# N286AS: 1992 Embraer EMB-120ER, registration cancelled 2015-04-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 23, 2015 - Exported to: Turks and Caicos Islands - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203) - Engine: [Pratt & Whitney Canada PW118B](https://openairdocs.org/engine/pratt-whitney-canada-pw118b) (registry code 52131) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 120.268 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: June 18, 2002 - Certificate issued: December 11, 2014 - Last registry action: December 11, 2014 - Mode S code: A2E456 - Owner when cancelled: [Aharon Deborah C Trustee](https://openairdocs.org/faa-owner/AHARON%20DEBORAH%20C%20TRUSTEE) - Location: [Davie, FL](https://openairdocs.org/faa-place/FL/Davie) - Owner type: Individual - Owner's area on the map: 26.0693° N, 80.2757° W: Placed by OpenAirDocs at the center of ZIP code 33328, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N286AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=286AS - Page: https://openairdocs.org/deregistered/N286AS-2015-04-23 From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-120ER: https://openairdocs.org/model/embraer-emb-120er.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA02293](https://openairdocs.org/sdr/ASOA02293), May 25, 2002: BRACKET. CRACKED. 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 A - [SDR ASOA02131](https://openairdocs.org/sdr/ASOA02131), Feb 27, 2002: SILL. CORRODED. 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 - [SDR ASOA02130](https://openairdocs.org/sdr/ASOA02130), Feb 27, 2002: BUTT STRAP. CORRODED. 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 RE - [SDR ASOA02129](https://openairdocs.org/sdr/ASOA02129), Feb 27, 2002: BUTT STRAP. CORRODED. 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 IA - [SDR ASOA02128](https://openairdocs.org/sdr/ASOA02128), Feb 27, 2002: CROSSBEAM. CORRODED. 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. MAINTENANC - [SDR ASOA02127](https://openairdocs.org/sdr/ASOA02127), Feb 27, 2002: CROSSBEAM. CORRODED. 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 FRA - [SDR ASOA02126](https://openairdocs.org/sdr/ASOA02126), Feb 27, 2002: STRINGER. CORRODED. 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 51-2 - [SDR ASOA02125](https://openairdocs.org/sdr/ASOA02125), Feb 27, 2002: STRINGER. CORRODED. 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 - [SDR ASOA02124](https://openairdocs.org/sdr/ASOA02124), Feb 27, 2002: STRINGER. CORRODED. 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 - [SDR ASOA02123](https://openairdocs.org/sdr/ASOA02123), Feb 27, 2002: STRINGER. CORRODED. 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 FRA - [SDR ASOA02136](https://openairdocs.org/sdr/ASOA02136), Feb 27, 2002: CROSSBEAM. CORRODED. 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 - [SDR ASOA02135](https://openairdocs.org/sdr/ASOA02135), Feb 27, 2002: STRINGER. CORRODED. 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 - [SDR ASOA01234](https://openairdocs.org/sdr/ASOA01234), Nov 13, 2001: ODOR. DETECTED. 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 SME - [SDR 20000810SH016](https://openairdocs.org/sdr/20000810SH016), Jun 19, 2000: SKIN. CRACKED. 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 76 - [SDR ASOA99013](https://openairdocs.org/sdr/ASOA99013), Jan 19, 1999: SEAL. DETACHED. 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. LAND - [SDR 98ZZZX4703](https://openairdocs.org/sdr/98ZZZX4703), Nov 18, 1998: FRAME. CRACKED. FLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISCREPANCY AS PREVIOUSLY DETAILED AND REPOR - [SDR 98ZZZX4702](https://openairdocs.org/sdr/98ZZZX4702), Nov 18, 1998: FRAME. CRACKED. FLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LEFT ENGINE FORWARD NACELLE NR 1 FRAME. SEEMS TO BE A REPETITIVE DISPREPANCY AS PREVIOUSLY DETAILED AND REP - [SDR ASOA98101](https://openairdocs.org/sdr/ASOA98101), Nov 16, 1998: FRAME. CRACKED. 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 ## Other aircraft with N286AS - [Registered now](https://openairdocs.org/aircraft/N286AS): Direct Fly S R O ALTO NG, S/N DF158/2022, built 2022 --- 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.