Embraer EMB-145LR
Service difficulty reports · 36,797
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 = 'EMB145LR' 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 = 'EMB145LR' 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 SIMA20150130006Wire · brokenCABIN AISLE FLOOR EMER LIGHT STRIP NR 5 WIRES BROKEN OFF. R & R CABIN AISLE FLOOR EMER LIGHT STRIP NR 5 IAW AMM 33-50-12.SDR SIMA20150130011Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IS CRACKED, 1/2" LONG. REPAIRED RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE NR 4 IAW ETN-EM-53-142.SDR NE2R2015FA0000071Housing · cutTHE GENERATOR WAS RETURNED FOR O/H. DURING THE TEAR DOWN AND INSPECTION OF THE GENERATOR IT WAS DISCOVERED THAT THE HOUSING HAD A DEEP CUT IN IT THAT APPEARED TO HAVE BEEN REPAIRED USING SOME SORT OF BONDING MATERIAL. THE CUT WAS APPROXIMATELY 3.25" LONG ANDSDR UHLA2015013000107Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM FLANGE ON THE LT SIDE ON THE CENTER OMEGA AT FRAME 23. THE ANGLE WAS REPLACED IAW ETD 2015-145-012887.SDR UHLA2015013000105Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN BETWEEN FRAMES 61 AND 62 AND STRINGERS 21L AND 21R. THE SKIN WAS REPAIRED IAW SRM 53-31-01.SDR UHLA2015013000103Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER CARGO DOOR STOP. THE FRAME SECTION WAS REPLACED IAW SRM 53-31-04 AND SRM 51-40-02.SDR UHLA2015013000102Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER ON THE LEFT OMEGA BEAM AT FRAME 20. THE DOUBLER WAS REPLACED IAW SRM 51-40-02.SDR SIMA20150130003Skin · crackedRIGHT FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACKS AROUND 3 FASTENERS ON FRAME 75 BETWEEN STRINGER 2R & 3R. ACCOMPLISHED PERMANENT REPAIR OF RT FUSELAGE EXTERNAL SKIN FRAME 75 BETWEEN STRINGER 2R & 3R IAW ERS-EM-53MR-1023. SEE WIPS & TASKS FOR DETAILS.SDR SIMA20150130002Light · inoperativeDURING PS 2 CHECK, FOUND RT OVERWING EMER LIGHT INOPERATIVE. R & R RT OVERWING EMER LIGHT BULB IAW AMM 33-50-07. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR UHLA2015012900106Skin · dentedDURING INSPECTION, A DENT IN ZONE 311 AT FRAME 79 AND STRINGERS 6L AND 8L WAS FOUND. THE DENT WAS REPAIRED IAW SRM 51-40-02 AND SRM 53-32-01.SDR SIMA20150129005Light · inoperativeNUMBER 1 EMER AISLE LIGHT STRIP INOPERATIVE. R & R NR 1 EMER AISLE LIGHT STRIP IAW AMM 33-50-12. OPERATIONS CHECKED GOOD. FOUND DURING CLOSE UP.SDR RAIA201501290001Bulb · inoperativeLEFT OVERWING EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BULB, OPS CHECKED GOOD.SDR SIMA20150129002Light · inoperativeRIGHT AFT OVERWING EXTERNAL EMER LIGHT INOPERATIVE. R & R RT AFT OVERWING EXTERNAL EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.SDR SIMA20150129001Warning System · false activationUPON ENTERING THE AIRPLANE TRIPLE CHIME HEARD & LAVATORY SMOKE ON EICAS OBSERVED. OPERATIONS CHECK LAVATORY SMOKE. OPERATIONS CHECKED GOOD 26-14-00.SDR SIMA20150128014Support · crackedCARGO DOOR CUP SUPPORT AT FRAME 68 IS CRACKED AT THE LOWER LOCK FASTENER. CRACK IS .25 INCHES LONG.SDR SIMA20150128008Support · crackedLEFT PYLON PRE-COOLER FWD BRACKET SUPPORT ASSEMBLY IS CRACKED. R & R LT PYLON PRE-COOLER FWD BRACKET SUPPORT ASSEMBLY IAW SRM 51-40-02 & ETN EM-54-056.SDR SIMA20150128009Attach Angle · crackedRIGHT OMEGA BEAM INBD ATTACH ANGLE CRACKED BETWEEN FRAMES 47 & 48. REPAIRED RT OMEGA BEAM INBD ATTACH ANGLE BETWEEN FRAMES 47 & 48. BRACKET PN 140-04214-609 IAW SRM 53-23-02.SDR UHLA2015012800057Connector · unsecureDURING INSPECTION, THE FLOOR PROXIMITY STRIP EMERGENCY LIGHT AT ROWS 17 AND 18 WAS FOUND TO BE INOPERATIVE. MAINTENANCE SECURED A LOOSE CONNECTOR. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.SDR ASOA20150128005Transducer · faultyPILOT REPORTED AN INTERMITTENT LOSS OF BRAKES ON LANDING WITH BRAKES DEGRADED EICAS MESSAGE. MX R & R NR 3 WHEEL SPEED TRANSDUCER WITH OPS CHECK GOOD. AC WAS APPROVED FOR RETURN TO SERVICE.SDR RAIA201501280001Outflow Valve · failedLOSS OF CABIN PRESSURE IN FLIGHT, MADE UNSCHEDULED LANDING. MAINTENANCE INSPECTED ACFT AND SAFE FOR 1 TIME FERRY FLIGHT. MAINTENANCE REPLACED GROUND AIR VALVE, OPS CHECK GOOD.SDR ASOA20150128008Light · smokeTHE CREW REPORTED SMOKE IN CABIN COMING FROM VICINITY OF SEAT 4A. MAINTENANCE INSPECTED AND REPLACED SEAT 4A SIDEWALL CABIN LIGHT ASSY. OPS CHECKS WERE GOOD.SDR SIMA20150128005Flashlight · defectiveAFT CABIN FLASHLIGHT INDICATES NORMAL CHARGING BUT DOES NOT HOLD A CHARGE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16.SDR SIMA20150127009Attach Angle · crackedRIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 1/2" ON THE PREVIOUS REPAIR OF THE LE. RT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1" ON THE PREVIOUS REPAIR OF THE TE. INSTALLED NEW ANGLES IAW ETN-EM-53?142.SDR SIMA20150127007Life Vest · unserviceableRESTORE INFANT LIFE VEST. INSTALLED SERVICEABLE INFANT LIFE VEST.SDR SIMA20150127004Attach Angle · crackedLEFT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IS CRACKED 3/8 INCH ON THE TE. COMPLIED WITH REPAIR OF LT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IAW ETN-EM-53-142.SDR SIMA20150127005Attach Angle · crackedLEFT HAND OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 2 INCHES ON PREVIOUS REPAIR OF THE LE. LEFT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 1 IS CRACKED 1 INCH ON THE PREVIOUS REPAIR OF THE TE. REPAIRED LT LOWER OVERWING TO FUSELAGE LOWESDR SIMA20150127006Bracket · crackedPASSENGER DOOR BRACKET THAT INNER HANDLE TORQUE BOX MOUNTS TO HAS TWO 1/4 INCH CRACKS IN THE AFT UPPER CORNER. REPAIRED PAX DOOR BRACKET THAT INNER HANDLE TORQUE BOX MOUNT TO IAW EO-EM-52MR-250.SDR SIMA20150127003Duct · crackedBURNING SMELL FROM PACK 2 UNDER FLIGHT ATTENDANT CONTROL. IN AUTO MODE UNDER PILOT CONTROL THE SMELL WENT AWAY. REF LOG PAGE 3754935 ITEM 2 RT ENG DUE REPLACEMENT. REF NRWC 620-ORD-02391. END DURING TROUBLESHOOTING OF BURNING SMELL FOUND RT RAM AIR DISTRIBSDR SIMA20150127001Battery · dischargedRIGHT & LEFT AFT EXTERIOR OVERWING EMER LIGHTS INOPERATIVE. R & R NR 4 EPSU BATTERY & CHARGER ASSEMBLY IAW AMM 33-50-04. OPERATIONS CHECKED GOOD IAW AMM 33-50-00. EMER LIGHTING BATTERY PN 2013-1A SN 110790.SDR ASOA20150127015VDoor Sill · corrodedSERVICE DOOR CENTER SILL CORRODED. R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20150126007Structure · secondary damageRIGHT INBOARD FLAP DAMAGED BY TIRE TREAD SEPARATION. TEARS IN SKIN 5 INCHES & 2 INCHES LONG. R & R RT INBD FLAP IAW AMM 27-50-00. OPERATIONS CHECKED GOOD.SDR ASOA20150126007Battery · dischargedDURING ROUTINE MAINTENANCE BOTH EMERGENCY EXIT AFT OVERWING LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.SDR SIMA20150126006Proximity Sensor · failedDURING DESCENT EICAS MSG, SPOILER FAIL, PRESENTED. SPOILERS DID NOT INDICATE OPEN. AOM 1 PROCEDURES COMPLIED WITH. POST FLIGHT INSPECTION FOUND THE RT INBD SPOILER PANEL FLOATING SLIGHTLY UP. NO OTHER DEFECTS NOTED. R & R LT OTBD PROX SWITCH & CONNECTOR ISDR SIMA20150126002Power Supply · inoperativeGATE AGENT REPORTS