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 SIMA200832201Power Supply · unknownON FLIGHT 3023 CREW REPORTED EXIT SIGN FWD OF SEAT 3 B/C AND FLOOR PROX STRIPS FORWARD OF ROW 6 ARE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NUMBER 2 IAW EMB -140 AMM 33-50-04, OPERATION CHECK GOOD. AIRSDR SIMA200831502Unlock Cylinder · malfunctionedON FLIGHT 4662 CREW REPORTED THAT GEAR FAILED TO RETRACT DURING TAKE OFF. AIRCRAFT RETURNED TO FIELD. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED UNLOCK BOX IAW EMB AMM B32-33-10. PERFORMED EXTENSION AND RETRACTION IAW AMM 32-30-00, OPERATIONAL CHECK GOODSDR SIMA200830101Relay · failedFLIGHT 4886 - CREW REPORTED WHEN ANTI-ICE TURNS ON IT GETS VERY HOT IN THE COCKPIT WITH A SMELL OF MELTING PLASTIC AND UNABLE TO BRING TEMP DOWN TILL ANTI-ICE TURNS OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RELAYS K0186 CAPT RECIRC AND K0321 CSDR SIMA200829801Inverter · inoperativeFLIGHT 3852 - CREW REPORTED CABIN EMERGENCY LIGHTING FLOOR STRIP AT SEATS 1 AND 2 INOPERATIVE AT THE MOST FORWARD STRIP. CREW RESET AIRCRAFT POWER NO CHANGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED & REPLACED NR 2 BATTERY POWER SUPPLY IAW EMB AMM 33-50-04, NSDR SIMA200829403Battery Pack · dischargedON FLIGHT 4606 CREW REPORTED SEVERAL EMERGENCY LIGHTS NOT WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY PACK IAW EMB AMM 33-50-04, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200829103Charger · defectiveCREW REPORTED ON FLIGHT 4247 EMERGENCY LIGHT AT MAIN CABIN DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY AS PER EMB AMM 33-50-04 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200829102Inverter · defectiveCREW REPORTED ON PRE FLIGHT THAT THE EMERGENCY EXIT SIGN IN CABIN CEILING ONLY ILLUMINATING ON FWD FACE DURING TEST. AFT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 AC/DC POWER INVERTER IAW EMB AMM 33-50-11, OPERATIONAL CHECK GOOD.SDR CHQA200800191Hose · looseON INITIAL CLIMBOUT, THE FLIGHT CREW RECEIVED A HYD SYS 1 LO QTY EICAS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP ON THE MFD AND THE HYDRAULIC SYS 1 INDICATED IN THE AMBER RANGE AND THE PRESSURE WAS FALLING. WHILE FOLLOWING THE QRH IT WAS NOTED THAT THE NOSE GSDR CHQA200800190Trim System · malfunctionedAFTER ROTATION ON TAKE-OFF, THE FLIGHT CREW RECEIVED A MAIN PATCH TRIM INOPERATIVE MESSAGE ON EICAS. THE BACK TRIM SYS FUNCTIONED NORMALLY AND TERE WAS NO RUN-AWAY TRIM SITUATION. THE QRH WAS FOLLOWED BUT THE MAIN TRIM WOULD NOT OPERATE. THE AIRCRAFT LANDED BSDR SIMA200828001Actuator · corrodedWHILE PERFORMING BACKLASH INSPECTION PER AMM WHILE AIRCRAFT WAS IN MAINTENANCE IT WAS DISCOVERED THAT BOTH THE MAIN LANDING GEAR MANEUVERING ACTUATORS HAD BACKLASH PLAY BEYOND LIMITS OF AMM. IT WAS DETERMINED THAT THE PLAY WAS THE RESULT OF CORROSION. ACTUATSDR SIMA200830501Proximity Switch · faultyON FLIGHT 3116 CREW REPORTED AFTER RETRACTING LANDING GEAR CAPTAIN AND FLIGHT ATTENDANT FELT AND HEARD LOUD THUMPING NOISE 4 TIMES. CREW ALSO NOTED LEFT RUDDER PEDAL VIBRATED. