N286AS, cancelled Apr 23, 2015

Service difficulty reports · 18

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N286AS' AND deregistration_id = 'N286AS-2015-04-23'
  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 ASOA02293Bracket · crackedDURING HANGER MAINTENANCE, THE LEFT MAIN LANDING GEAR FORWARD OUTBOARD DOOR AFT TENSIONER BRACKET HAD A CRACK. THE LEFT MAIN LANDING GEAR FORWARD INBOARD DOOR AFT HINGE ANGLE WAS ALSO DISCOVERED WITH A CRACK. MAINTENANCE REMOVED AND REPLACED BOTH THE CRACKEDMay 25, 2002 · N286AS · Emb EMB120RT · Landing Gear DoorsSDR ASOA02131Sill · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL PLATE BETWEEN FRAMES 13 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SILL PLATE IAW SRMS 51-25-00, 51-21-04, AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA02130Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 15 AND 21 AND ALSO FROM FRAME 21 TO FRAME 25. MAINTENANCE REMOVED AND REPLACED THE TWO CORRODED SECTIONS OF BUTT STRAP IAW SRM 51-25-00, 51-21-00, AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02129Butt Strap · corrodedDURING C-CHECK INSPECTION IN BNA, THE CENTER BUTT STRAP WAS FOUND CORRODED BETWEEN FRAMES 16 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP IAW SRMS 51-40-02, 51-25-00, 51-21-02 AND 51-21-00. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02128Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT INBOARD CROSSBEAM HAD CORROSION AT FRAME 16. THE RIGHT OUTBOARD CROSSBEAM ALSO HAD CORROSION AT FRAME 18. MAINTENANCE REMOVED AND REPLACED CORRODED CROSSBEAMS IAW SRM 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02127Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND ON THE LEFT OUTBOARD CROSSBEAM AT FRAME 16. CORROSION WAS ALSO FOUND ON THE LEFT INBOARD CROSS BEAM AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRM'S 51-40-05, 51-40-02, AND Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02126Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT HAD CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02125Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 17 LEFT BETWEEN FRAMES 18 AND 20. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRIGNER IAW SRM 51-40-00. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02124Stringer · corrodedDURING C-CHECK INSPCTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-02, 51-25-00, AND 51-21-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02123Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 19 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15A. CORROSION WAS ALSO FOUND ON THE SAME STRINGER BETWEEN FRAMES 16 AND 18A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-40-00, 51-25-0Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA02136Crossbeam · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT OUTBOARD CROSSBEAM WAS CORRODED AT FRAME 20. CORROSION WAS ALSO FOUND ON THE LEFT OUTBOARD CROSS BEAM (P/N 120-14243-001) AT FRAME 15. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAMS IAW SRMS 51-21-04, 51-Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02135Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 20 LEFT WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 18 AND 19. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM'S 51-25-00 AND 51-40-02. (M)Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01234Odor · detectedUPON DEPARTURE FROM OKC, AT APPROXIMATELY 5000 FEET, CAPTAIN STARTED TO SMELL A HOT BURNING ODOR COMING FROM THE AIR VENTS. HE TURNED THE PACKS OFF, AND THE SMELL WENT AWAY. NO WARNING INDICATIONS WERE RECEIVED FROM THE AIR CONDITIONING SYSTEM. AIRCRAFT LANNov 13, 2001 · N286AS · Emb EMB120RT · Air Distribution SystemSDR 20000810SH016Skin · crackedFUSELAGE SKIN BULGES WITH .50 INCH CRACK IN OUTER SKIN AT FR 23 BS 7654.7 BETWEEN STR 20L AND STR 21L. ALSO, A .50 INCH CRACK BETWEEN STR 21L AND STR 21R, BS 7654.7. THIS CORROSION IS A RESULT OF THE DIRECT CONTACT BETWEEN THE FUSELAGE SKIN PANEL AND THE TITJun 19, 2000 · N286AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA99013Seal · detachedFLT 4067 - EN ROUTE ATL-CRW, LOST PRESSURIZATION AT 25,000 FEET AND PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET. OXYGEN MASKS WERE DEPLOYED IN THE CABIN. LANDING WAS MADE SAFELY AT CRW WITHOUT FURTHER INCIDENT. LOCAL MTC FOUND CARGO DOOR SEAL DETACHED FROJan 19, 1999 · N286AS · Emb EMB120RT · Cargo/Baggage DoorsSDR 98ZZZX4703Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRANov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR 98ZZZX4702Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISPREPANCY AS PREVIOUSLY DETAILED AND REPORTED. SUBMITTER STATED CAUSE REMAINS UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO Nov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR ASOA98101Frame · crackedDURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD OF MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (Nov 16, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib
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