Embraer EMB-145

Service difficulty reports · 3,003

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 = 'EMB145'
  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.

SDR SIMA200208803Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19R CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOUBLER AND SHIMS IAW EMB GST-0898/02, AND STANDARD SRM PRACTICES. (M)Mar 24, 2002 · N610AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR SIMA200208804Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND STRINGER 19L CHAFED AT AFT BELLY PANEL. BLENDED OUT CHAFE. FABRICATED A DOUBLER AND SHIMS IAW EMB-GST-0898/02, AND STANDARD PRACTICES. (M)Mar 24, 2002 · N610AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR C2XA02IA079Proximity Switch · damagedIAH- FLIGHT 4172, AFTER TAKEOFF LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND REMAINED ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES IN FLIGHT. NORMAL LANDING OCCURRED AT IAH. MAINTENANCE FOUND THAT THE LEFT GEAR WEIGHT Mar 24, 2002 · N14972 · Emb EMB145 · Landing Gear Position and WarningSDR C2XA02IA078Control Unit · faultyIAH- FLIGHT 4172, AFTER TAKEOFF, LD/AIR GROUND FAIL MESSAGE AND THRUST REV DISAGREE MESSAGE APPEARED EICAS AND, REMAINED ON ENTIRE FLIGHT QRH'S COMPLETED. NO SPEED BRAKES INFLIGHT. NORMAL LANDING OCCURRED IN IAH. REMOVED AND REPLACED THE LANDING GEAR ELECTMar 24, 2002 · N14972 · Emb EMB145 · Landing Gear SelectorSDR SIMA200209324Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 43 AND 44. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02. RETREATED AREA IAW EMB145 CPM 51-21-04 AND 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209323Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED BETWEEN FRAMES 48 AND 49. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST 1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209320Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209319Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING, CENTER GUSSET IN LAVATORY HAS CORROSION. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209313Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, LEFT SILL CORRODED AT FRAME 49. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209308Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT CROSSMEMBER CORRODED AT FRAME 59. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. TREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209307Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 58 AND 59. REMOVED CORRODED, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200209303Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT SILL CORRODED AT FRAME 20. REMOVED CORROSION AND FOUND TO BE ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB145 CPM 51-21-04, 51-21-05. (M)Mar 23, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208802Floorbeam · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND FORWARD DIGITAL IN GALLEY AREA CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A STRAP, DOUBLERS AND A SHIM IAW EMB145 SRM 145-1142 CHAPTER 53, REV 17, 53-21-10, AND STANDARD SRM PRACTICES. (M)Mar 23, 2002 · N610AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200208903Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND REPLACED DOOR FORWARD SILL IAW EMB 145 SRM 51-40-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208904Sill · corrodedTHIS IS LEVEL 2 FINDING. SERVICE DOOR AFT SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB 145 SRM 51-40-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208905Crossbeam · corrodedABI - THIS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM CORRODED AT FRAME 23. REMOVED AND REPLACED CROSS BEAM IAW EMB 145 SRM 51-40-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208906Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. CROSS BEAM PROFILE AT FRAME 23 CORRODED. REMOVED AND REPLACED CROSS BEAM PROFILE IAW EMB 145 SRM 51-40-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208907Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. CABIN FLOOR CROSS BEAM AT FRAME 23 END BRACKET AT RIGHT SILL CORRODED. REMOVED AND REPLACED CROSS BEAM IAW EMB 145 SRM 51040-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210016Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IS