# Service difficulty reports: N286AS, cancelled Apr 23, 2015 A list on [N286AS, cancelled Apr 23, 2015](https://openairdocs.org/deregistered/N286AS-2015-04-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ASOA02293](https://openairdocs.org/sdr/ASOA02293.md): Bracket · cracked · May 25, 2002 · N286AS · Emb EMB120RT · Landing Gear Doors > DURING 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 CRACKED - [SDR ASOA02131](https://openairdocs.org/sdr/ASOA02131.md): Sill · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 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) - [SDR ASOA02130](https://openairdocs.org/sdr/ASOA02130.md): Butt Strap · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Structure > DURING 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) - [SDR ASOA02129](https://openairdocs.org/sdr/ASOA02129.md): Butt Strap · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Structure > DURING 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) - [SDR ASOA02128](https://openairdocs.org/sdr/ASOA02128.md): Crossbeam · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Structure > DURING 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) - [SDR ASOA02127](https://openairdocs.org/sdr/ASOA02127.md): Crossbeam · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Structure > DURING 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 - [SDR ASOA02126](https://openairdocs.org/sdr/ASOA02126.md): Stringer · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 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) - [SDR ASOA02125](https://openairdocs.org/sdr/ASOA02125.md): Stringer · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 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) - [SDR ASOA02124](https://openairdocs.org/sdr/ASOA02124.md): Stringer · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 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) - [SDR ASOA02123](https://openairdocs.org/sdr/ASOA02123.md): Stringer · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 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, 51-25-0 - [SDR ASOA02136](https://openairdocs.org/sdr/ASOA02136.md): Crossbeam · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Structure > DURING 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- - [SDR ASOA02135](https://openairdocs.org/sdr/ASOA02135.md): Stringer · corroded · Feb 27, 2002 · N286AS · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 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) - [SDR ASOA01234](https://openairdocs.org/sdr/ASOA01234.md): Odor · detected · Nov 13, 2001 · N286AS · Emb EMB120RT · Air Distribution System > UPON 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 LAN - [SDR 20000810SH016](https://openairdocs.org/sdr/20000810SH016.md): Skin · cracked · Jun 19, 2000 · N286AS · Emb EMB120RT · Fuselage Main, Plate/Skin > FUSELAGE 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 TIT - [SDR ASOA99013](https://openairdocs.org/sdr/ASOA99013.md): Seal · detached · Jan 19, 1999 · N286AS · Emb EMB120RT · Cargo/Baggage Doors > FLT 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 FRO - [SDR 98ZZZX4703](https://openairdocs.org/sdr/98ZZZX4703.md): Frame · cracked · Nov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > FLUORESCENT 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 VIBRA - [SDR 98ZZZX4702](https://openairdocs.org/sdr/98ZZZX4702.md): Frame · cracked · Nov 18, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > FLUORESCENT 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 - [SDR ASOA98101](https://openairdocs.org/sdr/ASOA98101.md): Frame · cracked · Nov 16, 1998 · N286AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING 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. ( ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N286AS-2015-04-23/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.