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO FIELD. AIRCRAFT REMOVED FROM SDR SIMA200827301Engine · smokeON FLIGHT 3540 DURING CLIMB OUT AT APPROX FL180 CREW DETECTED SMOKE IN THE COCKPIT FOLLOWED BY A LAV SMOKE INDICATION. CREW CONFIRMATION SMOKE IN THE CABIN. CREW THEN NOTICED A LOW OIL QUANTITY ON THE NR 1 ENG (3QTS) AND COMPLETED A PRECAUTIONARY ENGINE SHUTSDR CHQA200800184Carbon Seal · leakingFLIGHT 5286, STL TO RDU. WHILE CLIMBING THROUGH FL240 THE FLIGHT CREW RECEIVED A E2 LOW OIL PRESSURE EICAS MSG. WHEN THE ENGINE PAGE WAS BROUGHT UP ON THE DISPLAY E2 SHOWED 4 QUARTS OF OIL. THE CREW FOLLOWED THE QRH AND PULLED POWER BACK TO 88% WITH NO CHANSDR SIMA200826802Light · burnedON FLIGHT 4354 CREW REPORTED ON ARRIVAL THAT THE FLIGHT ATTENDANT SMELLED SMOKE COMING FROM LAV AREA NEAR THE ELT. CREW CONFIRMED SMELL BUT NO VISIBLE SMOKE. ACFT REMOVED FROM SERVICE. C/A FOUND FLUORESCENT BULB ABOVE TOILET WITH BURNT SOCKET. REMOVED BULBSDR SIMA200826602Unknown · vibrationON FLIGHT 4108 CREW REPORTED A FLUTTER/VIBRATION IN THE FLIGHT CONTROLS DURING ALL PHASES OF FLIGHT. STARTED AT 150KTS, VIBRATION FELT WITH GEAR IN UP OR DOWN POSITION. VIBRATION FELT WITH AUTO PILOT ON AND OFF, PACKS ON, CREW NOTED THE VIBRATION THROUGH FLISDR SIMA200826801Floor Support · corrodedDURING CPCP INSPECTION FOUND OMEGA BEAM SSI 53-20-11 CORRODED. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10 BY REMOVING CORROSION AND INSTALLING A DOUBLER OVER THE CUTOUT AREA. ACFT RETURNED TO SERVICE.SDR SIMA200826606Beam · corrodedDURING MBV INSPECTION THE CENTER BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE AL2024T3 .071 FILLER AND 2 SHIMS. DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 51-00-10. ACFT RETURNED TO SERSDR SIMA200826605Floor Support · corrodedDURING MBV INSPECTION THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE (AL2024T3.050), FILLER (AL2024T3.050) AND 2 SHIMS (AL2024T3.040). DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRSDR CHQ2008F00011Socket · burnedDURING CRUISE, THE FLIGHT CREW RECEIVED A PITOT 1 INOP EICAS MESSAGE AND SMELLED SMOKE. IMMEDIATELY AFTER THEY RECEIVED AN AOA 1 HEAT INOP MESSAGE AND THE FLIGHT INSTRUMENTS ON THE CAPTAIN`S PFD BEGAN TO GIVE ERRONEOUS INDICATIONS. THE FLIGHT CONTROLS WERE TRASDR SIMA200826103Floor Support · corrodedDURING A MBV INSPECTION. A PREV REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. MARKED, DRILLED AND CLEANED REPAIR PARTS. REPAIR DONE IAW SRM145SDR SIMA200826102Battery · dischargedON FLIGHT, CREW REPORTED EMERGENCY LIGHTS ON FLOOR AND EXIT SIGNS WILL NOT ILLUMINATE. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 BATTERY PACK IAW WORK CARD NR 33-700-19. OPERATIONAL CHECK GOOD AT THIS TIME. ACFT RETURNED TO SERVICE. (K)SDR CHQ2008F00006Unknown · smokeWHILE CLIMBING THROUGH 8,000 FT THE FLIGHT CREW WAS INFORMED OF SMOKE OR STEAM COMING FROM THE FLOOR OF THE CABIN BY THE F/A. THE QRH CHECKLISTS WERE COMPLIED WITH AND THE AC LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE FAULT WHESDR SIM2008F00024Switch · failedAT CRUISE CREW REPORTED TANK 1 FUEL QUANTITY WENT FROM DASHES TO 0 IN FLIGHT. CREW DECLARED FUEL EMERGENCY TO GET PRIORITY HANDLING. ACFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IN REF TO FIM 27-43-0-810-802-A REMOVED AND REPLACED BACK UP SYSTEM CUT OUSDR CHQA200800173Solenoid · faultyFLIGHT 5325 ICT TO STL. THE FLIGHT CREW REPORTED A LOUD AIR SOUND FROM THE NLG AREA DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE NLG DOOR COMMAND CIRCUIT BREAKER TRIPPED. THROUGH FURTHER TROUBLESHOOTING, IT WAS FOUNDSDR CHQ2008F00005Light · malfunctioned2 FLOOR LEVEL LIGHT STRIPS WERE REPORTED TO NOT ILLUMINATE WHEN TESTED. MX OPS CHECKED THE LIGHTS IN ACCORDANCE WITH EMB AMM 33-50-00 WITH NO