# N502AS: 1992 Embraer EMB-120ER, registration cancelled 2010-12-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 21, 2010 - 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 PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118) (registry code 52116) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 120274 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: December 8, 2000 - Certificate issued: July 14, 2010 - Last registry action: July 14, 2010 - Mode S code: A6416F - Owner when cancelled: [Aharon Deborah C](https://openairdocs.org/faa-owner/AHARON%20DEBORAH%20C) - Location: Providenciales, Turks & Caicos Islands - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N502AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=502AS - Page: https://openairdocs.org/deregistered/N502AS-2010-12-21 From the FAA registry file of October 29, 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 (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA02645](https://openairdocs.org/sdr/ASOA02645), Dec 26, 2002: ANGLE. CRACKED. DURING HANGAR INSPECTION IN MCN, THE VERTICAL STABILIZER RIGHT ATTACH ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT ATTACH ANGLE I - [SDR ASOA02637](https://openairdocs.org/sdr/ASOA02637), Dec 22, 2002: WIRE. BROKEN. DURING HANGAR INSPECTION AT MCN, THE EMERGENCY FLOOR TRACK LIGHT BY SEAT 5A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE FORWARD EMERG - [SDR ASOA02376](https://openairdocs.org/sdr/ASOA02376), Jun 30, 2002: DOUBLER. CRACKED. DURING C-CHECK INSPECTION IN BNA, THE FUSELAGE EXTERNAL SKIN DOUBLER AT FRAME 21 HAD SEVERAL BULGES AND CRACKED RIVET HEADS BETWEEN STRINGERS 20 LEFT AND 21 RIG - [SDR ASOA02375](https://openairdocs.org/sdr/ASOA02375), Jun 30, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION IN BNA, FOUND CORROSION OUT OF LIMITS ON STRINGER 19 LEFT BETWEEN FRAMES 13A AND 18A. MAINTENANCE REMOVED AND REPLACED THE CORRODED SE - [SDR ASOA02374](https://openairdocs.org/sdr/ASOA02374), Jun 30, 2002: STRINGER. CORRODED. DURING C-CHECK INSPECTION IN BNA, STRINGER 18 LEFT WAS FOUND CORRODED BETWEEN FRAME 13A AND SPLICE JUST FORWARD OF FRAMES 15 AND 16. MAINTENANCE REMOVED AND REP - [SDR ASOA02321](https://openairdocs.org/sdr/ASOA02321), Jun 10, 2002: WARNING SYSTEM. MALFUNCTIONED. DURING CLIMBOUT, AT 12000 FEET, THE AURAL WARNING LIGHT ILLUMINATED FOLLOWED BY THE ILLUMINATION OF THE LEFT DUCT LEAK LIGHT. THE CAPTAIN FOLLOWED THE QRH PROCE - [SDR ASOA02324](https://openairdocs.org/sdr/ASOA02324), Jun 10, 2002: WIRE. BROKEN. DURING CLIMB OUT, AT APPROXIMATELY 19,000 FEET, CAPTAIN REPORTED THAT DUCT LEAK WARNING WAS RECEIVED WITH CORRESPONDING LEFT DUCT LEAK LIGHT ILLUMINATING. CAPTA - [SDR ASOA00107](https://openairdocs.org/sdr/ASOA00107), Sep 28, 2000: STRINGER. CORRODED. DURING OVERNIGHT HANGAR VISIT, MAINTENANCE FOUND CORRSION BETWEEN STRIGNER 20R AND 21R. MAINTENANCE IS REPAIRING CORROSION FOLLOWING EO 120-53-0141 WHICH OUTLIN - [SDR ASOA990998](https://openairdocs.org/sdr/ASOA990998), Sep 15, 1999: UNKNOWN. SMOKE. TEN MILES FROM MEL, SMOKE EVIDENT IN COCKPIT. CRWE REQUESTED PRIORITY TO LAND AND FIRE EQUIPMENT. SMOKE CLEARED FROM AIRCRAFT. UPON SHUTDOWN, FIRE CREW AND STAT - [SDR ASOA99099](https://openairdocs.org/sdr/ASOA99099), Sep 15, 1999: ENGINE. FAILED. TEN MILES FROM MEI, SMOKE EVIDENT IN COCKPIT. CREW REQUESTED PRIORITY TO LAND AND FIRE EQUIPMENT. SMOKE CLEARED FROM AIRCRAFT. UPON SHUTDOWN, FIRE CREW AND STAT - [SDR ASOA99036](https://openairdocs.org/sdr/ASOA99036), Apr 14, 1999: FRAME. CRACKED. DURNG C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACEL - [SDR 99ZZZX1967](https://openairdocs.org/sdr/99ZZZX1967), Apr 14, 1999: FRAME. CRACKED. DURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENI - [SDR ASOA97016](https://openairdocs.org/sdr/ASOA97016), Mar 26, 1997: OIL SYSTEM. REQ'D SERVICE. FLT 7400 - DURING CLIMB-OUT FYV-DFW, LEFT ENGINE OIL PRESSURE MOMENTARILY WENT OT 35-45 PSI. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FYV WHERE LANDING WA - [SDR ASOA96053](https://openairdocs.org/sdr/ASOA96053), Nov 21, 1996: AIR DISTR. COCKPIT SMOKE. ON TAKEOFF MCN-ATL, SMOKE AND FUMES (OIL SMELL) BEGAN COMING INTO THE COCKPIT. NO PACK FAIL OVERHEAT OR BLEED LEAK NOTED ON OVERHEAD PANEL. SMOKE EVACUATED NORM ## Other aircraft with N502AS - [Cancelled 2026-09-18](https://openairdocs.org/deregistered/N502AS-2026-09-18): DJI AGRAS T40, S/N 1581F574B226D00100XU. Owner: [Agri Spray Drones LLC](https://openairdocs.org/faa-owner/AGRI%20SPRAY%20DRONES%20LLC), [Boonville, MO](https://openairdocs.org/faa-place/MO/Boonville) --- 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.