Embraer EMB-120ER

Service difficulty reports · 8,287

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 = 'EMB120ER'
  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 HKGA201910108027Floorbeam · bentFUSELAGE, FLOOR BEAM 36 UPPER FLANGE IS BENT LEFT OF BL0. INSTALLED NEW FLOOR BEAM (REF EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR HKGA201910108026Floorbeam · bentFUSELAGE FLOOR BEAM 33 UPPER FLANGE IS BENT LEFT OF BL0. INSTALLED NEW FLOOR BEAM (REF EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR HKGA201910108025Stop Fitting · corrodedPAX DOOR, INTERNAL BACK UP FITTING FOR AFT LOWER STOP FITTING IS CORRODED (WITH DOOR CLOSED). MATCH DRILLED NEW INTERNAL BACKUP FITTING, INSTALLED NEW INTERNAL BACKUP FITTING (IAW EMB120 SRM 51-25-00, 51-40-02 REV 58). INSTALLED AFT LOWER STOP FITTING HAND RAIOct 8, 2019 · N235SW · Emb EMB120ER · Passenger/Crew DoorsSDR HKGA201910108024Skin · corrodedPAX DOOR OUTER SKIN, INNER SURFACE HAS A SPOT OF CORROSION AFT OF FWD FRAME BETWEEN BEAMS 5 & 6 (WITH PAX DOOR CLOSED). REPAIR FILLER FROM 2024-T3 .404" (PER ETD 2019-120-111246 REV 1). INSTALLED REPAIR (PER ETD 2019-120-111246 REV 1).Oct 8, 2019 · N235SW · Emb EMB120ER · Passenger/Crew DoorsSDR HKGA201910108023Attach Angle · chafedRH WING LEADING EDGE ATTACH ANGLE RIB AT INBOARD SIDE OF NACELLE IS CHAFED IN MULTIPLE AREAS. LOCATED AND DRILLED NEW ATTACH ANGLE AND INSTALLED NUTPLATES (IAW EMB120 SRM 51-40-02 REV 58). INSTALLED NEW L/E ATTACH ANGLE (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Attach FittingsSDR HKGA20191008022Skin · crackedRH NACELLE FLAP TRAILING EDGE LOWER SKIN ATTACH FLANGE IS CRACKED. LOCATED AND DRILLED NEW RH NACELLE FLAP TRAIILING EDGE LOWER SKIN ATTACH FLANGE (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED ATTACH FLANGE (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Center BoxSDR HKGA201910108021Rib · crackedRH NACELLE FLAP TRAILING EDGE STUB RIB BETWEEN THE IB AND CENTER RIB IS CRACKED. LOCATED AND DRILLED NEW STUB RIB (IAW EMB120 SRM 51-40-03 REV 58). INSTALLED NEW STUB RIB (REF EMB120 CPM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201910108020Frame · crackedLH NACELLE FRAME 10 WEB IS CRACKED ON IB SIDE LOWER CORNER. COMPLETED REPAIR STEPS OF REPAIR PROCEDURE (REF EMB ETD 2019-120-099295 REV A).Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/RibSDR HKGA20191008019Rib · crackedRH NACELLE FLAP INTERNAL TRAINING EDGE STUB RIB AFT OF LOWER SKIN ACCESS HOLE IS CRACKED & HAS ENLARGED FASTENER HOLES. MATCHDRILLED NEW STUB RIB (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW STUB RIB (REF EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Wing Main, Frame StructureSDR HKGA201910108018Door · chafedRH NACELLE COWL DOOR 423 INNER SKIN IS CHAFFED THROUGH AT THE UPPER FWD CORNER OF THE OIL FILL DOOR. C/W REPAIR (ETD 2019-120-10557).Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201910108017Doubler · chafedRH NACELLE COWL DOOR 424 INNER SKIN EXISTING REPAIR DOUBLER IS CHAFFED. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER (IAW EMB120 ETD 2019-120-105571).Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Plate/SkinSDR HKGA201910108016Doubler · crackedRH NACELLE COWL DOOR 424 INNER SKIN IS CRACKED BELOW HOLD OPEN ROD STOWAGE BRACKET. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER (IAW EMB120 ETD 2019-120-105571).Oct 8, 2019 · N235SW · Emb EMB120ER · Nacelle/Pylon, Plate/SkinSDR HKGA201910108015Support · crackedAPU COWL LH UPPER MOUNT FITTING, LOWER SUPPORT STRUCTURE IS CRACKED AT RIVET HOLE. MATCH DRILLED NEW SUPPORT (IAW EMB120 SRM 51-25-00 REV 58). INSTALLED NEW SUPPORT (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · APU Cowling/ContainmentSDR HKGA201910108014Support · buckledAPU COWL RH LOWER MOUNT FITTING, UPPER SUPPORT STRUCTURE IS BUCKLED. MATCH DRILLED NEW SUPPORT (IAW EMB120 SRM 51-25-00 REV 58). INSTALLED NEW SUPPORT (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · APU Cowling/ContainmentSDR HKGA2019101080Intercostal · crackedINTERCOSTAL BETWEEN FRAMES 39-40, STRINGER 3R IS CRACKED. LOCATED AND DRILLED NEW INTERCOSTAL (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED INTERCOSTAL AND SUPPORT BRACKET BETWEEN FRAMES 39-40 STR3R (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108012Floor Support · corrodedFUSELAGE, CENTER LONGITUDINAL FLOOR BEAM UPPER SURFACE HAS AREAS OF CORROSION AND MISSING SURFACE PROTECTION FR 38-40. MIN REMAINING THICKNESS NOTED ON FWD FLOOR BEAM UPPER SURFACE FOUND TO BE .038" (REF EMB NDI 51-00-04 REV 3). PERFORMED MATCH DRILL OF LONGITOct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108011Floor Support · corrodedFUSELAGE, RH LONGITUTINAL FLOORBEAM UPPER SURFACE HAS AREAS OF CORROSION AND MISSING SURFACE PROTECTION BETWEEN FR 38-42. MIN REMAINING THICKNESS .027" (REF EMB NDI 51-00-04 REV 3). DRILLED NEW FAILSAFE (IAW EMB120 SRM 51-26-00 REV 58). INSTALLED NEW FAILSAFE Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108010Floor Support · bentLH FLOOR SUPPORT BETWEEN FRAMES 28-29 IS BENT AND CREASED. LOCATED AND DRILLED NEW FLOOR SUPPORT (IAW EMB120 SRM 51-40-04 REV 58). INSTALLED PULLEY BRACKET (PER EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108009Floor Support · corrodedLEFT LONGITUDINAL FLOORBEAM PPER SILL HAS AREAS OF CORROSION BETWEEN FRAMES 20-22. MATCHDRILLED NEW FLOORBEAM UPPER SILL (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW UPPER SILL (REF EMB120 SRM 51-40-02 REV 58)Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108008Failsafe · corrodedFRAME 17 FAILSAFE BETWEEN STRINGERS 20R-21R HAS CORROSION. MIN REMAINING THICKNESS .027" (REF EMB NDI 51-00-04 REV 3). DRILLED NEW FAILSAFE (IAW EMB120 SRM 51-26-00 REV 58). INSTALLED NEW FAILSAFE (IAW EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Main, StructureSDR HKGA201910108007Floor Support · corrodedLEFT LONGITIDUNAL FLOORBEAM UPPER SILL BETWEEN FRAMES 15-16 HAS AREAS OF CORROSION. MATCHDRILLED NEW UPPER SILL (PER EMB120 51-40-02 REV 58). INSTALLED NEW UPPER SILL (PER EMB120 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108006Floor Support · corrodedRH LONGITUDINAL FLOORBEAM UPPER SILL BETWEEN FRAMES 13-15 HAS AREAS OF CORROSION. MATCHDRILLED NEW FLOORBEAM UPPER SILL (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW UPPER SILL (REF EMB120 SRM 51-40-02 REV 58).Oct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108005Floor Support · corrodedCENTER LONGITUDINAL FLOORBEAM UPPER STILL BETWEEN FRAMES 13-16 HAS AREAS OF CORROSION. REMOVED CORROSION ON CENTER FLOORBEAM UPPER SILL BETWEEN FR 13-16 (IAW EMB120 CPM 51-14-00 REV 10). REMAINING THICKNESS .030 (IAW EMB120 SRM 53-10-10, 53-00-00 REV 58). MATCOct 8, 2019 · N235SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA201910108004Skin · corrodedLH WING UPPER SKIN HAS CORROSION AFT OF THE VORTEX GENERATOR AT RIB 23. NOMINAL THICKNESS .080" OUT OF LIMITS (REF EMB120 SRM 57-20-01 AND 57-00-01 REV 58). CUTOUT BLENDED AREA (IAW EMB120 SRM 57-20-01 REV 58). LAYED OUT AND FABIRCATED DOUBLER FROM .080" 2024TOct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/SkinSDR HKGA201910108003Skin · corrodedLH WING UPPER SKIN HAS CORROSION AFT OF VORTEX GENERATOR BETWEEN RIBS 22 AND 23. NOMINAL THICKNESS .080" OUT OF LIMITS (REF EMB120 