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 SIMA201107602Fitting · chafedDURING MAINTENANCE BASE INSPECTION FOUND RIGHT AILERON DAMPER FITTING CHAFED FROM DAMPER ROD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING AND PCA FITTINGS IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SDR SIMA201108001Window Frame · crackedDURING MAINTENANCE BASE VISIT FOUND UPPER CENTER WINDSHIELD CUTOUT CRACKED AT 2 EACH HANDLE ATTACH NUT PLATES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED COCKPIT OVERHEAD RIB AT 2 EACH HANDLE ATTACH NUT PLATES IAW ETN EM-53-145. THE AIRCRAFT WAS RETURNSDR SIMA201107501Fitting · chafedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPER FITTING CHAFING AGAINST THE ROD END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201107302Wire · brokenDURING MAINTENANCE BASE VISIT MAINTENANCE ACCIDENTLY BROKE A WIRE TO THE EMERGENCY LIGHT STRIP AT PANEL 251 DF. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW CONTACT ON EMERGENCY LIGHT STRIP AT PANEL 251DF IAW EMB 140 SWPM 20-21-00, 20-50-01. THE OPERATSDR SIMA201107301Light · inoperativeFOR FLIGHT 4060 DURING PREFLIGHT INSPECTION FOUND THAT THE RIGHT OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. SDR SIMA201107306Fitting · crackedDURING MAINTENACE BASE VISIT FOUND SHEAR CLIP CRACKED AT FRAME 80, STRINGER 7 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1789. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA201100057Brake Sys · contaminatedCREW REPORTED THAT AFTER LANDING THE BRAKES WERE SLUGGISH AND THAT THE PEDALS HAD TO BE PUSHED ALL THE WAY TO THE FLOOR BEFORE THEY WERE EFFECTIVE. MAINTENANCE BLED ALL 4 BRAKE SYSTEMS. AIR WAS FOUND TO BE PRESENT IN THE INBOARD AND OUTBOARD BRAKE SYSTEMS. SDR CHQA201100056Carbon Seal · leakingCREW REPORTED THAT AFTER TAKEOFF AT BETWEEN 600-700FT THERE WAS VISIBLE SMOKE IN THE CABIN FOLLOWED BY A LAVATORY SMOKE INDICATION ON EIACS. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN BOTH ENGINES AND BLEEDS WITH PACKS IN MULTISDR SIMA201107601Unknown · odorON FLIGHT 4417 DURING CLIMB THROUGH AT FLIGHT LEVEL 190-2000 IN MODERATE TURBURLANCE THE CREW REPORTED, BEGAN TO SMELL A STRONG ELECTRICAL BURNING ODOR LASTING ABOUT 1 MINUTE. THE CREW COULD NOT ISOLATE IT BUT SOMETHING WAS THERE. ICE PROTECTION WAS NOT ON. SDR CHQA201100054Air Duct · contaminatedSHORTLY AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED THAT A LARGE AMOUNT OF WATER SPILLED OUT OF THE GALLEY CART AND RAN BACK INTO THE FLOOR AIR CONDITIONING INLET AT ROW 3. SHORTLY AFTER, THERE WAS A SMALL AMOUNT OF SMOKE REPORTED IN THE CABIN ALONG WITH A LSDR SIMA201106902Sign · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT PLACARD AT FORWARD OVERHEAD AISLE WING EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT PLACARD AT FORWARD OVERHEAD AISLE WING EXIT IAW EMB 140 AMM 33-50-15SDR CHQA201100051Controller · inoperativeCREW REPORTED, AFTER TAKEOFF WERE UNABLE TO CONTROL THE CABIN ALTITUDE IN MANUAL MODE WHILE THE AUTO MODE WAS ON DEFERRAL. IT WAS REPORTED THAT THE CABIN ALTITUDE WAS CLIMBING AT APPROXIMATELY THE SAME RATE AS THE AIRCRAFT AT ALL SETTINGS. THE AIRCRAFT RETURSDR SIMA201106801Unknown · smokeON FLIGHT 3118 THE CREW REPORTED THAT ON SELECTING TAKEOFF THRUST (ALT T/O-1) EXPERIENCED SMOKE AND FUMES IN COCKPIT OUT OF THE AIR CONDITIONING VENTS (SMELLED LIKE BURNT OIL). THE FLIGHT ATTENDANT REPORTED HAZE AND FUMES IN CABIN ALSO. THE SMOKE AND FUMES DSDR SIMA201106904Light · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE FORWARD FLOOR EMERGENCY PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLOOR EMERGENCY PROXIMITY LIGHT IAW EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICSDR SIMA201106901Frame · crackedDURING MAINTENANCE BASE VISIT INSPECTION FRAME 23 CRACKED AT RIGHT FLOOR SILL NEAR SERVICE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 WITH DOUBLER IAW ETD2011-145/00044 AND SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201106705Attach Angle · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE, SECOND ONE AFT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW ATTACH ANGLE IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201106704Frame · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED JUST BELOW FLOOR LEVEL BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME IAW EO EM-53MR-1779. