Embraer EMB-120RT

Service difficulty reports · 5,310

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 = 'EMB120RT'
  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 COMA9710380Tee Section · corrodedDURING 2C INSPECTION TASK 5310-131/132-O1I, FOUND LEFT MID T-SECTION TO BE CORRODED AT FRAME 16. REMOVED CORRODED T-SECTION AND INSTALLED SERV PART IAW EMB 120 SRM CHAPTER 51.Aug 20, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710379Sill · corrodedDURING 4C INSPECTION TASK 5320-151/152 O1I, FOUND RT NR 3 SILL AT AFT EXIT TO BE CORRODED. REMOVED CORRODED SILL AND INSTALLED SERV PART IAW EMB SRM CHAPTER 51.Aug 20, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710373Skin · corrodedDURING COMPLIANCE OF E-6 INSPECTION, THE FUSELAGE LOWER SKIN WAS FOUND CORRODED AT FRAMES NR 21, 22 AND 23. THREE SEPARATE REPAIRS WERE PERFORMED. THE DAMAGE AT FRAMES 21 AND 22 WERE REPAIRED PER SRM 53-00-01, FIGURE 202. THE DAMAGE AT FRAME 23 WAS REPAIREDAug 20, 1997 · N241CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9710351Brake Disk · brokenLEFT BRAKE LOCKED UP WHILE TAXIING OUT TO RUNWAY. FOUND BRAKE DISC HAD BROKEN. REMOVED AND REPLACED BRAKE ASSY WITH SERVICEABLE UNIT.Aug 20, 1997 · N196CA · Emb EMB120RT · BrakeSDR COMA9710388Lav Base Support · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1F, FOUND TOILET BASE SUPPORT STRUCTURE CORRODED. REMOVED CORRODED BASE AND INSTALLED SERV BASE IAW EMB 120 MM.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710386Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131/132-01I, REVEALED RIGHT HAND FLOOR CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710385Crossbeam · corrodedDURING 2C INSEPCTION TASK 5310-131/132-01I, REVEALED LEFT HAND FLOOR CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710384Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND LEFT HAND FLOOR CROSSBEAM AT FRAME 20 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERV PART IAW EMB 120 SRM CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710383Crossbeam · corrodedDURING 2C INSPECTION TASK 5310-131/132-O1I, FOUND RT CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CORRODED PART AND INSTALLED SERV PART IAW EMB 120 SRM CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710382Angle · corrodedWHILE PERFORMING TASK 5320-152-01I, FOUND CORROSION BETWEEN ANGLE AND RECEPTACLE FOR AFT EMERGENCY EXIT. REMOVED ITEMS AND REPLACED WITH SERV ITEMS IAW EMB 120 SRM CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Emergency ExitsSDR COMA9710378Angle · corrodedWHILE PERFORMING TASK 5320-152-01F, FOUND CORROSION BETWEEN ANGLE AND RECEPTACLE FOR AFT EMERGENCY EXIT. REMOVED ITEMS AND REPLACED WITH SERV ITEMS IAW EMB120 SRM CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710377Buttstrap · corrodedDURING 2C INSPECTION TASK 5310-131/132-O1I, REVEALED FWD BUTT STRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710376Butt Plate · corrodedDURING 2C INSPECTION TASK 5310-131/132-01I, REVEALED CENTER BUTT PLATE TO BE HEAVILY CORRODED. REMOVED BUTT PLATE AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710375Butt Strap · corrodedDURING 2C INSPECTION TASK 5310-131/132-01I, REVEALED FWD BUTT STRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710374Sill · corrodedDURING 2C