SRM 57-20-01 AND 57-00-01 REV 58). CUTOUT BLENDED AREA (IAW EMB120 SRM 57-20-01 REV 58). LAYED OUT AND FABIRCATED DOUBLER FROM .0Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/SkinSDR HKGA201910108002Attach Angle · chafedLH WING LEADING EDGE ATTACH ANGLE RIB AT INBOARD SIDE OF NACELLE IS CHAFED IN MULTIPLE AREAS. MATCHDRILLED NEW LEADING EDGE ATTACH (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW LEADING EDGE ATTACH (REF EMB120 SRM 51-40-02 REV 58). APPLIED SURFACE PROTECTION Oct 8, 2019 · N235SW · Emb EMB120ER · Leading Edge DevicesSDR HKGA201910108001Skin · corrodedLH WING UPPER SKIN HAS CORROSION AFT OF THE VORTEX GENERATOR AT RIB 21. FABRICATED REPAIR DOUBLER AND FILLER PIECE FROM 2024-T3 .080" (PER ETD 2019-120-101457). INSTALLED DOUBLER AND VORTEX GENERATOR (PER 2019-120-101457). APPLIED CAP SEAL TO FASTENERS WITHIN Oct 8, 2019 · N235SW · Emb EMB120ER · Wing, Plate/SkinSDR KCQA201911010001Eec · malfunctionedDURING FLIGHT RH ENGINE EEC FAILURE ANNUNCIATED WITH POWER REDUCTION TO ZERO PERCENT TORQUE. CREW PERFORMED QRH PROCEDURE, UNABLE TO RESTORE POWER ABOVE FLT IDLE. AIRCRAFT DIVERTED TO SUITABLE AIRPORT WITH PROPELLER IN FEATHER. AFTER LANDING ENGINE POWER AND EOct 7, 2019 · N121CZ · Emb EMB120ER · Fuel Controlling SystemSDR JIKA2019091001Hmu · erraticTHE FLIGHT CREW REPORTED THAT AT APPROXIMATELY 800-1000' AGL, THE LT PROPELLER INADVERTENTLY FEATHERED. THE FLIGHT CREW RAN THE "INADVERTENT PROPELLER FEATHER" QRH AND WAS ABLE TO UNFEATHER THE PROPELLER, PERFORMED A PRECAUTIONARY AIR RETURN WITH BOTH ENGINES Sep 3, 2019 · N567SW · Emb EMB120ER · Fuel Control/Turbine EnginesSDR JIKA2019083001Torque Sensor · intermittentTHE FLIGHT CREW REPORTED THAT DURING INITIAL CLIMB OUT AT APPROXIMATELY 500 FEET, THERE WAS A PARTIAL LOSS OF POWER ON THE LEFT HAND ENGINE. THIS LOSS COULD BE BOTH FELT AND HEARD, AND WAS ACCOMPANIED BY A SLIGHT DROP IN TORQUE AND A SIGNIFICANT DROP IN PROP SAug 27, 2019 · N567SW · Emb EMB120ER · Propeller Feathering/ReversingSDR HKGA20190620040Cowling · crackedFABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER (PER EMB120 SRM 51-40-04 REV 58 AND ETD 2019-120-067917). INSTALLED REPAIR DOUBLER (PER EMB120 SRM 51-40-02 REV 58 AND ETC 2019-120-067917). PN: 120-37974-001 RH INTERMEDIATE COWL SHIMJun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Plate/SkinSDR HKGA201906260039Skin · damagedCUT REPLACEMENT INNER PAN REPAIR SECTION (PER ETD 2019-120-050341). MATCH DRILLED AND TRIMMED DOUBLER REPAIR (IAW EMB120 ETD 2019-120-050341 REV A). INSTALLED REPAIR (PER EMB120 ETD 2019-120-050341 REV A). PN: 120-25601-029 DOOR SKIN, 120-25601-005 INNER SKIJun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Plate/SkinSDR HKGA20190626038Panel · chafedPANEL CHAFED. REMOVED DAMAGED SEAL RING, MATCH DRILLED NEW PART, INSTALLED NEW SEAL RING (REF. EMB120 SRM 51-40-02 REV 58, EMB120 SRM 51-25-00 REV 58, EMB120 SRM 51-40-02 REV 58). LOCATED AND DRILLED NEW PNL 429AT (PER EMB120 SRM 51-40-04 REV 58).Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201906260037Support Channel · crackedSUPPORT CHANNEL CRACKED. MATCH DRILLED NEW HALF FRAME TO COWLING STRUCTURE IAW SRM 51-25-00 REV 58. MATCH DRILLED LATCH PIN GUIDE ASSY'S AND DOOR HOLD OPEN ROD PINS AND INSTALLED ON NEW HALF FRAME IAW AMM 20-10-01-2, REV 43, SRM 51-40-02-PR, AND 51-25-00-PR Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201906260036Skin · damagedTAILCONE SKIN DAMAGED. FABRICATED A DOUBLER AND MATCH DRILLED REPAIR PARTS IAW ETD 209-120-046706, AND SRM 53-31-17, REV 58. INSTALLED THE REPAIRED DOUBLER AND FILLER IAW ETD 2019-120-046706, REV A.Jun 20, 2019 · N233SW · Emb