CORRODED AT FRAME 39. REPAIRED RIGHT SILL AT FRAME 39 IAW EMB 145 GST-1014/02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210015Floor Support · corrodedTHIS IS A LEVEL 2 FINDING. LEFT HAT BEAM GUSSET IS CORRODED BETWEEN FRAMES 65 AND 68. INSTALLED SERVICEABLE GUSSET IAW EMB 145 SRM 51-40-02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200210014Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. GUSSET CORRODED AT FRAME 19 ON RIGHT HAT BEAM. BLENDED OFF CORROSION IAW EMB 145 CPM 51-41-02. REPAIRED IAW EMB GST 1014/02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209318Sill · corrodedABI - THIS IS A LEVEL 2 FINDNG, LEFT SILL CORRODED BETWEEN FRAMES 20-22. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02. RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209305Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT SILL IS CORRODED BETWEEN FRAMES 61 AND 62. REMOVED CORROSION, ACCEPTED AS IS IAW EMB GST-1014/02, RETREATED AREA IAW EMB 145 CPM 51-21-04, 51-21-05. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200209302Beam · corrodedABI - THIS IS A LEVEL 2 FINDING, RIGHT HAT BEAM IN GALLEY CORRODED BETWEEN FRAMES 17 AND 19. REPAIRED RIGHT HAT BEAM IN GALLEY BETWEEN FRAME 17 AND 19 IAW GST-1014/02. (M)Mar 22, 2002 · N611AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208805Floorbeam · corrodedABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM AT FRAME 24 BEYOND SRM LIMITS AFTER BLENDING. REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLER, AND TWO SHIMS. REPAIRED IAW EMB145 SRM (SRM 145-1142 CHAPTER 53, REV 17) Mar 22, 2002 · N610AE · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA02TY057Bellcrank · crackedTYS, DURING A SCHEDULED INSPECTION, THE RIGHT ELEVATOR QUADRANT BELL CRANK WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BELL CRANK IAW-EMB-145-AMM-27-31-03, OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE.Mar 22, 2002 · N13958 · Emb EMB145 · Elevator Control SystemSDR C2XA02IA073Garlock Seal · leakingLCH- DURING FLIGHT 3788, THE CREW NOTED NUMBER 1 ENGINE LOW OIL QUANTITY AND PRESSURE, DECLAIRED EMERGENCY, AND DIVERTED TO LCH, (ACTUAL DESTINATION WAS HSV). LCH- MAINTENANCE REMOVED AND REPLACED THE #3 GENERATOR GARLOCK SEAL, SERVICED THE ENGINE OIL SYSTMar 21, 2002 · N14972 · Emb EMB145 · Engine Oil QuantitySDR SIMA200210703Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. GALLEY CROSSBEAM AND PROFILE CORRODED. REMOVED AND INSTALLED NEW GALLEY CROSSBEAM IAW EMB 145 51-40-02, 51-40-06, 51-20-03. (M)Mar 20, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208808Floor Support · corrodedDURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY CENTER FLOOR SUPPORT BEYOND SRM LIMITS. REMOVED CORRODED GALLEY CENTER FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT IAW EMB145 SRM 145-1142 CHAPTER 51, REV 17, 51-40-02, GST-0844/02, ITEM 4, AND STANDARDMar 20, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207907Sill · corrodedTHIS IS A LEVEL 2 FINDING. CARGO DOOR LOWER SILL CORRODED. REMOVED DAMAGED CARGO DOOR SILL AND INSTALLED SERVICEABLE ONE IAW EMB145 SRM 51-40-02, 51-40-05, 51-20-03. (M)Mar 19, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207906Sill · corrodedABI - THIS IS A LEVEL 2 FINDING. SERVICE DOOR FORWARD SILL CORRODED. REMOVED CORRODED SERVICE DOOR FORWARD SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 51-40-02 AND 51-20-03. (M)Mar 19, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207902Doubler · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20. REMOVED PREVIOUS REPAIR (CORROSION LIMITED TO PREVIOUS REPAIR). FABRICATED A DOUBLER ANGLE, FILLER, A PLATE, AND SHIMS. REPAIRED IAW EMB 145 SRM 9SMar 19, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208801Frame · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND THE LOWER EDGE OF FRAME 81 CHAFED APPROXIMATELY 12 INCH. RAI FRAME 81 IAW EMB 145 (SRM 145-1142 CHAPTER 51, REV 17) 51-20-01, 51-40-02, 51-40-04, 51-40-07 AND STANDARD SRM PRACTICES. (M)Mar 19, 2002 · N610AE · Emb EMB145 · Fuselage Main, FrameSDR RAIA00203100Windshield Wiper · deteriorated5282-STL- CAPTAINS WINDSHIELD WIPER CAME OFF DURING TAXI. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD WIPER, OPS CK OK.Mar 17, 2002 · N803HK · Emb EMB145 · Windshield/Door Rain/Ice RemovalSDR SIMA200208908Sill · corrodedABI - THIS IS A LEVEL 2 FINDING ON CRIC NR 35576. RIGHT CABIN SILL HAS CORROSION BETWEEN FRAMES 23-29. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208701Support · corrodedTHIS IS A LEVEL 2 FINDING. GALLEY RAMP SUPPORT CORRODED. INSTALLED SERVICEABLE GALLEY RAMP SUPPORT IAW EMB145 SRM 51-40-02. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207805Sill · corrodedABI - THIS IS LEVEL 2 FINDING ON A CRIC NR 35573. LEFT SILL IS CORRODED BETWEEN FRAMES 19 AND 23. MAINTENANCE REMOVED LEFT SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200208703Doubler · corrodedABI - THIS IS LEVEL 2 FINDING, DOUBLER ON LEFT HAT BEAM BETWEEN FRAMES 65 AND 68 CORRODED. REMOVED DAMAGED DOUBLER, INSTALLED NEW DOUBLER IAW EMB 145 SRM 51-40-02, 51-40-06, 51-20-03. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208704Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER GUSSET IN LAVATORY CORRODED. INSTALLED NEW GUSSET IAW EMB145 SRM 51-40-02, 51-40-06, 51-20-03. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208705Crossbeam · corrodedABI - THIS IS LEVEL 2 FINDING. FOUND CORROSION ON GALLEY CROSSBEAM AND PROFILE. INSTALLED SERVICEABLE CROSS BEAM AND PROFILE IAW EMB145 SRM 51-20-03, 51-40-02 AND 51-40-06. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200208706Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. GALLEY AREA FORWARD DIAMOND GUSSET CORRODED. INSTALLED NEW FORWARD GUSSET IAW EMB 145 SRM 51-40-02, 51-20-03, 51-40-06. (M)Mar 12, 2002 · N610AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR CHQ000999Socket · shortedSMELL OF ELECTRICAL SMOKE IN THE AFT CABIN, TRACE AMOUNTS OF SMOKE COMING FROM ABOVE 17A. DEFERRED SIDEWALL LIGHTS, FIXTURE WAS SHORTING OUT.Mar 12, 2002 · N273 · Emb EMB145 · Passenger Compartment LightingSDR SIMA200206901Fire Warning · activatedTVC - FLT 4253 - CREW REPORTED, A E1 FIRE WARNING JUST AFTER CLIMB-OUT AND THEN IT WENT OUT. THE CREW DECLARED AN EMERGENCY AND SHUTDOWN THE ENGINE. THE AIRCRAFT WAS RETURNED TO TVC AND LANDED WITH NO FURTHER INCIDENTS. (M)Mar 10, 2002 · N613AE · Emb EMB145 · Fire DetectionSDR SIMA200207211Duct · damagedTVC - FLT 4253 - ENGINE FIRE WARNING JUST AFTER CLIMB-OUT, THEN EXTINGUISHED. THE CREW SHUT DOWN NR 1 ENGINE, DECLARED EMERGENCY AND RETURNED TO TVC FOR MAINTENANCE, LANDED SAFELY. REPLACED BROKEN DUCT BETWEEN HIGHT STAGE VALVE AND ENGINE ANTI-ICE VALVE. (MMar 10, 2002 · N613AE · Emb EMB145 · Engine Bleed Air SystemSDR RAIA00203098Engine · malfunctioned5291-PIT- AT 40 KTS GOT WARNING "E2 ATTCS NO MARGIN". MAINTENANCE REMOVED AND REPLACED #2 ENGINE, OPS AND LK CK OK.Mar 9, 2002 · N807HK · Emb EMB145 · Engine (Turbine/Turboprop)SDR C2XA02IA057Lamp · burned outAGU - During scheduled maintenance the left overwing emergency light was found to be inoperative. Maintenance relamped the light assembly, performed an operational check, and approved the aircraft for return to service.Mar 9, 2002 · N16963 · Emb EMB145 · Emergency LightingSDR C2XA02IA058Light · inoperativeEWR - During scheduled maintenance the right over wing emergency light was found to be inoperative. Maintenance removed and replaced the emergency light, performed an operational check and approved the aircraft for return to service.Mar 9, 2002 · N14974 · Emb EMB145 · Emergency LightingSDR RAIA00203094Vane · inoperative5270-PIT- CREW ALERT MESSAGE "AOA #1 INOP”. MAINTENANCE REMOVED AND REPLACED THE #1 ANGLE OF ATTACK VANE, OPS CK OK.Mar 9, 2002 · N809HK · Emb EMB145 · Elevator Control SystemSDR CHQ000133Flap · malfunctionedAFTER TAKEOFF WHEN FLAPS SELECTED UP EICAS FLAP FAIL MESSAGE APPEARED UNABLE TO RAISE LOWER FLAPS. FLAPS REMAINED AT 0 DEGREES.Mar 9, 2002 · N262 · Emb EMB145 · Trailing Edge Flap Control SystemSDR SIMA200207008Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY AREA FORWARD DIGITAL. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPLACEMENT STRAP, TWO DOUBLERS AND A SHIM. WORK DONE IAW EMB 145 SRM 145/1Mar 8, 2002 · N608AE · Emb EMB145 · Fuselage Main, Floor Beam
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