INSPECTION TASK 5310-131/132-O1I, REVEALED CORROSION ON LEFT FORWARD SILL TO BE BEYOND LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES FOR LIKE PART REPLACEMENT.Aug 19, 1997 · N267CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710350Tr Unit · inoperativeRADAR INOPERATIVE. REMOVED AND REPLACED TRANSCEIVER WITH A SERVICEABLE UNIT.Aug 19, 1997 · N261CA · Emb EMB120RT · Weather Radar SystemSDR WTAA970161Tire · failedFAT - RT NOSE TIRE TREAD SEPARATED FROM TIRE ON ROTATION DURING TAKEOFF AT SFO. A/C CONTINUED TO STA LANDING WITHOUT INCIDENT. MX INSPECTED A/C FOR DAMAGE. DISCOVERED SECONDARY DAMAGE RT TAXI LIGHT ASSEMBLY AND SMALL DENT IN UNDERSIDE OF FUSELAGE AFT OF NOSAug 15, 1997 · N276UE · Emb EMB120RT · TireSDR MASA97120Bulbs · failedFLT 5496 - GNV-MIA - AFTER LANDING IN MIA, THE CREW FOUND THAT THE FORWARD EMERGENCY EXIT LIGHT ON THE LEFT SIDE WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE LIGHT PER MEL 33-50-1. THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE THE BULBS Aug 15, 1997 · N283UE · Emb EMB120RT · Emergency LightingSDR COMA9710349Torque Sensor · inoperativeLEFT ENGINE TORQUE GAUGE READS ZERO. REMOVED AND REPLACED LEFT ENGINE TORQUE SENSOR WITH SERVICEABLE UNIT.Aug 15, 1997 · N246CA · Emb EMB120RT · Engine BMEP/Torque IndicatingSDR MASA97119Fuel Nozzles · leakingAIR SHUTTLE 5271 - TPA-PNS - AT 10,000 FT AND APPROX 1500 LBS OF TQ, THE TQ STARTED TO FLUCTUATE. THE CREW ADVANCED THE POWER LEVER TO ATTEMPT TO MAINTAIN POWER. WHEN THE POWER LEVER WAS AT MAX THE TQ ONLY SHOWED 46 PERCENT AND THE FUEL FLOW SHOWED 900PPH. Aug 14, 1997 · N341JS · Emb EMB120RT · Fuel Injector NozzleSDR C2XA97CL068Oil Cooler · leakingMDT - FLT 9510 - THE CREW REPORTED THAT DURING CRUISE, THE RIGHT HAND ENGINE LOST OIL PRESSURE. THE CREW ACCOMPLISHED AN IN-FLIGHT ENGINE SHUT DOWN AND DIVERTED THE AIRCRAFT TO MDT. MAINTENANCE INSPECTED THE ENGINE THEN REMOVED AND REPLACED THE OIL COOLER ANAug 14, 1997 · N26714 · Emb EMB120RT · Engine Oil CoolerSDR WTAA970159Structure · bird strikeFAT - BIRD STRIKE REPORTED ON LANDING. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION IAW EMB120 MM 5-50-08, NO DEFECTS NOTED. AIRCRAFT RETURN TO SERVICE. (M)Aug 12, 1997 · N455UE · Emb EMB120RT · Aircraft StructuresSDR COMA9710372Tee Section · corrodedDURING 4C INSEPCTION TASK 5320-151-01I, REVEALED RIGHT T-SECTION AT FRAME 28 TO BE CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710371Sill · corrodedDURING 4C INSPECTION TASK 5330-161-01I, REVEALED RIGHT CARGO COMPARTMENT SILL TO BE CORRODED BEYOND LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710370Floorbeam · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED RIGHT FLOORBEAM AT FRAME 33 TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51 FOR LIKE TO LIKE PART REPLACEMENT.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9710369Angle · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN FITTINGS AND THE EXIT SILL LOWER ATTACHE ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES. REPAug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710368Fitting · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN THE FITTINGS AND THE EXIT SILL LOWER ATTACH ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES. Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR WTAA970157Nose Gear · bird strikePSP - BIRD STRIKE REPORTED AT NOSE LANDING GEAR ON APPROACH. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURN TO SERVICE. (M)Aug 11, 1997 · N216YV · Emb EMB120RT · Nose/Tail Landing GearSDR WTAA970155Flap Annunciator · failedSFO - FLAP CONTROL FAULT ON TAKEOFF ROLL. ABORTED TAKEOFF. MAINTENANCE REPLACED FLAP ANNUNCIATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)Aug 11, 1997 · N455UE · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR MASA97107Light · inoperativeAIRSHUTTLE 5498, TLH-MIA - DURING THE PREFLIGHT INSPECTION, THE CREW FOUND THAT THE EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE LIGHTING SYSTEM PER MEL 33-50-1. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 11, 1997 · N287UE · Emb EMB120RT · Emergency LightingSDR COMA9710348Frame · chafedRIGHT AFT EMERGENCY EXIT FRAME NIB HAS GOUGES AT FORWARD SECTION OF NIB. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-002 IN ACCORDANCE WITH EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.Aug 10, 1997 · N256CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710347Frame · chafedRIGHT AFT EMERGECY EXIT AFT FUSELAGE FRAME HAS CHAFE DAMAGE FROM SCREW HEAD. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-001 IAW EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.Aug 9, 1997 · N256CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA9710346Battery · dischargedEMERGENCY EXIT LIGHTING INOP.Aug 9, 1997 · N246CA · Emb EMB120RT · Emergency LightingSDR WTAA970152Switch · out of adjustRDD - CARGO DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED. DEFERRED DOOR WARNING PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY ADJUSTING MICROSWITCH. OPERATIONAL CHECK SATISFACTORY. (X)Aug 8, 1997 · N455UE · Emb EMB120RT · Door Warning SystemSDR MASA97105Connector · shortedAIRSHUTTLE 5310 - TLH-MIA - DURING THE PREFLIGHT INSPECTION, THE CREW FOUND THAT THE EMERGENCY LIGHTS AT ROW 5 BOTH UPPER AND LOWER WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE EMERGENCY TRACK LIGHTING PER MEL 33-50-1. AIRCRAFT WAS RETURNED TO SERVICE. INAug 8, 1997 · N287UE · Emb EMB120RT · Emergency LightingSDR MASA97104Light · shortedAIRSHUTTLE 5563 - FLL-JAX - DURING THE PREFLIGHT INSPECTION, THE CREW FOUND ONE WHITE EMERGENCY PATH LIGHT AT ROW 3A INOP. MAINTENANCE DEFERRED THE LIGHTING SYSTEM PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE THE LIGHT RECEPTAug 8, 1997 · N270UE · Emb EMB120RT · Emergency LightingSDR 97ZZZM950Connector · shortedAIRSHUTTLE 5310 - TLH-MIA - DURING THE PREFLIGHT INSPECTION, THE CREW FOUND THAT THE EMERGENCY LIGHTS AT ROW 5 BOTH UPPER AND LOWER WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE EMERGENCY TRACK LIGHTING PER MEL 33-50-1. AIRCRAFT WAS RETURNED TO SERVICE. INAug 8, 1997 · N287UE · Emb EMB120RT · Emergency LightingSDR MASA97099Battery · dischargedAIRSHUTTLE 5497 - MIA-TLH - ON PREFLIGHT INSPECTION, ONE OF TWO RED EMERGENCY FLOOR PATH LIGHTS FAILED TO ILLUMINATE. MAINTENANCE DEFERRED THE FLOOR PATH LIGHTS PER MEL 33-51-1. AIRCRAFT WAS RELEASED FOR SERVICE. IN SUBSEQUENT MAINTENANCE, THE AFT EMERGENCYAug 7, 1997 · N289UE · Emb EMB120RT · Emergency LightingSDR XC4R643MDisk · wornNR 1 ROTATING DISK BROKEN AND MISSING. OTHER ROTATING DISKS AND WEAR PADS