MAIN-DOOR ACTUATING AND LOCKING MECHANISM IAW EMB AMM 52-11-00. OPS CHECK GOOD. THE AIRCRAFT WAS SDR SIMA20130428009Mechanism · lack of lubeON FLIGHT 4435 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE CREW HAD TO HAVE THE GATE AGENT HELP OPEN THE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED AND LUBRICATED MAIN-DOOR ACTUATING MECHANISM IAW EMB 140 AMM 52-11-00. THE OSDR SIMA20130427004Unknown · smokeON FLIGHT 2998 THE CREW REPORTED THEY NOTICED A BURNING ODOR AND SMOKE FROM INBOARD BRAKE ON RIGHT MAIN GEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TAXI CHECK WITH CREW NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA20130426155Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 53-31-04.SDR CHQA20130426154Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8R AND 9R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426152Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP ON FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426150Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE CENTER OMEGA LEFT SIDE BETWEEN FRAMES 24 AND 25. THE CENTER OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008055.SDR CHQA20130426149Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA AT THE CARBON CROSS MEMBER FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.SDR CHQA20130426148Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.SDR CHQA20130426147Bracket · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE BRACKET BETWEEN FRAME 64 AND FRAME 65 AT STRINGER 5L. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-30-01, AND 53-31-02.SDR CHQA20130426146Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER LEFT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.SDR SIMA20130425007Light · inoperativeDURING MAINTENANCE INSPECTION FOUND THE LEFT OVER WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB FOR THE LEFT AFT OVER WING EMERGENCY LIGHT IAW EMB MM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE SDR SIMA20130425005Power Supply · inoperativeDURING B INSPECTION FOUND NUMEROUS EMERGENCY LIGHTS IN THE FORWARD CABIN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRASDR SIMA20130425003Light · improper partON FLIGHT 2805 THE FLIGHT ATTENDANT REPORTED THE FLOOR EMERGENCY LIGHT NOT CORRECT COLOR NEXT TO SEAT 2A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CABIN FORWARD FLOOR EMERGENCY PROXIMITY STRIP LIGHT IAW EMB 140 AMM 33-50-12THE OPERATIOSDR SIMA20130425002Flashlight · missingDURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED CAPTAIN’S FLASHLIGHT IAW 20-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130423005Light · inoperativeDURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-30-01-000-801-A AND 33-30-01-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THSDR SIMA20130423002Light · misinstalledON FLIGHT 3402 THE CREW REPORTED THE FLOOR EMERGENCY LIGHTING STRIPS WERE INSTALLED INCORRECTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. SWAPPED FLOOR STRIPS 1 & 5 IAW AMM 33-50-12, FLOOR STRIP NR 1 AND THE OPERATIONAL CHECK WAS OK IAW AMM 33-50-12. HOWEVER SDR SIMA20130422003Handle · malfunctionedFLIGHT 3370. MAIN CABIN DOOR WAS DIFFICULT TO OPEN & CLOSE. REMOVED MAIN DOOR HANDLE, RETORQUED PIVOT BUSHING BOLT IAW AMM 20-10-01. RETORQUED BOLTS ON INNER HANDLE BOX ASSEMBLY IAW AMM 20-10-01. COMPLIED WITH PROC ETN EM 52-037 SUPPORT BRACKET NO DEFECTSSDR SIMA20130422001Floor Support · corrodedDURING MAINTENANCE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 25 AND 28. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR IAW EMBRAER STRUCTUAL REPAIR MANUAL 53-22-10 AND 53-00-10 FIGURE 202 SHEET 2. THE CORROSION LEVEL IS NOT SPECISDR SIMA20130421002Fitting · gougedDURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON BRACKET WHERE DAMPER ATTACHES GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20130421001Flashlight · inoperativeDURING B INSPECTION FOUND THE CAPTAINS FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS FLASHLIGHT IAW EMB AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RSDR SIMA20130420012Angle · crackedRT FWD VERTICAL TO FUSELAGE ANGLE CRACKED. REPAIRED ANGLE IAW AEA EM-53MR-1281.SDR SIMA20130420011Gusset · corrodedDURING B INSPECTION, FOUND THE LAV RT BEAM GUSSET CORRODED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LAV RT BEAM GUSSET IAW SRM 51-40-02. THE ACFT WAS RETURNED TO SERVICE.SDR SIMA20130420010Cover · damagedDURING B INSPECTION, FOUND THE FOUR PROXIMITY LIGHT STRIP COVER PANELS DAMAGED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FOUR EMERGENCY LIGHT PROXIMITY STRIP PANEL COVERS AS REQUIRED. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Back to Embraer EMB-135KL