# N16702: Embraer EMB-120ER, registration cancelled 1999-06-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 30, 1999 - Exported to: Canada - Status when cancelled: Sale reported - Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO) (OpenAirDocs) - Serial number: 120.078 - Type of aircraft: Fixed wing multi engine - Last registry action: June 30, 1999 - Mode S code: A10E22 - Location: [South Bend, IN](https://openairdocs.org/faa-place/IN/South%20Bend) - Owner type: Individual - Owner's area on the map: 41.6834° N, 86.2500° W: Placed by OpenAirDocs: center of South Bend, IN, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N16702 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=16702 - Page: https://openairdocs.org/deregistered/N16702-1999-06-30 From the FAA registry file of October 31, 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 (47) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR C2XA99IA330](https://openairdocs.org/sdr/C2XA99IA330), Jun 1, 1999: ANGLE. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT SIDEWALL/FLOOR ANGLE FROM FRAME 41 TO 44. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT APP - [SDR C2XA99IA329](https://openairdocs.org/sdr/C2XA99IA329), Jun 1, 1999: ANGLE. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT SIDEWALL/FLOOR ANGLE FROM FRAME 31-35. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02. AIRCRAFT APPROVE - [SDR C2XA99IA328](https://openairdocs.org/sdr/C2XA99IA328), Jun 1, 1999: SILL. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT OUTBOARD BUTT STRAP FROM FRAME 15 TO FRAME 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIR - [SDR C2XA99IA327](https://openairdocs.org/sdr/C2XA99IA327), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD BUTT STRAP FROM FRAME 14 TO FRAME 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. REMO - [SDR C2XA99IA326](https://openairdocs.org/sdr/C2XA99IA326), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 30 TO FRAME 35. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAF - [SDR C2XA99IA324](https://openairdocs.org/sdr/C2XA99IA324), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FROM FRAME 35 TO FRAME 38. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAF - [SDR C2XA99IA323](https://openairdocs.org/sdr/C2XA99IA323), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT LBL 19 FRAMES 40, 42 AND 44. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT APP - [SDR C2XA99IA322](https://openairdocs.org/sdr/C2XA99IA322), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT RBL 19 FROM FRAME 39 TO FRAME 40. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAF - [SDR C2XA99IA321](https://openairdocs.org/sdr/C2XA99IA321), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON LEFT INBOARD STRAP FROM STATION 66531.1 TO 87280.0. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIR - [SDR C2XA99IA320](https://openairdocs.org/sdr/C2XA99IA320), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CENTER BUTT STRAP FROM STATION 87280.0 TO 99645.0. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRC - [SDR C2XA99IA319](https://openairdocs.org/sdr/C2XA99IA319), Jun 1, 1999: BEAM. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON OMEGA BEAM LBL 19 AT FRAMES 40, 42 AND 44. REPAIRED OMEGA BEAM IAW EC5310-01043. AIRCRAFT APPROVED FOR RE - [SDR C2XA99IA318](https://openairdocs.org/sdr/C2XA99IA318), Jun 1, 1999: CROSSBEAM. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON CROSSBEAM FROM RBL 19 TO RBL 31 AT FRAME 38. REMOVED AND REPLACED CROSSBEAM IAW SRM 51-40-02. AIRCRAFT AP - [SDR C2XA99IA317](https://openairdocs.org/sdr/C2XA99IA317), Jun 1, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON RIGHT INBOARD BUTT STRAP FROM FRAME 13 TO 20. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT - [SDR C2XA99IA325](https://openairdocs.org/sdr/C2XA99IA325), Jan 6, 1999: STRAP. CORRODED. DURING CONTINENTAL EXPRESS C-CHECK, FOUND CORROSION ON BUTT STRAP AT BL 0 FROM FRAME 35 TO FRAME 39. REMOVED AND REPLACED BUTT STRAP IAW SRM 51-40-02. AIRCRAFT - [SDR C2XA98CL009](https://openairdocs.org/sdr/C2XA98CL009), Feb 4, 1998: NP GAUGE. INOPERATIVE. CLE - FLT 3172 - CREW REPORTED THAT WHILE TAXIING FOR TAKEOFF THE RIGHT ENGINE NP GAUGE WAS INOPERTIVE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE AIR - [SDR C2XA97IA174](https://openairdocs.org/sdr/C2XA97IA174), May 23, 1997: POWER SUPPLY. INOPERATIVE. IAH - DURING PREFLIGHT INSPECTION, THE PILOT REPORTED THAT THE FORWARD EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENC - [SDR C2XA97CL045](https://openairdocs.org/sdr/C2XA97CL045), Apr 19, 1997: BULB. FAILED. CLE - DURING A SCHEDULED INSPECTION, LEFT HAND AFT FUSELAGE EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND AFT F - [SDR C2XA97CL044](https://openairdocs.org/sdr/C2XA97CL044), Apr 19, 1997: BULB. BURNED OUT. CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND FORW - [SDR C2XA97CL024](https://openairdocs.org/sdr/C2XA97CL024), Mar 19, 1997: BULB. FAILED. CLE - DURING A SCHEDULED INSPECTINO THE FORWARD CEILING MOUNTED EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY, THEN REMO - [SDR C2XA97CL013](https://openairdocs.org/sdr/C2XA97CL013), Feb 5, 1997: DE-ICE BOOT. RUPTURED. CLE - FLT 3293 - CREW REPORTED THAT BOTH THE LEFT AND RIGHT ENGINE AIR INLET DE-ICE SYSTEMS FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPEC - [SDR C2XA96CL040](https://openairdocs.org/sdr/C2XA96CL040), Nov 11, 1996: GARLOCK SEAL. WORN. CLE - FLT 3121 - CREW REPORTED THAT THEY NOTICED A OIL LEAK ON THE RIGHT ENGINE IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVE - [SDR C2XA95IA383](https://openairdocs.org/sdr/C2XA95IA383), Dec 5, 1995: RIB. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 20 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED NOSE RIB, AND THE AIRCRAFT - [SDR C2XA95IA382](https://openairdocs.org/sdr/C2XA95IA382), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA381](https://openairdocs.org/sdr/C2XA95IA381), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA380](https://openairdocs.org/sdr/C2XA95IA380), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA379](https://openairdocs.org/sdr/C2XA95IA379), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA378](https://openairdocs.org/sdr/C2XA95IA378), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA377](https://openairdocs.org/sdr/C2XA95IA377), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 19, LOWER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA376](https://openairdocs.org/sdr/C2XA95IA376), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA375](https://openairdocs.org/sdr/C2XA95IA375), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKE - [SDR C2XA95IA374](https://openairdocs.org/sdr/C2XA95IA374), Dec 5, 1995: SUPPORT. CRACKED. IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 23, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET - [SDR C2XA95IA372](https://openairdocs.org/sdr/C2XA95IA372), Dec 5, 1995: MOUNT. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND THE CARGO DOOR TORSION BAR FORWARD MOUNT TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE MOUNT, AND THE AIRCRAFT WAS - [SDR C2XA95IA371](https://openairdocs.org/sdr/C2XA95IA371), Dec 5, 1995: PROFILE. CORRODED. IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE, AND THE - [SDR C2XA95IA370](https://openairdocs.org/sdr/C2XA95IA370), Dec 5, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT FORWARD LOWER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT W - [SDR C2XA95IA369](https://openairdocs.org/sdr/C2XA95IA369), Dec 5, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPRO - [SDR C2XA95IA368](https://openairdocs.org/sdr/C2XA95IA368), Dec 5, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT LOWER FORWARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO - [SDR C2XA95IA367](https://openairdocs.org/sdr/C2XA95IA367), Dec 5, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO - [SDR C2XA95IA366](https://openairdocs.org/sdr/C2XA95IA366), Dec 5, 1995: FLOOR SUPPORT. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SUPPORT CORRODED FROM FRAME 38.5 TO 40. MAINTENANCE REMOVED AND REPLACED THE SECTION OF FLOOR SUPPORT. AI - [SDR C2XA95IA365](https://openairdocs.org/sdr/C2XA95IA365), Dec 5, 1995: SEAT TRACK. CORRODED. IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERV - [SDR C2XA95IA364](https://openairdocs.org/sdr/C2XA95IA364), Dec 4, 1995: ANGLE. CRACKED. IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT AN - [SDR C2XA95CL108](https://openairdocs.org/sdr/C2XA95CL108), Aug 3, 1995: CONTROL PANEL. MALFUNCTIONED. FLT NR 3265 - CLE-CVG - RADAR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECK - [SDR C2XA95CL107](https://openairdocs.org/sdr/C2XA95CL107), Aug 3, 1995: RT UNIT. FAILED. FLT NR 3265 - CLE-CVG - RADR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKE - [SDR C2XA95CL052](https://openairdocs.org/sdr/C2XA95CL052), Mar 26, 1995: CLIP. SHEARED. FLT 3232 - DAY-CLE - BRAKES FAILED WITH ANTI-SKID ON. MAINTENANCE REMOVED AND REPLACED NR 3 WHEEL SPEED TRANSDUCER CLIP. OPS CHECK GOOD IAW EMB-120 MM 32-42-00. - [SDR C2XA95CL025](https://openairdocs.org/sdr/C2XA95CL025), Feb 11, 1995: ROLLERS. BINDING. FLT NR 3337 - PIT-CLE - FLAP DISAGREEMENT AFTER TAKEOFF, 1 MINUTE LATER CLEARED ITSELF. AFTER LANDING IN CLE MAINTENANCE CLEANED FLAP TRACKS AND ROLLERS. AIRCRA - [SDR C2XA95CL018](https://openairdocs.org/sdr/C2XA95CL018), Feb 7, 1995: HYD PUMP. FAILED. CLE-DAY - FLT 3223 - THE LT MAIN HYDRAULIC PUMP FAILED IN FLIGHT. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW EMB MM 29-10-03 - [SDR C2XA95CL006](https://openairdocs.org/sdr/C2XA95CL006), Jan 19, 1995: PROX SENSOR. FAILED. DAY\CLE - FLT 3285 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT AIR RETURNED TO DAY. MAINTENANCE SWAPPED LEFT UPLOCK 'A' AND 'B' SYSTEM CANNON PLUGS IAW SNL - [SDR C2XA95CL004](https://openairdocs.org/sdr/C2XA95CL004), Jan 16, 1995: CONTROL BOX. FAILED. CORRECTED SDR. DTW\CLE - FLT 3142 - ON CLIMB-OUT, SELECTED GEAR RETRACTION. SIX GREEN LIGHTS REMAIN ILLUMINATED ALONG WITH FIVE RED GEAR LIGHTS. LEFT 'B' RED GE ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19961111039599I](https://openairdocs.org/incident/19961111039599I), Nov 11, 1996: Emb EMB120 (N16702), Cleveland, OH. Narrative: aircraft departed & returned to cle w.o.I. Due to low oil indication from #2 engine. Continental express maintenance removed and replaced the #2… - [Incident 19950205002709I](https://openairdocs.org/incident/19950205002709I), Feb 5, 1995: Emb EMB120RT (N16702), Buffalo, NY. Narrative: on 2/5/95 at approx. 1900 EST, an Embraer Emb-120, registration N16702, being operated by Continental express as flight 3118 made a precautionary… - [Incident 19940129006939I](https://openairdocs.org/incident/19940129006939I), Jan 29, 1994: Emb EMB120RT (N16702), Mobile, AL, Minor damage. Narrative: on climb-out of Mobile, windshield cracked,and aircraft returned to mob for landing. --- 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.