OKAY. WEAR PIN INDICATES 90 PERCENT WORN. PACKINGS AND RETAINERS SHOW NORMAL WEAR. NO OTHER DAMAGE NOTED. SUBMITTER STATED HAVE WITNESSED THE OLD P/N BRAKE ASSEMBLY 2-1479 HAVE THE Aug 6, 1997 · Emb EMB120RT · BrakeSDR MASA97097Wire · chafedAIRSHUTTLE 5548 - EYW-TPA - ON PREFLIGHT, ONE WHITE LIGHT ON FLOOR TRACK AT SEAT 11A WOULD NOT ILLUMINATE. MAINTENANCE DEFERRED THE FLOOR PATH LIGHTS PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MX, THE WIRING TO THE EMERGENCY LIGHTS WASAug 6, 1997 · N340JS · Emb EMB120RT · Light System WiringSDR C2XA97IA225Fitting · chafedIAH - INSPECTION CHECK 1C, 2C, DURING ROUTINE INSPECTION, THE RIGHT OUTBOARD FLAP WAS FOUND TO BE CHAFED BEYOND LIMITS AT INBOARD ROLLER ATTACHMENT AREA. MAINTENANCE REPLACED THE INBOARD END CLOSURE FITTING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICEAug 6, 1997 · N31711 · Emb EMB120RT · Trailing Edge FlapsSDR C2XA97IA224Connect Section · crackedIAH - INSPECTION CHECK 1C, 2C, DURING ROUTINE INSPECTION, THE VERTICAL STABILIZER TO HORIZONTAL STABILIZER LEFT FORWARD CONNECTING SECTION WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A REPAIR PER COEX EX NR 5530-01013, AND THE AIRCRAFT WAS LATER APPROVED FAug 6, 1997 · N31711 · Emb EMB120RT · Portable Oxygen SystemSDR WTAA970148Prox Sensor · out of adjustFAT - LANDING GEAR DOORS FAILED TO RETRACT AFTER TAKEOFF. RIGHT 'A' INTRANSIT LIGHT REMAINS ON. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN GEAR 'A' SYSTEM PROXIMITY SENSOR. OPERATIONAL CHECK NORMAL ON GROUND. TEST FLIGHAug 5, 1997 · N201YW · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9710367Tee Section · corrodedDURING 2C INSPECTION TASK 5310-131-00I, REVEALED RIGHT T-SECTION TO BE CORRODED AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE T-SECTION USING EMB 120 SRM STANDARD PRACTICES CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710366Tee Section · corrodedDURING 2C INSPECTION TASK 5310-131-01I, REVEALED RIGHT T-SECTION AT FRAME 16 TO BE CORRODED. REMOVED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710365Sill · corrodedON 2C INSPECTION TASK 5310-131-01I, REVEALED PAX DOOR LOWER SILL TO BE HEAVILY CORRODED. REMOVED PART AND INSTALLED SERVICEABLE PART AS PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710364Fitting · corrodedDURING 4C INSPECTION TASK 5320-254-01I, REVEALED LIGHT SURFACE CORROSION BETWEEN AFT EMERGENCY EXIT GUIDE PIN RECEPTICALS AND THE LOWER FRAME OF EXIT CUTOUT. THESE RECEPTICALS WERE ORIGINALLY INSTALLED WITHOUT PRIMER OR SEALANT BETWEEN THEM AND THE MATING SURAug 5, 1997 · N462CA · Emb EMB120RT · Emergency ExitsSDR COMA9710363Butt Plate · corrodedON 2C INSPECTION TASK 5310-131-01I, REVEALED LEFT BUTT PLATE TO BE CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-2.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710362Sill · corrodedON 2C INSPECTION TASK 5310-142-01I, REVEALED RIGHT FORWARD SILL TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES, CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710361Butt Strap · corrodedON 2C INSPECTION TASK 5310-131-01I, REVEALED LEFT BUTT STRAP TO BE CORRODED. REMOVED DAMAGED PART AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 5, 1997 · N462CA · Emb EMB120RT · Fuselage Miscellaneous Structure
Back to Embraer EMB-120RT