DEFECTS NOTED.SDR CHQ2008F00004Fuel Control · failedFLIGHT 5346, STL TO MSY. WHILE ON DESCENT INTO MSY, AT APPROXIMATELY FL285 THE FLIGHT CREW NOTICED ABNORMAL INDICATIONS ON EICAS FROM E2. THE N1 INDICATIONS WERE INCREASE AND DECREASING RAPIDLY BUT WERE STAYING WITHIN LIMITS AS WELL AT THE ITT. IT WAS ALSO SDR CHQA200800163Control Panel · intermittentFLIGHT 5302, STL TO AUS - DURING CRUISE THE CREW RECEIVED AN ELECTRICAL ABNORMAL MESSAGE. THE ELECTRICAL STATUS PAGE WAS CHECKED AND FOUND THAT THE BATTERIES WERE NOT CHARGING. THE CREW FOLLOWED THE QRH AND STARTED THE APU BUT THE MESSAGES DID NOT CLEAR. THSDR SIMA200822402Solenoid Valve · failedON FLIGHT 3111 CREW REPORTED FLYING AT 11,000. AT 310KTS A LOUD BANG WAS HEARD FROM NOSE AREA AND THEN A LOUD ROAR UNTIL LANDING GEAR WAS DOWN AND LOCKED, 3 GREEN AND NO CMC INDICATIONS WITH NO EICAS MESSAGES. EMERGENCY WAS DECLARED. LANDING WAS NORMAL. ACSDR SIMA200822204Valve · failedON FLIGHT 4600 CREW REPORTED UPON TOUCHDOWN ALL FOUR BRAKES LOCKED AND ALL FOUR TIRES BLEW OUT. THE WHEEL RIMS WERE GROUND AWAY AND CAUSED A LOT OF SPARKS AND FLAMES. THE TOWER CALLED CRASH, FIRE RESCUE AND REPORTED AN ACFT FIRE. THE PASSENGERS PERFORMED ANSDR CHQA200800160Acm · seizedFLIGHT 5285, BDL TO STL. SHORTLY AFTER TAKEOFF WHILE PASSING THROUGH 2000 FT THE FLIGHT CREW NOTICED SMOKE IN THE COCKPIT ALONG WITH A LIGHT HAZE. THE ODOR AND HAZE WAS CONFIRMED BY THE FLIGHT ATTENDANT. THERE WERE NO FIRE WARNINGS OR EICAS MESSAGES. THE HSDR CHQA200800158Proximity Sensor · faultyFLIGHT 5360, STL TO ATL. DURING CLIMB, AFTER RETRACTING THE LANDING GEAR, THE FLIGHT CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS ALONG WITH AURAL WARNINGS FOR FLAPS AND TRIM. THE FLIGHT LEVELED OFF AND THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED. THE SDR SIMA200821002Sill · corrodedDURING MBV INSPECTION THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL, TREATED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A)SDR CHQ2008F00001Light · inoperativeMAINTENANCE FOUND THE EMERGENCY PROXIMITY LIGHT FORWARD OF THE WING EXIT TO BE INOPERATIVE. THE EMERGENCY LIGHT STRIP WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. (S)SDR CHQ2008F00000Windshield · crackedFLIGHT 5349, MSY TO STL. DURING CRUISE THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND NOTICED THAT THE FIRST OFFICER’S WINDSHIELD HAD CRACKED. THE FLIGHT THEN DIVERTED TO CGI WHERE THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS THEN FERRIED TO STL WHERE TSDR SIMA200820704Switch · malfunctionedON FLIGHT 3888 DURING CRUISE CREW REPORTED PARKING BRAKE LIGHT ON INDICATION WHILE IN FLIGHT SUBSEQUENTLY ON THE GROUND. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO PRESSURE NOTED ON PARKING BRAKE WHILE RELEASED. REPLACED PRESSURE SWITCH EMERGENSDR SIM2008F00019Squat Switch · failedON FLIGHT, CREW REPORTED A LG AIR/GRD FAIL ANNUNCIATION AFTER TAKEOFF. LANDING GEAR HANDLE STUCK IN DOWN POSITION. OTHER ANNUNCIATIONS INCLUDED 1-2 WOW INOP AND SPS ADVANCED. AC RETURNED TO FIELD. AC REMOVED FROM SERVICE. REMOVED AND REPLACED NLG WOW SWITSDR SIM2008F00017Floor Support · corrodedDURING MBV A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THAT EXISTING REPAIR DOUBLER AND CLEANED THE AREA. POSITIONED, MARKED, DRILLED, TREATED AND INSTALLED NEW REPAIR DOUBLER PN EPNEM53EP54701. REPAIRS PERFORMED IAW SRM 53SDR SIMA200820305Sill · corrodedDURING MBV THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A)SDR SIMA200820302Fire Loop · malfunctionedON FLIGHT 4278 UPON LANDING CREW REPORTED, AN ENGINE 1 FIRE INDICATION. NO EMERGENCY DECLARED AND FIRE BOTTLE WAS NOT DISCHARGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE FIRE DETECTION LOOP IAW EMB 140 AMM 26-11-01. FIRE DETECTISDR SIMA200819902Battery Pack · dischargedON FLIGHT 3643 CREW REPORTED EMERGENCY LIGHTING INOPERATIVE ON PREFLIGHT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 AND 4 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECKS GOOD. AFT RETURNED TO SERVICE. (S)SDR SIM2008F00004Wire Harness · corrodedCREW REPORTED ON CLIMB OUT THAT THEY RECEIVED LDG AIR/ GROUND FAIL MESSAGE AFTER THEY RETRACTED GEAR. GOT 3-GREEN LIGHTS. LND/AIR GROUND MESSAGE DID NOT GO AWAY WHEN GEAR LEVER WAS RETRACTED. T/R DISAGREE MESSAGE ON EICAS BUT MESSAGE WENT AWAY WHEN GEAR WASSDR SIM2008F00003Brake Assy · disintegratedON FLIGHT 3127, CREW REPORTED ON TAXI OUT THE BRAKE DEGRADE/BRAKE LO PRESS AND HYD SYS 2 AT BOTTOM OF YELLOW BAND AND EVIDENCE OF HYDRAULIC LEAK AT RT MAIN LANDING AREA. AIRCRAFT REMOVED FROM SERVICE C/A: INSPECTED AND FOUND NR 3 BRAKE HAD DISINTEGRATED REMOVSDR SIM2008F00002Landing Gear · malfunctionedON FLIGHT 3394, CREW REPORTED ON CLIMBOUT THAT THE GEAR WOULD NOT RETRACT WITH A GEAR LEVER DISAGREE MSG ON EICAS NO CMC MESSAGES. AIRCRAFT LANDED WITHIN WEIGHT LIMITS AND NO EMERGENCY WAS DECLARED. ACFT REMOVED FROM SERVICE. OPS CHECK FOR LG/LEVER DISAGREEMSDR SIMA200818401Proximity Switch · inoperativeON FLIGHT 4431 - CREW REPORTED AFTER TAKEOFF LDG AIR/GND FAIL EICAS MESSAGE AND THE LANDING GEAR WILL NOT RETRACT. CREW ELECTED TO DIVERT TO ALB. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR AIR/GROUND PROX SWITCH PER EMB 140 AMM 32SDR SIMA200816503Sill · corrodedDURING A MBV INSPECTIONS, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED WITH LEVEL TWO CORROSION. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED AND DRILLED NEW PART, CLEANED AND INSTALLED, WORK DONE IAW EMB 145 SRM (SRM EMB 14511142 REV SDR SIMA200816504Floorbeam · corrodedDURING A MBV INSP, THE GALLEY FLOOR CENTER BEAM AT FR 20 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. PERFORMED CUT OUT OF THE CENTER BEAM TO REMOVE THE DAMAGE. FAB A DOUBLER, DRILLED, APPLIED PREVENTIVE AND INSTALLED. WORK DONE IAW EMB 145 SRM (SRM EMB-145SDR SIMA200815105Sill · corrodedDURING A MBV INSPECTION, FOUND CARGO DOOR SLLL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL, DRILLED AND ALODINED NEW PART. INSTALLED NEW SLLL IAW EMB SRM (SRM145/1142 REV. 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200815104Sill · corrodedDURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL. CLEANED AND ALODINED NEW SLLL AND INSTALLED IAW EMB 145 SRM (SRM EMB-14511142 REV 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200814303Engine · malfunctionedON FLIGHT 3882, DURING TAKEOFF CREW REPORTED THERE WAS A VERY PRONOUNCED EXCESSIVE VIBRATION DURING TAKEOFF ROLL AND DURING GEAR RETRACTION FROM NOSE GEAR. DURING TAKEOFF DEADHEAD EMJ CAPTAIN REPORTED 3 LOUD BANGS SIMILAR TO A COMPRESSOR STALL ON TAKEOFF. MOSDR SMIA200812904Floor Support · corrodedON MBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION AT CROSS MEMBER FRAME 25. REPAIRED OMEGA BEAM IAW SRM 53-00-10 FIG 202. AIRCRAFT RETURN TO SERVICE.
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