EMER LIGHTS ON BATTERY DEAD. R & R EMER BATTERY POWER SUPPLY 1 IAW AMM 33-50-04. PERFORMED OPERATIONS CHECK IAW AMM 33-50-04. OK FOR SERVICE. REF ITEM 2, 3 & 4 FOR OTHER POWER SUPPLY REMOVAL.SDR SIMA20150126005Power Supply · failedNUMBER 2 EMER BATTERY POWER SUPPLY REQUIRES REMOVAL IAW ITEM 1. R & R E BATTERY POWER SUPPLY NR 2 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR SIMA20150126003Power Supply · failedNUMBER 4 POWER SUPPLY REQUIRES REPLACEMENT IAW ITEM 1. R & R E BATTERY POWER SUPPLY NR 4 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR SIMA20150126004Power Supply · failedNUMBER 3 POWER SUPPLY REQUIRES REPLACEMENT IAW ITEM 1. R & R BATTERY POWER SUPPLY NR 3 IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. OK FOR SERVICE.SDR SIMA20150126001Potentiometer · failedON LANDING ACFT PULLED HARD TO RIGHT, DID NOT TOUCH TILLER, APPLIED 3/4 FULL LEFT RUDDER PEDAL & BRAKE, ACFT WENT STRAIGHT AT THAT POINT. THEN CAME FULL LEFT RUDDER PEDAL AT APPROX 60KTS TAKING HIGH SPEED. ACFT RESPONDED FINE BUT SEEMED SLUGGISH. TAXI WITH SDR SIMA20150125004Rib · damagedHAIL DAMAGE EVENT, HORIZONTAL STAB RIB 8 HAS ELONGATED HOLE. ACCOMPLISHED REPAIR OF RIB 8 IAW ERS-EM-55MR-235.SDR SIMA20150125003Rib · damagedHORIZONTAL STAB RIB 8 HAS ELONGATED HOLE. ACCOMPLISHED REPAIR OF RIB 8 IAW ERS-EM-55MR-235.SDR RAIA20151250001Engine · malfunctionedNR 1 ENGINE SHUTTERED AND OIL TEMP AND ITT INCREASED, OIL QTY WENT TO 3 AND EICAS SHOWED E1 EXCEEDENCE, ENGINE WAS SHUTDOWN. MAINTENANCE REPLACED NR 1 ENGINE, OPS CHECKED GOOD.SDR ASOA20150125012Firewall · crackedDURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE 5 AND 7 O'CLOCK POSITIONS. MAINTENANCE PERFORMED 2 DOUBLER REPAIRS IAW SRM 53-32-13. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150125011Fitting · wornDURING C-CHECK THE RT AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW EC5760-01044. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150125010Fitting · crackedDURING C-CHECK THE LT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01128. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR UHLA2015012400047Bleed Valve · failedTHE CREW REPORTED THAT THEY RECEIVED A NR 1 BLEED VALVE FAIL MESSAGE AND A STAB ANIT-ICE VALVE FAIL MESSAGE DURING CLIMB OUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE BLEED VALVE. OPS CHECKED GOOD WITHSDR SIMA20150124005Skin · meltedFOUND LT ELEVATOR REPLACEABLE TIP & SURROUNDING SKIN TO BE MELTED NRWC 620-MQT- 02377. PERFORMED PERMANENT REPAIR IAW ERS-EM-55MR-232.SDR SIMA20150124004Battery · dischargedDURING PS 1 INSPECTION FOUND MAIN DOOR EXIT SIGN INOPERATIVE. R & R NR 1 BATTERY & NR 1 CHARGER IAW AMM 33-50-04. OPERATIONS CHECKED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 14895.SDR SIMA20150124002Unknown · malfunctionedSLIP SKID INDICATOR UNCOMMANDED, TOO FAR RIGHT, WE CORRECTED TURN & IT WENT TOO FAR LEFT. NO INDICATION ON EICAS, YAW INDICATION. CORRECT INDICATION ON STANDBY & SLIP SKID. COMPLIED WITH RUDDER MANUAL & AUTH SHUTOFF ADJUSTMENT. TESTED IAW 24-25-00 & YAW TRSDR UHLA2015012300070Attach Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD PASSENGER DOOR ATTACH FITTING BELOW THE HINGE ARM. THE ATTACH FITTING WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-008649.SDR SIMA20150123007Yoke · crackedLEFT ENG FWD LOWER FWD YOKE CRACKED AFT UPPER RADIUS. ACCOMPLISHED REPAIR TO LT PYLON FWD LOWER YOKE FWD ENG MOUNT SUPPORT IAW EO EM-54MR-386 PT A.
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