EMB120ER · Aerodynamic FairingsSDR HKGA201906260035Shear Tie · crackedSHEAR TIE CRACKED AT FRAME 16, STRINGER 15R. FABRICATED A NEW SUPPORT IAW DRAWING 120-09850 REV E AND SRM 51-30-01 REV 58. LOCATED AND MATCH DRILLED IAW SRM 51-40-04 REV 58. INSTALLED NEW SUPPORT / SHEAR TIE LESS FASTENERS THRU SKIN IAW SRM 51-40-02 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Internal Mounting StructureSDR HKGA201906260034Skin · gougedSKIN GOUGED BETWEEN FRAMES 39-40, STRINGERS 18-19L. FABRICATED A DOUBLER AND FILLER SHIM AND APPLIED ALODINE AND EPOXY PRIMER TO DOUBLER AND SHIM PARTS IAW SRM 50-00-01 REV 58. APPLIED EDGE SEAL AND TOP COAT IAW SRM 51-22-00.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Plate/SkinSDR HKGA201906260033Floorbeam · corrodedFLOORBEAM CORRODED. MATCH DRILLED BEAM CAP AND INSTALLED LT FLOOR BEAM UPPER SURFACE AND BRACKET, RIB IAW SRM 51-40-02 REV 58. APPLIED SURFACE PROTECTION IAW CPM 51-21-00 REV 10.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR HKGA201906260032Floorbeam · corrodedFLOORBEAM CORRODED. MATCH DRILLED NEW BUTT STRAP AND INSTALLED BUTT STRAP IAW SRM 51-40-02 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Floor BeamSDR HKGA201906260031Pan · crackedPAN CRACKED. INSTALLED REINFORCING ANGLE IAW SRM 52-10-02 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Miscellaneous StructureSDR HKGA20190626030Door · damagedDOOR CHAFED. BLENDED CHAFFING IAW CPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOP COAT IAW COM 51-21-03 REV DATE 6/30/17.Jun 20, 2019 · N233SW · Emb EMB120ER · DoorsSDR HKGA201906260029Trunnion · damagedTRUNNION DAMAGED. INSTALLED A NEW LT MLG WELDED TRUNNION LUG ASSY IAW CMM 32-12-01 REV 15.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage, Landing Gear Attach FittingsSDR HKGA201906260028Plate · crackedPLATE CRACKED. REMOVED DOOR STOP PLATE, MATCH DRILLED NEW PART AND INSTALLED IAW SRM 51-40-02, AND 51-25-00 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Structure (General)SDR HKGA201906260027Fitting · chafedFITTING CHAFED. BLENDED CHAFFING (IAW EMB120 CPM 51-14-00).Jun 20, 2019 · N233SW · Emb EMB120ER · Fuselage Main, Attach FittingsSDR HKGA201906260026Shear Tie · crackedRT WING SHEAR TIE CRACKED. MATCH DRILL NEW SHEAR CLIP IAW SRM 51-40-02 REV 58. INSTALLED CLIP WITH SEALANT IAW SRM 51-40-02 REV 58. APPLIED TOP COAT IAW CPM 51-21-06 REV 6/30/17.Jun 20, 2019 · N233SW · Emb EMB120ER · Wing Main, Frame StructureSDR HKGA201906260025Rib · chafedRIB FLANGE CHAFED AND CORRODED. REMOVED CORROSION AND CHAFFING IAW CPM 51-14-00 REV DATE 6/30/17. MATCH DRILLED NEW LEADING EDGE RIB FLANGE IAW SBM 51-5-00 REV 58. INSTALLED THE RIB FLANGE IAW SRM 51-40-02 REV 58. APPLIED PRIMER AND TOP COAT IAW CPM 512106 RJun 20, 2019 · N233SW · Emb EMB120ER · Empennage StructureSDR HKGA201906260024Support · burnedFABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW ETD 2019-120-045306 AND SRM 54-30-02 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201906260023Flap · crackedFLAP CRACKED. R & R 18 FASTENERS PER EMB120 SRM 51-40-02 REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Nacelle/Pylon, Main FrameSDR HKGA201906260022Doubler · crackedDOUBLER CRACKED. MATCH DRILLED AND INSTALLED NEW DOUBLER IAW SRM 54-30-01, REV 58.Jun 20, 2019 · N233SW · Emb EMB120ER · Passenger/Crew DoorsSDR HKGA201906260021Hinge Fitting · corrodedRUDDER HINGE FITTING CORRODED. LOCATED AND DRILLED NEW HINGE FITTING IAW SRM 51-40-04 REV 58. APPLIED CHEMICAL CONVERSION COATING AND PRIMER TO HOLES IAW CRM 51-21-07 REV 4.Jun 20, 2019 · N233SW · Emb EMB120ER · Rudder Structure
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