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201106701Engine · malfunctionedON FLIGHT 4521 THE CREW REPORTED A HEAVY OIL ODOR THROUGHOUT THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE PER AE WORKCARD 71-000-00. THE LEAK AND OPERATIONAL CHECKS WERE GOOSDR SIMA201106202Unknown · vibrationON FLIGHT 3045 THE CREW REPORTED A NOISE AND SMALL VIBRATION IN NOSE AREA AFTER TAKEOFF. APPROXIMATLEY 20 MINUTES AFTER LIFTOFF THE NOISE SUDDENLY STOPPED. THE CAPTAIN DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEN. AFTER SECOND GEAR RETRACTION AT 10,000SDR SIMA201106008Attach Bracket · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND BAGGAGE DOOR TORSION BAR FORWARD SUPPORT ATTACH BRACKET AT FRAME 61 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE DOOR TORSION BAR SUPPORT ATTACH BRACKET AT FRAME 61 IAW SRM 51-40-SDR SIMA201106007Angle · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE FORWARD ANGLE CRACKED ON AFT END. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE IAW EO EM-53MR-1281 PART A. THE AIRCRAFT WAS RETURNED TO SERVICSDR SIMA201106002Frame · crackedDURING MAINTENANCE BASE VISIT FOUND FRAME 23 BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BY SPLICING IN A NEW SECTION OF FRAME IAW AE EO EM-53MR-1775. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201106003Landing Gear · malfunctionedON FLIGHT 4469 THE CREW REPORTED THAT AFTER TAKE OFF DURING GEAR RETRACTION THE LANDING GEAR FAILED TO RETRACT FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO IAD. CRASH, FIRE AND RESCUE WERE CALLED FOR THE LANDING. THE ASDR SIMA201105903Sign · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE FORWARD WING EMERGENCY EXIT LOCATING SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EXIT LOCATING SIGN AND EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-15. THE OPERATIONAL CHSDR SIMA201106006Frame · crackedDURING MAINTENANCE BASE VISIT FOUND FRAME 77 CRACKED NEAR STRINGER 18 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACK ON FRAME 77 AT STRINGER 18 LEFT IAW EMB SRM 53-00-04 ITEM 14. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105602Structure · dentedWHILE ON THE RAMP THE AIRCRAFT WAS STRUCK BY A DEICE TRUCK NEAR THE SERVICE DOOR. SKIN HAS SEVERAL DENTS ON FRAME 22 BETWEEN STRINGERS 20 AND 18. THE SHEAR CLIP FROM 18 TO 19 CRACKED. SHEAR CLIP FROM 19 TO 20 WAS DENTED. THE AIRCRAFT WAS REMOVED FROM SERVISDR CHQA201100120Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB SKIN ON THE RIGHT HAD SIDE. MAINTENANCE REPAIRED THE ANGLE AT THE RIGHT OMEGA BEAM AT THE WING STUB SKIN IAW SRM 53-23-02. THE ANGLE WAS FABRICATED LOCALLY IAW ETD20SDR CHQA201100119Floor Support · crackedDURING INSPECTION A CRACK WAS FOUND ON THE ANGLE THAT JOINS THE OMEGA BEAM AND THE WING STUB SKIN ON THE RIGHT HAD SIDE. MAINTENANCE REPAIRED THE ANGLE AT THE RIGHT OMEGA BEAM AT THE WING STUB SKIN IAW SRM 53-23-02. THE ANGLE WAS FABRICATED LOCALLY IAW ETD201SDR CHQA201100040Engine · malfunctionedCREW REPORTED THAT AFTER LEVELING OFF AT 23,000FT, REPORTED SMELLING A BURNING OIL/ELECTRICAL ODOR. THE CAPTAIN AND FIRST OFFICER DONNED OXYGEN MASKS AND PROCEEDED TO DIVERT TO IND. THE ODOR WAS CONTAINED MAINLY TO COCKPIT BUT FLIGHT ATTENDANT DID REPORT A SSDR SIMA201105303Frame · crackedDURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 CRACKED BETWEEN STRINGER 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT IAW EO EM-63MR-1766. THE AIRCRAFT WAS RETURNED TO SERVICSDR SIMA201105302Sill · corrodedDURING MAINTENANCE BASE VISIT INSPECTION FOUND THE SERVICE DOOR CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SERVICE DOOR, CENTER SILL IAW EMBRAER SRM 51-40-02 AND ETA-EM-5300-1706. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA201100121Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON AN EXISTING REPAIR ON THE LEFT OMEGA BEAM FLANGE AT FRAME 25. THE LEFT OMEGA BEAM FLANGE AT FRAME 25 CORROSION REPAIR WAS REPLACED IAW SRM 53-00-10.SDR CHQA201100114Skin · damagedDURING INSPECTION DAMAGE FROM A LIGHTNING STRIKE WAS FOUND ON CENTER FUSELAGE SKIN, SECTION II, AT FRAME 26, BETWEEN STRINGERS 4L AND 5L. MAINTENANCE PERFORMED AN EDDY CURRENT INSPECTION ON THE CUT-OUT IAW ETD2010-145-00077 AND NO CRACKS WERE FOUND. THE LIGHSDR SIMA201105411Frame · crackedDURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED IN 2 AREAS JUST BELOW FLOOR LEVEL BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 RIGHT 2 AREAS BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT IAW EO EM53MR1774. THESDR SIMA201105410Support · crackedDURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR CABLE DRUM SUPPORT AT FRAME 68 CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR CABLE DRUM SUPPORT AT FRAME 68 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105409Support · crackedDURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR TORSION BAR SUPPORT AT FRAME 61 CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SUPPORT IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105408Attach Angle · crackedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT SIDE FUSELAGE TO VERTICAL STABILIZER FORWARD ATTACH ANGLE CRACKED NEAR 3RD RIVET FROM AFT EDGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SIDE FUSELAGE TO VERTICAL STAB FORWARD ATTACH SDR SIMA201105407Attach Angle · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT SIDE FUSELAGE TO VERTICAL STABILIZER, FORWARD ATTACH ANGLE CRACKED NEAR 3RD RIVET FROM AFT EDGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED VERTICAL STABILZER L ANGLE TO FUSELAGE FORWARD SECTION IAW EO EM53MSDR SIMA201105406Fitting · crackedDURING MAINTENANCE BASE VISIT FOUND SHEAR CLIP AT FRAME 73, BETWEEN STRINGER 9 AND 10 RIGHT CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SHEAR CLIP AT FRAME 73 BETWEEN STR'S 9 AND 10R IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TSDR SIMA201105404Frame · damagedDURING MAINTENANCE BASE VISIT FOUND RIVET HOLES FOR FAIRLEAD AT FRAME 55 ELONGATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 55 IAW EO EM-53MR-1772. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105403Frame · crackedDURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED IN 2 PLACES ON THE RIGHT SIDE AT FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 RIGHT SIDE IAW EO EM-53MR-1771. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105402Fitting · gougedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPER FITTING GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105401Fitting · damagedDURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON DAMPER FITTING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201105301Fitting · gougedDURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT AILERON DAMPNER AND PCA FITTINGS DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AILERON DAMPNER AND PCA FITTINGS IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201104801Flashlight · lowON FLIGHT 4555 THE FIRST OFFICERS FLASHLIGHT WAS FOUND TO BE DIM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SESDR CHQA201100037Connector · looseCREW REPORTED THAT ON APPROACH WHEN THE LANDING GEAR WAS SELECTED DOWN, THERE WAS A RED NOSE LANDING GEAR INDICATION AND A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. THE GEAR WAS RETRACTED AGAIN AND THEN EXTENDED WITH NO FURTHER DIFFICULTIES. THE AIRCRAFTSDR SIMA201104602Floorbeam · corrodedDURING MAINTENANCE BASE VISIT FOUND THE CENTER FLOORBEAM CORRODED AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED DAMAGED AREA BY PERFORMING CUTOUT AND INSTALLING A DOUBLER IAW EO EM-53MR-1767. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CHQA201100035Handle · misinstalledDURING AN INSPECTION, THE LEFT OVERWING EMERGENCY EXIT HATCH UPPER HANDLE WAS FOUND TO BE INSTALLED UPSIDE DOWN. MAINTENANCE REMOVED THE HANDLE AND RE-INSTALLED IT IN THE CORRECT ORIENTATION WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100034Light · inoperativeDURING INSPECTION, THE LEFT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE LEFT AFT EMERGENCY EXIT LIGHT WITH NO FURTHER DEFECTS NOTED.SDR CHQA201100113Skin · dentedDURING INSPECTION A DENT WAS FOUND ON THE LOWER FORWARD FUSELAGE BETWEEN FR19 AND FR20 ON STR 21L AND 21R. MAINTENANCE BLENDED THE GOUGE IAW 51-10-03 AND PERFORMED A HIGH FREQUENCY EDDY CURRENT INSPECTION IAW 51-10-03, WITH NO CRACK FOUND. THE DENT WAS REPAI
Back to Embraer EMB-135KL