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 SIMA200422409Floor Support · corrodedDURING AN IMBV INSPECTION, THE GALLEY CENTER OMEGA BEAM WAS FOUND CORRODED BEYOND SRM LIMITS. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR STATEMENT IC2004-145/3307A, PARA 1 DATED JULY 23, 2004. (M)SDR C2XA04TY141Selector · defectiveCLE - UPON GEAR RETRACTION OF FLIGHT 2127 THE LANDING GEAR AURAL WARNING INDICATION CAME ON. REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB 135/145 AMM 27-51-03. OPS CHECKS WERE GOOD OF THE FLAPS AND LANDING WARNING SYSTEM IAW EMB AMM 27-50-00 AND 32-6SDR C2XA04SH465Floorbeam · corrodedDURING (C) CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10, STEP 2 FIG. 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH471Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAME 35 AND 39. MAINTENANCE REMOVED THE DAMAGED AREA AND FOUND IT TO BE GREATER THAN 30 PERCENT OF ORIGINAL MATERIAL THICKNESS, BUT WITHIN REPAIRABLE LIMITS. A DYE PENETRANT INSPECTIONSDR C2XA04SH464Floorbeam · corrodedDURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20040502Control Unit · inoperativeLGA - FLT 5023 - CREW ABORTED TAKEOFF AT 100 KTS DUE OT CONFIG WARNING FOR TRIM. TRIM INDICATED 7 UNITS ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICESDR SIMA200420101Pitot System · contaminatedDUIRNG CRUISE FLIGHT, NR 1 ENGINE LOST POWER, REGAINED POWER TWO TIMES, THEN RAN NORMALLY. AFTER LANDING NR 1 ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. PERFORMED TROUBLESHOOTING IAW FAULT ISOLATION MANUAL AND FOUND WATER IN BOTH PITOT SYSTEMS. DRAINED PITSDR SIMA200419706Plate · corrodedDURING A CPCP INSPECTION, MAINTENANCE FOUND THE CABIN INTERIOR STRUCTURE FORWARD RIGHT SERVICE DOOR SIDE JUNCTION PLATE FOR FLOORBEAM CONNECTION HAS CORROSION. INSTALLED NEW JUNCTION PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA04IA081Rotary Switch · inoperativeIAH - FLIGHT 3407, DURING CLIMBOUT OF IAH THE CREW REPORTED AN EMERGENCY ELECTRICAL ABNORMAL TRANSFER CAUTION INDICATION, APU AUTO-SHUTDOWN IN FLIGHT, AND EMERGENCY LIGHTS ON. THE CREW RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RSDR SIMA200419702Gusset · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR CENTER SUPPORT BEAM AT FRAME 19 CORRODED. REMOVED AND REPLACED GUSSETT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419705Threshold · corrodedSAW - DURING AN IMBV INSPECTION, MAINTENANCE FOUND THE INTERIORS STRUCTURE RIGHT SERVICE DOOR ENTRANCE THRESHOLD TO HAVE CORROSION. INSTALLED NEW RIGHT SERVICE DOOR THRESHOLD IAW EMB SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419703Beam · corrodedDURING A CPCP INSPECTON, MAINTENANCE FOUND CORROSION ON CENTER HAT BEAM AT FRAME 20. REMOVED AND REPLACED HAT BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419704Support · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND CABIN INTERIOR FORWARD STRUCTURE CENTER SUPPORT AT FRAME 17 CORRODED. REMOVED AND REPLACED CABIN INTERIOR FORWARD STRUCTURE SUPPORT TEE FRAME 17 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200419701Bracket · corrodedSAW - DURING A CPCP INSPECTION, MAINTENANCE FOUND INTERNAL FUSELAGE JUST INSIDE PASSENGER DOOR, TWO BRACKETS HAVE CORROSION. REMOVED AND REPLACED BRACKETS P/N 145-24131-005, 145-24131-007, IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA04TY099Threshold · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PASSENGER ENTRY DOOR THRESHOLD PLATE. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD PLATE IAW EMB SRM 51-21-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA04SH377Floorbeam · corrodedDURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 14. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 55320-01125. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200417202Control Unit · inoperativeNAS - FLT 4739 - DURING TAKEOFF ROLL THRUST LEVERS AT THRUST SETTING, SPOILER DEPLOYED UNCOMMANDED. CREW REPORTED A TAKEOFF MISCONFIG MESSAGE AND WHLE TAXIING BACK TO GATE RECEIVED DAU 1 MISCOMPARE. MAINTNENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT SDR C2XA04SH374Bracket · corrodedSHV - DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH373Bracket · corrodedSHV - DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH372Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT FORWARD BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 20 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH371Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 135 SRM 53-21-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH370Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH369Buttstrap · corrodedDURING C-CHECK THE CENTER FLOORBEAM BUTTSTRAP (AFT DIGITAL) WAS FOUND TO BE CORRODED AT FRAME 18. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH368Sill · corrodedDURING C-CHECK THE LEFT FLOOR SILL WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH367Sill · corrodedDURING C-CHECK THE LEFT HAND CARGO SILL WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH366Firewall · crackedDURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH365Stringer · corrodedDURING C-CHECK THE UPPER STRINGER ON THE CENTER FLOORBEAM BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200416701Connector · looseBGR - FLT 4655 - EMERGENCY EXIT LIGHT ON AFT GALLEY BULKHEAD INOPERATIVE. RESECURED LOOSE CONECTOR OVER GALLEY CEILING LIGHT. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M)SDR CHQA000505Manifold · malfunctionedUPON LANDING INTO DFW FROM FLIGHT 6490, AIRCRAFT WAS PULLING TO THE RIGHT AND THERE WAS NO LEFT RUDDER RESPONSE. THE AIRCRAFT VEERED OFF RUNWAY AND WAS STUCK IN MUD. NO APPARENT DAMAGE TO THE AIRCRAFT. AFTER RECOVERING THE AIRCRAFT AND INVESTIGATING THE PROSDR SIMA200415802Light · malfunctionedRDU - FLT 4634 - DURING CRUISE FLIGHT, CREW REPORTED THE EMERGENCY LIGHT ILLUMINATED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. NO MESSAGES WERE FOUND ON THE CMC. AN OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS THEN RETURNED TO SESDR SIMA200415402Display · inoperativeDCA - FLT 4753 - CREW REPORTED SMOKE SMELL AND NR 2 PFD WENT BLANK. REPLACED NR 2 MFD IAW EMB AMM 34-22-00-700-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M0SDR SIMA200415301Charger · inoperativeDCA - FLT 4606 - EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT 9A. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AND CHARGER IAW EMB 135 AMM CH 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CHQA000499Connector · disconnectedROW 1 EXIT LOCATOR SIGN IS INOP. RECONNECTED CONNECTOR PLUG IAW AMM 33-50-15. OPS CHECK GOOD.SDR SIMA200414602Stringer · crackedAIRCRAFT STRUCK BY GPU ON RT SIDE JUST AFT OF RADOME. REPLACED 2 SKIN PANELS, 1 STRINGER, AND 1 FRAME. IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406972)SDR SIMA200414601Power Supply · inoperativeTOP AND LOWER LT EXIT LIGHTS ON SERVICE DOOR WILL NOT REMAIN ILLUMINATED. REPLACED NR 2 BATTERY POWER SUPPLY. AC RETURNED TO SERVICE. (SW21200407048)SDR SIMA200414402Computer · failedIN CRUISE AT FL 290 CAPTAIN MULITFUNCTIONAL DISPLAY AND EICAS FAILED WITH BURNING ODOR. DIVERTED, OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200407047)SDR SIMA200413201Engine · malfunctionedPWM - FLT 4645 - A/C LEVEL AT 21K FT JUST ABOUT TO SET CRUISE MODE FELT YAW AND HEARD LOUD BANG NOISE. NR 1 ENGINE UNCOMMANDED SHUTDOWN. AIRCRAFT DECLARED EMERGENCY AND LANDED IN PWM. REPLACED NR 1 ENGINE ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERSDR C2XA04CL051Solenoid Valve · faultyCLE FLIGHT 2234 THE CREW REPORTED NOISE AND VIBRATION COMING FROM THE NOSE OF THE AIRCRAFT. RECYCLED LANDING GEAR WITH NO CHANGE. AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, FOUND NOSE GAER DOORS WOULD NOT CLOSE. REMOVED AND REPLSDR C2XA04TY080Plate · corrodedTYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-01 AND CPM 51-21-04,05,06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA04TY079Floorbeam · corrodedTYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP. MAINTENANCE REMOVED AND REPLACED THE TOP CAP IAW EMB SRM 51-30-01, 51-20-03, 51-60-02, CPM 51-21-04, 51-21-06, 51-21-06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETIONSDR C2XA04TY078Plate · corrodedTYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT DIGITAL PLATE AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE AFT DIGITAL PLATE IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR CHQA000491Light · inoperativeMAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT BULB IAW 135 AMM CH 33-50-10-4. OPS CHECKED GOOD.SDR CHQA000489Light · inoperativeLEFT SIDE FUSELAGE UPPER EMERGENCY LIGHT INOP. OPS CHECKED GOOD IAW E33-50-00-710-001.SDR C2XA04TY077Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE MOUNTING SURFACE FOR PASSENGER SEAT TRACK NR LF1. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02, CPM 51-14-00. THE AIRCRAFT WILL BE RELEASED UPON COMPLETIOSDR C2XA04TY076Floorbeam · corrodedTYS-DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE LEFT HAND OMEGA BEAM TOP CAP AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE OMEGA BEAM TOP CAP IAW EMB SRM 51-40-02. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR SIMA200412702Apu · failedRIC - FLT 4507 - DURING TAXI CREW RECEIVED APU GEN OFF BUSS MESSAGE. RESET GENERATOR WHILE PARKING AIRCRAFT. DC BUSS FAILED CAUSING NUMEROUS ELECTRICAL WARNINGS AND NOTICED SMOKE FROM RIGHT SIDE OF AIRCRAFT. APU SHUTDOWN AND FIRE BOTTLE EXTINGUISHED. SMOKE SDR SIMA200412704Odor · detectedJFK - FLT 4754 - DURING CLIMB, CREW REPORTED A STRONG BURNING ODOR IN COCKPIT. AIRCRAFT WAS RETURNED TO JFK AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN OPERATIONAL CHECK OF THE PACKS WAS GOOD AND AIRCRAFT WSDR C2XA04BT055Cable · bindingCREW REPORTED, FLAP FAIL INFLIGHT DURING DESCENT AT APPROXIMATELY 9000 MSL, APPROXIMATELY 240 KNOTS, SPEED BRAKE DEPLOYED OPEN. FLAP INDICATOR ON EICAS AMBER WITH DASHED LINE. QRH FLAP FAILURE CHECKLIST COMPLETED. ZERO FLAP LANDING PERFORMED. MAINTENANCE RSDR SIMA200412001Battery Pack · dischargedCREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY THE FIRST FOUR ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406977)SDR C2XA04BT053Smoke Detector · faultyCREW REPORTED, LAV SMOKE WARNING AFTER TAKEOFF FROM NEWARK, CONDITION CLEARED WHEN CIRCUIT BREAKER PULLED PER QRH, WITH SMELL IN THE CABIN. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB135 AMM 26-14-01. OPS CHECKED GOOD. NO SMOKE NOTED.
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